# A300

REVISION 30, APR 01/10

ISSUE 00, APR 01/10 

# MAINTENANCE PLANNING

DOCUMENT

MPD

ENV

The content of this document is property of Airbus. It is supplied in confidence and

commercial security on its content must be maintained. It must not be used for any

purpose other than for which it is supplied, nor may information contained in it be

disclosed to unauthorized persons. It must not be reproduced in whole or in part

without permission in writing from the owners of the copyright. Requests for

reproduction of any data in this document and the media authorized for it must be

addressed to AIRBUS.

© AIRBUS 2006. All rights reserved.

Customer Services Directorate

Maintenance Planning and Services

31707 Blagnac Cedex

FRANCE

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 Transmittal Letter Page 1 

# TRANSMITTAL LETTER REVISION 30 ISSUE APR 01/10

1. FILING INSTRUCTIONS

This A300 MPD Revision 30 replaces MPD Revision 29 (OCT 01/09). All file formats are now available

in AirN@v / Planning.

2. REASON FOR REVISION

• To reflect changes resulting from MRBR Revision 6, dated March 1981.

• General task review/correction.

• To incorporate EWIS Requirements to reflect SIL 20–032 DATE MARCH 10 / 2010.

• Introduction of various maintenance requirements arising from e.g.:

– Modifications

– Service Bulletins

– Service Information Letters

– Airworthiness Directives

– All Operator Telexes

– Airworthiness Limitation Items

– Corrosion Prevention and Control Program revisions

3. HIGHLIGHTS OF CHANGES

– Due to ATA requirements, an additional document format (SGML) is introduced with this revision. To

be in line with the ATA Spec 2200, the structure of the A300 MPD needed to be adjusted.

– The A300 MPD now has the same structure as the A300–600, A310, A320 Family, A330, A340 and

A380 MPDs.

NEW STRUCTURE FEATURES: ( has been introduced A300 MPD Revision 29 ; OCT 01/2009)

• One MPD volume

– Section 1:

Manual Front Matter: Transmittal Letter(s), Summary of Changes, General Introduction,

Abbreviations, Effectivity Cross Reference List and Service Bulletin List.

– Section 2:

Systems, APU and Powerplant Section

– Section 3:

Structures Section

– Section 4:

Zonal Section

– Appendices:

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 Transmittal Letter Page 2 

# List of Deleted Tasks, Cross Reference Lists, Vendor Recommendations, Planning Examples and

Former Volume 2 and 3 Content.

– MPD task changes are highlighted in the Summary of Changes (SOC), which was amended with a

“Reason/Justification” column.

– Former Volume 2 and 3 content, which is covered by other Airbus documents, has been taken out of

the scope of the A300 MPD. Please regard the table in Appendix 5 for more information.

– ALI, ASM and FAL requirements are now referenced with their source task number.

– Paragraph “Exceptional Variations to Maintenance Program Periods” added to General Introduction.

– Paragraph “Implementation Periods” added to General Introduction.

– The Transmittal Letter contains now a list of missing AMM References with scheduled incorporation

dates.

– Man Hour Information for Task (Task-MH) and Access (Access-MH) has been amended with this

MPD revision.

– MPD Skill– and Task Codes have been improved.

4. IMPORTANT NOTES

On AirbusWorld you will find answers for “MPD Frequently Asked Questions”. Go to “Maintenance &

Engineering -> Prepare Maintenance -> Know more about”.

For some MPD tasks, an AMM procedure could not be referenc ed. The AMM procedures were not yet

available at the time of the MPD compilation.

The A300 MPD provides references to the AMM only for tasks from Section 2 (Systems, APU and

Powerplant).

NOTE: Please turn to the AMM department's frontdesk “account.sdm rfirfr@airbus.com”, if you urgently

need an AMM procedure prior to the scheduled AMM incorporation date listed below.

MPD TASK NUMBER AMM revision date

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 1 

# SUMMARY OF CHANGES

MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

2-20 201210-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201210-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201210-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201210-0505-4 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201210-0505-5 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201210-0505-6 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201210-0505-7 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201230-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201310-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201310-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201310-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201330-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201330-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201370-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201370-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201370-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201410-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201410-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201430-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201450-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201450-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201470-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 2 MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

20-032

2-20 201510-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201510-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201530-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201530-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201610-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201630-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 201710-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202110-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202110-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202110-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202210-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202230-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202230-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202230-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202310-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202310-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202310-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202330-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202330-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202410-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202410-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202410-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202430-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 3 MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

2-20 202430-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202510-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202510-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202510-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202530-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202530-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202610-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202610-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202610-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202630-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202630-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202630-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 202630-0505-4 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 203110-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 203130-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 203150-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 203150-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 203150-0505-3 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 203340-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204110-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204130-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204130-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204150-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 4 MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

2-20 204330-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204330-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204350-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204510-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204530-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204710-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 204730-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205120-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205120-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205130-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205130-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205230-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205230-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205240-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205240-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205300-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205410-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205410-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205420-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205420-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205430-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205430-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205500-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 5 MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

2-20 205500-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205710-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205710-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205720-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205720-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205750-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205770-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205810-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205810-0505-2 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 205910-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 207110-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-20 207310-0505-1 N NEW TASK ADDED IN ACCORDANCE WITH SIL

20-032

2-26 262111-0504-1 R 100% INTERVAL CHANGED FROM: "1 YE", TO:

"NOTE 5-1" EDITORIAL CHANGES

2-26 262111-0504-2 R IN DESCRIPTION: "IN ACCORDANCE WITH LOCAL

NATIONAL REQUIREMENTS OR PRIOR TO NEXT

FULL OR PARTIAL REFILLING AFTER 60 MONTHS

SINCE LAST HYDROSTATIC TEST. (MAX.SERVICE

LIFE IN ACCORDANCE WITH NATIONAL REQTS./

VENDOR RECOMMENDATIONS)" REMOVED 100%

INTERVAL: "OR NOTE 5-1" ADDED DESCRIPTION AND

INTERVAL CHANGED

2-26 262312-0504-1 R IN REFERENCE(S): "AMM 262312/401" ADDED AND

"AMM 62312/401" REMOVED EDITORIAL CHANGES

2-27 272100-0502-1 R SAMPLE INTERVAL: "2 C" ADDED SAMPLE SIZE:

"20% 1/5" ADDED 100% INTERVAL: "COVERED BY"

ADDED INTERVAL CHANGED

2-27 274211-0502-2 R IN DESCRIPTION: "NOTE: THRESHOLD IS 4000 FH

AFTER THE LAST THSA OVERHAUL OR WITHIN 250

FH AFTER THE EFFECTIVE DATE OF THE AD

WHICHEVER OCCURS LATER." ADDED 100%

THRESHOLD: "NOTE" ADDED

IN SOURCE: "AD" ADDED

IN REFERENCE(S): "AD 2009-0111" ADDED DESCRIPTION, INTERVAL

AND REFERENCE

CORRECTED

2-27 274211-0503-5 D TASK DELETED DELETED TASK

2-27 274211-0505-5 N NEW TASK ADDED EASA AD 2010-0019

2-28 281800-0502-3 R IN SOURCE: "FAL" ADDED AND "MRB 9" REMOVED EDITORIAL CHANGES

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 6 MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

IN REFERENCE(S): "FAL" ADDED AND "MRB 9"

REMOVED

2-28 281800-0502-5 R IN SO URCE: "FAL" ADDED AND "MRB 9" REMOVED

IN REFERENCE(S): "FAL" ADDED AND "MRB 9"

REMOVED EDITORIAL CHANGES

2-28 281800-0502-6 R IN SO URCE: "FAL" ADDED AND "MRB 9" REMOVED

IN REFERENCE(S): "FAL" ADDED AND "MRB 9"

REMOVED EDITORIAL CHANGES

2-28 281800-0502-7 R IN SO URCE: "FAL" ADDED AND "MRB 9" REMOVED

IN REFERENCE(S): "FAL" ADDED AND "MRB 9"

REMOVED EDITORIAL CHANGES

2-28 281800-0502-8 R IN SO URCE: "FAL" ADDED AND "MRB 9" REMOVED

IN REFERENCE(S): "FAL" ADDED AND "MRB 9"

REMOVED EDITORIAL CHANGES

2-28 281800-0502-9 R IN SO URCE: "FAL" ADDED AND "MRB 9" REMOVED

IN REFERENCE(S): "FAL" ADDED AND "MRB 9"

REMOVED EDITORIAL CHANGES

2-28 281801-0502-1 R IN SO URCE: "FAL" ADDED AND "MRB 9" REMOVED

IN REFERENCE(S): "FAL" ADDED AND "MRB 9"

REMOVED EDITORIAL CHANGES

2-32 323300-0503-1 R APPLICABILITY CHANGED FROM: "POST 02781 (32-

0272) OR PRE 03433", TO: "POST 02781 (32-0272)

PRE 03433" APPLICABILITY CHANGED

2-32 323300-0503-4 R APPLICABILITY CHANGED FROM: "PRE 04443 (32-

0425) POST 02781 (32-0272) OR PRE 03433", TO:

"PRE 04443 (32-0425) POST 02781 (32-0272) PRE

03433" APPLICABILITY CHANGED

2-34 344200-0503-2 N NEW TASK ADDED REFER TO SIL 34-099

2-49 493000-0703-3 N NEW TASK ADDED REFER TO SIL 49-056

3-53 531252-0605-1 D TASK DELETED DELETED TASK

3-53 531252-0605-2 D TASK DELETED DELETED TASK

3-53 531253-0604-1 N NEW TASK ADDED REFER TO ISB 53-0388

3-53 531933-0603-1 R IN SOURCE: "AD" ADDED

IN REFERENCE(S): "AD F-2004-193; ISB 53-0363"

ADDED AND "CN F-1989-068-093; FAA AD 90-03-08;

ISB 53-0217" REMOVED SOURCE AND

REFERENCE CORRECTED

3-53 531933-0603-2 R IN SOURCE: "AD" ADDED

IN REFERENCE(S): "AD F-2004-193; ISB 53-0363"

ADDED AND "CN F-1989-068-093; FAA AD 90-03-08;

ISB 53-0217" REMOVED SOURCE AND

REFERENCE CORRECTED

3-53 536114-0606-2 R 100% INTERVAL CHANGED FROM: "14000 FC", TO:

"40000 FC" EDITORIAL CHANGES

3-53 536514-0606-1 D TASK DELETED DELETED TASK

3-53 536514-0606-2 D TASK DELETED DELETED TASK

3-53 536561-0606-1 R #N REFERENCE(S): "ISB 53-0381" ADDED AND "ISB

57-6102" REMOVED EDITORIAL CHANGES

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 7 MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

3-53 536561-0606-2 R IN REFERENCE(S): "ISB 53-0383" ADDED AND "ISB

57-6102" REMOVED EDITORIAL CHANGES

3-53 539013-0603-1 R IN ZONE "123" ACCESS: "121NF; 122HF; 811" ADDED

AND "131AZ" REMOVED

IN ZONE "124" ACCESS: "831" ADDED DESCRIPTION

CHANGED FROM: "CONNECTING FITTING IN NLG

BAY BETWEEN FR 13A AND", TO: "LOWER HOLES

OF THE KEEL BEAM OF NLG BAY CONNECTING

FITTING IN NLG BAY BETWEEN FR 13 AND FR"

IN REFERENCE(S): "NTM 513010 PART 1" ADDED

IN ZONE "123" ACCESS MH CHANGED FROM: "0.06",

TO: "0.60"

IN ZONE "124" ACCESS MH CHANGED FROM: "0.06",

TO: "0.16" DESCRIPTION, ACCESS

AND REFERENCE

CORRECTED

3-54 546014-0606-1 R IN DESCRIPTION: "NOTE: THIS TASK IS AN

ALTERNATIVE TO THE TASK 546014-0607-1 AND

546014-0608-1" ADDED DESCRIPTION CHANGED

3-54 546014-0606-2 R IN DESCRIPTION: "NOTE: THIS TASK IS AN

ALTERNATIVE TO THE TASK 546014-0607-2 AND

546014-0608-2" ADDED DESCRIPTION CHANGED

3-54 546014-0606-3 R IN DESCRIPTION: "NOTE: THIS TASK IS AN

ALTERNATIVE TO THE TASK 546014-0607-3 AND

546014-0608-3" ADDED DESCRIPTION CHANGED

3-54 546014-0606-4 R IN DESCRIPTION: "NOTE: THIS TASK IS AN

ALTERNATIVE TO THE TASK 546014-0607-4 AND

546014-0608-4" ADDED DESCRIPTION CHANGED

3-54 546014-0606-5 R IN DESCRIPTION: "NOTE: THIS TASK IS AN

ALTERNATIVE TO THE TASK 546014-0607-5 AND

546014-0608-5" ADDED DESCRIPTION CHANGED

3-54 546014-0607-1 R IN DESCRIPTION: "NOTE: THIS TASK IS AN

ALTERNATIVE TO THE TASK 546014-0606-1 AND

546014-0608-1" ADDED DESCRIPTION CHANGED

3-57 574212-0602-1 R APPLICABILITY CHANGED FROM: "PRE 11932 (57-

0235)", TO: "POST 11932 (57-0235)" APPLICABILITY CHANGED

3-57 574212-0602-2 R IN ZONE "571" ACCESS: "575AB" ADDED

IN ZONE "671" ACCESS: "675AB" ADDED

IN ZONE "571" ACCESS MH: "0.04" ADDED

IN ZONE "671" ACCESS MH: "0.04" ADDED

APPLICABILITY CHANGED FROM: "PRE 11932 (57-

0235)", TO: "POST 11932 (57-0235)" APPLICABILITY CHANGED

3-57 574212-0602-3 R APPLICABILITY CHANGED FROM: "POST 11932 (57-

0235)", TO: "PRE 11932 (57-0235)" APPLICABILITY CHANGED

3-57 574212-0602-4 R APPLICABILITY CHANGED FROM: "POST 11932 (57-

0235)", TO: "PRE 11932 (57-0235)" APPLICABILITY CHANGED

3-57 576041-0606-4 R IN REFERENCE(S): "ALI 576041-01-6" ADDED AND

"ALI 576041-01-4" REMOVED REFERENCE CHANGED

3-57 576041-0606-5 R IN REFERENCE(S): "ALI 576041-01-4" ADDED AND

"ALI 576041-01-5" REMOVED REFERENCE CHANGED

3-57 576041-0606-6 R IN REFERENCE(S): "ALI 576041-01-5" ADDED AND REFERENCE CHANGED

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SUMMARY OF CHANGES Page 8 MPD

SEC TASK

NUMBER MVT DESCRIPTION REASON / JUSTIFICATION

"ALI 576041-01-6" REMOVED

3-57 576041-0606-7 D TASK DELETED DELETED TASK

3-57 576051-0606-3 R APPLICABILITY CHANGED FROM: "B4-100", TO: "B4-

200 C4 F4 FROM 0 FC TO 34000 FC" APPLICABILITY CHANGED

3-57 576051-0606-5 R APPLICABILITY CHANGED FROM: "B4-200", TO: "B4-

100 FROM 40000 FC TO LOV" APPLICABILITY CHANGED

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 GENERAL INTRODUCTION Page 1 

# GENERAL INTRODUCTION

1. INTRODUCTION

The A300 Maintenance Planning Document (MPD) is an AIRBUS envelope repository document, which

provides direct access to repetitive scheduled maintenance tasks required by various sources.

The main objective of this document is to provide maintenance planning information necessary for each

operator to develop a customized scheduled maintenance program.

The Maintenance Planning Document (MPD) is neither a controlling document nor an approved

document.

The maintenance tasks in this document,should not be considered with the same ranking of

requirement except for those mandated by AD or CN and maintenance requirements arising from ALS

Parts. Each individual airline has final responsibility to decide with their respective national authority

what to do and when to do it.

NOTE: MRBR Requirements and intervals are considered as initial minimum program for entry into

service. Additional requirements in the form of Service Information Letters, non-mandatory SBs

are the responsibility of the individual airline to assess the need for incorporation in their

Program.

2. GENERAL

The A300 Maintenance Planning Document contains recommended scheduled maintenance

requirements arising from:

– The A300 Maintenance Review Board (MRB) Document dated March 1981

– The Supplemental Structure Inspection Document (SSID) dated June 1994

– The Corrosion Prevention and Control Program (CPCP) dated November 1992.

– Repetitive tasks promulgated by Airworthiness Directives (CNs/ADs),

– All Operator Telexes (AOT), Inspection Service Bulletins (ISBs)

– Service Information Letters (SILs) and Modification (MOD/SB).

Attention is drawn to the fact that although the Maintenance Planning Document will reflect all repetitive

scheduled maintenance tasks promulgated by ISB, AOT, SIL, CN/AD, etc., it is the operators

responsibility to adjust their program on receipt of the source document and not to wait until the

amended A300 MPD revision.

The A300 MPD comprises the following sections:

Section 1: Manual Front Matter

Section 2: Systems, APU and Powerplant

Section 3: Structure

Section 4: Zonal

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 GENERAL INTRODUCTION Page 2 

# Appendices: List of Deleted Tasks

Cross Reference List

Vendor Recommendation

Maintenance Event Planning Examples

Former Volume 2 and 3 content

3. SCOPE AND PURPOSE

This MPD provides the scheduled maintenance tasks and their frequencies for the Systems, APU,

Power Plant and Structure of the Airbus A300 aircra ft. It is intended that th is MPD will be used as a

basis for each operator to develop his own maintenance program subject to the approval of his

Regulatory Authority.

The tasks and their frequencies given in this MPD, together with the Certification Maintenance

Requirements and Airworthiness Limitations, form part of the instructions considered essential for

proper maintenance as required by certification requirements for JAR 25.1529 and JAR 25 Appendix H,

Instructions for Continued Airworthiness.

The information and instructions included herein are applicable to the following A300 models and

powerplants:

– A300-B2-1A

– A300-B2-1C

– A300-B2K-3C

– A300-B2-202

– A300-B2-203 incl. FF variant

– A300-B2-320

– A300-B4-2C

– A300-B4-102

– A300-B4-103

– A300-B4-120

– A300-B4-203 incl. FF variant

– A300-C4-203

– A300-F4-203

– A300-B4-220 incl. FF variant

– GARRETT TSCP 700 APU

– GENERAL ELECTRIC CF6-50C, C1, C2, C2T

– PRATT & WHITNEY JT9D-59A

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# 4. BASIS FOR STANDARD AND PROCEDURES

For the purposes of program development, it was assumed that the 2500 FH "C-Check" would be

accomplished approximately every 12 to 15 months. If actual utilisation is significantly different from this

it may be necessary to adjust the program. Airbus recommend that operators should consider

maintaining aircraft that fly less than 2000 FH within a 12 month period according to the alternative

"Low Utilisation Program" given in Appendix 5 of this MPD.

5. REVISION POLICY

The need for revision will be considered depending on the issuance/revision of A300 MPD related

Source documents.

6. OVERALL DOCUMENT DESCRIPTION

The maintenance tasks and their frequencies are presented in the Systems/APU/Powerplant, Structure

and Zonal sections.

– The Systems, APU and Powerplant section define specific tasks at the level of each Maintenance

Significant Item (MSI) considering the failure effects and failure causes.

– The Structures section defines the necessary inspections for each Structural Significant Item (SSI)

developed through evaluation with respect to environmental and ageing deterioration, accidental and

fatigue damage. A Corrosion Prevention and Control Program (CPCP) was integrated into the

Structures section in the April 1998 MRB Report revision.

– The Zonal Inspection section defines General Visual Inspections of system installations and structure

by aircraft zone.

7. INSPECTION INTERVALS

SYSTEMS, APU AND POWERPLANT SECTION

All task intervals are expressed in terms of usage parameters, i.e. FH, FC or calendar time (years,

months, days) and/or in letter check concept (“A” and “C)

* Pre-Acceptance (PRE-ACPT)

Tasks to be accomplished prior to the first flight of the day and at each crew change.

* Daily (DY-TERM)

Tasks to be accomplished every calendar day, 24 hours elapsed time, (aircraft in service).

* Weekly Check (WEEKLY)

Tasks to be accomplished every 7 calendar days (aircraft in service).

NOTE:

The definition of the term Daily and Weekly serves only as a guide and may be adapted to suit

existing airline policy as approved by the local Regulatory Airworthiness Authority.

* * "A" and "A multiples":

Tasks to be accomplished every 250 FH (Flight Hours) and multiples.

* "C" and "C multiples":

Tasks to be accomplished every 2500 FH (Flight Hours) and multiples.

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# The MPD is not intended to be the total maintenance program. There are items which are typically

performed by each operator in his maintenance program more frequent than “A”–Check. The routine

content of checks occurring more frequently than “A”–Check shall be developed by the operator and

approved/accepted by their local Regulatory Authority.

8. TASK INTERVAL FRAME

The following intervals are in accordance with the MRB Report approved by EASA, FAA and Transport

Canada.

Operational units (usage parameters)

– "FH" (Flight hours) : Elapsed time between wheel lift off and touchdown.

– "FC" (Flight cycle) : A complete take off and landing sequence.

Calendar units

– "HR" (Hours) : One Calendar hour elapsed.

– "DY" (Day) : 24 Calendar hours elapsed.

– "MO" (Month) : One Calendar month.

–“YE" (Year) : One Calendar year.

Other codes

–“NR” (National Requirement). : Task known as being subject to national

regulatory requirement.

–“VR” (Vendor Recommendation). : Interval value dependent on task vendor

recommendation.

–“NOTE” : Refer to the note in the task description

9. ASSISTANCE AND INFORMATION

Operators having any queries or comments regarding the A300 MPD should contact :

AIRBUS

Customer Service

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 GENERAL INTRODUCTION Page 5 

# Maintenance Planning & Services

B.P. No. 33

F-31707 Blagnac Cedex

FRANCE

FAX : 33 (0) 5 61 93 28 72

or TLX : 530 526 F

SITA: TLSBT7X

sched.maint@airbus.com

10. GENERAL RULES

The A300 MPD Document defines general rules to be used for all maintenance Programs. These rules

apply to the requirements arising from the MRB Document and are quoted here for reference.

The following applies to the DGAC/LBA MRB Document.

1. The operators manuals shall contain the details and responsibilities for accomplishing the

maintenance required by this document.

2. The overall reliability of the A300 will be monitored by each carrier's system for continuous analysis

and surveillance as required by the operator's Regulatory Authorities.

3. All Maintenance Significant Items not identified by the Hard Time (HT) or On Condition (OC)

primary maintenance process shall be controlled by a Condition Monitoring Program. In addition,

the operator's Condition Monitoring Program(s) shall be described or appropriately referenced in its

Operations Specifications Maintenance.

4. Each operator should be aware of the various inspection techniques such as X-ray, ultrasonic, eddy

current, radio isotope, ... which are available and described in the NDT-Manual. The use of such

techniques can be developed to provide a valuable adjunct to the prescribed visual inspections

specified. For any substitution of such inspection technique, it must be ensured that the defined

detectable crack length given in the NDT Manual will be detectable by the new technique.

5. An inspection of the adjacent area for general condition will be accomplished as far as possible

whenever the area is entered for scheduled maintenance or rectification.

6. Where an internal inspection is specified, an adequate number of access openings shall be opened

to facilitate a detailed visual inspection.

7. A300 Airframe and Systems items which are life limited are listed in chapter 5 of the Airbus

Maintenance Manual and must be replaced as indicated therein. For APU and POWERPLANT life

limited items, see respective program rules.

8. Inspection intervals and maintenance processes may be changed in accordance with Regulator

Authority Practices in consideration of the respective program rules and notes.

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# The following applies to the FAA MRB Report.

1. The carrier's manual shall contain the details and responsibilities for accomplishing the

maintenance required by this schedule.

2. The overall reliability of the A300 will be monitored by each carrier's system for continuous analysis

and surveillance as required by FAR 121.373 and in sufficient depth to satisfy the assigned FAA

Inspector.

3. Condition monitoring programs shall be established and administered in accordance with the

procedure described in FAA Order 8310.4A.

4. All units identified in this program, except those items listed with a hard time overhaul, or "On

Condition" (OC), will be controlled on a Condition Monitoring Program. In addition, the Operator's

Condition Monitoring Program(s) must be either described or appropriately referenced in his

Operations Specifications - Maintenance.

5. On all items for which the inspection or overhaul interval has been established as "On Condition"

(OC), the requirements of advisory Circular 121-1 apply. Refer to Definitions.

6. The inspection periods and overhaul times shown in this document may be escalated in

accordance with accepted FAA practices after sampling requirements have been met.

7. Each operator should be cognizant of the numerous inspection techniques, such as "X-Ray",

"sonic", "eddy current", "radio isotope", etc. which are available. The use of such techniques can be

developed to provide a valuable adjunct to the prescribed visual inspection specified in the A300

maintenance Program. Any substitution of inspection techniques mentioned above, in lieu of visual

inspections, must have prior FAA approval.

8. Actual flight hours (time in service) or cycles if specified, for each individual aircraft must be applied

in determining when the maintenance check periods, reliability integrity checks or overhaul intervals

are required.

9. An inspection of the adjacent area will be accomplished whenever other scheduled maintenance is

specified, such as when cable inspections or structural inspections are made.

10. Wherever an internal inspection is specified, an adequate number of access openings, external and

internal, shall be opened to facilitate a thorough visual inspection of the specified zone.

11. A300 airplane components which are life limited are listed in Chapter 5 of the DGAC - Approved

Airbus Maintenance Manual - and must be replaced as indicated therein.

12. Within this document the terms "checks", "inspection" and "examination" are used interchangeably

and are not intended to imply a level of skill required to accomplish the task.

13. Inspections, hydrostatic test and life limits will be accomplished as set forth in Part 173, Chapter 1,

Subpart B of CFR 49 currently in effect. For foreign manufactured containers identify, retire and test

per manufacturer's technical data currently in effect.

11. IMPLEMENTATION PERIOD

A. General

The IMPLEMENTATION PERIOD is a Grace period for the first time accomplishment of new tasks

added to a Maintenance Program of an aircraft already in service.

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# The MPD provides a summary of tasks originating from other documents such as the MRB Report,

CMRs, ALIs, Inspection Service Bulletins and Service Information Letters. Since the origin of these

recommendations varies from 'mandatory' to 'potential economic benefit' it is not appropriate to

have a common policy regarding 'implementation period' that can be applied to all tasks.

Airbus provides this information for guidance to those operators who do not already have locally

agreed procedures. It is not intended that introduction of this paragraph in the MPD causes any

operator or Regulatory Authority to have to change existing practices.

The following paragraphs suggest Implementation Periods for the tasks originating from the various

MPD source documents. The Implementation Period, often referred to as a “Grace” period, is to

assist with first time accomplishment of new tasks added to a maintenance program of an aircraft

already in service.

B. AD/CN

The compliance date is identified in the CN/AD. This is mandatory though operators may have a

process to discuss Alternate Means of Compliance.

C. Airworthiness Limitations Items (ALIs) – ALS Part 2

ALIs are added to a program after entry into service since the figures are not determined until

completion of full scale fatigue tests (typically 5 to 6 years after EIS). These tasks have intervals

quoted in FH/FC, not calendar time. To ensure they are included in operators programs, the EASA

and FAA now intend to issue an AD/CN. This will only be issued when an ALI issue contains more

restrictive data than the previous issue.

Airbus plan to publish ALIs at least two years bef ore they become due on the first aircraft. In cases

where this two year period is not achieved, it is recognized that it may be difficult (or impossible) to

schedule the task on a particular airframe before it comes due. In such cases, Airbus will review the

particular utilization and type of operation to determine if an alternate means of compliance can be

developed.

Airbus is not normally able to issue a generic grace period for ALIs. ALI grace periods must be

handled on a case by case basis, using specific utilization data from concerned aircraft. Operators

should ensure they do not exceed the limitation without prior agreement with the manufacturer, the

local airworthiness authority and the certificating authority. In exceptional circumstances an ALI

may be issued which is already overdue on a par ticular aircraft. In such cases Airbus will provide

guidance in the transmittal letter. Operators may also contact Airbus for specific advice.

D. Certification Maintenance Requirements (CMRs) – ALS Part 3

In theory, a CMR cannot be added, or an existing CMR made more restrictive, to an in-service

aircraft. All CMRs should be published before the subject design feature enters service, whether

this is on the basic aircraft or as a result of a modification. If delays occur in CMR document

approval it is possible that a CMR becomes valid after EIS. In this case, the CMR document

transmittal letter will advise an appropriate grace period before first time accomplishment.

E. Aging System Maintenance (ASM) – ALS Part 4

ASM tasks were added before first aircraft reached the original Design Service Goal - DSG (60.000

FH / 48.000 FC). Tasks have a threshold at or beyond the DSG figure and shall be accomplished

when due.

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# F. Fuel Airworthiness Limitation Items (FAL) – ALS Part 5

On aircraft that have already exceeded the task threshold, Airbus recommend that the FAL tasks

are performed at the operator's next scheduled structural inspection at 5 YE or 9 YE.

G. MRB Report and MRB Report Temporary Revision (TR)

MRB Report (MRBR) tasks arise fr om a theoretical analysis of the aircraft prior to entry into service.

Tasks are categorized according to whether they are associated with hidden or evident conditions

and according to their contribution to the avoidance of safety and non-safety related failure effects.

These categories give an idea of 'importance' or 'criticality' (FEC 5, 8, 9, 6 and 7 decreasing order

of importance) and allow a different grace period policy to be established for different groups.

The MRBR is a report containing the initial minimum scheduled maintenance/inspection

requirements for derivative or newly type certified transport category aircraft. Operators of the

aircraft type should implement the MRB Report, or revisions thereto, in accordance with established

procedures. It should be noted that the MRBR is not the aircraft maintenance program but does

provide the initial basis for such a program. Depending on an operator's qualifications and overall

maintenance experience, adjustments to initial maintenance program tasks and intervals may be

approved by the operator's National Aviation Authority.

National regulations vary as to how an operator controls his program after entry into service.

Typically, a Reliability Control Program (RCP) will be developed that will identify changes

necessary to maintain an acceptable level of continued airworthiness, operational capability and

economic operation. Some operators may move off the MRBR and rely entirely on their RCP

together with CN/ADs and, sometimes, Service Bulletins.

According to regulations, operators are required to assess all new recommendations made in

revisions to MRB Reports. Though Airbus expect operators to reflect these in their programs there

is no requirement for this (though an operator will normally be asked to justify any deviations).

Airbus leave it to the operator’s engineering judgment as to when a new task should be applied for

the first time, or when a revised task should be applied at the next time after interval change.

Operators are normally able to understand the reasons for the task and thus assess the relative risk

and impact caused by delayed accomplishment (if they chose to incorporate it at all).

Airbus suggest that a local guideline could be as follows:

– For Systems/APU/Powerplant and ZIP tasks

Perform at the next due interval. This might not be the next interval (for which the planning may be

completed) but it would be expected in the following one.

NOTE: If task elapsed time is short and any possible corrective action is easily addressed, operator

should consider first performance of at least the FEC 5 and 8 tasks in the next convenient

A– CHECK package.

NOTE: It is recognized that in some cases access is not available at the first two C– CHECK

intervals, for example, fuel tank entry, galley or lavatory removal. In these cases, unless

stated otherwise in the MRB Report transmittal letter, Airbus recommend accomplishment at

the next due interval.

– For CPCP related tasks

A revised CPCP requirement is normally associated with corrosion findings. In case of overruns,

the concerned operator needs to consider his local operating conditions in order to assess the

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# potential for corrosion in this area on his particular aircraft. It is recommended to perform the task

as soon as possible on at least one aircraft in the fleet in order to help make this assessment.

Delay in accomplishment may lead to higher repair costs but not a loss of continued airworthiness.

Note that if a safety concern exists, a new CPCP task recommendation on an in-service aircraft

would be promulgated by ISB (and possibly CN/AD) in addition to inclusion in the MRB Report.

– For EZAP Tasks

On aircraft that have already exceeded the task threshold, Airbus recommend that the EZAP tasks

are performed at the operator's next convenient C-check opportunity unless access is assessed as

insufficient to perform the task without exceeding the scheduled out-of-service period.

H. Inspection Service Bulletins / All Operator Telexes

As for AD/CN, these documents normally include a recommended compliance time. Where this is

not stated, it is recommended that the operator follows the guidance given under para E (MRB

Report).

I. Service Information Letters

It is recommended that operators follow the guidance given under paragraph E in the MRB Report.

12. EXCEPTIONAL VARIATIONS TO MAINTENANCE PROGRAM PERIODS

GENERAL

A permitted variation should normally be granted by the Authority, unless the Authority has agreed to

delegate such possibility to the operator. A permitted variation to a period required by the maintenance

programme may be granted by the Authority on a case-by-case basis on occasions where the operator

does not have the ability to perform the required maintenance within the prescribed limits. Contrary to

an amendment to the Maintenance Programme, a permitted variation applies to a unique aircraft, for a

unique occasion.

A permitted variation should not be understood to be a maintenance planning tool, but as an

exceptional means to allow the operator to fly for a limited period of time until the required maintenance

is performed. It therefore follows, that acceptable reasons for requesting a permitted variation may

include unforeseen workload peak in the maintenance organization, so that it is not physically possible

to perform the required maintenance on time.

Permitted variations do not apply to:

1. Life limitations

2. Airworthiness Directives

3. Maintenance Programme tasks which have been classified as mandatory by the TC Holder or the

Authority

4. Certification Maintenance Requirements, unless specified otherwise in the MRB Report, and

agreed by the Authority (ref. “Two star” CMR’s from ACJ 25.1309)

NOTE: The above does not mean that the Authority cannot vary an AD, Life Limitation etc., but that this

paragraph does not apply to such variations.

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# MAXIMUM VARIATIONS

The maximum variation of a prescribed period is indicated below:

1. Items controlled by flight hours:

(i) 5000 flying hours or less: 10%

(ii) More than 5000 flying hours: 500 flying hours

2. 2. Items controlled by calendar time:

(i) 1 year or less: 10% or 1 month whichever is the lesser

(ii) More than 1 year, but not exceeding 3 years: 2 months

(iii) More than 3 years: 3 months

3. Items controlled by landing/cycles:

(i) 500 landings/cycles or less: 5% or 25 landing/cycles, whichever is the lesser.

(ii) More than 500 landings/cycles: 5% or 250 landings/cycles, whichever is the lesser.

4. Items controlled by more than one limit:

For items controlled by more than one limit, e.g. items controlled by flying hours and calendar time

or flying hours and landings/cycles, the more restrictive limit should be applied.

13. METHOD OF MPD TASK PRESENTATION

A typical example of the A300 task presentation form is shown on the next page.

A. Task Number

The task number consist of eleven digits grouped as follows:

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# B. ATA reference or Zone

– Systems and Components, APU and Powerplant task numbers use the ATA 100 Breakdown

classification.

– Structure task number refer to the SSI, ALI or CPCP numbers as indicated in the relevant source

document.

– Zonal task numbers are identified by the letter code "ZL" followed by the concerned major zone or

sub-major zone in accordance with the A300 Aircraft Zoning (Ref. to Appendix).

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# C. Section and Task Code

Task Sections and Task Codes differ as follows:

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# Task Section 4 –0402– External Inspections

–0403– Internal Inspections

Task Section 5 –0502– Visual Checks and Inspections

–0503– Functional and Operational Checks

–0504– Off Aircraft Maintenance

–0505– Servicing and Lubrication Tasks

Task Section 6 –0602– External Inspections

–0603– Internal Maintenance Tasks

–0604– Internal Inspections (for alternative sampling inspections

ref. to section 16)

Task Section 7 –0702– Garret APU TSCP 700 Inspections

–0702– Inspections At Opportunity of APU Change

–0702– Servicing and Lubrication Tasks

Task Section 8 –0801– GE CF6-50

–0802– On Aircraft Opportunity Inspection

–0603– Off Aircraft Opportunity Inspection at Shop Visit

–0804– At Shop-Visit Disassembly

–0805– Servicing and Lubrication Tasks

–0811– PW JT6D-59A

–0812– On Aircraft Opportunity Inspection

–0813– Off Aircraft Opportunity Inspection at Shop Visit

–0814– At Shop-Visit Disassembly

–0815– Servicing and Lubrication Tasks

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# D. Zone Column

The zone column defines where the major part of the maintenance task requirement is to be carried

out on the aircraft.

E. Description Column

This column provides the following information:

1. Task Title

Identifies the system/sub-system/component, zone , SSI, SSD or CPCP item concerned.

2. Task Code

Specifies the type of task to be carried out:

CHK: Check

CLN: Cleaning

DET: Detailed Inspection

DRN: Drain, Servicing

FUC: Functional Check/Test

GVI: General Visual Inspection

LUB: Lubrication

OPC: Operational Check/Test

RAR: Remove and Replace

SDI: Special Detailed Inspection

SEV: Servicing

3. – Skill Code

Specifies the type of skill required for task accomplishment.

ELO:

Tasks related to the electronic parts of the following systems:

– Autoflight (ATA 22),

– ECAM, DFDR and optional computers in AIDS,

– Navigation (ATA 34 including DADC and FMS),

– Air data,

– Indicating systems.

Systems and components but involving A/C computers or control boxes such as:

– Operational test of system monitoring circuits (e.g. flight control jamming detection), Flap Slat

asymmetry,

– System BITE.

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# ENG:

Tasks related to powerplant/APU and including zonal related tasks.

ERI:

Tasks related to:

The electrical power generation and distribution (servicing of IDGs and APU generators not

Included).

The electrical part of systems and components such as:

– Ignition system,

– Electrical valves,

– The internal and external lighting,

– All pressure switches, differential pressure switches, control and indicating sensors.

This does not encompass systems/components involving computers.

INS:

Tasks related to oxygen system.

MEC:

Typical airframe task such as:

– General visual checks/inspections,

– Zonal inspections.

Servicing tasks requiring a certain qualification level such as:

– Flaps/slats gearboxes/screwjacks,

– Landing gear shock absorbers,

– Landing gear pitch dampers,

– THS actuator.

Tasks related to:

– The hydromechanical part of systems and components,

– The structure and requiring a certain qualification level for proper detection of expected

damage,

– Pneumatic valves (ATA 21),

– The airframe, systems and components but requiring no special qualification such as

lubrication (with spray, brush, oil can or grease gun) or cleaning (LDG sliding tubes, flaps/slats

tracks and rollers).

NDT:

Non-Destructive testing.

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# RAD:

Tasks related to radio and radio-navigation systems such as:

– Receivers, transceivers, transponders,

– Antennas,

– Audio interphone system, CVR, Passenger Address system.

4. Task Description

Contains concise description of the maintenance task to be performed.

5. Note

Where given it states further requirements and/or provides useful information.

6. Access

Where given it lists all access panels and doors that are required to be opened/removed prior

to the task accomplishment.

7. Preparation

Where given, specifies the preliminary steps to be performed prior to the maintenance task.

F. Threshold/Interval Column

This column is used to record the selected interval (I) and threshold (T) for the task. The interval (I)

and threshold (T) may be expressed in terms of "Letter Checks", "Usage Parameters" or "Program

Notes". The interval defines for a specific maintenance task the maximum period between two

successive inspections.

For Letter Check. Usage parameters can be expressed in:

"FH" (Flight Hours)

"FC" (Flight Cycles)

"LG" (Landings)

"CY" (Cycles)

"AH" (APU Hours)

"MO" (Months)

"YE" (Years)

Other interval expressions and program notes ) are explained hereafter:

Note 5-1: To be accomplished in accordance with vendor recommendation.

Note 5-2: To be determined by individual operator experience.

Note 5-3: To be accomplished in accordance with national requirements.

“VR” according to Vendor's Recommendations

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# Where two intervals are given the task is due at the interval which comes first.

G. Source Code Column

As a general rule, each scheduled maintenance task requires an initial source document prior to its

introduction in the A300 MPD. The abbreviations located in this column indicate the origin of the

task.

MRB : arising from the MRB.

MRB ** : arising from the MRB as a "MUST BE DONE" task or included

to comply with certification requirements.

MRB S : arising from the MRB as a structural sensitive area/zone.

MRB Z : arising from the MRB Zonal Inspection Program.

CMR* : Task intervals quoted in the document AI/ST5/849/85 cannot

be increased unless advised by the manufacturer following

approval by the Type Certification Authority. In general, world

fleet in-service experience will not provide escalation

justification.

CMR** : Task intervals quoted in the document AI/ST5/849/85 may be

increased only in accordance with escalation by the operator's

Maintenance Authority.

CPCP : arising from the Corrosion Prevention and Control Program.

ALI : arising from the A300 Airworthiness Limitation Items

Document.

CN, AD : Task originated by an Airworthiness Directive.

AOT, ISB, SIL, OIT : Task originated by an All Operator Telex (AOT), OIT Inspection

Service Bulletin (ISB), Service Information Letter (SIL) or

Operator Information Telex (OIT).

AOW : Task originated by an All Operator Wire (AOW) for engine

manufacturer only.

CESM, MAN, EMP : Task originated by a Commercial Engine Service Memorandum

(CESM), a Maintenance Advisory Notice (MAN) or a Engine

Management Plan (EMP), for engine manufacturer only.

MPD : Task recommended from the manufacturer.

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# H. Reference Column

This column provides reference to technical documentation where maintenance

practices/Procedures necessary for the task accomplishment are provided, e.g.:

AMM - Aircraft Maintenance manual

NTM - Non-Destructive Testing Manual

ALI - Airworthiness Limitation Items Document

and, for special requirements, reference of originating documents, where appropriated, e.g.:

AD, CN – Airworthiness Directives

AOW – All Operator Wire

C – Corrosion Prevention and Control Program

ISB – Inspection Service Bulletin

SIL – Service Information Letter

OIT – Operator Information Telex

CESM – Commercial Engine Service Memorandum

MAN – Maintenance Advisory Notice

EMP – Engine Management Plan

I. Men - M/H (Manhours) Columns

The information quoted in these columns indicate the required manpower and time for

accomplishment of the task and opening/closing the access. These manhours are expressed in

hours and in tenth of hours.

The quotation for the manhours assume the following conditions:

1. Good environmental, e.g. clean, dry adequate lighting.

2. Access platforms in position.

3. Standard tools, special tools and ground support equipment readily available.

4. Skilled maintenance personnel familiar with the aircraft.

5. Availability of all maintenance documentation.

6. All required spare parts and consumables are available.

7. All access panels, linings and/or insulation are open/removed.

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# The required number of persons for the ACCESS is indicated in the “MEN” column with a "*" only.

The quoted access time includes the opening and closing time for the listed access panel(s).

J. Applicability Column

The APPLICABILITY column indicates the applicability as follows:

(a) Aircraft series and model

e.g.:

ALL : effective for all A300 models.

B2 : effective for all A300B2 models.

Bx–xxxFF : effective for all A300B2-203FF, A300B4-203FF, A300B4 220FF

models.

B4 : effective for all B4-100 and B4-200 models.

B4–100 : effective for all A300B4-100.

B4–200 : effective for all A300B4-200.

C4 : effective for all A300C4-203 models.

F4 : effective for all A300F4-203 models.

GE : effective for a/c equipped with GE engines.

PW : effective for a/c equipped with PW engines.

(b) Modification Configuration (PRE or POST Mod. status)

e.g.:

PRE 2988 : stands for all aircraft on which Modification 2988 is NOT

embodied.

POST 5366

27–1057 : stands for all aircraft on which Modification 5366 is embodied or

where the associated SB 27-1057 is embodied.

POST 4356

PRE 4698 : stands for all aircraft on which Modification 4356 is embodied and

on which modification 4698 is NOT embodied.

POST 4356 : stands for all aircraft on which Modification 4356 is embodied or

Modification 4698 is NOT embodied.

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# or

PRE 4698

POST 4356

POST 4698

or

POST 6005 : stands for all aircraft on which, either both, Modification 4356 and

Modification 4698 are embodied or Modification 6005 is

embodied.

(c) Individual Items

e.g.:

MSN 256 : stands for MSN 256 only.

MSN 001

to

MSN 015 : MSN 001 up to and including 015.

ALL EXCL.

MSN 001

to

MSN 015 : excludes MSN 001 thru 015 from all other A300

models.

KRUG. FLAP : identifies all a/c equipped with Krueger Flaps.

NON KRUG.

FLAP : identifies all a/c not equipped with Krueger Flaps.

AIR CHILLER

P/N XXXXXX : identifies all affected Air Chiller P/N(s).

NON-FWD FACE

POST 2372 : identifies all a/c not equipped with a “FORWARD

FACE” Cockpit.

PW

NON-FWD FACE : identifies all a/c equipped with PW engines and not

equipped with a “FORWARD FACE” Cockpit.

LOV : identifies structural inspection tasks for which the

Operation is allowed up to the 'Limit of Validity' (LOV)

as defined in A300 ALI. The relevant LOV values are

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ISSUE:APR 01/10 GENERAL INTRODUCTION Page 21 

# stated below for each aircraft model.

– A300-B2-1C 60000 FC / 65000 FH whichever comes FIRST

– A300-B2K-3C 60000 FC / 65000 FH whichever comes first

– A300-B2-202 60000 FC / 65000 FH whichever comes first

– A300-B2-203 60000 FC / 65000 FH whichever comes first

– A300-B4-2C 57000 FC / 76000 FH whichever comes first

– A300-B4-103 57000 FC / 76000 FH whichever comes first

– A300-B4-120 57000 FC / 76000 FH whichever comes first

– A300-B4-203 57000 FC / 118000 FH whichever comes first

– A300-B4-220 57000 FC / 118000 FH whichever comes first

– A300-C4-203 57000 FC / 118000 FH whichever comes first

– A300-F4-203 57000 FC / 118000 FH whichever comes first

From 0 FC

to

xxx FC : This column indicates the period to which the specific

task is due. In cases where “LOV” is indicated, refer to

the above-mentioned limits.

14. GLOSSARY

APU Change (AC)

The interval term "APU Change" means the opportunity arising at some time between initiating removal

of an APU and completing installation of an APU, irrespective of whether the same APU is reinstalled or

it is replaced by a new or overhauled one.

APU Cycle(s) (CY)

A complete APU cycle.

APU Hour(s) (AH)

The APU operating time from start-up to shut-down.

Calendar Times (DY MO, YE)

Day : A period of 24 consecutive hours.

Month(s) : A period of one calendar month.

Year(s) : A period of 12 consecutive months.

Detailed Inspection (DVI, DET)

An intensive visual examination of a specific detail, assembly or installation.

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ISSUE:APR 01/10 GENERAL INTRODUCTION Page 22 

# It searches for evidence of damage or irregularity using adequate lighting and, where necessary,

inspections aids such as mirrors, hand lens, etc. Surface cleaning and elaborate access procedures

(including removal of components where necessary) may be required.

Discard (DIS)

The removal from service of an item at a specific life limit.

Engine Change (EC)

The interval term "Engine Change" means the opportunity arising at some time between initiating

removal of an Engine and completing installation of an Engine, irrespective of whether the same Engine

is reinstalled or it is replaced by a new or overhauled one.

Engine Cycle(s) (CY)

A complete engine thermal cycle which includes the application of take-off power.

Flight Cycle(s) (FC)

A complete take-off and landing sequence.

Flight Hour(s) (FH)

The accumulated time interval between "wheels-off" until "wheels-on".

Functional Test (FUC)

A quantitative check to determine if one or more functions of an item performs within specified limits.

General Visual Inspection (GVI)

A visual examination of an interior or exterior area, including structure, systems, installation and

assembly, to detect obvious damage, failure or irregularity. This level of inspection is made under

normally lighting conditions such as daylight, hangar light or flashlight by approx. "arm length"

inspection distance to the object. This type of inspection may require removal of fillets, fairings, access

panels/doors, etc., as well as ladders, platforms or workstands.

Interval

The period expressed in letter code, cycles, hours and/or calendar time, between successive

accomplishment of a specific task.

Landing

An operation of an aircraft touching the runway and coming to a complete stop or performing a "touch

an go".

Lubrication and Servicing (LUB)

Term covering all types of lubrication (by application of e.g. grease gun, squirt can, spray, brush or

hand), or servicing (e.g. top-up of hydraulic fluid/oil) for the purpose of maintaining the inherent design

operating capabilities of an item.

Maintenance Task

An action or set of actions required to achieve a desired outcome which restores an item (area,

component, system, subsystem, structure) or maintains an item in serviceable condition, including

inspection and determination of condition.

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# Maintenance Significant Item (MSI)

A system related item identified by the manufacturer whose failure:

– Could affect safety (ground or flight), and/or

– Is undetectable during operation, and/or

– Could have significant operational economic impact, and/or

– Could have significant non operational economic impact.

NDT-Inspection

Non-destructive inspection procedure, e.g. eddy current, ultra sonic.

Operational Test (OPC)

A qualitative check to determine qualitatively that an item is fulfilling its intended purpose. It is a failure

finding task and does not require quantitative tolerances.

Restoration (RES)

That work necessary (ON/OFF aircraft) to return an item to a specific standard. Restoration may vary

from cleaning or replacement of single parts up to a complete overhaul.

Sampling Inspection Program

Inspection of specific aircraft selected from those which have the highest age to identify the first

evidence of deterioration in their condition caused by corrosion or fatigue damage.

Special Detailed Inspection (SDET)

An intensive examination of a specific item(s), installation or assembly to detect damage, failure or

irregularity. The examination is likely to made extensive use of specialized inspection techniques, e.g.

dye penetrant, ultra sonic, eddy current, etc. Cleaning and substantial access or disassembly

procedures may be required.

Structural Significant item (SSI)

A structural detail, element or assembly which contributes significantly to carrying flight, ground,

pressure or control loads and whose failure could affect the structural integrity necessary for the safety

of the aircraft.

Threshold (TH)

The initial accomplishment of a specific maintenance task. It may be expressed in letter code, cycles,

hours, and/or calendar time.

Touch and Go

A "Touch and Go" is a landing in which an aircraft touches the runway and does not come to a full stop

prior to commencing an additional flight.

Visual Check (VC)

An observation to determine that an item is fulfilling its intended purpose. It does not require quantitative

tolerances. This is a failure finding task.

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# ABBREVIATIONS

The following abbreviations are used through out the present document :

AA : Airworthiness Authorities

A/C : Aircraft

AC : Alternating Current

AC : APU Change

ACARS : Aircraft Communication Addressing and Reporting System

ACC : Active Clearance Control

ACT : Additional Center Tank

ACAS : Airborne Collision Avoidance System

ACMS : Aircraft Condition Monitoring System

ACP : Area Call Panel

ACR : Avionics Communication Router

AD : FAA Airworthiness Directive

AD : Accident Damage

ADCN : Aircraft Data Communication Network

ADF : Automatic Direction Finder

ADIRS : Air Data and Inertial Reference System

ADIRU : Air Data/Inertia Reference Unit

AESS : Aircraft Environment Surveillance System

AFDX : Avionics full Duplex

AFM : Airplane Flight Manual

AFMS : Auxiliary Fuel Management System

AFS : Automatic Flight System

AFT : Rear

AGCM : Airborne Ground Check Module

AGU : Air Generation Units

AH : APU Operating Hours

AIB : Airbus

AIDS : Aircraft Integrated Data System

ALI : Airworthiness Limitation Item

AMM : Aircraft Maintenance Manual

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# AMTOSS : Aircraft Maintenance Task Oriented Support System

AOL : All Operators Letter

AOT : All Operator Telex

AOW : All Operator Wire

AP : Autopilot

APU : Auxiliary Power Unit

ARO : Anti Roll Out

ASB : Alert Service Bulletin

ASSY : Assembly

ATA : ATA Specification

ATC : Air Traffic Control

ATT : Attitude

BAT : Battery

BCL : Battery Charge Limiter

BCRC : Bulk Crew Rest Compt.

BITE : Built-In Test Equipment

BSI : Borescope Inspection

CAS : Cabin Attendant Seat

CESM : Commercial Engine Service Memorandum

CFDS : Centralized Fault Display System

CFMI : CFM International

CHG : Change

CHK : Check

CLN : Cleaning

CMP : Configuration, Maintenance and Procedure Standards (ETOPS)

CMR : Certification Maintenance Requirements

CN : Consigne de Navigabilité (French Airworthiness Directive)

COMPT : Compartment

CPCP : Corrosion Prevention and Control Program

CRR : Crew Rest Room

CSU : Command Sensor Unit

CVR : Cockpit Voice Recorder

CWB : Center Wing Box

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# CY : Cycle

D : Deleted

DC : Direct Current

DDRMI : Digital Data Radio Magnetic Indicator

DET : Detailed Inspection

DFDR : Digital Flight Data Recorder

DGAC : Direction Générale de l’Aviation Civile (French Airworthiness Authority)

DI : Detailed Inspection

DMC : Display Management Computer

DRN : Drainage

DS : Discard

DS : Discard

DU : Display Unit

DY : Day

EASA : European Aviation Safety Agency

EC : Engine Change

ECAM : Electronic Centralized Aircraft Monitoring

ECU : Engine Control Unit

ED : Environmental Deterioration

EDP : Engine Driven Pump

EFIS : Electrical Flight Instrument System

EIS : Electronic Instrument System

ELAC : Elevator and Aileron Computer

ELT : Elapsed Time

ELT : Emergency Locator Transmitter

EMER : Emergency

EMP : Engine Management Plan

ESS : Essential

ETOPS : Extended Range Twin Engined Aircraft Operations

EVAC : Evacuation

EVMU : Engine Vibration Monitoring Unit

EWIS : Electrical Wiring Interconnection System

EZAP : Enhanced Zonal Analysis Procedure

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ISSUE:APR 01/10 ABBREVIATION S Page 4 

# EXTIR : Extinguisher

FAA : United States Federal Aviation Administration

FAC : Flight Augmentation Computer

FAL : Fuel Airworthiness Limitations

FADEC : Full Authority Digital Engine Control

FC : Flight Cycle

FC : Functional Check

FCOM : Flight Crew Operating Manual

FCRC : Flight Crew Rest Compt.

FD : Flight Director

FDUI : Flight Data Interface Unit

FH : Flight Hours

FL : Flight Hours

FR : Frame

FUC : Functional Test

FWD : Forward

GAPCU : Ground and Auxiliary Power Control Unit

GCU : Generator Control Unit

GE : General Electric

GLC : Generator Line Contactor

GPCU : Ground Power Control Unit

GPWS : Ground Proximity Warning System

GSE : Ground Support Equipment

GRP x : Weight variant group “x”

GSE : Ground Support Equipment

GVI : General Visual Inspection

HDG : Heading

HIRF : High Intensity Radiated Fields

HP : High Pressure

HPT : High Pressure Turbine

HR : Hour

I : Repeat Interval

IAE : International Aero Engine

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# IDG : Integrated Drive Generator

IFES : In Flight Entertainment System

INTRO : Introduction

ISB : (Inspection) Service Bulletin

ISIS : Integrated Standby Instrument System

JAA : Joint Aviation Authorities

JAR : Joint Aviation Requirement

LD : Landing

LD : Lower Deck

LDF : Lower Deck Facility

LDG : Landing (s)

LDL : Lower Deck Lavatory

LDMCR : Lower Deck Mobile Crew Rest

LE : Leading Edge

LEP : List of Effective Pages

LGCIU : Landing Gear Control and Interface Unit

LH : Left Hand

LOV : Limit of Validity

LP : Low Pressure

LPC : Low Pressure Compressor

LPT : Low Pressure Turbine

LTA : German Airworthiness Directive

LU : Lubrication

LUB : Lubrication

LUP : Low Utilization Program

LUR : Low Utilization Recommendation

LWR : Lower

MAN : Maintenance Advisory Note

MCDU : Multipurpose Control and Display Unit

MH : Man hours

MLG : Main Landing Gear

MO : Month(s)

MOD : Modification

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ISSUE:APR 01/10 ABBREVIATION S Page 6 

# MPD : Maintenance Planning Document

MRB : Maintenance Review Board

MSG : Maintenance Steering Group

MSI : Maintenance Significant Item

MSN : Manufacturer Serial Number

N : New

ND : Navigation Display

NDT : Non Destructive Testing

NLG : Nose Landing Gear

NR : National Requirements

NRV : Non Return Valve

NT : Note

NTM : Non Destructive Testing Manual

OC : On Condition

OIT : Operator Information Telex

OP : Operational Check

OPC : Operational Test

PCU : Power Control Unit

PFD : Primary Flight Display

POB : Pressure off Brakes

PREP : Preparation

PTT : Press To Test

PTU : Power Transfer Unit

PW : Pratt & Whitney

PWS : Predictive Windshear System

QAD : Quick Attach Detach

R : Revised

RAR : Removal and Replacement

RAT : Ram Air Turbine

RES : Restoration

RH : Right Hand

RMP : Radio Management Panel

RPL : Replenishment

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# RS : Restoration

RSVR : Reservoir

S : Sampling

SB : Service Bulletin

SDET : Special Detailed Inspection

SDI : Special Detailed Inspection

SIL : Service Information Letter

SMR : Scheduled Maintenance Report (engine)

SOV : Shut off Valve

SPL : Fluid Sampling

SRV : Servicing

SSD : Significant Structural Detail

SSI : Structure Significant Item

SSID : Supplemental Structural Inspection Document

ST(G)R : Stringer

SV : Servicing

SV : Shop Visit

SYS : System

T : Transferred

TC : Tire Change

TCAS : Traffic Collision Avoidance System

TBD : To be determined

TE : Trailing Edge

TH : Threshold

THS : Trimmable Horizontal Stabilizer

TOC : Table of Content

TPIS : Tyre Pressure Indication System

TPS : Temporary Protection System

TR : Temporary Revision

TSN : Time Since New (Whatever the unit may be)

TVC : Thorough Visual Inspection

TUP : Fluid Level Check and Top Up

UD : Upper deck

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# ULB : Underwater Locating Beacon

VC : Visual Check

VCC : Video Control Center

VHF : Very High Frequency

VR : Vendor Recommendation

YE : Year

ZL : Zonal

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 EFFECTIVITY CROSS REFERENCE TABLE Page 1 

# EFFECTIVITY CROSS REFERENCE TABLE

It is intended to supply the Effectivity Cross Reference Table within this section in future revisions.

Version Rank Model MSN Registration STD Engine Operator

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SERVICE BULLETIN LIST Page 1 

# SERVICE BULLETIN LIST

It is intended to supply the Service Bulletin List within this section in future revisions.

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 SYSTEMS, APU AND POWERPLANT Page 1 

# INTRODUCTION

1. GENERAL

This section includes all scheduled maintenance tasks related to the aircraft systems including the tasks

for power plants (accessories, engine mounts, cowlings and thrust reverser) and auxiliary power unit.

NOTE: Zonal inspections and structural inspections of powerplant are provided in their own section of

this MPD respectively.

Shop maintenance tasks (off-wing) may not be included in the A300 MPD.

The Systems, APU and Powerplant Program includes scheduled maintenance tasks such as:

– visual checks and inspections,

– servicing and lubrication task,

– operational and functional checks,

– on/off a/c maintenance tasks.

– GARRETT APU TSCP 700 Inspections,

– Inspection at opportunity of APU change,

These tasks have to be accomplished on 100% basis unless otherwise stated.

Limitations of life limited parts are controlled by the manufacturer and are published in Airbus AMM

Chapter 05 "SERVICE LIFE LIMITS".

For the servicing and lubrication items this A300 MPD provides additional information in appendix 5

(Ref. to the "SERVICING CHARTS").

2. NOTES

Limitations as published by the manufacturer are available in the GARRETT APU TSCP 700

Maintenance Manual Chapter 49-20-66 and should be adhered to. This chapter contains life-limited

items which constitute the hard time (HT) parts of the program.

"Note 5-1"

means the interval for this task should be in accordance with the vendor recommendation. Refer to the

relevant Component Maintenance Manual (CMM).

"Note 5-2"

means the interval for this task should be determined by the individual operator in accordance with his

experience and environmental conditions.

"Note 5-3"

means the interval has to be in accordance with the operators national requirements.APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 201210-0505-1 121 AVIONICS COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7011 0.20 PRE 2574122 SIL 20-0321 0.20CLEANING OF EWIS INSTALLED IN THE AVIONICSCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)ACCESS: 121AF 121AL 121BF 121BL 121CF 121DF* 4.09121EF 121FF 121GF 121HF 121JF 121KF121LF 121MF 121NF 121PF 121QF 121RF121SF 121TF 121UF 121VF 121WF 121XF121YF 121ZF 131AZ 811122AF 122AR 122BF 122CF 122CR 122DF* 2.20122EF 122FF 122GF 122HF 122JF 122KF122LF 122MF 122NF 122PF 122QF 132AZ811N 201210-0505-2 121 AVIONICS COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7011 0.20 POST 2574122 SIL 20-0321 0.20CLEANING OF EWIS INSTALLED IN THE AVIONICSCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)ACCESS: 121AF 121AL 121BL 121CF 121DF 121EF* 3.73121FF 121GF 121HF 121KF 121LF 121MF121NF 121PF 121QF 121RF 121SF 121TF121UF 121VF 121WF 121XF 121YF 121ZF131AZ 811121BG 121CG 122AG 122AR 122BF 122CF* 2.41122CR 122DF 122EF 122GF 122HF 122JF122KF 122LF 122MF 122NF 122PF 122QF132AZ 811N 201210-0505-3 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.20 PRE 2574122 SIL 20-0321 0.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAVIONICS COMPARTMENT (EWIS)ACCESS: 121AF 121AL 121BF 121BL 121CF 121DF* 4.09121EF 121FF 121GF 121HF 121JF 121KF121LF 121MF 121NF 121PF 121QF 121RF121SF 121TF 121UF 121VF 121WF 121XF121YF 121ZF 131AZ 811122AF 122AR 122BF 122CF 122CR 122DF* 2.20122EF 122FF 122GF 122HF 122JF 122KF122LF 122MF 122NF 122PF 122QF 132AZ* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)201210-0505-3 * * * * * C O N T I N U E * * * * *811N 201210-0505-4 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.20 POST 2574122 SIL 20-0321 0.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAVIONICS COMPARTMENT (EWIS)ACCESS: 121AF 121AL 121BL 121CF 121DF 121EF* 3.73121FF 121GF 121HF 121KF 121LF 121MF121NF 121PF 121QF 121RF 121SF 121TF121UF 121VF 121WF 121XF 121YF 121ZF131AZ 811121BG 121CG 122AG 122AR 122BF 122CF* 2.41122CR 122DF 122EF 122GF 122HF 122JF122KF 122LF 122MF 122NF 122PF 122QF132AZ 811N 201210-0505-5 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 PRE 2574122 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF G ROUTES AND 105VU,106VU AND APU BUS (EWIS)PREP.: ELECTRICAL PANEL COVER TO BE OPENEDACCESS: 121AF 121AL 121BF 121BL 121CF 121DF* 4.09121EF 121FF 121GF 121HF 121JF 121KF121LF 121MF 121NF 121PF 121QF 121RF121SF 121TF 121UF 121VF 121WF 121XF121YF 121ZF 131AZ 811122AF 122AR 122BF 122CF 122CR 122DF* 2.20122EF 122FF 122GF 122HF 122JF 122KF122LF 122MF 122NF 122PF 122QF 132AZ811N 201210-0505-6 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 POST 2574122 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF G ROUTES AND 105VU,106VU AND BUS APU (EWIS)PREP.: ELECTRICAL PANEL COVER TO BE OPENED* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)201210-0505-6 * * * * * C O N T I N U E * * * * *ACCESS: 121AF 121AL 121BL 121CF 121DF 121EF* 3.73121FF 121GF 121HF 121KF 121LF 121MF121NF 121PF 121QF 121RF 121SF 121TF121UF 121VF 121WF 121XF 121YF 121ZF131AZ 811121BG 121CG 122AG 122AR 122BF 122CF* 2.41122CR 122DF 122EF 122GF 122HF 122JF122KF 122LF 122MF 122NF 122PF 122QF132AZ 811N 201210-0505-7 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS ANDEWIS INSIDE 101VU (EWIS)PREP.: ELECTRICAL PANEL COVER TO BE OPENEDACCESS: 121BL 131AZ 132AZ 811* 0.17N 201230-0505-1 123 NOSE GEAR BAY MEC GVI I: 24 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THENOSE GEAR WELL (EWIS)ACCESS: 713 714* 0.12N 201310-0505-1 131 FORWARD CARGO COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF ALL POWER FEEDER ROUTES INSTALLED (ONLYIF CONTAMINATED) (EWIS)PRP.: CEILING AND LINING PANELS TO BE REMOVEDACCESS: 132BZ 132CZ 132DZ 811* 0.45N 201310-0505-2 131 FORWARD CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEFWD CARGO COMPARTMENT (EWIS)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)201310-0505-2 * * * * * C O N T I N U E * * * * *PRP.: CEILING AND LINING PANELS TO BE REMOVEDACCESS: 132BZ 132CZ 132DZ 811* 0.45N 201310-0505-3 131 FORWARD CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS IN CB BOX 921 VU(EWIS)PRP.: CEILING AND LINING PANELS TO BE REMOVED (DOORAREA), ELECTRICAL PANEL COVER TO BE OPENEDACCESS: 132AR 811* 0.53N 201330-0505-1 133 BAY UNDER FWD CARGO COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7011 0.30 ALLSIL 20-032CLEANING OF ALL PDU SUPPLY ROUTES (ONLY IFCONTAMINATED) (EWIS)PRP.: ROLLERS TO BE REMOVEDACCESS: 131AAF 131ABF 131ACF 131ADF 131AEF 131AF* 9.66131AFF 131AGF 131AHF 131AJF 131AKF 131BF131CF 131DF 131EF 131FF 131GF 131HF131JF 131PF 131QF 131RF 131SF 131TF131UF 131VF 131WF 131XF 131YF 131ZF132AF 132BF 132CF 132DF 132EF 132FF132GF 132HF 132JF 132KF 132LF 132MF132NF 133AL 133AR 133BL 133BR 133CL133DL 133EL 811N 201330-0505-2 133 BAY UNDER FWD CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPCTION OF EWIS BUNDLES WITHINTHE ZONE (EWIS)PRP.: ROLLERS TO BE REMOVEDACCESS: 131AAF 131ABF 131ACF 131ADF 131AEF 131AF* 9.66* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)201330-0505-2 * * * * * C O N T I N U E * * * * *131AFF 131AGF 131AHF 131AJF 131AKF 131BF131CF 131DF 131EF 131FF 131GF 131HF131JF 131PF 131QF 131RF 131SF 131TF131UF 131VF 131WF 131XF 131YF 131ZF132AF 132BF 132CF 132DF 132EF 132FF132GF 132HF 132JF 132KF 132LF 132MF132NF 133AL 133AR 133BL 133BR 133CL133DL 133EL 811N 201370-0505-1 137 BAY AFT OF FWD CARGO COMPARTMENT MEC CLN I: 60 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS IN THE AREA AROUND OF THE PDU FEEDERPRESSURE SEALS (ONLY IF CONTAMINATED) (EWIS)ACCESS: 131BZ 131CZ 132EZ 811* 0.54N 201370-0505-2 137 BAY AFT OF FWD CARGO COMPARTMENT MEC DET I: 36 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032DETAILED INSPECTION OF EWIS IN AREA OF PRESSURE SEALSLH/RH (EWIS)ACCESS: 131BZ 131CZ 132EZ 811* 0.54N 201370-0505-3 137 BAY AFT OF FWD CARGO COMPARTMENT MEC GVI I: 60 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS WITHIN THEZONE (EWIS)ACCESS: 131BZ 131CZ 132EZ 811* 0.54N 201410-0505-1 141 CENTER WING BOX MEC GVI I: 144 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THECENTER BOX (EWIS)ACCESS: 147AZ 148AZ 734 744* 0.65SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 201410-0505-2 141 CENTER WING BOX MEC DET I: 144 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032DETAILED INSPECTION OF EXPOSED EWIS WITHIN THEZONE (EWIS)ACCESS: 147AZ 148AZ 734 744* 0.65N 201430-0505-1 143 AIR CONDITIONING COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAIR CONDITIONING COMPARTMENT (EWIS)ACCESS: 143AF 143BF 143CF 143DF 143FL 144DR* 0.81144FR 147BZ 734 744N 201450-0505-1 145 PRESSURIZED ZONE BETWEEN WING CENTER BOX MEC CLN I: 72 MO SIL AMM 249200/7011 0.60 ALLMAIN GEAR WELL AND CABIN FLOOR SIL 20-032CLEANING OF EWIS INSTALLED IN THE PRESSURIZED ZONEBETWEEN WING CENTER BOX MAIN GEAR WELL AND CABINFLOOR (ONLY IF CONTAMINATED) (EWIS)PRP.: TOILETS, GALLEYS (IF INSTALLED), SEATS ANDINSULATION TO BE REMOVEDACCESS: 241AYF 241BBF 241BCF 241BDF 241BEF 241CZ* 4.76241DZ 242AAF 242ABF 242ADF 242AEF 242AFF242AHF 242AJF 242AKF 242ALF 242AMF 242ANF242APF 242AQF 242ARF 242ASF 242ATF 242AUF242CZ 242DZ 242VF 242WF 242XF 242YF242ZF 831 841N 201450-0505-2 145 PRESSURIZED ZONE BETWEEN WING CENTER BOX MEC GVI I: 72 MO SIL AMM 249200/6011 0.90 ALLMAIN GEAR WELL AND CABIN FLOOR SIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEPRESSURIZED ZONE BETWEEN WING CENTER BOX MAIN GEARWELL AND CABIN FLOOR (EWIS)PRP.: TOILETS, GALLEYS (IF INSTALLED), SEATS ANDINSULATION TO BE REMOVED* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)201450-0505-2 * * * * * C O N T I N U E * * * * *ACCESS: 241AYF 241BBF 241BCF 241BDF 241BEF 241CZ* 4.76241DZ 242AAF 242ABF 242ADF 242AEF 242AFF242AHF 242AJF 242AKF 242ALF 242AMF 242ANF242APF 242AQF 242ARF 242ASF 242ATF 242AUF242CZ 242DZ 242VF 242WF 242XF 242YF242ZF 831 841N 201470-0505-1 147 MAIN LANDING GEAR WELL AND HYDRAULIC MEC GVI I: 12 MO SIL AMM 249200/6011 0.60 ALLCOMPARTMENT SIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN MAINLANDING GEAR WELL AND HYDRAULIC COMPARTMENT (EWIS)ACCESS: 734 744* 0.20N 201510-0505-1 151 AFT CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS IN CB BOX 923VU(EWIS)PRP.:CEILING AND LINING PANELS REMOVED, ELECTRICALPANEL COVER TO BE OPENEDACCESS: 812* 0.01N 201510-0505-2 151 AFT CARGO COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAFT CARGO COMPARTMENT (EWIS)PRP.:CEILING AND LINING PANELS REMOVEDACCESS: 812* 0.01N 201530-0505-1 153 BAY UNDER AFT CARGO COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF PDU SUPPLY EWIS (ONLY IF CONTAMINATED)(EWIS)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)201530-0505-1 * * * * * C O N T I N U E * * * * *PRP.:ROLLERS TO BE REMOVEDACCESS: 151AF 151BF 151CF 151DF 151EF 151FF* 15.27151GF 151HF 151JF 151KF 151LF 151MF151NF 151PF 151QF 151RF 151SF 151TF151UF 151VF 151WF 151XF 151YF 152AF152BF 152CF 152DF 152EF 152FF 152GF152HF 152JF 152KF 812N 201530-0505-2 153 BAY UNDER AFT CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEBAY UNDER AFT CARGO COMPARTMENT (EWIS)PRP.:ROLLERS TO BE REMOVEDACCESS: 151AF 151BF 151CF 151DF 151EF 151FF* 15.27151GF 151HF 151JF 151KF 151LF 151MF151NF 151PF 151QF 151RF 151SF 151TF151UF 151VF 151WF 151XF 151YF 152AF152BF 152CF 152DF 152EF 152FF 152GF152HF 152JF 152KF 812N 201610-0505-1 161 BULK CARGO COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEBULK CARGO COMPARTMENT(EWIS)PRP.:LININGS AND CEILING PANELS TO BE REMOVEDACCESS: 813* 0.01N 201630-0505-1 163 BAY UNDER BULK CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEBULK CARGO COMPARTMENT(EWIS)ACCESS: 161AF 161BF 161CF 161DF 161EF 161FF* 3.12161GF 162AF 162BF 162CF 162DF 162EF162FF 162GF 813SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 201710-0505-1 171 AFT CABIN UNDERFLOOR COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAFT CABIN UNDERFLOOR COMPARTMENT(EWIS)ACCESS: 162AZ 171AF 171AZ 172AF 172BF 813* 0.31N 202110-0505-1 211 FLIGHT COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.30 ALLSIL 20-032CLEANING OF EWIS INSTALLED IN THE FLIGHTCOMPARTMENT(ONLY IF CONTAMINATED) (EWIS)PRP.:(IF INSTALLED), SIDEWALL AND CEILING PANELS,REMOVABLE VERTICAL LINING, LININGS, SEATS - ALLELECTRICAL PANEL COVERS "VU" TO BE OPENEDACCESS: 211AF 211AZ 211BF 211CF 211DF 211EF* 3.24211FF 211GF 211HF 211JF 211KF 211LF211MF 211NF 211PF 212AF 212BF 212CF212DF 212EF 212FF 212GF 212HF 212JF212KF 212LF 212MF 831 841N 202110-0505-2 211 FLIGHT COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEFLIGHT COMPARTMENT (EWIS)PRP.:(IF INSTALLED), SIDEWALL AND CEILING PANELS,REMOVABLE VERTICAL LINING, LININGS, SEATS - ALLELECTRICAL PANEL COVERS "VU" TO BE OPENEDACCESS: 211AF 211AZ 211BF 211CF 211DF 211EF* 3.24211FF 211GF 211HF 211JF 211KF 211LF211MF 211NF 211PF 212AF 212BF 212CF212DF 212EF 212FF 212GF 212HF 212JF212KF 212LF 212MF 831 841N 202110-0505-3 211 FLIGHT COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSIDE THEPANEL 120VU (EWIS)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)202110-0505-3 * * * * * C O N T I N U E * * * * *PRP.:(IF INSTALLED), ELECTRICAL PANEL COVER 120 VUTO BE OPENEDACCESS: 831 841* 0.20N 202210-0505-1 221 FORWARD MAIN DECK UTILITY AREAS MEC GVI I: 144 MO SIL AMM 249200/6011 0.60 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED ATFORWARD MAIN DECK UTILITY AREAS (EWIS)PRP.:(IF INSTALLED), GALLEYS AND TOILETS , (IFINSTALLED) SIDEWALL LININGS TO BE REMOVEDACCESS: 831 841* 0.20N 202230-0505-1 223 FWD MAIN DECK UTILITY OVERHEAD MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLCOMPARTMENT SIL 20-032CLEANING OF G, E AND P ROUTES WITHIN THE ZONE (ONLYIF CONTAMINATED) (EWIS)PRP.:(IF INSTALLED), CEILING PANELS, GALLEYS TOILETSIF INSTALLED) TO BE REMOVEDACCESS: 831 841* 0.20N 202230-0505-2 223 FWD MAIN DECK UTILITY OVERHEAD MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLCOMPARTMENT SIL 20-032GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS ANDEWIS INSIDE 800VU (EWIS)PRP.:(IF INSTALLED), ELECTRICAL PANEL COVER TO BEOPENEDACCESS: 831 841* 0.20SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 202230-0505-3 223 FWD MAIN DECK UTILITY OVERHEAD MEC GVI I: 144 MO SIL AMM 249200/6011 0.50 ALLCOMPARTMENT SIL 20-032GENERAL VISUAL INSPECTION OF EWIS IN THE FWD MAINDECK UTILITY OVERHEAD COMPARTMENT (EWIS)PRP.:(IF INSTALLED), CEILING PANELS, GALLEYS, TOILETS(IF INSTALLED) TO BE REMOVEDACCESS: 831 841* 0.20N 202310-0505-1 231 FWD MAIN DECK COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS CONNECTIONSBETWEEN SEATS AND AIRCRAFT AND THE WIRING AT THESEATS INSTALLED AS FAR AS VISIBLE, IN THE FWD MAINDECK COMPARTMENT AREANOTE:THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS ONLY, AND IF ELECTRONICALLY EQUIPED.(EWIS)ACCESS: 831 841* 0.20N 202310-0505-2 231 FWD MAIN DECK COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS INSTALLED FWD MAIN DECK COMPARTMENT(ONLY IF CONTAMINATED) (EWIS)PRP.:(IF INSTALLED),GALLEYS AND TOILETS (IFINSTALLED, IF NECESSARY), SEATS (IF INSTALLED)AND SIDEWALL LININGS IN EWIS AREASACCESS: 831 841* 0.20N 202310-0505-3 231 FWD MAIN DECK COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEEWIS INSTALLED IN THE FWD MAIN DECK COMPARTMENT.(EWIS)PRP.:(IF INSTALLED),GALLEYS AND TOILETS (IF* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)202310-0505-3 * * * * * C O N T I N U E * * * * *INSTALLED, IF NECESSARY), SEATS (IF INSTALLED)AND SIDEWALL LININGS IN EWIS AREASACCESS: 831 841* 0.20N 202330-0505-1 233 FWD MAIN DECK OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS INSTALLED IN THE FWD MAIN DECKOVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS(IF INSTALLED)ACCESS: 831 841* 0.20N 202330-0505-2 233 FWD MAIN DECK OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEFWD MAIN DECK OVERHEAD COMPARTMENT (EWIS)PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS(IF INSTALLED)ACCESS: 831 841* 0.20N 202410-0505-1 241 CENTER MAIN DECK COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032(SEE NOTE)GENERAL VISUAL INSPECTION OF EWIS CONNECTIONSBETWEEN SEATS AND AIRCRAFT AND THE EWIS AT THE SEATSINSTALLED AS FAR AS VISIBLE, IN THE CENTER MAINDECK COMPARTMENT AREA (EWIS)NOTE:THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS ONLY, AND IF ELECTRONICALLY EQUIPED.ACCESS: 831 841* 0.20N 202410-0505-2 241 CENTER MAIN DECK COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)202410-0505-2 * * * * * C O N T I N U E * * * * *CLEANING OF EWIS INSTALLED IN THE CENTER MAIN DECKCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PRP.:(IF INSTALLED),GALLEYS AND TOILETS (IFINSTALLED, IF NECESSARY), SEATS (IF INSTALLED)AND SIDEWALL LININGS IN EWIS AREASACCESS: 831 841* 0.20N 202410-0505-3 241 CENTER MAIN DECK COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THECENTER MAIN DECK COMPARTMENT (EWIS)PRP.:(IF INSTALLED),GALLEYS AND TOILETS (IFINSTALLED, IF NECESSARY), SEATS (IF INSTALLED)AND SIDEWALL LININGS IN EWIS AREASACCESS: 831 841* 0.20N 202430-0505-1 243 CENTER MAIN DECK OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS INSTALLED IN THE CENTER MAIN DECKOVERHEAD COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS(IF INSTALLED)ACCESS: 831 841* 0.20N 202430-0505-2 243 CENTER MAIN DECK OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.20 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THECENTER MAIN DECK OVERHEAD COMPARTMENT (EWIS)PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS(IF INSTALLED)ACCESS: 831 841* 0.20SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 202510-0505-1 251 AFT MAIN DECK COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032(SEE NOTE)GENERAL VISUAL INSPECTION OF EWIS CONNECTIONSBETWEEN SEATS AND AIRCRAFT AND THE EWIS AT THE SEATSINSTALLED AS FAR AS VISIBLE, IN THE AFT MAINDECK COMPARTMENT AREA (EWIS)NOTE:THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS ONLY, AND IF ELECTRONICALLY EQUIPED.ACCESS: 833 843* 0.20N 202510-0505-2 251 AFT MAIN DECK COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS INSTALLED AFT MAIN DECK COMPARTMENT(ONLY IF CONTAMINATED) (EWIS)PRP.:GALLEYS AND TOILETS (IF INSTALLED, IF NECESSARY)SEATS (IF INSTALLED) AND SIDEWALL LININGS INEWIS AREASACCESS: 833 843* 0.20N 202510-0505-3 251 AFT MAIN DECK COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAFT MAIN DECK COMPARTMENT (EWIS)PRP.:GALLEYS AND TOILETS (IF INSTALLED, IF NECESSARY)SEATS (IF INSTALLED) AND SIDEWALL LININGS INEWIS AREASACCESS: 833 843* 0.20N 202530-0505-1 253 AFT MAIN DECK OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS INSTALLED AFT MAIN DECK OVERHEADCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PRP.:CEILING PANELS, STOWAGE BINS (IF INSTALLED)ACCESS: 833 843* 0.20SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 202530-0505-2 253 AFT MAIN DECK OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAFT MAIN DECK OVERHEAD COMPARTMENT (EWIS)PRP.:CEILING PANELS, STOWAGE BINS (IF INSTALLED)ACCESS: 833 843* 0.20N 202610-0505-1 261 AFT MAIN DECK UTILITY AREA MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS INSTALLED IN THE AFT MAIN DECKUTILITY AREAS (ONLY IF CONTAMINATED) (EWIS)PRP.:SEATS AND SIDEWALL LININGS, GALLEYS AND TOILETS(IF INSTALLED, IF NECESSARY)ACCESS: 833 843* 0.20N 202610-0505-2 261 AFT MAIN DECK UTILITY AREA MEC GVI I: 72 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSIDE THE811VU PANEL (EWIS)PRP.:ELECTRICAL PANEL COVER 811VU TO BE OPENEDACCESS: 833 843* 0.20N 202610-0505-3 261 AFT MAIN DECK UTILITY AREA MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEAFT MAIN DECK OVERHEAD COMPARTMENT (EWIS)PRP.:SEATS AND SIDEWALL LININGS, GALLEYS AND TOILETS(IF INSTALLED, IF NECESSARY)ACCESS: 833 843* 0.20N 202630-0505-1 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7011 0.20 ALLSIL 20-032CLEANING OF EWIS INSTALLED IN THE AFT MAIN DECK* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)202630-0505-1 * * * * * C O N T I N U E * * * * *UTILITY OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)PRP.:CEILING PANEL (IF INSTALLED) GALLEYS AND TOILETS(IF INSTALLED, IF NECESSARY)ACCESS: 833 843* 0.20N 202630-0505-2 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF APU FEED LINE AND POWERG, E AND P ROUTE EWIS IN CEILING AREA (EWIS)PRP.:CEILING PANEL (IF INSTALLED)ACCESS: 833 843* 0.20N 202630-0505-3 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC DET I: 144 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032DETAILED INSPECTION OF APU FEEDERS AND STARTER CABLEAT REAR BULKHEAD PRESSURE SEALS (EWIS)PRP.: AFT G & T MOUNTS.ACCESS: 833 843* 0.20N 202630-0505-4 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS IN MAIN DECKUTILITY OVERHEAD COMPARTMENT (EWIS)PRP.:CEILING PANEL (IF INSTALLED), GALLEYS ANDTOILETS (IF INSTALLED, IF NECESSARY)ACCESS: 833 843* 0.20N 203110-0505-1 311 HORIZONTAL AND VERTICAL ATTACHMENT AREA MEC GVI I: 72 MO SIL AMM 249200/6011 0.50 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS AT HORIZONTAL AND* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)203110-0505-1 * * * * * C O N T I N U E * * * * *VERTICAL ATTACHMENT AREA (EWIS)ACCESS: 312AR 313AL* 0.15N 203130-0505-1 313 TAIL CONE - APU INTAKE AREA MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS AT TAIL CONE - APUINTAKE AREA (EWIS)ACCESS: 312AR 313AL* 0.15N 203150-0505-1 315 TAIL CONE - APU AND ACCESSORY MEC CLN I: 24 MO SIL AMM 249200/7011 0.20 ALLCOMPARTMENT SIL 20-032CLEANING OF ALL POWER FEEDER ROUTES (ONLY IFCONTAMINATED) (EWIS)ACCESS: 315AL 316AR* 0.05N 203150-0505-2 315 TAIL CONE - APU AND ACCESSORY MEC GVI I: 24 MO SIL AMM 249200/6011 0.30 ALLCOMPARTMENT SIL 20-032GENERAL VISUAL INSPECTION OF G ROUTE WITHIN THEZONE (EWIS)ACCESS: 315AL 316AR* 0.05N 203150-0505-3 315 TAIL CONE - APU AND ACCESSORY MEC GVI I: 24 MO SIL AMM 249200/6011 0.40 ALLCOMPARTMENT SIL 20-032GENERAL VISUAL INSPECTION OF EWIS AT TAIL CONE - APUAND ACCESSORY COMPARTMENT (EWIS)ACCESS: 315AL 316AR* 0.05N 203340-0505-1 334 HORIZONTAL STABILIZER TIP MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALLSIL 20-032GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)203340-0505-1 * * * * * C O N T I N U E * * * * *TRAILING EDGE EWIS, LH/RH (EWIS)ACCESS: 334AB 334AT 334BB 334BT 334CB 334CT* 11.94334DB 334DT 334EB 334ET 334FT 334GT334HT 334JT 334KT 334LT 344AB 344AT344BB 344BT 344CB 344CT 344DB 344DT344EB 344ET 344FT 344GT 344HT 344JT344KT 344LTN 204110-0505-1 411 PYLON LEADING EDGE MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALL421 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN PYLONLEADING EDGE (EWIS)ACCESS: 411AL* 0.29421AL* 0.29N 204130-0505-1 413 FWD UPPER PYLON MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 PRE 2434423 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN FWDUPPER PYLON (EWIS)ACCESS: 413AL 413BL 413CL 413DL 413EL 413FL* 2.11414AR 414BR 414CR 414DR423AL 423BL 423CL 423DL 423EL 423FL* 2.11424AR 424BR 424CR 424DRN 204130-0505-2 413 FWD UPPER PYLON MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 POST 2434423 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN FWDUPPER PYLON (EWIS)ACCESS: 413AL 413BL 413DL 413EL 413FL 413GL* 2.24413HL 414AR 414BR 414CR 414DR 414ER423AL 423BL 423DL 423EL 423FL 423GL* 2.24423HL 424AR 424BR 424CR 424DR 424ERN 204150-0505-1 415 FORWARD LOWER PYLON MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALL425 SIL 20-0321 0.30* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)204150-0505-1 * * * * * C O N T I N U E * * * * *GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN FWDLOWER PYLON (EWIS)ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13N 204330-0505-1 433 ENGINE AIR INTAKE (NOSE COWL) MEC GVI I: 72 MO SIL AMM 249200/6011 0.20 GE443 SIL 20-0321 0.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED INENGINE AIR INTAKE (EWIS)ACCESS: 433AL 434AR 434BR* 0.81443AL 444AR 444BR* 0.98N 204330-0505-2 433 ENGINE AIR INTAKE (NOSE COWL) MEC GVI I: 72 MO SIL AMM 249200/6011 0.20 PW443 SIL 20-0321 0.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED INENGINE AIR INTAKE (EWIS)ACCESS: 433EL 434CR 434ER 434FR* 0.84443EL 444CR 444ER 444FR* 0.84N 204350-0505-1 435 FAN CASE AND FAN COWL MEC GVI I: 24 MO SIL AMM 249200/6011 0.30 ALL445 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN ENGINEFAN CASE AND FAN COWL (EWIS)ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02N 204510-0505-1 451 THRUST REVERSER MEC GVI I: 24 MO SIL AMM 249200/6011 0.20 ALL461 SIL 20-0321 0.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN ENGINETHRUST REVERSER (EWIS)PRP.:THRUST REVERSER DEPLOYEDSYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 204530-0505-1 453 HOT SECTION MEC GVI I: 24 MO SIL AMM 249200/6011 0.20 ALL463 SIL 20-0321 0.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN ENGINEHOT SECTION (EWIS)ACCESS: 451AL 452AR* 0.02461AL 462AR* 0.02N 204710-0505-1 471 PYLON TO WING LEADING EDGE MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALL481 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN PYLONTO WING LEADING EDGE (EWIS)PRP.:SLATS TO BE EXTENDEDACCESS: 471AL 471BL 472AR 472BR* 0.88481AL 481BL 482AR 482BR* 0.91N 204730-0505-1 473 AFT UPPER PYLON MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALL483 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN AFTUPPER PYLON (EWIS)ACCESS: 473AL 473BL 473DL 474AR 474BR 474CR* 1.94483AL 483BL 483DL 484AR 484BR 484CR* 1.94N 205120-0505-1 512 INBOARD FIX ED L.E. AREA MEC GVI I: 72 MO SIL AMM 249200/6011 1.50 ALL612 SIL 20-0321 1.50GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN SLATTRACK / SCREW JACK AREA (EWIS)PRP.:SLATS TO BE EXTENDEDACCESS: 512AB 512AT 512BB 512CB 512DB 512EB* 1.70512FB 512GB 512HB 512JB 512KB 512LB612AB 612AT 612BB 612CB 612DB 612EB* 1.67612FB 612GB 612HB 612JB 612KB 612LBN 205120-0505-2 512 INBOARD FIX ED L.E. AREA MEC GVI I: 72 MO SIL AMM 249200/6011 1.50 ALL612 SIL 20-0321 1.50GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 20APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)205120-0505-2 * * * * * C O N T I N U E * * * * *INBOARD FIXED L.E. AREA (EWIS)PRP.:SLATS TO BE EXTENDEDACCESS: 512AB 512AT 512BB 512CB 512DB 512EB* 1.70512FB 512GB 512HB 512JB 512KB 512LB612AB 612AT 612BB 612CB 612DB 612EB* 1.67612FB 612GB 612HB 612JB 612KB 612LBN 205130-0505-1 513 FORWARD WING ROOT AND KRUEGER FLAP MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 B2613 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEZONE (EWIS)PRP.:KRUEGER FLAP EXTENDED, COVER PLATE REMOVEDACCESS: 513AB 513BB 513CB* 0.78613AB 613BB 613CB* 0.55N 205130-0505-2 513 FORWARD WING ROOT AND KRUEGER FLAP MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 B4613 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEZONE (EWIS)PRP.:KRUEGER FLAP EXTENDED, COVER PLATE REMOVEDACCESS: 513AB* 0.40613AB* 0.18N 205230-0505-1 523 CENTER FIXED L.E. AREA (FROM RIB7 TO 17) MEC GVI I: 72 MO SIL AMM 249200/6011 1.20 ALL623 SIL 20-0321 1.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN SLATTRACK / SCREW JACK AREA (EWIS)PRP.:SLATS TO BE EXTENDEDACCESS: 523AB 523BB 523CB 523DB 523EB 523FB* 1.11523GB 523HB 523JB 523KB 523LB 523MB623AB 623BB 623CB 623DB 623EB 623FB* 1.11623GB 623HB 623JB 623KB 623LB 623MBSYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 21APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)N 205230-0505-2 523 CENTER FIXED L.E. AREA (FROM RIB7 TO 17) MEC GVI I: 72 MO SIL AMM 249200/6011 1.20 ALL623 SIL 20-0321 1.20GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THECENTER FIXED L.E. AREA (EWIS)PRP.:SLATS TO BE EXTENDEDACCESS: 523AB 523BB 523CB 523DB 523EB 523FB* 1.11523GB 523HB 523JB 523KB 523LB 523MB623AB 623BB 623CB 623DB 623EB 623FB* 1.11623GB 623HB 623JB 623KB 623LB 623MBN 205240-0505-1 524 OUTBOARD FIXED L.E. AREA (FROM RIBS 17 MEC GVI I: 72 MO SIL AMM 249200/6011 0.80 ALL624 TO 28) SIL 20-0321 0.80GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN SLATTRACK / SCREW JACK AREA (EWIS)PRP.:SLATS TO BE EXTENDEDACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KBN 205240-0505-2 524 OUTBOARD FIXED L.E. AREA (FROM RIBS 17 MEC GVI I: 72 MO SIL AMM 249200/6011 0.80 ALL624 TO 28) SIL 20-0321 0.80GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEOUTBOARD FIXED L.E. AREA (EWIS)PRP.:SLATS TO BE EXTENDEDACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KBN 205300-0505-1 530 FLAP TRACK FAIRING AND WING TIP MEC GVI I: 72 MO SIL AMM 249200/6011 0.80 ALL630 SIL 20-0321 0.80GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEFLAP TRACK FAIRING AND WING TIP AREA (EWIS)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 22APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)205300-0505-1 * * * * * C O N T I N U E * * * * *PRP.:FLAPS TO BE EXTENDED, FIXED AND MOVINGFAIRINGS TO BE REMOVEDACCESS: 531AB 531BB 532AB 532BB 533AB 533BB* 0.61534AB 534BB 535AB 535BB 536AB 536BB631AB 631BB 632AB 632BB 633AB 633BB* 0.64634AB 634BB 635AB 635BB 636AB 636BBN 205410-0505-1 541 FWD INBOARD SECTION OF INNER FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6011 0.40 ALL641 SIL 20-0321 0.40DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUELTANK (EWIS)ACCESS: 541AB 541BB 541CB 542EB* 6.00641AB 641BB 641CB 642EB* 6.00N 205410-0505-2 541 FWD INBOARD SECTION OF INNER FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6011 0.30 ALL641 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS IN FWD INBOARDSECTION OF INNER FUEL TANK AREA (EWIS)ACCESS: 541AB 541BB 541CB 542EB* 6.00641AB 641BB 641CB 642EB* 6.00N 205420-0505-1 542 AFT INBOARD SECTION OF INNER FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6011 0.40 ALL642 (RIBS 1 TO 9) SIL 20-0321 0.40DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUELTANK (EWIS)ACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50N 205420-0505-2 542 AFT INBOARD SECTION OF INNER FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6011 0.30 ALL642 (RIBS 1 TO 9) SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS IN THE AFT INBOARDSECTION OF INNER FUEL TANK AREA (EWIS)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 23APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)205420-0505-2 * * * * * C O N T I N U E * * * * *ACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50N 205430-0505-1 543 OUTBOARD SECTION OF INNER FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6011 0.40 ALL643 (RIBS 9 TO 14) SIL 20-0321 0.40DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUELTANK (EWIS)ACCESS: 543AB 543BB 543CB 543DB* 6.00643AB 643BB 643CB 643DB* 6.00N 205430-0505-2 543 OUTBOARD SECTION OF INNER FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6011 0.30 ALL643 (RIBS 9 TO 14) SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THEFUEL TANK (EWIS)ACCESS: 543AB 543BB 543CB 543DB* 6.00643AB 643BB 643CB 643DB* 6.00N 205500-0505-1 550 OUTBOARD FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6011 0.40 ALL650 SIL 20-0321 0.40DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUELTANK (EWIS)ACCESS: 550BB 550DB 550EB 550FB 550GB 550HB* 19.50550JB 550KB 550LB 550MB 550NB 550PB550QB650BB 650DB 650EB 650FB 650GB 650HB* 19.50650JB 650KB 650LB 650MB 650NB 650PB650QBN 205500-0505-2 550 OUTBOARD FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6011 0.30 ALL650 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THEFUEL TANK (EWIS)ACCESS: 550BB 550DB 550EB 550FB 550GB 550HB* 19.50* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 24APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)205500-0505-2 * * * * * C O N T I N U E * * * * *550JB 550KB 550LB 550MB 550NB 550PB550QB650BB 650DB 650EB 650FB 650GB 650HB* 19.50650JB 650KB 650LB 650MB 650NB 650PB650QBN 205710-0505-1 571 MAIN GEAR WELL MEC GVI I: 144 MO SIL AMM 249200/6011 0.30 ALL671 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS WITHIN THEFAIRINGS (EWIS)PRP.:UNDER WING FAIRINGS TO BE REMOVEDN 205710-0505-2 571 MAIN GEAR WELL MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALL671 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS WITHIN THEZONE (EWIS)N 205720-0505-1 572 TRAILING EDGE AREA (SHROUD BOX) MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALL672 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN FLAPTRACK 2 GEARBOX AREA (EWIS)PRP.:FLAPS AND SPOILERS TO BE EXTENDEDACCESS: 572AB 572CB 572DB 572EB 572FB 572GB* 0.48572HB 572JB 572KB 572LB 572PB672AB 672CB 672DB 672EB 672FB 672GB* 0.52672HB 672JB 672KB 672LB 672PBN 205720-0505-2 572 TRAILING EDGE AREA (SHROUD BOX) MEC GVI I: 48 MO SIL AMM 249200/6011 0.30 ALL672 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS WITHIN THEZONE (EWIS)PRP.:FLAPS AND SPOILERS TO BE EXTENDEDACCESS: 572AB 572CB 572DB 572EB 572FB 572GB* 0.48572HB 572JB 572KB 572LB 572PB* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 25APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)205720-0505-2 * * * * * C O N T I N U E * * * * *672AB 672CB 672DB 672EB 672FB 672GB* 0.52672HB 672JB 672KB 672LB 672PBN 205750-0505-1 575 FIXED TRAILING EDGE AREA (FROM SHROUD MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 ALL675 BOX TO RIB 9) SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS WITHIN THE FIXEDTRAILING EDGE AREA (EWIS)PRP.:FLAPS TO BE EXTENDEDACCESS: 575AB 575BB 575CB 575DB 575EB 575FB* 0.46575GB675AB 675BB 675CB 675DB 675EB 675FB* 0.46675GBN 205770-0505-1 577 AFT WING ROOT MEC GVI I: 72 MO SIL AMM 249200/6011 0.30 ALL677 SIL 20-0321 0.30GENERAL VISUAL INSPECTION OF EWIS WITHIN THE AFTWING ROOT AREA (EWIS)PRP.:FLAPS TO BE EXTENDEDACCESS: 577AB 577AT 577BB 577BT 577CT 577DT* 4.02577ET 577FT 577GT677AB 677AT 677BB 677BT 677CT 677DT* 4.02677ET 677FT 677GTN 205810-0505-1 581 FIXED TRAILING EDGE AREA (RIBS 9 TO 25) MEC GVI I: 144 MO SIL AMM 249200/6011 0.40 ALL681 SIL 20-0321 0.40GENERAL VISUAL INSPECTION OF EWIS WITHIN THEFAIRING (EWIS)PRP.:UNDER WING FAIRINGS TO BE REMOVEDN 205810-0505-2 581 FIXED TRAILING EDGE AREA (RIBS 9 TO 25) MEC GVI I: 48 MO SIL AMM 249200/6011 0.40 ALL681 SIL 20-0321 0.40GENERAL VISUAL INSPECTION OF EWIS WITHIN THEFAIRING (EWIS)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 26APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)205810-0505-2 * * * * * C O N T I N U E * * * * *PRP.:FLAPS AND SPOILERS TO BE EXTENDEDACCESS: 581AB 581BB 581CB 581DB 581EB 581FB* 0.87581GB 581HB 581JB681AB 681BB 681CB 681DB 681EB 681FB* 0.90681GB 681HB 681JB 681KBN 205910-0505-1 591 TRAILING EDGE AREA BETWEEN REAR SPAR AND MEC GVI I: 72 MO SIL AMM 249200/6011 0.40 ALL691 LOW SPEED AILERON SIL 20-0321 0.40GENERAL VISUAL INSPECTION OF EWIS WITHIN THEZONE (EWIS)ACCESS: 591AB 591BB 591CB 591DB* 0.17691AB 691BB 691CB 691DB* 0.26N 207110-0505-1 711 NOSE LANDING GEAR AND DOORS MEC GVI I: 12 MO SIL AMM 249200/6011 0.30 ALLSIL 20-032GENERAL VISUAL INSPECTION OF EWIS WITHIN THEZONE (EWIS)ACCESS: 713 714* 0.12N 207310-0505-1 731 MAIN LANDING GEAR INCLUDING FIXED AND MEC GVI I: 12 MO SIL AMM 249200/6011 0.30 ALLMOVABLE DOORS SIL 20-032GENERAL VISUAL INSPECTION OF EWIS WITHIN THEZONE (EWIS)ACCESS: 734 744* 0.20* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION:2-20 PAGE 27APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)212000-0505-1 200 DISTRIBUTION MEC CLN I: 5 A MPD AMM 212100/3011 0.20 ALLOR AMM 212200/301CLEAN LAVATORY AIR EXTRACTION GRILLS NOTE 5-2212100-0503-1 131 AIR DISTR/EXTR. FWD FUSELAGE MEC FUC I: 3 C MRB ** AMM 212100/5011 6.00 ALLFUNCTIONAL CHECK OF PRESSURE SWITCH (35 HR).PREP.: REMOVE LININGS BETWEEN FR.20 AND 24 IN FWDCARGO COMPARTMENT L/H.212100-0503-2 121 AIR DISTR/EXTR. FWD FUSELAGE MEC FUC I: 3 C MRB AMM 212400/5011 2.00 FWD-FACEFUNCTIONAL TEST, IN SITU, OF FLOW DETECTOR SETTINGSWITCH (77 HQ).ACCESS: 131AZ* 0.01212100-0503-3 121 AIR DISTR/EXTR. FWD FUSELAGE MEC FUC I: 3 C MRB AMM 212400/5011 1.00 FWD-FACEFUNCTIONAL TEST,IN SITU,OF FAN SPEED SWITCH (69 HQ)ACCESS: 131AZ* 0.01212100-0503-4 210 AIR DISTR/EXTR. FWD FUSELAGE MEC OPC I: 1 C MRB AMM 212400/5011 0.10 FWD-FACEOPERATIONAL TEST OF AURAL WARNING(BY PULLING FANS CIRCUIT BRAKERS.)212100-0505-1 121 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 5 A SIL AMM 212421/4011 1.50 FWD-FACEOR AMM 212422/401PRE 05119- CLEAN (AFTER DISASSEMBLY) DUST SEPARATOR UNIT, NOTE 5-2 AMM 212423/401PRE 04770- CLEAN DUST SEPARATOR SCAVENGE LINE, SIL 21-017(21-0112)- CLEAN AIR INLET GRILL OF SOUND REDUCER,- REPLACE FILTER CARTRIDGE.PREP.: REMOVE AIR FILTER UNIT AND SOUND REDUCER.ACCESS: 121BL 131AZ* 0.01SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)212100-0505-2 121 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 5 A MPD AMM 212421/4011 1.50 FWD-FACEOR AMM 212422/401POST 0477001. REMOVE SOUND REDUCER NOTE 5-2(21-0112)02. CLEAN MESHED FILTER AT AIR INLET TO SOUNDORREDUCERPOST 0511903. REMOVE AND REPLACE FILTER ELEMENT04. REINSTALL SOUND REDUCERACCESS: 121BL 131AZ* 0.01212100-0505-3 131 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 2 C MPD AMM 212100/7011 0.30 PRE 02022(21-0055)CLEAN VENTURI GRIDS IN AIR EXTRACTION DUCT.PRE 02599PREP.: REMOVE SIDE WALL LINING BETWEEN FR.22 ANDFR.23 IN FWD CARGO COMPARTMENT.212100-0505-4 122 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 2 C MPD AMM 212100/7011 0.30 PRE 02022(21-0055)CLEAN GRIDS OF RELAY BOXES.PRE 02599PREP.: REMOVE COVERS OF RELAY BOXES 250VU, 251VU,252VU, IN AVIONICS COMPARTMENT.ACCESS: 132AZ* 0.01212100-0505-5 210 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 2 C MPD AMM 212500/7011 0.50 PRE 02022(21-0055)CLEAN GRIDS BEHIND INSTRUMENT PANELS.PRE 02599PREP.: REMOVE INSTRUMENT PANELS OF PILOT,CO-PILOT,F/EAND C/B PANEL AS REQUIRED.212200-0505-1 154 AIR DISTR/EXTR. AFT FUSELAGE MEC CLN I: 2 C MPD AMM 212200/7011 0.30 PRE 02022(21-0055)CLEAN GRIDS IN AIR EXTRACTION DUCTS BELOW AFTPRE 02599CARGO COMPARTMENT.PREP.: REMOVE AFT CARGO COMPARTMENT FLOOR PANELS ASREQUIRED.SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)212200-0505-2 130 AIR DISTR/EXTR. FORWARD FUSELAGE MEC CLN I: 2 C MPD AMM 212100/7011 0.30 PRE 02022(21-0055)CLEAN GRIDS IN AIR EXTRACTION DUCTS BELOW FWD.PRE 02599CARGO COMPARTMENT (ZONES 133/134/135/136).PREP.: REMOVE FWD.CARGO COMPARTMENT FLOOR PANELS ASREQUIRED.212200-0505-3 100 AIR DISTRIBUTION/EXTRACTION FUSELAGE MEC CLN I: 1 C MPD AMM 212100/3011 1.00 ALL200 AMM 212200/3011 1.00CLEAN TOILET AIR EXTRACTION DUCTS OFALL LAVATORIESACCESS: LAVATORY FLOORACCESS: 162AZ 812* 0.02131AZ 811* 0.16212200-0505-4 100 AIR DISTRIBUTION/EXTRACTION FUSELAGE MEC CLN I: 4 A MPD AMM 212200/3012 4.00 POST 00854200 AMM 261711/4012 4.00 (26-0011)1. REMOVE LAVATORY SMOKE DETECTORS SIL 26-018OR2. REMOVE AIR EXTRACTION DUCTS BETWEENPOST 02503SMOKE DETECTORS AND EXTRACTION DUCT INLET(26-0030)3. CLEAN DUCTSOR4. REINSTALL LAVATORY AIR EXTRACTION DUCTSPOST 063355. REINSTALL LAVATORY SMOKE DETECTOR(26-0049)ACCESS: 131AZ 131HF 162AZ* 0.14212200-0505-5 131 DOOR ACCESS AIR CONDITIONING SYSTEM MEC DET I: 4 C SB SB 21-01201 0.50 ALLSIL SIL 21-0148DETAILED INSPECTION OF LOW PRESSURE GROUND CONNECTIONCOVER ASSEMBLY.212300-0502-1 121 AIR DISTR/EXTR. - BATTERIES MEC GVI I: 1 A MRB AMM 212300/0011 0.10 ALLCHECK EXTERNAL BATTERY COOLING ORIFICES FOROBSTRUCTIONSYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)212300-0503-1 121 AIR DISTR/EXTR. - BATTERIES ERI OPC I: 3 C MPD AMM 212300/6011 0.10 ALLOPERATIONAL TEST OF BATTERY COOLING SYSTEMACCESS: 131AZ* 0.01212300-0505-1 222 AIR DISTR/EXTR. - BATTERIES ERI CLN I: 2 C MPD AMM 212300/7011 0.50 PRE 02022232 AMM 212400/7011 0.50 (21-0055)CLEAN AIR EXTRACTION GRIDS/BAFFLES OF BATTERY ANDPRE 02599ELECTRONIC RACK 90 VU.PREP.: REMOVE LOWER SIDEWALL/DADO PANELS BETWEENFRAME 17 AND FRAME 19 ABOVE PASS.CABIN FLOORAS REQUIRED.212400-0503-1 121 AIR DISTR/EXTR.ELECTR.RACKS ERI FUC I: 3 C MPD AMM 212400/5011 0.75 PRE 01819(21-0047)FUNCTIONAL TEST OF ELECTRONIC RACKS, VENTILATION,OVERHEAT DETECTOR AND ASSOCIATED CIRCUITACCESS: 131AZ* 0.01212700-0505-1 200 GALLEY VENTILATION FILTER MEC CLN I: NOTE 5-2 MPD AMM 253000/3011 1.60 ALLCLEAN GALLEY VENTILATION FILTERS - CHANGE IFNECESSARY213100-0503-1 137 RECIRCULATION VALVE MEC OPC I: 1 C MRB ** AMM 213114/5011 0.10 ALL1711 0.10OPERATIONAL TEST OF RECIRCULATING VALVE AS FOLLOWS:01. MANUALLY CHECK THAT FLAPS MOVE FULLY AND SMOOTHLY(FOR INFORMATION: THE VALVE STARTS OPENING WHENDIFFERENTIAL PRESSURE IS 6 MB.)02. ENSURE THAT VALVE SEAT AND GRID ARE CLEANACCESS: 131BZ* 0.13162AZ 171AZ* 0.09213100-0503-2 134 NEGATIVE PRESS.SAFETY VALVE MEC OPC I: 1 C MRB AMM 213115/5011 0.25 ALL1711 0.25* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)213100-0503-2 * * * * * C O N T I N U E * * * * *OPERATIONAL CHECK OF NEGATIVE PRESSURE SAFETY VALVEAS FOLLOWS:01. MANUALLY CHECK THAT FLAP MOVES FULLY AND SMOOTHLY(FOR INFORMATION: THE VALVE STARTS OPENING WHENDIFFERENTIAL PRESSURE IS 6 MB.)02. ENSURE THAT VALVE SEAT AND GRIDS ARE CLEANACCESS: 132JF* 0.28162AZ 171AZ* 0.09213100-0503-3 210 VALVE - PRESSURE REGULATING MEC OPC I: 3 C MRB ** AMM 213100/5011 0.30 ALLOPERATIONAL TEST OF ELECTRICAL CLOSING OFPRESS.REGULATING VALVES (DITCHING CONFIGURATION)213100-0503-4 210 RECIRCULATION VALVE MEC OPC I: 1 C MRB AMM 213100/5011 0.10 FWD-FACEON PANEL 433 VU:01. OPERATIONAL TEST OF STEADY "CAB RATE" WARNING02. OPERATIONAL TEST OF DEPRESS.VALVE "FAULT" WARNING(POSITION DISAGREE)03. OPERATIONAL TEST OF DEPRESS VALVE IN "MAN CTL"(MANUAL CONTROL) MODE213100-0503-5 210 AUTO CABIN PRESSURE CONTROL MEC OPC I: WEEKLY MRB AMM 213100/5011 0.10 FWD-FACE"TEST OK" OF AUTOMATIC CABIN PRESSURE CONTROL SYSTEM213100-0505-1 136 VALVE - PRESSURE REGULATING MEC CLN I: 5 A MRB AMM 213100/3011 1.00 NON FWD-FACE1701 1.00CLEAN PRESSURE REGULATING VALVE SEAT AND GRID(MAY BE CARRIED OUT IN SITU)ACCESS: 136AR* 0.01171AZ* 0.08SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)213100-0505-2 136 VALVE - PRESSURE REGULATING MEC CLN I: 2 C MRB AMM 213100/3011 1.00 FWD-FACE1701 1.00FOWARD AND AFT VALVES:01. CLEAN TEFLON COATING OF PRESSURE REGULATINGVALVES SEATS02. CLEAN ANNULAR GRIDS(TASK MAY BE CARRIED OUT IN SITU)ACCESS: 136AR* 0.01171AZ* 0.08213117-0503-1 137 VALVE-PRESS.RELIEF,GRD.AUTO MEC FUC I: 3 C MRB AMM 213117/5011 2.00 NON FWD-FACEFUNCTIONAL TEST OF PNEUMATIC LOCKINGACCESS: 131CZ* 0.13213400-0503-1 121 CABIN PRESSURE RELIEF ERI FUC I: 3 C MRB AMM 213411/5011 2.00 PRE 06857(21-0113)FUNCTIONAL TEST OF "CAB.PRESS." MANOMETRIC SWITCH ANDASSOCIATED WARNINGACCESS: 131AZ* 0.01213500-0503-1 212 EMERGENCY CABIN DEPRESS. MEC OPC I: 2 C MRB ** AMM 213500/5011 0.50 ALLMANUAL OPERATIONAL TEST OF EMERGENCY CABINDEPRESSURIZATION AS FOLLOWS:01. ROTATE HANDWHEEL ON FLIGHT ENGINEER ́S PANEL INTHE OPEN DIRECTION UNTIL IT STOPS,THE MOVEMENTMUST BE SMOOTH WITHOUT ANY HARD POINTS02. TURN THE HANDWHEEL IN CLOSE DIRECTION UNTIL ITSTOPS (FULL CLOSING OF THE VALVE) THEN LOCK HAND-WHEEL215000-0502-1 140 RAM AIR INLET MEC GVI I: 1 A MRB AMM 215100/6011 0.25 ALLCHECK COOLING AIR INLETS/OUTLETS FOR GENERALCONDITIONSYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)215115-0504-1 135 CHECK VALVE - CABIN MEC OPC I: 4 C MRB AMM 215115/4011 2.00 ALLAMM 215115/601CHECK VALVE FOR WEAR AND FREEDOM OF FLAPPERS,CHECK MANUALLY THAT VALVE OPERATES CORRECTLY.PREP.: REMOVE/INSTALL CHECK VALVE.ACCESS: 131BZ 137ALF* 0.45215116-0505-1 143 SEPARATOR - WATER MEC CLN I: 5 A MRB AMM 215116/3011 1.00 ALL1441 1.00CHECK COALESEUR FOR CONDITION AND CLEANINESS:01. REMOVE COALESEUR FROM WATER SEPARATOR,02. CLEAN COALESEUR AND CHECK FOR EVIDENCE OF DAMAGEOR CONTAMINATION,03. REINSTALL COALESEUR (ENSURE INDICATOR ROD OFCLOGGING INDICATOR IS NOT PROTRUDING(PRE MOD 03696 ONLY)ACCESS: 147FZ* 0.04215121-0503-1 143 REFRIGERATION UNIT MEC OPC I: 3 C MRB AMM 215000/5011 0.30 ALL1441 0.30LEAK CHECK OF REFRIGERATION UNIT WITH RUNNING PACK:01. PERFORM OPERATIONAL TEST OF REFRIGERATION UNIT.02. CHECK UNIT AND DUCTS WITHIN AIRCONDITIONINGCOMPARTMENT FOR CONDITION AND LEAKS.ACCESS: 147FZ* 0.04215300-0503-1 143 EMERGENCY RAM AIR INLET MEC OPC I: 2 C MRB ** AMM 215300/5012 0.50 ALLAMM 215300/601- OPERATIONAL TEST OF EMERGENCY RAM AIR INLET SCOOP.- GENERAL VISUAL INSPECTION OF EMERGENCY RAM AIRSCOOP AND DUCT.ACCESS: 147FZ* 0.04215300-0504-1 135 RAM AIR INLET CHECK VALVE MEC OPC I: 4 C MRB AMM 215312/4011 2.00 ALLAMM 215312/601CHECK RAM AIR INLET CHECK VALVE AS FOLLOWS:* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)215300-0504-1 * * * * * C O N T I N U E * * * * *01. REMOVE CHECK VALVE02. CLEAN VALVE AND CHECK FOR WEAR AND FREEDOM OFFLAPPERS03. REINSTALL CHECK VALVEACCESS: 131CZ* 0.13215311-0502-1 140 ACTUATOR-EMER.RAM AIR INLET MEC GVI I: DY-TERM MRB AMM 215300/6011 0.10 ALLCHECK THAT RAM AIR INLET FLAP IS CLOSED215500-0503-1 210 GROUND COOLING ERI OPC I: 2 C MPD AMM 212400/5011 0.10 FWD-FACEPOST 03347OPERATIONAL CHECK OF ELECTRIC RACKS GROUND COOLINGSYSTEM "FAULT" WARNING216200-0503-1 211 COCKPIT & CABIN DUCT TEMP. ERI OPC I: 5 A MPD AMM 216216/4011 1.50 PRE 01820232 AMM 216222/4011 1.50 (21-0048)242 REMOVE SENSORS AND INSPECT SENSORS AND SCREENS1 1.50252 FOR CLEANLINESS, SATISFACTORY CONDITION AND PERFORM1 1.50OPERATIONAL TEST OF SENSOR AIRFLOW FAN216200-0505-1 200 COCKPIT & CABIN TEMP.CONTR. ERI CLN I: 1 C MRB AMM 216218/4011 10.00 POST 01820AMM 216222/401(21-0048)REMOVE, CLEAN AND REINSTALL COCKPIT TEMPERATURESENSOR, TRANSMITTER AND VENT LINE (BETWEEN FRAMES8 AND 9) AND CABIN TEMPERATURE SENSORS AND TRANS-MITTERS (AT FRAMES 25, 42 AND 62).216200-0505-2 130 COCKPIT & CABIN DUCT TEMP. ERI CLN I: 1 C MRB AMM 216217/4011 1.00 ALLAMM 216221/401REMOVE, CLEAN AND REINSTALL DUCT TEMPERATURESENSORS AND TRANSMITTERS (AT FRAMES 32/36, ZONE 131/132 - AND FRAMES 24/28, ZONE 131 ONLY)SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)216300-0503-1 136 TRIM AIR TEMP.CONTROL MEC FUC I: 3 C MRB AMM 216313/5011 2.00 ALLFUNCTIONAL TEST OF TRIM AIR DIFFERENTIAL PRESSURESWITCH.ACCESS: 136AR* 0.01216311-0503-1 143 VALVE-TRIM AIR PRESS.REGUL. MEC FUC I: 4 C MPD AMM 216311/5011 1.50 ALLFUNCTIONAL TEST OF TRIM AIR PRESSURE REGULATINGVALVES.ACCESS: 147FZ* 0.04216312-0504-1 136 CHECK VALVE, HOT AIR MANIF. MEC OPC I: 4 C MRB AMM 216312/4011 2.00 ALLAMM 216312/601CHECK FOR WEAR AND FREEDOM OF FLAPPERS:01. REMOVE CHECK VALVE02. CLEAN CHECK VALVE WITH MEK - SOLVENT (MATERIAL11-003) AND INSPECT FOR CONDITION03. OPERATE FLAPS OF CHECK VALVE MANUALLY AND CHECKTHAT THEY MOVE FREELY WITH NO HARD POINTS04. REINSTALL CHECK VALVENOTE: TORQUE VALUE IS GIVEN ON THE CLAMPSACCESS: 136AR* 0.01* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION:2-21 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)221000-0503-1 210 AUTOPILOT ELO OPC I: 4000 FH MRB AMM 221000/5011 0.10 FWD-FACECNPOST 11150OPERATIONAL TEST OF AP DISCONNECTION WHEN AP PITCH 94-185-165(B)(22-0112)ACTUATOR IS MANUALLY OVERRIDDEN221000-0503-2 210 AUTOPILOT ELO OPC I: 2000 FH AD AD1 0.50 POST 12790CN 2007-04-05 CN(22-0117)OPERATIONAL TEST FOR AP DISCONNETION BY STICK FORCE FAA AD CNAPPLICATION ISB F-2005-107(B)FAA AD2007-04-5ISB 22-0118221100-0503-1 210 AP/FD ROLL / YAW CHANNEL ELO FUC I: 1 A MRB ** AMM 224200/5011 0.75 NON FWD-FACEFUNCTIONAL TEST OF COMPARATOR THRESHOLD BY AFCSSAFETY TEST:01. AP/FD ROLL/YAW CHANNEL02. AP/FD PITCH CHANNEL03. AP/FD LOGIC/MONITOR CHANNEL04. YAW DAMPER COMPUTER05. AUTOMATIC PITCH TRIM COMPUTER06. AUTOTHROTTLE CONTROL COMPUTER221200-0503-1 210 AP/FD MECHANICAL OVERRIDE ELO OPC I: 1 C MRB ** AMM 221000/5011 0.33 ALLOPERATIONAL TEST OF MECHANICAL OVERRIDE LEVERS(TORQUE LIMITER LEVERS) FOR CORRECT OPERATION OF:- ROLL MECHANICAL OVERRIDE- YAW MECHANICAL OVERRIDE- PITCH MECHANICAL OVERRIDE221512-0503-1 210 FLIGHT CONTROL UNIT ELO OPC I: DY-TERM MRB AMM 220000/5011 0.20 FWD-FACEPOST 02574LAMP TEST OF THE UNIT TO CHECK CORRECT OPERATION OFDISPLAYSYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION:2-22 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)221521-0503-1 210 FLIGHT MODE ANNUNCIATOR ELO OPC I: DY-TERM MRB AMM 220000/5011 0.10 FWD-FACEPOST 02574LAMP TEST OF THE FLIGHT MODE ANNUNCIATOR TO CHECKCORRECT OPERATION OF DISPLAY.222000-0503-1 210 SPEED - ATTITUDE CORRECTION ELO OPC I: 1 A MRB AMM 222700/5011 0.25 FWD-FACE- OPERATIONAL TEST OF ELECTRIC PITCH TRIM MECHANICALDISCONNECTION AND OVERRIDE.- OPERATIONAL TEST OF AUTOTRIM MECHANICAL OVERRIDETO CHECK PITCH TRIM DISENGAGEMENT.222000-0503-2 210 SPEED - ATTITUDE CORRECTION ELO OPC I: 1 A MRB AMM 224000/5011 0.16 FWD-FACEPOST 02574READ "MTP" SEQUENCE TO ASSESS STATUS OF ANGLEOF ATTACK SENSORS222000-0504-1 210 SPEED - ATTITUDE CORRECTION MEC DET I: 500 FH AD AD 2006-15-061 1.00 FWD-FACECN CN 2005-111(B)DETAILED VISUAL INSPECTION OF THE AUTOTRIM FUNCTION. ISB ISB 22A0115222100-0503-1 210 YAW DAMPER ELO OPC I: WEEKLY MRB ** AMM 222100/5011 0.10 NON FWD-FACEOPERATIONAL TEST TO VERIFY CORRECT OPERATION OFMECHANICAL CONTROL BETWEEN YAW DAMPER SYSTEM 2 ANDTHE RUDDER222300-0503-1 210 AUTOMATIC PITCH TRIM ELO OPC I: 3000 FH MRB ** AMM 222300/5012 0.33 NON FWD-FACECNPOST 01508OPERATIONAL TEST OF SAFETY DEVICE IN PITCH TRIM 1980-222-030(B) (22-0025)ENGAGEMENT (ENGAGEMENT AND WARNING TEST) FAA AD 80-18-02222300-0503-2 210 MICROSWITCHES - THS ELO FUC I: 1 C MRB ** AMM 222300/5012 1.00 NON FWD-FACE3102 1.00FUNCTIONAL CHECK OF THS TRAVEL LIMIT SWITCHES* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION:2-22 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)222300-0503-2 * * * * * C O N T I N U E * * * * *ACCESS: 312AR* 0.01222300-0503-3 210 AUTOMATIC PITCH TRIM ELO OPC I: 1000 FH AD AD 2006-25-031 0.50 NON FWD-FACECN CNOPERATIONAL TEST OF PITCH TRIM SYSTEM 2 AT HIGH ISB CNSPEED OF TRIM F-2005-157(B)ISB 22-0121222300-0504-1 311 SPEED - ATTITUDE CORRECTION MEC RAR I: 12000 FH AD AD 2006-26-101 0.50 POST 13043312 CN CN1 0.50 (22-0119)REMOVAL OF PITCH TRIM SERVOMOTOR FOR RESTORATION ISB CNF-2005-109(B)ISB 22-0120222339-0504-1 110 AUTOMATIC PITCH TRIM MEC RAR I: 8000 FH CN CN1 TBD B2OR FAA AD F-2003-457(B)PRE 03686REMOVE HONEYWELL AOA SENSOR P/N 965-4020-007 FOR 8 YE OIT FAA AD(34-0092)SHOP INSPECTION 2006-01-03B4OIT SEPRE 03686ACCESS: 110AL 999.0029/03/VHR * 0.01 (34-0092)222600-0503-1 210 YAW DAMPER ELO OPC I: WEEKLY MRB ** AMM 222600/5011 0.10 FWD-FACEOPERATIONAL TEST TO VERIFY CORRECT OPERATION OFMECHANICAL CONTROL BETWEEN YAW DAMPER SYSTEM 2 ANDTHE RUDDER222634-0504-1 121 FLIGHT AUGMENTATION COMPUT. ELO FUC I: SHOP VIS MRB AMM 222634-4011 0.50 FWD-FACEPOST 02574A COMPLETE ATEC TEST OF THE FAC INCLUDING FOLLOWINGFUNCTIONS:- ALPHA-FLOOR PROTECTION- AIRCRAFT CONFIGURATION SIGNALSACCESS: 131AZ* 0.01SYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION:2-22 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)222700-0503-1 210 ELECTRIC PITCH TRIM ELO OPC I: 3000 FH MPD AMM 222700/5011 0.50 FWD-FACEPOST 01508OPERATIONAL TEST OF SAFTY DISENGAGEMENT DEVICES IN(22-0025)PITCH TRIM ENGAGEMENT(OVERRIDE TEST)222700-0503-2 210 MICROSWITCHES-THS ELO OPC I: 1 C MPD AMM 222700/5011 0.50 FWD-FACE3101 0.50OPERATIONAL CHECK OF THS TRAVEL LIMIT SWITCHESACCESS: 312AR* 0.01223000-0503-1 210 AUTOTHROTTLE SYSTEM ELO OPC I: 5 A MRB AMM 341700/5011 0.17 FWD-FACEAMM 342000/501POST 02574CHECK CORRECT OPERATION OF ATTITUDE HEADINGREFERENCE UNITS (AHRU) AND HYBRID AIR DATA COMPUTERS(HADC) SWITCHING.223100-0503-1 210 AUTOTHROTTLE CONTROL ELO FUC I: 5 A MPD AMM 223100/5011 0.50 GEFUNCTIONAL TEST OF FULL THROTTLE LIMIT STOP AND N1LIMIT STOP.223100-0503-2 210 AUTOTHROTTLE CONTROL ELO FUC I: 5 A MPD AMM 223100/5011 0.50 PWFUNCTIONAL TEST OF FULL THROTTLE LIMIT STOP AND EPRLIMIT STOP.223512-0503-1 210 THRUST RATING PANEL ELO OPC I: 1 C MRB AMM 223000/5011 0.17 FWD-FACEPOST 02574CHECK CORRECT OPERATION OF AUTOMATIC CHANGEOVER OF T.A.T. DISPLAY (HADC1 / HADC2)223512-0503-2 210 THRUST RATING PANEL ELO OPC I: DY-TERM MRB AMM 220000/5011 0.10 FWD-FACEPOST 02574LAMP TEST OF THE PANEL TO CHECK CORRECT OPERATION OFDISPLAYSYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION:2-22 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)223634-0503-1 210 THRUST CONTROL COMPUTER ELO OPC I: DY-TERM MRB1 0.10 FWD-FACEPWOPERATIONAL TEST OF EPR LIMIT COMPUTATION (WITHPOST 02574THRUST RATING PANEL).POST 02689223634-0503-2 210 THRUST CONTROL COMPUTER ELO OPC I: DY-TERM MRB AMM 220000/5011 0.10 FWD-FACEGEOPERATIONAL TEST OF N1 LIMIT COMPUTATION (WITHPOST 02574THRUST RATING PANEL).POST 02689224200-0502-1 210 AUTOMATIC FLIGHT CONTROL SYSTEM TEST ELO OPC I: NOTE MRB AMM 224200/5011 0.10 NON FWD-FACECHECK THE STATE OF TEST PANEL MAGNETIC INDICATORS.NOTE: AFTER EACH AUTOMATIC LANDING OR AUTOMATICLANDING ATTEMPT WITH AP1 AND AP2 ENGAGED(CAT III CONDITIONS)* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION:2-22 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)231100-0503-1 210 HF-SYSTEM RAD OPC I: DY-TERM MRB ** AMM 231100/5011 0.10 ALLOPERATIONAL TEST OF HF SYSTEM (IF REQUIRED FORFLIGHT).235100-0503-1 210 AUDIO INTERGRATING RAD OPC I: WEEKLY MRB ** AMM 235100/5011 0.10 ALLOPERATIONAL TEST OF AUDIO INTEGRATING SYSTEM236000-0502-1 300 STATIC DISCHARGING RAD GVI I: 1 A MRB AMM 236000/0011 0.15 ALL5001 0.15600 CHECK PRESENCE OF ALL STATIC DISCHARGERS LOCATED1 0.15ON THE WINGS AND EMPENNAGE236000-0503-1 500 STATIC DISCHARGING RAD FUC I: 2 C MRB AMM 236000/6011 0.65 ALL6001 0.65FUNCTIONAL TEST OF STATIC DISCHARGERS ON THE WING:01. CHECK RESISTANCE BETWEEN RETAINER AND AIRCRAFTSTRUCTURE (MAX. AUTHORIZED VALUE: 1 OHM),02. CHECK FOR CONDITION.236000-0503-2 300 STATIC DISCHARGING RAD FUC I: 2 C MRB AMM 236000/6011 1.20 ALLFUNCTIONAL TEST OF STATIC DISCHARGERS ON THE RUDDERAND ELEVATOR:01. CHECK RESISTANCE BETWEEN RETAINER AND AIRCRAFTSTRUCTURE.(MAX.AUTHORIZED VALUE: 1 OHM),02. CHECK FOR CONDITION.237100-0503-1 171 COCKPIT VOICE RECORDER RAD FUC I: 2 C MRB AMM 237100/5011 0.50 ALLCMM 277001FUNCTIONAL TEST OF UNDERWATER LOCATOR BEACON ANDREPLACE BATTERY IF NECESSARYACCESS: 162AZ* 0.01237100-0503-2 210 COCKPIT VOICE RECORDER RAD OPC I: DY-TERM MRB ** AMM 237100/5011 0.10 ALL* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : COMMUNICATIONS REV. DATE: APR 01/10 SECTION:2-23 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)237100-0503-2 * * * * * C O N T I N U E * * * * *SELF TEST OF COCKPIT VOICE RECORDING SYSTEM237100-0504-1 171 COCKPIT VOICE RECORDER RAD RAR I: VR MRB CMM 2370011 0.25 ALLREMOVE AND REPLACE BATTERY OF UNDERWATERLOCATOR BEACON ATTACHED TO THE COCKPIT VOICE RECORDERACCESS: 162AZ* 0.01* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : COMMUNICATIONS REV. DATE: APR 01/10 SECTION:2-23 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)240000-0503-1 120 ELECTRICAL POWER GENERAL ERI DET I: 18 MO CN CN1 0.10 PRE 10929FAA AD 1994-187-163(B) (24-0086)DETAILED INSPECTION OF 104 VU ELECTRICAL LOOM FAA AD 95-10-14INSTALLATION ISB 24-0087NOTE: THIS TASK IS RELATED TO MECHANICAL INSPECTIONOF AVIONIC COMPARTMENT LADDER, REF TASK532411-0502-1.ACCESS: 121BL* 0.01240000-0503-2 200 ELECTRICAL POWER-GENERAL ERI OPC T: 24 MO SIL AMM 240000/6011 1.00 ALLI: 36 MO SIL 20-0017OPENING AND CLOSING OF ALL CIRCUIT BREAKERS.PREP.: ELECTRICAL POWER OFF241111-0503-1 436 CONSTANT SPEED DRIVE ENG OPC I: CSD CHG MRB ** AMM 241100/5011 0.50 ALL446 ENG.CHG1 0.50OPERATIONAL TEST OF CSD DISCONNECT AND RESET SYSTEM(WITH ENGINE STOPPED)ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02241111-0504-1 435 CONSTANT SPEED DRIVE MEC RAR I: 4 C MPD AMM 241121/4011 1.00 GE445 OR NOTE SIL SUN 1921 1.0001. REMOVE CSD OIL HEAT EXCHANGER AND OIL COOLINGTUBING02. CLEAN CSD OIL HEAT EXCHANGER AND OIL COOLINGTUBING03. REINSTALL CSD OIL HEAT EXCHANGER AND OIL COOLINGTUBINGNOTE: TASK MAY BE ACCOMPLISHED AT THE OPPORTUNITYOF THE ENGINE SHOP VISITACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02SYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION:2-24 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)241111-0504-2 435 CONSTANT SPEED DRIVE MEC RAR I: 4 C MPD AMM 792106/4011 1.50 PW445 OR NOTE SIL SUN 1921 1.5001. REMOVE CSD OIL HEAT EXCHANGERS AND OIL COOLINGTUBING02. CLEAN CSD OIL HEAT EXCHANGERS AND OIL COOLINGTUBING03. REINSTALL CSD OIL HEAT EXCHANGERS AND OIL COOLINGTUBINGNOTE: TASK MAY BE ACCOMPLISHED AT THE OPPORTUNITYOF THE ENGINE SHOP VISITACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02241111-0505-1 436 CONSTANT SPEED DRIVE ENG RPL I: 1 A MRB AMM 121324/0011 0.20 ALL446 AMM 241100/3011 0.2001. CHECK OIL LEVEL OF CONSTANT SPEED DRIVE AND AMM 241100/601REPLENISH IF NECESSARY02. CHECK CSD SCAVENGE FILTER AND CHARGE FILTERCLOGGING INDICATORS ARE NOT PROTRUDING (ASAPPLICABLE)03. CHECK MANUALLY THE QAD RING FOR EVIDENCE OF PLAYACCESS: 436AR* 0.01446AR* 0.01241111-0505-2 436 CONSTANT SPEED DRIVE ENG RPL I: 3 A MRB AMM 241100/3011 0.50 ALL446 OR SB SUN 24-13411 0.50REPLACE SCAVENGE FILTER ELEMENT AND CHECK FOR SB SUNCONTAMINATION 24-1341ACCESS: 436AR* 0.01446AR* 0.01242111-0505-1 436 GENERATOR - AC - ENGINE ENG RPL I: 3 A MRB AMM 121324/0011 0.25 ALL4461 0.25CHECK OIL LEVEL OF GENERATOR AND REPLENISH IFNECESSARYACCESS: 436AR* 0.01446AR* 0.01SYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION:2-24 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)242112-0503-1 121 GENERATOR CONTROL UNIT ERI OPC I: 1 C MRB ** AMM 242112/4011 0.50 ALLOPERATIONAL TEST OF GENERATOR CONTROL UNITS (APU GCUINCLUSIVE)ACCESS: 132AZ* 0.01242200-0502-1 261 APU GENERATOR FEEDER CABLES ERI GVI I: 200 FC CN CN1 0.50 MSN 003-116262 FAA AD 1981-058-033(B) 1 0.50 PRE (24-0048)VISUAL INSPECTION OF APU GENERATOR FEEDER CABLE FAA AD 80-26-07SLICES AT FRAME 78 AND 79 FOR SATISFACTORY CONDITION. ISB 24-0048242200-0503-2 471 AC GENER.FEEDERS/ENG.WIRING ENG DET I: 1000 FH CN CN 2001-555(B)1 0.30 PRE 11349481 FAA AD FAA AD1 0.30 (54-0095)CHECK CONDITION OF FILLET SEAL, GENERATOR 2002-04-05FEEDERS AND ENGINE WIRING HARNESS IN PYLON ISB 24-0053(INCLUDING ZONE 472 AND 482) ISB 24-0083ACCESS: 471AL 472AR* 0.61481AL 482AR* 0.62242211-0505-1 315 GENERATOR-AC-APU ENG RPL I: 3 A MRB AMM 121324/0011 0.25 ALLCHECK OIL LEVEL OF GENERATOR AND REPLENISH IFNECESSARYACCESS: 315AL 316AR* 0.05242311-0503-1 210 INVERTER-115V/600VA STATIC ERI OPC I: DY-TERM MRB ** AMM 242311/4011 0.10 ALLOPERATIONAL TEST OF STATIC INVERTERS242400-0503-1 210 SWITCHING-AC GEN./ESS.CIRCT ERI OPC I: ENG. CHG MRB ** AMM 242400/5011 0.10 ALLOPERATIONAL TEST OF THE AC ESS BUS OVERRIDE SUPPLYSYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION:2-24 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)242400-0503-2 210 SWITCHING-AC GEN./ESS.CIRCT ERI OPC I: ENG. CHG MRB AMM 242400/5011 0.10 FWD-FACEOPERATIONAL TEST OF THE SMOKE DRILL CONFIGURATION(OVRD SUPPLY 1 AND 2) INCLUDING THE AUTOMATIC CHANGEOVER243100-0503-1 210 BATTERIES ERI OPC I: DY-TERM MRB AMM 243111/4011 0.30 ALLCHECK BATTERIES FOR CORRECT VOLTAGE243111-0502-1 122 BATTERIES ERI DET I: 750 FH MRB AMM 243100/3011 0.90 ALL01. CHECK ACCUMULATORS AND CONNECTIONS FOR SIGNS OFOVERHEATING OR ELECTROLYTE OVERFLOW02. CHECK NO-LOAD VOLTAGE OF ACCUMULATORS03. CHECK BATTERY MOUNTING RACK FOR CLEANLINESS,SECURITY OF ATTACHMENTS AND SATISFACTORY CONDI-TIONACCESS: 132AZ* 0.01243111-0504-1 122 BATTERIES ERI RAR I: NOTE 5-1 MRB AMM 243111/4011 0.30 ALLREMOVE BATTERIES FOR SHOP VISITACCESS: 132AZ* 0.01243112-0503-1 121 MONITORING UNIT-BATT CHARGE ERI OPC I: 1 C MRB ** AMM 243112/4012 0.25 ALLOPERATIONAL TEST OF BATTERY CHARGE LIMITER (CHARGEMONITORING UNIT) BY BITEACCESS: 132AZ* 0.01243211-0503-1 120 TRANSFORMER RECTIFIER-150A ERI OPC I: 2 A MPD AMM 243211/6012 0.50 ALLSIL 24-025OPERATIONAL TEST OF TRANSFORMER RECTIFIER COOLINGFANS, ENSURE FAN GRIDS ARE CLEAN.* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION:2-24 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)243211-0503-1 * * * * * C O N T I N U E * * * * *ACCESS: 132AZ* 0.01245000-0503-1 210 ELECTR.LOAD DISTRIBUTION ERI OPC I: 1 C MRB ** AMM 245000/5011 0.10 NON FWD-FACEOPERATIONAL TEST OF "NORM EQPT/ESS BUS MIN EQPT"SWITCH AND "SMOKE DRILL NAV SELECT" SWITCH245000-0503-2 210 ELECTR.LOAD DISTRIBUTION ERI OPC I: 1 C MRB ** AMM 245000/5011 0.10 FWD-FACEOPERATIONAL TEST OF "ESSENTIAL AND EMERGENCY BUS"(SHED) AND "LAND RECOVERY" SELECTION* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION:2-24 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)251100-0502-1 210 FLIGHT COMPARTMENT SEATS MEC DET I: 2 C MRB AMM 251111/6011 1.00 ALLAMM 251112/601DETAILED INSPECTION OF CREW SEAT STRUCTURE AND AMM 251113/601SEAT TO FLOOR ATTACHMENTS251100-0503-1 210 FLIGHT COMPARTMENT SEATS MEC OPC I: 2 C MRB AMM 251111/5011 1.00 ALLAMM 251112/501OPERATIONAL TEST OF CREW SEATS IN MECHANICAL AND AMM 251113/501ELECTRICAL MODES, CHECK PROPER OPERATION OF INERTIAREELS AND GENERAL CONDITION OF HARNESS.252100-0502-1 200 PASSENGER COMPARTMENT SEATS MEC DET I: 2 C MRB AMM 252000/0011 14.00 ALLEXCL. F41. DETAILED INSPECTION OF PASSENGER ANDCABIN ATTENDANT SEAT TO FLOOR ATTACHMENTS FORSATISFACTORY CONDITION, CRACKS, AND CORROSION2. GENERAL VISUAL INSPECTION OF SEATS INCLUDINGLEGS, FRAME, BACKREST, ARMREST AND TABLERETAINER FOR SATISFACTORY CONDITION, CRACKSAND CORROSION252100-0502-2 200 CREW REST UNIT MEC GVI I: 2 C MRB AMM 253111/6011 3.00 F4GENERAL VISUAL INSPECTION OF CREW REST UNIT SEATS ANDFURNISHING INCLUDING SEAT BELT ASSY AND FLOORATTACHMENT STRUCTURE.252331-0502-1 200 PANELS-LOWER SIDEWALL MEC DET I: 1 C MPD SIL 25-0851 0.30 ALLREMOVE PANEL AND CARRY OUT DETAILED INSPECTIONOF LOWER SIDE WALL PANEL AND OF AREA BEHIND LOWERSIDE WALL PANEL FOR FOREIGN MATERIAL ACCUMULATION.NOTE: 01. ONE LOWER SIDE WALL PANEL IN FWD MID ANDAFT PASSENGER CABIN SHOULD BE REMOVED INORDER TO ACCESS THE NEED FOR MOREEXTENSIVE PANEL REMOVAL.(APPROX. 2,5 M/H).* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION:2-25 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)252331-0502-1 * * * * * C O N T I N U E * * * * *02. ALTERNATE SIDEWALL PANEL IS RECOMMENDEDAT NEXT INSPECTION.03. INTERVAL MAY BE ADJUSTED ACCORDING TOOPERATOR EXPERIENCE.252331-0503-1 200 PANELS-LOWER SIDE WALL MEC OPC I: 2 C MRB ** AMM 256610/2011 0.20 POST 01545(53-0050)OPERATIONAL TEST OF DECOMPRESSION PANELS, TEST ATLEAST ONE PANEL IN EACH ZONE:01. PRESS SPRING-LOADED MOVABLE (DECOMPRESSION)PANELS AT LOWER REGION OF GRILL TOWARDS REAR02. PANEL MUST BE CLOSED AUTOMATICALLY253000-0502-1 200 BUFFET AND GALLEY MEC GVI I: 1 C MRB AMM 253000/6011 2.00 ALLGENERAL VISUAL INSPECTION OF SLIDING COMPONENTS,HINGES, LATCHES, LOCKS, BUMPERS AND STOPS.253000-0502-2 200 GALLEY LOWER ATTACHMENTS MEC DET I: 5 YE MRB AMM 253111/4011 1.00 ALLAMM 253211/401DETAILED INSPECTION OF GALLEY LOWER AMM 253311/401ATTACHMENTS.EFERENCE:REMARKS: CARRY OUT THIS TASK TOGETHER WITHZL-220-0403-5254000-0502-1 200 LAVATORY COMPARTMENTS MEC DET I: NOTE 5-3 MPD FAA AD 74-08-09 1 0.50 ALLORDETAILED INSPECTION OF ALL LAVATORY PAPER AND CLINEN WASTE RECEPTACLE ENCLOSURE ACCESS DOORS ANDDISPOSAL DOORS FOR PROPER OPERATION, FIT, SEALING ANDLATCHING FOR THE CONTAINMENT OF POSSIBLE TRASH FIRESNOTE: 1000 FH INTERVAL FOR OPERATORS FLYINGUNDER FAA REGULATIONS AS PER AD 74-08-09R2255000-0502-1 100 CARGO COMPARTMENTS MEC GVI I: 1 A MRB AMM 255180/0011 1.50 ALLAMM 255280/001* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION:2-25 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)255000-0502-1 * * * * * C O N T I N U E * * * * *GENERAL VISUAL INSPECTION OF FWD, AFT AND BULK CARGO AMM 523000/301COMPARTMENTS, INCL. DOORS AND CARGO LOADING SYSTEMFOR CONDITION AND CLEANLINESS (CHECK DRAIN PANS FORANY EVIDENCE OF DRAINAGE SYSTEM OBSTRUCTION).255120-0502-1 100 LININGS AND CEILINGS MEC GVI I: DY-TERM CN CN1 0.70 PRE 01878FAA AD 1982-022-044(B) (25-0149)GENERAL VISUAL INSPECTION OF DECOMPRESSION PANELS FAA AD 85-17-06 PRE 02506IN PARTITION WALL, SIDEWALLS AND CEILING LININGS FOR ISB 25-0138(25-0248)CONDITION AND CORRECT ATTACHMENT IN PANEL CUT-OUT.255120-0502-2 100 LININGS AND CEILINGS MEC GVI I: 600 FH CN CN1 0.70 POST 01878FAA AD 1982-022-044(B) (25-0149)CHECK FWD,AFT AND BULK CARGO COMPARTMENTS MRB ** FAA AD 85-17-06 POST 02506DECOMPRESSION PANELS IN POSITION AND CORRECTLY ISB 25-0138(25-0248)ATTACHED (ZONE 130,150,160)PRE 03361(25-0332)255130-0502-1 130 FWD CARGO COMPARTMENT MEC GVI I: NOTE 5-2 MRB AMM 255100/7011 0.50 ALL01. VACUUM CLEANING OF FWD CARGO CONVEYANCESYSTEM.02. GENERAL VISUAL INSPECTION OF FWD CARGO LATCHES,END STOPS AND GUIDES.255230-0502-1 150 AFT CARGO COMPARTMENT MEC GVI I: NOTE 5-2 MRB AMM 255100/7011 0.50 ALL01. VACUUM CLEANING OF AFT CARGO CONVEYANCE SYSTEM.02. GENERAL VISUAL INSPECTION OF AFT CARGO LATCHES,END STOPS AND GUIDES.255820-0502-1 200 BARRIER NET AND SMOKE CURT. MEC GVI I: 1 A MRB ** AMM 255800/6011 0.10 C4IN CARGO CONFIGGENERAL VISUAL INSPECTION OF BARRIER NET AND SMOKEF4PROTECTIVE CURTAIN IN CABIN.SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION:2-25 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)255820-0503-1 200 BARRIER NET AND SMOKE CURT. MEC FUC T: 3 YE MRB ** CMM 2558531 0.25 C4I: 1 YEF4REMOVE TEST NET STRAP AND PERFORM FUNCTIONALTEST (A SAMPLE TEST PROOF LOADING)255820-0504-1 200 BARRIER NET AND SMOKE CURT. MEC RAR I: NOTE 5-1 MRB ** AMM 255823/4012 1.50 C4AMM 255824/401F4REMOVE BARRIER NET AND SMOKE CURTAIN, SEND TOWORKSHOP OR MANUFACTURER FOR OVERHAUL255830-0502-1 200 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 3 A MRB AMM 255810/0011 2.50 C4IN CARGO CONFIGGENERAL VISUAL INSPECTION OF CARGO LOADING SYSTEM,F4CLEAN IF NECESSARY.255830-0502-2 200 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: NOTE 5-2 MRB AMM 255800/7011 1.00 C4F401. VACUUM CLEANING OF UDC CARGO CONVEYANCE SYSTEM.02. GENERAL VISUAL INSPECTION OF UDC CARGO COMPART-MENT LATCHES, END STOPS AND GUIDES.03. GENERAL VISUAL INSPECTION OF DRAIN SYSTEMINSTALLATION.256100-0502-1 830 ESCAPE FACILITIES MEC GVI I: WEEKLY MRB ** AMM 256100/6011 0.60 ALL8401 0.60CHECK ESCAPE SLIDE/RAFT BOTTLES FOR CORRECTPRESSURE AND CONTAINER FOR SATISFACTORY CONDITION (INSITU)256111-0503-1 830 SLIDE/RAFT - ESCAPE MEC FUC I: 6 MO MRB ** AMM 256100/5011 1.00 ALL8401 1.0001. FUNCTIONAL TEST OF ESCAPE SLIDE/RAFT LIGHTING REFERENCE:SYSTEM (BATTERY CAPACITY CHECK).02. BULB CONTINUITY CHECK.256111-0503-2 830 SLIDE/RAFT ESCAPE MEC OPC I: 18 MO MRB ** AMM 256100/3012 2.50 ALL840 OR AMM 256100/5012 2.50OPERATIONAL TEST OF ESCAPE SLIDE/RAFT NOTE 5-3* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION:2-25 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)256111-0503-2 * * * * * C O N T I N U E * * * * *NOTE: - DEPLOYMENT OF ONE SLIDE/RAFT PER DOORPOSITION, (831 OR 841), (832 OR 842),(833 OR 843), (834 OR 844).- ONE SAMPLE PER OPERATOR FLEET.- ALTERNATE DOOR POSITION AT NEXT INTERVALRECOMMENDED.- CREW TRAINING MAY BE USED TO SATISFY THISREQUIREMENT.NOTE: REFER TO TASK 256111-0504-2256111-0503-3 830 SLIDE/RAFT - ESCAPE MEC RAR I: NOTE 5-3 MRB ** AMM 256111/4012 2.00 ALL840 AMM 256112/4012 2.00REMOVE ESCAPE SLIDE/RAFTS FOR SHOP RESTORATION AMM 256115/401256111-0504-2 830 SLIDE/RAFT-ESCAPE BATTERIES MEC RAR I: 4 YE MRB ** AMM 256100/5011 6.00 ALL8401 6.00REPLACE ESCAPE SLIDE/RAFT BATTERIES (MODELBAS 10-1 OR BAS 19)NOTE: REFER TO TASK 256111-0503-2256111-0504-3 830 SLIDE/RAFT - AIR BOTTLE MEC RAR I: NOTE 5-3 MRB ** AMM 256111/4011 3.00 ALL840 AMM 256112/4011 3.00HYDROSTATIC TEST OF AIR BOTTLES IN ACCORD. WITH LOCAL AMM 256115/401NATIONAL REQUIREMENTS OR PRIOR TO NEXT FULL ORPARTIAL REFILLING AFTER 36 MONTHS SINCE LASTHYDROSTATIC TEST. (MAX. SERVICE LIFE IN ACCORD. WITHNAT.REQTS/MANUF. RECOMMENDATIONS).256113-0503-1 210 DESCENT DEVICE-EMERGENCY MEC RAR I: 60 MO MRB AMM 256113/4011 2.00 ALLREMOVE EMERGENCY DECENT DEVICES AND SEND TOVENDORSYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION:2-25 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)256200-0502-1 200 FLOTATION & SURVIVAL EQUIP. MEC GVI I: WEEKLY MRB ** AMM 256200/6001 0.50 ALLGENERAL VISUAL INSPECTION OF FLOTATION AND SURVIVALEQUIPMENT.256200-0504-1 200 FLOAT. AND SURVIVAL EQUIP. MEC RAR I: NOTE 5-3 MRB ** AMM 256200/0011 8.00 ALL- REMOVE/REPLACE LIFE VESTS FOR OVERHAUL.(IF INSTALLED).256300-0503-1 210 EVACUATION SIGNALING EQUIP. MEC OPC I: 2 A MRB ** AMM 256300/5011 0.10 ALLOPERATIONAL TEST OF EVACUATION SIGNALING EQUIPMENT.256531-0503-1 200 TRANSMITTER-BEACON ERI OPC I: NOTE 5-1 MRB ** AMM 256533/4011 0.20 POST 02475REMOVE EMERGENCY LOCATOR TRANSMITTER FORWORKSHOP TEST (BATTERY CHECK AND FUNCTIONALTEST)256532-0503-1 200 MEGAPHONE ERI OPC I: 1 C MRB AMM 256532/6011 0.10 ALLOPERATIONAL TEST OF MEGAPHONE256532-0504-1 200 MEGAPHONE ERI RAR I: NOTE 5-1 MRB ** AMM 256532/6011 0.20 ALLCMM 256504DISCARD MEGAPHONE BATTERIES.257200-0502-1 147 WHEEL WELLS MEC DET I: 2 YE ISB ISB 25-04771 TBD PRE 129381481 TBD (25-0479)DETAILED INSPECTION OF THE ATTACHMENT FITTINGSOF THE ACCESS PANELS BETWEEN THE AIR CONDITIONING-AND THE MAIN LANDING GEAR BAYSACCESS: 147FZ 147GZ 147MZ* 0.13* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION:2-25 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)257200-0502-1 * * * * * C O N T I N U E * * * * *148GZ 148HZ* 0.05* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION:2-25 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)261100-0503-1 120 AVIONICS COMP. SMOKE DETECT. ERI FUC I: 1 C MRB ** AMM 261100/5012 0.50 ALLFUNCTIONAL TEST OF POWER SUPPLY AND FAULT MONITORINGCIRCUITACCESS: 132AZ* 0.01261100-0503-2 210 AVIONICS COMP. SMOKE DETECT. ERI OPC I: WEEKLY MRB ** AMM 261100/5011 0.10 ALLAMM 261400/501OPERATIONAL TEST OF SMOKE DETECTION SYSTEM AMM 261700/501AVIONICS/CARGO COMPARTMENT, TOILET VENTILATION SYSTEM261112-0505-1 100 DETECTOR-SMOKE ERI CLN I: 4000 FH MRB ** AMM 261112/4011 21.00 POST 02672NOTE AMM 261411/401(26-0036)REMOVE,CLEAN AND INSPECT SMOKE DETECTORS FOR SIL 26-015SATISFACTORY CONDITION IN ZONES 120,130,150,160AND 170 AND CLEAN ASSOCIATED INLET AND OUTLETDUCTINGS OF DUCT SMOKE DETECTORS IN ZONE 120NOTE: INTERVAL 4000 FH RECOMMENDED BUT TO BEADJUSTED TO SUIT OPERATING ENVIRONMENTACCESS: 132AZ 134AR* 0.01261112-0505-2 100 DETECTOR SMOKE ERI CLN I: 4000 FH MRB ** AMM 261112/4011 16.50 PRE 02672NOTE AMM 261411/401(26-0036)01. REMOVE CLEAN AND CHECK SMOKE DETECTORS IN FWD SIL 26-015CARGO COMPARTMENT INCLUDING DUCT SMOKE DETECTORSIN ZONE 133/134 FOR SATISFACTORY CONDITION02. REMOVE LININGS IN ZONE 162 AS REQUIRED03. REMOVE SMOKE DETECTORS OF AFT AND REAR CARGOCOMPARTMENT INCLUDING DUCT SMOKE DETECTORS INZONE 162, CLEAN AND INSPECT FOR SATISFACTORYCONDITION04. CLEAN ASSOCIATED INLET AND OUTLET DUCTINGSOF DUCT SMOKE DETECTORS IN ZONE 133/134/16205. INSTALL SMOKE DETECTORS06. REINSTALL LININGSNOTE: INTERVAL 4000 FH RECOMMENDED BUT TO BE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)261112-0505-2 * * * * * C O N T I N U E * * * * *ADJUSTED TO SUIT OPERATING ENVIRONMENTACCESS: 134AR 162AZ* 0.01261121-0503-1 210 FAN-SMOKE DETECTION SNIFFER ERI OPC I: 1 C MRB ** AMM 261121/4011 0.17 ALLOPERATIONAL TEST OF SMOKE DETECTION SNIFFER FAN (MINEQT BAY SNIFFER FAN)261200-0503-1 122 ENGINE FIRE DETECTION ELO OPC I: 1 C MPD AMM 261200/5011 0.10 FWD-FACEPRE 02424BITE TEST OF ENGINE FIRE DETECTION CONTROL UNITS(26-0029)ACCESS: 131AZ 132AZ* 0.01261200-0503-2 210 ENGINE FIRE DETECTION ELO OPC I: 2 C MPD AMM 261200/5011 0.10 FWD-FACEEXTENDED "LOOP TEST" ON ENGINE FIRE CONTROL PANELS(FIRE DETECTION IN "LOOP A OR LOOP B" CONFIGURATION)261200-0503-3 210 ENGINE FIRE DETECTION ELO OPC I: DY-TERM MRB ** AMM 261200/5011 0.10 ALLAMM 261300/501OPERATIONAL TEST OF ENGINE AND APU FIRE DETECTIONSYSTEM (LOOP TEST)261200-0503-4 210 ENGINE FIRE DETECTION ELO OPC I: DY-TERM MPD AMM 261200/5011 0.10 FWD-FACE"LOOP TEST" ON ENGINE FIRE CONTROL PANELS (FIREDETECTION IN "LOOP A AND LOOP B" CONFIGURATION).261600-0503-1 210 OVERHEAT DETECTION ERI OPC I: WEEKLY MRB ** AMM 261600/5011 0.10 NON FWD-FACEOPERATIONAL TEST OF MANIFOLD FAULT DETECTION SYSTEM(LOOPS TEST ON PANEL 59VU).SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)261600-0503-2 210 OVERHEAT DETECTION ELO OPC I: WEEKLY MRB ** AMM 261600/5011 0.10 FWD-FACEOPERATIONAL TEST OF MANIFOLD "LEAK" DETECTIONSYSTEM.(LOOPS TEST ON PANEL 471VU)261700-0503-1 120 SMOKE DETEC-LAVATORY VENT. ERI FUC I: 1 C MRB AMM 261700/5012 0.30 POST 00854(26-0011)FUNCTIONAL TEST OF POWER SUPPLY AND FAULT MONITORINGPRE 01928CIRCUIT(26-0028)PRE 02503ACCESS: 132AZ* 0.01 (26-0030)ORPRE 01928(26-0028)PRE 02503(26-0030)POST 06335(26-0049)261900-0503-1 120 SMOKE DETECTION - CABIN CARGO ERI FUC I: 1 C MRB ** AMM 261900/5012 0.50 C4F4FUNCTIONAL TEST OF POWER SUPPLY AND FAULT MONITORINGCIRCUIT.NOTE: IN CARGO CONFIGURATION ONLY.261900-0503-2 210 SMOKE DETECTION - CABIN CARGO ERI OPC I: DY-TERM MRB ** AMM 261900/5011 0.10 C4F4OPERATIONAL TEST OF SMOKE DETECTION SYSTEM CABINCARGONOTE: IN CARGO CONFIGURATION ONLY261911-0505-1 200 DETECTOR - SMOKE ERI CLN I: 2 C MRB ** AMM 261912/4011 12.00 C4SIL 26-015IN CARGO CONFIGCLEAN UPPER (MAIN) DECK SMOKE DETECTORS AND INSPECTF4FOR SATISFACTORY CONDITION.PREP.: REMOVE/INSTALL SMOKE DETECTORS.SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)262100-0502-1 415 ENGINE FIRE EXTINGUISHING MEC DET I: 8000 FH CN AMM 262100/6011 0.20 PRE 03599425 FAA AD CN1 0.20 PRE 08430DETAILED INSPECTION OF FIRE EXTINGUISHER PIPE 1990-056-106(B) (26-0055)AT RIB 12 OF ENGINE PYLON. FAA AD 92-23-05ACCESS: 415AL 416AR 473AL 474AR* 0.15425AL 426AR 483AL 484AR* 0.15262100-0503-1 473 ENGINE FIRE EXTINGUISHING ENG FUC I: 3 C MRB ** AMM 262100/5012 1.00 ALL4842 1.00FUNCTIONAL TEST OF ELECTRICAL PERCUSSION CIRCUITAND EXTINGUISHER BOTTLE LOW PRESSURE INDICATINGELECTRICAL CIRCUIT.ACCESS: 473AL* 0.01484AR* 0.01262100-0503-2 473 ENGINE FIRE EXTINGUISHING ENG OPC I: 3 C MRB ** AMM 262100/5011 1.00 ALL4841 1.00OPERATIONAL TEST OF CHECK VALVE AND CHECKEXTINGUISHER LINES FOR LEAKAGE AND SATISFACTORYCONDITIONACCESS: 435AL 436AR 473AL* 0.04445AL 446AR 484AR* 0.04262100-0503-3 474 ENGINE FIRE EXTINGUISHING ENG FUC I: NOTE CN AMM 262111/4011 0.30 POST 01988484 FAA AD CN1 0.30 (54-0022)BONDING CHECK OF FIRE-EXTINGUISHER BOTTLE 1988-181-089(B)INSTALLATION FAA AD 89-09-01NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITYOF TASK 262111-0504-1 AND 262113-0504-1ACCESS: 473AL* 0.01484AR* 0.01262100-0503-4 210 ENGINE FIRE EXTINGUISHING ENG OPC I: DY-TERM MRB ** AMM 262100/5011 0.10 ALLOPERATIONAL TEST OF ENGINE FIRE EXTINGUISHINGCIRCUITS (SQUIB TEST). CHECK THAT AGENT INDICATOR* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)262100-0503-4 * * * * * C O N T I N U E * * * * *DOES NOT INDICATE DISCHARGE262111-0503-1 474 BOTTLE - FIRE EXTING.ENGINE ENG FUC I: 2 C MRB AMM 262111/6011 3.00 POST 019884841 3.00 (54-0022)FUNCTIONAL CHECK OF SHOCK-ABSORBERS:01. COMPRESS SHOCK-ABSORBERS BY APPLICATION OF AFORCE EQUAL TO 1/4 OF BOTTLE WEIGHT02. CHECK HEIGHT OF SHOCK-ABSORBERS BETWEEN UPPERAND LOWER FASTENING POINT03. IF DIMENSION IS LOWER THAN, OR EQUAL TO, 8MM RE-PLACE SHOCK ABSORBERSACCESS: 473AL* 0.01484AR* 0.01R 262111-0504-1 474 BOTTLE - FIRE EXTING.ENGINE ENG RAR I: NOTE 5-3 MRB ** AMM 262111/6011 2.00 POST 01988484 OR1 2.00 (54-0022)WEIGHT CHECK OF ENGINE FIRE EXTINGUISHER BOTTLES. NOTE 5-1NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITYOF TASK 262100-0503-3ACCESS: 473AL* 0.01484AR* 0.01R 262111-0504-2 474 BOTTLE - FIRE EXTING.ENGINE ENG RAR I: NOTE 5-3 MRB ** AMM 262111/4011 2.00 ALL484 OR1 2.00HYDROSTATIC TEST OF ENGINE FIRE EXTINGUISHER NOTE 5-1BOTTLESACCESS: 473AL* 0.01484AR* 0.01262111-0504-3 474 ENGINE FIRE EXTING. BOTTLE ENG RAR I: 6 MO ISB AMM 262111/6011 2.50 PRE 01988484 ISB 26-0251 2.50 (54-0022)REMOVE FIRE EXTINGUISHING BOTTLE FOR WEIGHTCHECK, CHECK EXPIRATION DATE OF DISCHARGE CARTRIDGE,PERFORM DYE-PENETRANT CHECK OF MOUNTING LUGS* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)262111-0504-3 * * * * * C O N T I N U E * * * * *ACCESS: 473AL* 0.01484AR* 0.01262113-0504-1 474 CARTRIDGE-DISCHARGE-ENGINE ELO RAR I: NOTE 5-1 MRB AMM 262113/4011 1.00 ALL4841 1.00REPLACE DISCHARGE CARTRIDGE OF ENGINE FIREEXTINGUISHERSNOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITYOF TASK 262100-0503-3ACCESS: 473AL* 0.01484AR* 0.01262200-0502-1 313 APU FIRE EXTINGUISHING ENG GVI I: DY-TERM MRB AMM 262200/0011 0.10 ALLCHECK APU FIRE EXTINGUISHER BOTTLE DISCHARGEINDICATOR FOR PRESENCE262200-0503-1 313 APU FIRE EXTINGUISHING ERI FUC I: 3 C MRB ** AMM 262200/5012 1.00 ALL01. FUNCTIONAL TEST OF ELECTRICAL PERCUSSION CIRCUIT02. FUNCTIONAL TEST OF AUTOMATIC EXTINGUISHINGCIRCUIT03. FUNCTIONAL TEST OF THE EXTINGUISHER BOTTTLEPRESSURE DROP INDICATING CIRCUITACCESS: 313AL* 0.14262200-0503-2 210 APU FIRE EXTINGUISHING ERI OPC I: WEEKLY MRB ** AMM 262200/5011 0.10 ALLOPERATIONAL TEST OF APU FIRE EXTINGUISHING CIRCUIT(SQUIB TEST) PERFORM GROUND TEST OF THE APU AUTOMATICEXTINGUISHING CIRCUIT.262211-0504-1 313 BOTTLE - FIRE EXTING. APU ENG RAR I: NOTE 5-3 MRB ** AMM 262211/4011 1.00 ALLORWEIGHT CHECK OF APU FIRE EXTINGUISHER BOTTLE 1 YE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)262211-0504-1 * * * * * C O N T I N U E * * * * *ACCESS: 313AL* 0.14262211-0504-2 313 BOTTLE - FIRE EXTING. APU ENG RAR I: NOTE 5-3 MRB ** AMM 262211/4011 1.00 ALLHYDROSTATIC TEST OF APU FIRE EXTINGUISHER BOTTLE INACCORDANCE WITH LOCAL NATIONAL REQUIREMENTS OR PRIORTO NEXT FULL OR PARTIAL REFILLING AFTER 60 MONTHSSINCE LAST HYDROSTATIC TEST.(MAX.SERVICE LIFE IN ACCORDANCE WITH NATIONAL REQTS./VENDOR RECOMMENDATIONS)ACCESS: 313AL* 0.14262212-0504-1 313 CARTRIDGE - DISCHARGE APU ELO RAR I: NOTE 5-1 MRB AMM 262212/4011 0.50 ALLREPLACE DISCHARGE CARTRIDGE OF APU FIRE EXTINGUISHER.ACCESS: 313AL* 0.14262300-0503-1 132 CARGO COMPART FIRE EXTING. ELO FUC I: 3 C MRB ** AMM 262300/5012 0.75 ALL01. FUNCTIONAL TEST OF ELECTRICAL PERCUSSION CIRCUIT02. FUNCTIONAL TEST OF EXTINGUISHER BOTTLE PRESSUREDROP INDICATING CIRCUITACCESS: 132DZ* 0.10262300-0503-2 210 CARGO COMPART.FIRE EXTING. ELO OPC I: DY-TERM MRB ** AMM 262300/5011 0.10 ALLOPERATIONAL TEST OF CARGO COMPARTMENTS FIREEXTINGUISHING CIRCUITS (SQUIB TEST). CHECK THAT AGENTINDICATOR DOES NOT INDICATE DISCHARGE262300-0503-3 210 CARGO COMPART.FIRE EXTING. ELO OPC I: DY-TERM MPD AMM 262300/5011 0.10 POST 03255(26-0043)VALVE POSITION TEST OF AFT/BULK CARGO COMPARTMENTFIRE EXTINGUISHING DIRECTION VALVESYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)262311-0504-1 132 BOTTLE - FIRE EXTING. CARGO MEC RAR I: NOTE 5-3 MRB ** AMM 262311/4011 1.00 ALLORWEIGHT CHECK OF FWD CARGO COMPARTMENT FIRE 1 YEEXTINGUISHER BOTTLESACCESS: 132DZ* 0.10262311-0504-2 132 BOTTLE - FIRE EXTING.CARGO MEC RAR I: NOTE 5-3 MRB ** AMM 262311/4011 1.00 ALLHYDROSTATIC TEST OF FWD CARGO COMPARTMENT FIREEXTINGUISHER BOTTLES IN ACCORDANCE WITH LOCALNATIONAL REQUIREMENTS,OR PRIOR TO NEXT FULL ORPARTIAL REFILLING AFTER 60 MONTHS SINCE LASTHYDROSTATIC TEST.(MAX.SERVICE LIFE IN ACCORDANCE WITH NATIONAL REQTS./VENDOR RECOMMENDATIONS)ACCESS: 132DZ* 0.10R 262312-0504-1 132 BOTTLE - FIRE EXTING.CARGO MEC RAR I: NOTE 5-1 MRB AMM 262312/4011 0.50 ALLREPLACE DISCHARGE CARTRIDGE OF FWD CARGO COMPARTMENTFIRE EXTINGUISHERS.ACCESS: 132DZ* 0.10262411-0502-1 120 PORTABLE FIRE EXTINGUISHER MEC GVI I: 1 A MRB ** AMM 262400/0011 0.08 ALLCHECK PRESSURE OF PORTABLE FIRE EXTINGUISHERAT GAUGE IN AVIONICS COMPARTMENT262411-0502-2 200 PORTABLE FIRE EXTINGUISHER MEC GVI I: 1 A MRB ** AMM 262400/0011 0.50 ALLCHECK PRESSURE OF PORTABLE FIRE EXTINGUISHERSAT GAUGE IN CABIN AREA262411-0502-3 210 PORTABLE FIRE EXTINGUISHER MEC GVI I: 1 A MRB ** AMM 262400/0011 0.08 ALLCHECK PRESSURE OF PORTABLE FIRE EXTINGUISHERAT GAUGE IN FLIGHT COMPARTMENTSYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)262411-0504-1 121 PORTABLE FIRE EXTINGUISHER MEC RAR I: NOTE 5-3 MRB ** AMM 262400/0011 0.20 ALL200 OR1 1.20WEIGHT CHECK OF PORTABLE FIRE EXTINGUISHER BOTTLES. 1 YE262411-0504-2 121 PORTABLE FIRE EXTINGUISHER MEC RAR I: NOTE 5-3 MRB ** AMM 262400/0011 0.30 ALL2001 2.30HYDROSTATIC TEST OF PORTABLE FIRE EXTINGUISHERBOTTLES IN ACCORDANCE WITH LOCAL NATIONAL REQUIRE-MENTS, OR PRIOR TO NEXT FULL OR PARTIAL REFILLINGAFTER 60 MONTHS SINCE LAST HYDROSTATIC TEST.(MAXIMAL SERVICE LIFE IN ACCORDANCE WITH NATIONALREQUIREMENTS/VENDOR RECOMMENDATIONS)262411-0504-3 200 PORTABLE FIRE EXTINGUISHER MEC RAR I: NOTE 5-3 MRB ** AMM 262400/0011 1.00 C4ORIN CARGO CONFIGWEIGHT CHECK OF UPPER (MAIN) DECK CARGO COMPARTMENT 1 YEF4FIRE EXTINGUISHER BOTTLES.262500-0502-1 220 LAVATORY FIRE EXTINGUISHING MEC GVI I: 400 FH ISB AMM 262500/2011 0.40 PRE 08729ISB 26-057(26-0058)GENERAL VISUAL INSPECTION IN-SITU OF THELAVATORY FIRE EXTINGUISHER AND DISCHARGE TUBES262500-0502-2 200 LAVATORY FIRE EXTINGUISHING MEC GVI I: WEEKLY MRB ** AMM 262500/2011 0.20 POST 01796(26-0017)VISUAL INSPECTION OF LAVATORY FIRE EXTINGUISHINGORBOTTLE FOR SIGNS OF DISCHARGEPOST 02187(26-0031)262500-0504-1 200 LAVATORY FIRE EXTINGUISHING MEC RAR I: 2 C MRB ** AMM 262500/2011 5.25 POST 01796(26-0017)01. REMOVE BOTTLE FOR WEIGHT CHECKOR02. INSPECT BOTTLE AND PIPES FOR SATISFACTORY CON-POST 02187DITION(26-0031)03. CHECK DISCHARGE INDICATORS04. INSPECT MOUNTING BRACKETS FOR DAMAGE AND SECURITYOF ATTACHMENTS05. REINSTALL BOTTLE* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION:2-26 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)271100-0503-1 575 MECHANICAL CONTROL,AILERON MEC FUC I: 3 C MRB AMM 271000/6011 0.50 ALL6751 0.50CHECK CONTROL CABLE OF AILERON TRIM IN WING AREAFOR CORRECT TENSION WITH TENSIOMETER IN ACCORDANCEWITH THE RESP. AMM CABLE TENSION AND ADJUSTMENTGRAPH.ACCESS: 575AB* 0.04675AB* 0.04271100-0503-2 210 MECHANICAL CONTROL-LSA MEC OPC I: WEEKLY MRB ** AMM 271100/5011 0.10 ALLOPERATIONAL TEST OF LOW SPEED AILERON LOCK OUT SYSTEM271116-0503-1 120 SPRING ROD-INTERCONNECTING MEC OPC I: 4 C MPD AMM 271100/6012 0.50 ALL2102 0.50CHECK COMPRESSION AND EXTENSION OF SPRING ROD:(LOCATED BETWEEN PILOT/CO-PILOT CONTROL COLUMN INZONE 120)- SIMULATE PILOT OR CO-PILOT CONTROL SYSTEM JAMMINGBY INSERTING APPROPRIATE RIGGING PIN.ACCESS: 132AZ* 0.01271117-0503-1 120 REGULATOR - CABLE TENSION MEC FUC I: 3 C MPD AMM 271000/6011 2.00 ALLAMM 272000/60101. CHECK IN ACCORDANCE WITH THE RESPECTIVE AMM CABLE AMM 273000/601TENSION ADJUSTMENT GRAPH THE FOLLOWING MECHANICAL AMM 274000/601CONTROL CABLES IN ZONES 121/122 FOR CORRECT AMM 275000/601TENSION: AMM 761100/501- ALL SPEED AILERON, AILERON TRIM- RUDDER CONTROL, RUDDER TRIM- ELEVATOR CONTROL- TRIMABLE HORIZONTAL STABILIZER CONTROL- FLAP CONTROL- THROTTLE CONTROLNOTE: USE CABLE TENSIOMETER AND PLACE IT APPROX. ONE(1) METER NEAR THE CABLE TENSION REGULATOR02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLETENSION REGULATOR IS WITHIN LIMITS03. CHECK REGULATORS FOR CLEANLINESS,WEAR,CORROSION,* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)271117-0503-1 * * * * * C O N T I N U E * * * * *SECURITY OF ATTACHMENT AND INSTALLATIONACCESS: 121TF 121XF 132AZ* 0.42271122-0504-1 575 MECH.DIFF.DROOP&FEEL LH-RH MEC RAR I: NOTE MRB ** AMM 271122/4011 17.00 ALL675 ISB 05-00041 17.00SAMPLING INSPECTION OF DIFFERENTIAL DROOP AND FEELMECHANISM ASSEMBLY IN ACCORDANCE WITH MANUFACTURERSINSTRUCTIONS SAMPLE SIZE - ONE ITEM FROM EACHOPERATORS FLEETNOTE: INSPECTION TO BE CARRIED OUT BETWEEN23000 FH AND 27000 FHACCESS: 131DZ 132DZ 575AB 575AT 575BB 575BT* 0.74575CB 575DB 575FB 575GB131DZ 132DZ 675AB 675AT 675BB 675BT* 0.74675CB 675DB 675FB 675GB271122-0505-1 575 MECH.DIFF.DROOP & FEEL MEC LUB I: 1 C MRB AMM 122227/0011 0.50 ALL6751 0.50CLEAN, INSPECT AND LUBRICATE DROOP INPUT MECHANISM(AEROSOL SPRAY APPLICATION USING MINERAL OIL).NOTE: AILERON TO BE UNDROOPED AND FULLY UP ON SIDETO BE LUBRICATEDACCESS: 575AB* 0.04675AB* 0.04271122-0505-2 575 MECH.DIFF.DROOP & FEEL MEC LUB I: 2 C MPD AMM 122227/0011 0.25 ALL6751 0.25LUBRICATE TRIM SCREW JACK AND CHAIN OF AILERONACCESS: 575AB* 0.04675AB* 0.04271122-0505-3 121 MECH.DIFF.DROOP & FEEL MEC LUB I: 2 C MPD AMM 122227/0011 0.25 ALL* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)271122-0505-3 * * * * * C O N T I N U E * * * * *LUBRICATE CHAINS IN TRIM SYSTEM OF AILERON ANDRUDDER (BRUSH APPLICATION)ACCESS: 132AZ* 0.01271122-0505-4 143 MECH.DIFF.DROOP & FEEL MEC LUB I: 2 C MPD AMM 122227/0011 0.30 ALLLUBRICATE CHAIN IN AILERON TRIM SYSTEM (BRUSHAPPLICATION)ACCESS: 143BF* 0.09271141-0502-1 581 DETENT UNIT-FULL STROKE MEC DET I: 1 C MRB AMM 271100/0011 0.50 ALL6811 0.50DETAILED INSPECTION OF AILERON FULL STROKEDETENT UNIT FOR CLEANLINESS, SECURITY OF ATTACHMENTS,SATISFACTORY CONDITION AND IDLER (ROLLER) AND CAM FORWEAR.ACCESS: 575FB 575GB 581CB* 0.22675FB 675GB 681CB* 0.22271141-0503-1 581 DETENT UNIT-FULL STROKE MEC FUC I: 6 C MRB ** AMM 271141/4012 6.00 ALL681 AMM 271141/6012 6.00CHECK BREAK OUT LOAD OF AILERON FULL STROKEDETENT UNIT BY EITHER OF FOLLOWING METHODS:A. WITH DETENT UNIT REMOVAL01. REMOVE FULL STROKE DETENT UNIT02. CHECK BREAK OUT LOAD (REFER TO OVERHAULMANUAL)03. REINSTALL FULL STROKE DETENT UNITB. WITHOUT DETENT UNIT REMOVAL01. CHECK BREAK OUT LOAD USING SPECIAL TOOL98A 27308031ACCESS: 575FB 575GB 581CB* 0.22675FB 675GB 681CB* 0.22SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)271142-0503-1 581 REGULATOR CABLE TENSION-LSA MEC FUC I: 3 C MRB AMM 271000/6011 0.50 ALL6811 0.5001. CHECK IN ACCORDANCE WITH THE RESPECTIVE AMM CABLETENSION ADJUSTMENT GRAPH THE LOW SPEED AILERONCONTROL CABLES FOR CORRECT TENSIONNOTE: USE CABLE TENSIOMETER AND PLACE IT APPROX.ONE METER NEAR THE CABLE TENSION REGULATOR02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLETENSION REGULATOR IS WITHIN LIMITS03. CHECK REGULATOR FOR CLEANLINESS,WEAR,CORROSION,SECURITY OF ATTACHMENT AND INSTALLATIONACCESS: 581CB 581EB* 0.10681CB 681EB* 0.10271200-0503-1 210 AILERON TRIM-MECH.CONTROL MEC OPC I: 1 A MRB AMM 271200/5011 0.10 FWD-FACEOPERATIONAL TEST OF AILERON TRIM BY MEANS OF CONTROLWHEEL AND FLIGHT CONTROLS POSITION INDICATOR271216-0502-1 147 BRACKET - PULLEY MEC GVI I: 4400 FH ISB ISB 27-01071 0.30 MACHINED PULLEYS1481 0.30GENERAL VISUAL INSPECTION OF MACHINED AILERON TRIMCONTROL PULLEYS FOR HYDR. FLUID CONTAMINATION.271216-0502-2 500 BRACKET - PULLEY MEC GVI I: 4400 FH ISB ISB 27-01071 0.80 MACHINED PULLEYS6001 0.80GENERAL VISUAL INSPECTION OF MACHINED ALL SPEEDAILERON, AILERON TRIM, RAT, SPEED BRAKE AND LOWSPEED AILERON CONTROL PULLEYS FOR HYDR. FLUIDCONTAMINATIONACCESS: 571DB 575AB 581CB 581EB 591AB* 0.32671DB 675AB 681CB 681EB 691AB* 0.48271400-0503-1 210 SERVO CONTROLS MEC OPC I: 1 C MRB ** AMM 271400/5012 0.50 ALLOPERATIONAL TEST OF SERVO CONTROL JAMMING DETECTIONSYSTEM ( PITCH,ROLL,YAW )SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)271400-0504-1 500 LOW SPEED AILERON MEC RAR I: 9000 FC ISB ISB 27-01092 6.00 ALL6002 6.00REMOVE AND REPLACE LOW SPEED AILERON FLEXIBLEHYDRAULIC PRESSURE HOSES P/N:A2714201001000 ANDP/N: 660000040165RRK.ACCESS: 591AT* 0.11691AT* 0.11271412-0502-1 575 SERVO CONTROLS - AILERON MEC DET I: 1 C SIL AMM 271412/6011 0.20 PRE 12026675 SIL 27-0871 0.20 (27-0192)DETAILED INSPECTION OF ALL SPEEDAILERON SERVO CONTROL BEARINGS FOREVIDENCE OF EXTRUSION OF THE SELFLUBRICATION COATING AND FOR GENERALCONTIONACCESS: 575CB* 0.09675CB* 0.09271412-0503-1 210 SERVO CONTR.-ALL SPEED AIL. MEC OPC I: 5 A MRB ** AMM 271400/5012 0.20 ALLOPERATIONAL TEST OF ALL SPEED AND LOW SPEED AILERONSERVO CONTROLS WITH INDIVIDUAL HYDRAULIC SYSTEMS.271412-0503-2 210 SERVO CONTROLS MEC FUC I: 1300 FH ISB ISB 27-01891 1.50 ALLFUNCTIONAL TEST OF AILERON AND ELEVATOR SERVOCONTROLS WITH EACH HYDRAULIC SYSTEM PRESSURIZEDIN TURN.271414-0503-1 210 VALVE-PRIORITY MEC FUC I: 3 C MRB ** AMM 274200/5012 1.00 ALLAMM 275200/501FUNCTIONAL TEST OF PRIORITY VALVES (GREEN, BLUE, AMM 278200/501YELLOW).271414-0504-1 147 VALVE-PRIORITY MEC RAR I: 10000 FC MPD AMM 271414/4011 0.50 PRE 06675148 AMM 274216/4011 0.50 (29-0091)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)271414-0504-1 * * * * * C O N T I N U E * * * * *312 REPLACE PRIORITY VALVES IN BLUE AND YELLOW HYDRAULIC1 0.50SYSTEMS (TOTAL 3 OFF).271414-0504-2 147 VALVE-PRIORITY MEC RAR I: 10000 FC MPD AMM 271414/4011 0.50 PRE 06676(29-0092)REPLACE PRIORITY VALVE IN GREEN HYDRAULIC SYSTEM.R 272100-0502-1 311 RUDDER MECHANICAL CONTROL MEC GVI SI: 2 C MRB ** AMM 272000/6011 0.25 ALL323 I: COVERED1 0.25GENERAL VISUAL INSPECTION OF DUPLEX LINKAGE FOR BY AMMINTEGRITY, SECURITY OF ATTACHMENTS, SATISFACTORY 272000/CONDITION, WEAR, CORROSION AND CLEANLINESS. 601ACCESS: 312AR 313AL* 0.15325AL 325BL 325CL 325DL* 1.51272100-0504-1 325 RUDDER MECHANICAL CONTROL MEC RAR I: NOTE MRB ** AMM 272117/4011 10.00 ALLISB 05-0004SAMPLING INSPECTION OF DRIVE SHAFT ASSY AND BELLCRANKIN ACCORDANCE WITH MANUFACTURERS INSTRUCTIONS.SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́SFLEET.NOTE: INSPECTION TO BE CARRIED OUT BETWEEN23000 FH AND 27000 FHACCESS: 312AR 325DL* 0.21272200-0503-1 210 RUDDER TRIM-MECH.CONTROL MEC OPC I: 1 A MRB AMM 272200/5011 0.10 FWD-FACEOPERATIONAL TEST OF RUDDER TRIM BY MEANS OF CONTROLWHEEL AND FLIGHT CONTROLS POSITION INDICATOR272200-0505-1 311 RUDDER TRIM-MECHANICAL CONTROL MEC LUB I: 2 C MPD AMM 122227/0011 0.60 ALLLUBRICATE CHAINS IN TRIM SYSTEM (RUDDER)(BRUSH APPLICATION)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)272200-0505-1 * * * * * C O N T I N U E * * * * *ACCESS: 312AR* 0.01272311-0503-1 311 ARTIFICIAL FEEL-RUDDER MEC FUC I: 6 C MRB AMM 272100/5012 1.00 ALLWITH THREE (3) HYDRAULIC SYSTEMS PRESSURIZED:OPERATE RUDDER TO LEFT AND RIGHT FULL TRAVEL.OPERATING FORCES MUST INCREASE WITH INCREASINGRUDDER PEDAL DEFLECTION. CHECK THAT OPERATING FORCESAT TRAVEL ENDS ARE WITHIN SPECIFIED LIMITS.(REFER FOR LIMITS AMM 272100/500 SYSTEM TEST 3.C-3)272311-0504-1 311 ARTIFICIAL FEEL & TRIM UNIT MEC RAR I: NOTE MRB ** AMM 272118/4011 10.00 ALLAMM 272311/401SAMPLING INSPECTION OF ISB 05-0004- ARTIFICIAL FEEL AND TRIM UNIT- MAIN SHAFT, INNER SHAFT AND BELLCRANK ASSYIN ACCORDANCE WITH MANUFACTURERS INSTRUCTIONS.SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́S FLEET.NOTE: INSPECTION TO BE CARRIED OUT BETWEEN23000FH AND 27000FH.ACCESS: 312AR 325DL* 0.21272312-0503-1 210 VARIABLE LEVER ARM UNIT MEC FUC I: 950 FH MRB ** AMM 272300/5012 0.50 ALLFUNCTIONAL TEST OF RUDDER DEFLECTION VERSUS AIRSPEED272312-0503-2 210 VARIABLE LEVER ARM MEC OPC I: 1 A ISB AMM 272300/5011 0.20 PRE 02009ISB 27-0093(27-0097)JAMMING DETECTION TEST OF VARIABLE LEVER ARM UNIT272312-0504-1 311 VARIABLE LEVER ARM UNIT MEC RAR I: NOTE MRB ** AMM 272312/4012 3.00 ALLISB 05-0004SAMPLING INSPECTION OF VARIABLE LEVER ARM UNIT INACCORDANCE WITH MANUFACTURERS INSTRUCTIONS.SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́S FLEET* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)272312-0504-1 * * * * * C O N T I N U E * * * * *NOTE: INSPECTION TO BE CARRIED OUT BETWEEN23000 FH AND 27000 FHACCESS: 312AR 325DL* 0.21272400-0503-1 210 HYDRAULIC ACTUATION MEC OPC I: 1300 FH CN CN F-2004-0922 0.70 ALLFAA AD FAA ADOPERATIONAL TEST OF RUDDER SYSTEM USING EACH 2005-17-14HYDRAULIC SYSTEM IN TURN AND CHECK FOR RUDDER ISB 27-0188DESYNCHRONIZATION FROM THE GROUND.272411-0502-1 320 SERVO CONTROL MEC DET I: 1 C SIL AMM 272411/6011 0.20 PRE 12026SIL 27-087(27-0192)DETAILED INSPECTION OF RUDDER SERVO CONTROLBEARINGS FOR EVIDENCE OF EXTRUSION OF THE SELFLUBRICATION COATING AND FOR GENERAL CONDITIONACCESS: 325DL 326DL* 0.51272411-0503-1 210 SERVO CONTROL - RUDDER MEC OPC I: 1 A MRB ** AMM 271400/5012 0.10 ALLOPERATIONAL TEST OF RUDDER SERVO CONTROLS (WITHINDIVIDUAL HYDRAULIC SYSTEM) BY MOVING RH RUDDERPEDAL FULL FORWARD AND VISUALLY OBSERVE THAT RUDDERMOVES TO RIGHT. CHECK THAT RUDDER TRAVEL IS CONFIRMEDON THE FLIGHT CONTROL POSITION INDICATOR (FCPI).RELEASE RH PEDAL. REPEAT ABOVE TEST BY MOVING LHRUDDER PEDAL.273100-0502-1 310 ELEVATOR MECHANICAL CONTROL MEC GVI I: 2 C MRB ** AMM 273000/6011 0.30 ALL3341 1.00344 VISUAL INSPECTION OF DUPLEX LINKAGE FOR1 1.00INTEGRITY,SECURITY OF ATTACHMENTS,SATISFACTORYCONDITION,WEAR,CORROSION AND CLEANLINESS.ACCESS: 312AR 313AL* 0.15334AB 334BB* 0.41344AB 344BB* 0.41SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)273100-0503-1 210 ELEVATOR CHANNEL UNCOUPLING ERI OPC I: 2500 FH MRB ** AMM 273100/5011 0.50 ALLOPERATIONAL TEST OF ELEVATOR CHANNEL UNCOUPLINGCOMPUTER273100-0503-2 210 ELEVATOR CHANNEL UNCOUPLING ERI FUC I: 12000 FH MRB ** AMM 273100/5012 1.50 ALLFUNCTIONAL TEST OF ELEVATOR CHANNEL UNCOUPLING(SYSTEM)273100-0504-1 313 ELEVATOR MECHANICAL CONTROL MEC RAR I: 23000 FH MRB ** AMM 273121/4011 1.00 ALLTO ISB 05-0004INSPECTION OF DRIVE SHAFT ASSY IN ACCORDANCE WITH 27000 FHMANUFACTURERS INSTRUCTIONS.NOTE: SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́SFLEET.ACCESS: 313AL* 0.14273311-0503-1 210 ARTIFICIAL FEEL - ELEVATOR MEC OPC I: 1 C MRB AMM 273300/5012 0.50 ALLOPERATIONAL TEST OF PITCH ARTIFICIAL FEEL BYCOMPARING QUALITATIVELY OPERATING LOADS IN HIGH-SPEEDAND LOW-SPEED CONFIGURATIONS (WITH EACH INDIVIDUALHYDRAULIC SYSTEM)NOTE: REFER TO REFERENCED AMM CHAPTER SEC.2273311-0503-2 210 ARTIFICIAL FEEL - ELEVATOR MEC FUC I: 6 C MRB AMM 273300/5012 1.00 ALLFUNCTIONAL TEST OF PITCH ARTIFICIAL FEEL BY MEASURINGOPERATING LOADS IN HIGH-SPEED AND LOW-SPEEDCONFIGURATION273311-0504-1 311 ARTIFICIAL FEEL UNIT MEC RAR I: NOTE MRB ** AMM 273311/4012 5.00 ALLISB 05-0004SAMPLING INSPECTION OF ARTIFICIAL FEEL UNIT INACCORDANCE WITH MANUFACTURERS INSTRUCTION.SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́S FLEET* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)273311-0504-1 * * * * * C O N T I N U E * * * * *NOTE: INSPECTION TO BE CARRIED OUT BETWEEN23000 FH AND 27000 FHACCESS: 312AR 313AL* 0.15273313-0503-1 210 COMPUTER-ARTIFICIAL FEEL ELO OPC I: 3500 FH MRB ** AMM 272300/5011 0.50 ALLAMM 273300/501OPERATIONAL TEST OF ARTIFICIAL FEEL "PITCHFEEL"AND"RUDDER TRAVEL"MONITORING CIRCUITS(WARNING LIGHT TEST AND INDICATING SYSTEM TEST)273411-0502-1 334 SERVO CONTROLS - ELEVATOR ERI DET I: 1 C SIL AMM 273411/6011 0.50 PRE 12026344 SIL 27-0871 0.50 (27-0192)DETAILED INSPECTION OF ELEVATOR SERVO CONTROLBEARINGS FOR EVIDENCE OF EXTRUSION OF THE SELFLUBRICATION COATING AND FOR CONDITION.ACCESS: 334CB* 0.13344CB* 0.13273411-0503-1 210 SERVO CONTROL-ELEVATOR MEC OPC I: 5 A MRB ** AMM 271400/5012 0.10 ALLOPERATIONAL TEST OF SERVO CONTROLS WITH INDIVIDUALHYDRAULIC SYSTEMS273600-0503-1 210 AIR DATA WARN.(STALL WARN.) ELO FUC I: 6000 FH MRB ** AMM 273600/5011 0.50 ALLFUNCTIONAL TEST OF STALL WARNING IN ACCORDANCE WITHSLAT POSITION273600-0503-2 210 AIR DATA WARN.(STALL WARN.) ELO OPC I: 1200 FH MRB ** AMM 273600/5011 0.20 ALLOPERATIONAL TEST OF MONITORING CIRCUIT AND STALLWARNINGSYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)274100-0505-1 121 THS-MECHANICAL CONTROL MEC LUB I: 1 C MPD AMM 122227/0011 0.20 ALL3101 0.20LUBRICATE CHAINS IN TRIM SYSTEM (BRUSH APPLICATION).ACCESS: 132AZ* 0.01312AR* 0.01274211-0502-1 312 ACTUATOR GEARBOX - THS MEC GVI I: 1 C MRB AMM 274211/6011 0.25 POST 02787(27-0129)CHECK GEARBOX MAGNETIC DRAIN PLUG FOR EVIDENCEOF METAL PARTICLESACCESS: 312AR* 0.01R 274211-0502-2 311 ACTUATOR - THS MEC FUC T: NOTE AD AMM 274211/6011 5.00 ALL312 I: 2500 FH MRB AD 2009-01111 5.00FUNCTIONAL CHECK OF PHASING BETWEEN THSA MOTORS SB SBPHASING FOLLOWED BY, CHECK GEARBOX MAGNETIC DRAIN SB-A300-27-0201PLUG FOR EVIDENCE OF METAL PARTICLESNOTE: THRESHOLD IS 4000 FH AFTER THE LAST THSAOVERHAUL OR WITHIN 250 FH AFTER THE EFFECTIVEDATE OF THE AD WHICHEVER OCCURS LATER.ACCESS: 312AR* 0.01274211-0503-1 210 ACTUATOR - THS MEC OPC I: 2 C MRB ** AMM 274200/5012 0.50 ALLCONTROL VALVE JAMMING DETECTION TEST TO CHECKOPERATION OF JAMMING DETECTION CIRCUITSACCESS: 312AR* 0.01274211-0503-2 210 ACTUATOR - THS MEC OPC I: 1 C MRB AMM 274100/5011 0.25 ALLCHECK TRAVEL RANGE OF THS ACTUATOR IN ACCORDANCEWITH TRIM WHEEL POSITION POINTER AND INDEX ON FLIGHTCONTROL POSITION INDICATOR (WITH INDIVIDUAL HYDRAULICSYSTEM).SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)274211-0503-3 210 ACTUATOR - THS MEC OPC I: 1000 FH MRB ** AMM 274211/6012 0.30CNPOST 2684CONTROL VALVE JAMMING DETECTION CHECK TO DETECT 1981-085-036(B) (27-128)POSSIBLE HIDDEN JAMMED CONTROL VALVE FAA AD 85-09-05 P/N CHA723-20XXISB 27-0132ACCESS: 312AR* 0.01274211-0503-4 210 ACTUATOR - THS MEC OPC I: 550 FH MRB ** AMM 274211/6011 0.10 PRE 2684CN(27-128)CONTROL VALVE JAMMING DETECTION CHECK TO DETECT 1981-085-036(B) P/N CHA723-010POSSIBLE HIDDEN JAMMED CONTROL VALVE FAA AD 85-09-05 THRUISB 27-0132P/N CHA723-018274211-0504-1 310 ACTUATOR - THS MEC RAR I: 12500 FH MRB ** AMM 274211/4012 7.00 POST 02684(27-0128)REMOVE THS ACTUATOR FOR OVERHAULPOST 02787(27-0129)ACCESS: 312AR* 0.01274211-0504-2 310 ACTUATOR - THS MEC RAR I: 7500 FH MRB ** AMM 274211/4012 7.00 POST 02684CN(27-0128)REMOVE THS ACTUATOR FOR OVERHAUL 1981-085-036(B) PRE 02787FAA AD 85-09-05 (27-0129)ACCESS: 312AR* 0.01P/N CHA723-010THRUP/N CHA723-018P/N CHA723-20XX274211-0505-1 312 ACTUATOR - THS MEC RPL I: 5 A MRB AMM 121327/0011 0.50 ALLCHECK GEARBOX OIL LEVEL AS FOLLOWS:01. REMOVE OIL LEVEL AND FILLER PLUGS02. REPLENISH GEARBOX OIL AS NECESSARY UNTIL OILOVERFLOWS FROM THE LEVEL PLUG03. REPLACE PLUG SEALS,INSTALL PLUGS AND TIGHTEN TO* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)274211-0505-1 * * * * * C O N T I N U E * * * * *RECOMMENDED TORQUE VALUES04. SAFETY PLUGS WITH LOCKWIREACCESS: 312AR* 0.01274211-0505-2 312 ACTUATOR BALL NUT - THS MEC LUB I: 2 A MRB AMM 121327/0011 0.50 ALLLUBRICATE BALL NUT AND CHECK THS HYDROMECHANICALACTUATOR UNIT FOR FREEDOM OF OIL AND HYDRAULIC LEAKS.ACCESS: 312AR* 0.01274211-0505-3 312 ACTUATOR GEARBOX - THS MEC RPL I: 1 C MRB AMM 121327/0011 1.50 PRE 02787AMM 274211/601(27-0129)CHANGE OIL OF THS GEARBOX AS FOLLOWS:01. REMOVE OIL LEVEL AND FILLER PLUG02. REMOVE MAGNETIC DRAIN PLUG AND CHECK THE AMOUNTOF METAL PARTICLES AND DRAIN OIL03. INSTALL DRAIN PLUG WITH NEW O-RING04. FILL GEARBOX WITH OIL MIL-L-7808/G/2 (MAT.03-003)UNTIL OIL OVERFLOWS THE LEVEL PORT05. REINSTALL LEVEL AND FILLER PLUGS WITH NEWO-RINGS AND TIGHTEN TO RECOMMENDED TORQUE VALUES06. SAFETY PLUGS WITH LOCKWIREACCESS: 312AR* 0.01274211-0505-4 312 ACTUATOR GEARBOX - THS MEC RPL I: 2 C MRB AMM 121327/0011 1.50 POST 02787AMM 274211/601(27-0129)CHANGE OIL OF THS GEARBOX AS FOLLOWS:01. REMOVE OIL LEVEL AND FILLER PLUG02. REMOVE MAGNETIC DRAIN PLUG AND CHECK THE AMOUNTOF METAL PARTICLES AND DRAIN OIL03. INSTALL DRAIN PLUG WITH NEW O-RING04. FILL GEARBOX WITH OIL MIL-L-7808/G/2 (MAT.03-003)UNTIL OIL OVERFLOWS THE LEVEL PORT05. REINSTALL LEVEL AND FILLER PLUGS WITH NEWO-RINGS AND TIGHTEN TO RECOMMENDED TORQUE VALUES06. SAFETY PLUGS WITH LOCKWIRE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)274211-0505-4 * * * * * C O N T I N U E * * * * *ACCESS: 312AR* 0.01N 274211-0505-5 310 ACTUATOR THS MEC DET T: 2500 FH EASA AD EASA AD1 1.00 ALLA. EFFECT ISB 2010-0019DETAILED INSPECTION OF THSA UPPER ATTACHMENTS DATE OF ISB 27-0203AND BALL SCREW: THE AD01. CHECK FOR PRESENCE OF METALLIC PARTICLES. I: 2500 FH02. CHECK FOR CRACKS, SCRATCHES OR MATERIAL MISSING.ACCESS: 312AR* 0.01274300-0503-1 210 CONTROL SURFACES POS.INDIC. MEC OPC I: 1 A MRB AMM 274300/5011 0.10 FWD-FACEOPERATIONAL TEST OF VISUAL AND AURAL STAB.TRIMWARNINGS (STAB.TRIM OUT OF TAKE OFF RANGE)275100-0503-1 145 MECHANICAL CONTROL MEC FUC I: 3 C MRB AMM 275000/6011 0.50 ALLAMM 278000/601CHECK FOR CORRECT TENSION OF:- CABLE LOOP CONNECTING SLAT QUADRANT ASSY (FR.47)- CABLE FLAP QUADRANT ASSY (FR.54)WITH TENSIOMETER IN ACCORDANCE WITH AMM CABLE TENSIONADJUSTMENT GRAPH.ACCESS: 241AQ 241CZ* 0.38275121-0504-1 147 SHOCK ABSORBER FLAP MEC RAR I: 12000 FC MRB AMM 275121/4011 4.00 ALL148 CMM 2709011 4.00REMOVE FLAP SHOCK ABSORBER FOR WORKSHOP CHECK(COMPRISING OIL LEVEL CHECK AND FUNCTIONAL TEST).ACCESS: 147SZ* 0.02148SZ* 0.01275121-0505-1 147 SHOCK ABSORBER FLAP MEC RPL I: 3 C MRB AMM 121327/0011 0.50 ALL1481 0.50CHECK OIL LEVEL OF SHOCK ABSORBER:01. ALIGN OIL LEVEL OF SHOCK ABSORBER HORIZONTALLY* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275121-0505-1 * * * * * C O N T I N U E * * * * *02. REMOVE OIL LEVEL PLUG AND CHECK OIL LEVEL03. IF NECESSARY REMOVE VENT PLUG AND FILL SHOCK AB-SORBER WITH MATERIAL NO.03-006 (REFER TO AMM 20-31-00/13) UNTIL OIL OVERFLOWS THROUGH OIL LEVELPORT04. REPLACE SEALS,INSTALL PLUGS AND FULLY TIGHTEN OILLEVEL AND VENT PLUGACCESS: 147SZ* 0.02148SZ* 0.01275122-0505-1 147 TORQUE LIMITER FLAP MEC RPL I: 1 C MRB AMM 121327/0011 0.50 ALL1481 0.50CHECK TORQUE LIMITER FOR CORRECT OIL LEVEL ASFOLLOWS:01. REMOVE OIL LEVEL PLUG02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILLFLUID OVERFLOWS THROUGH OIL LEVEL PORT03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TORECOMMENDED VALUEACCESS: 147UZ* 0.02148UZ* 0.02275123-0504-1 577 TEE GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275123/4011 2.00 POST 01789677 SB 27-01011 2.00 (27-0084)REMOVE TEE GEARBOX FOR OVERHAUL OF HALO TYPEPRE 04494UNIVERSAL JOINT POSITION 4(27-0164)275123-0504-2 577 TEE GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275123/4011 2.00 PRE 01789677 SB 27-01011 2.00 (27-0084)REMOVE TEE-GEARBOX FOR OVERHAUL OF HOOKES-TYPEPRE 04494UNIVERSAL JOINT POSITION 4.(27-0164)275123-0505-1 500 GEARBOXES - FLAP MEC RPL I: 1 C MRB AMM 121327/0011 2.50 ALL6001 2.50CHECK FOR CORRECT OIL LEVEL* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275123-0505-1 * * * * * C O N T I N U E * * * * *- TEE FLAP GEARBOX- SIMPLEX BEVEL GEARBOX- DUPLEX BEVEL GEARBOX- SIGNAL UNIT AILERON DROOPAS FOLLOWS:01. REMOVE OIL LEVEL PLUG02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILLFLUID OVERFLOWS THROUGH OIL LEVEL PORT03. REPLACE PLUG SEAL.INSTALL PLUG AND TORQUETO RECOMMENDED VALUEACCESS: 575DB 577CT 577ET 577FT* 1.56675DB 677CT 677ET 677FT* 1.56275124-0504-1 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275124/4011 2.00 POST 01789148 SB 27-01011 2.00 (27-0084)REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FORPOST 04494OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 6(27-0164)275124-0504-2 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 8000 LG MRB AMM 275124/4011 2.00 POST 01789148 SB 27-01011 2.00 (27-0084)REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FORPRE 04494OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 6(27-0164)275124-0504-3 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275124/4011 2.00 PRE 01789148 SB 27-01011 2.00 (27-0084)REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FOR SB 27-0159POST 04494OVERHAUL OF HOOKE-TYPE UNIVERSAL JOINT POSITION 6(27-0164)275124-0504-4 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 8000 LG MRB AMM 275124/4011 2.00 PRE 01789148 CN1 2.00 (27-0084)REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FOR 1983-147-055(B) PRE 04494OVERHAUL OF HOOKE-TYPE UNIVERSAL JOINT POSITION 6 FAA AD 84-06-01 (27-0164)SB 27-0101SB 27-0159* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275124-0504-4 * * * * * C O N T I N U E * * * * *275125-0502-1 500 SCREWJACK 1 MEC CHK I: 6500 FC MRB ** AMM 275000/6011 2.00 POST 033246001 2.00 (27-0146)CHECK INTEGRITY OF PRIMARY AND SECONDARY LOADPATHS IN SCREWJACK,DUPLEX AND TEE GEARBOXES,SCREWJACKSHAFT AND SECONDARY TIE ROD.ACCESS: 577AB 577BB 577ET* 1.50677AB 677BB 677ET* 1.50275125-0504-1 500 SCREWJACK 1 MEC CHK I: 6500 FC MRB ** AMM 275000/6011 2.00 PRE 033246001 2.00 (27-0146)CHECK INTEGRITY OF PRIMARY LOAD PATHS AND SCREWJACKSHAFT. REMOVE DUPLEX GEARBOX AND CHECK INTEGRITYOF SECONDARY LOAD PATH IN TEE GEARBOX, DUPLEX SHAFTAND TIE ROD. MANUALLY CHECK PRIMARY AND SECONDARYDRIVES OF DUPLEX GEARBOX BEFORE REINSTALLATION.ACCESS: 577AB 577BB 577ET* 1.50677AB 677BB 677ET* 1.50275126-0502-1 500 SCREWJACK 2 TO 6 MEC CHK I: 6500 FC MRB ** AMM 275000/6011 1.50 ALL6001 1.50CHECK INTEGRITY OF PRIMARY AND SECONDARY LOADPATHS IN SREWJACK,DOWNDRIVE GEARBOX AND DUPLEX SHAFTAND SCREWJACK SECONDARY TIE RODACCESS: 572DB 572FB 572HB 572JB 581CB 581DB* 0.50581EB 581FB 581GB 581HB 581JB 581KB672DB 672FB 672HB 672JB 681CB 681DB* 0.50681EB 681FB 681GB 681HB 681JB 681KB275126-0502-2 500 SCREWJACK 1 TO 6 MEC CHK T: 10000 FC MRB AMM 275100/6011 1.80 ALL600 NOTE SIL 27-0761 1.80CHECK BACKLASH BETWEEN FLAP SCREWJACK BALL NUT AND I: 2500 FCSCREW OF SCREWJACKS 1 TO 6.* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275126-0502-2 * * * * * C O N T I N U E * * * * *NOTE: POSITION 1 10000 CYPOSITIONS 2 TO 6 12000 CY275126-0502-3 500 SCREW JACK 4,5 AND 6 MEC FUC I: ISB CN CN1 0.50 PRE 05240600 27-0172 FAA AD 1984-066-061(B) 1 0.50 (27-0173)CHECK BACKLASH OF FLAP SCREWJACK NO-BACK DEVICE NOTE CN 2001-184(B)FAA AD 87-21-03NOTE: DETAILS OF INSPECTION PROGRAM SEE LUCAS FAA AD 91-05-14SB 1058-27-608 0R AI.ISB 27-172. ISB 27-0172FOR SREWJACKS WITH BACKLASH LESS THAN0,331 MM (0,013 INCH) INSPECT EACH3600 LDGS275126-0502-4 500 SCREW JACK 4,5 AND 6 MEC FUC I: 12000 LG MPD AMM 275100/6011 0.50 POST 05240600 NOTE1 0.50 (27-0173)CHECK BACKLASH OF FLAP SCREWJACK NO-BACKDEVICENOTE: -INTERVAL OF 12000 LG TO BE CONFIRMED AFTERSAMPLING INSPECTION AT 6500 LG.-ONE A/C OF EACH OPERATOR ́S FLEET275126-0505-1 500 SCREWJACK 1 TO 6 MEC LUB I: 2 A MRB AMM 122227/0012 3.00 ALL600 SIL 27-0632 3.00LUBRICATION OF FOLLOWING ITEMS:01. BALL NUTS OF SCREW JACKS 1 TO 602. CARRIAGE ROLLERS OF FLAP TRACK 1 TO 603. RUBBING PADS (CARRIAGE SIDE LOCATION) TRACK NO.1ONLY(FLAPS EXTENDED)275126-0505-2 500 SCREWJACK 1 TO 6 MEC RPL I: 1 C MRB AMM 121327/0013 3.00 POST 10796600 SIL 27-0813 3.00CHECK FLAP SCREW-JACKS NO.1 TO 6 FOR CORRECTOIL LEVELNOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY OFTASK 283100-0502-1* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275126-0505-2 * * * * * C O N T I N U E * * * * *ACCESS: MOVABLE FLAP-TRACK FAIRINGS NO.1 TO 6,FIXED FAIRING NO.5275126-0505-3 500 SCREWJACK 1 TO 6 MEC RPL I: 5 A MRB AMM 121327/0013 3.00 PRE 10796600 SIL 27-0813 3.00 (27-0186)CHECK FLAP SCREWJACKS NO.1 TO 6 FOR CORRECTOIL LEVELACCESS: MOVABLE FLAP-TRACK FAIRINGS NO.1 TO 6,FIXED FAIRING NO.5275134-0505-1 500 GEARBOX - DOWNDRIVE,FLAP MEC RPL I: 1 C MRB AMM 121327/0011 3.00 ALL6001 3.00CHECK INNER/CENTER AND OUTER FLAP GEARBOX -DOWN DRIVES FOR CORRECT OIL LEVEL:01. EXTEND FLAPS AND LOCK FLAP CONTROL LEVER USINGTOOL P/N 98A2790102200002. REMOVE OIL LEVEL PLUG03. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILLFLUID OVERFLOWS THROUGH OIL LEVEL PLUG04. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TORECOMMENDED VALUE275136-0504-1 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4011 6.00 POST 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 5/6 ANDPOST 0449415/16 FOR OVERHAUL OF HALO-TYPES UNIVERSAL JOINT(27-0164)POSITION 5 AND 15275136-0504-2 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 8000 FC MRB AMM 275136/4011 6.00 POST 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 5/6 AND 15/16PRE 04494FOR OVERHAUL OF HALO-TYPES UNIVERSAL JOINT POSITION(27-0164)5 AND 15.275136-0504-3 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4011 6.00 PRE 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 5/6 AND SB 27-0159POST 04494* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275136-0504-3 * * * * * C O N T I N U E * * * * *15/16 FOR OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT(27-0164)5 AND 15275136-0504-4 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 8000 FC MRB AMM 275136/4011 6.00 PRE 01789600 CN1 6.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 5/6 AND 1983-147-055(B) PRE 0449415/16 FOR OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINTS FAA AD 84-06-01 (27-0164)5 AND 15 SB 27-0101SB 27-0159275136-0504-5 575 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4011 3.00 POST 01789675 SB 27-01011 3.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 13/14 FORPRE 04494OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 13(27-0164)275136-0504-6 575 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4011 3.00 PRE 01789675 SB 27-01011 3.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 13/14 FOR SB 27-0159PRE 04494OVERHAUL OF HOOKES TYPE UNIVERSAL JOINT POSITION 13(27-0164)275137-0504-1 581 COUPLING BOX - FLAP MEC RAR I: 16000 FC MRB AMM 275137/4011 3.00 POST 01789681 SB 27-01011 3.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HALO-TYPEPOST 04494UNIVERSAL JOINT POSITION 14(27-0164)ACCESS: 581AB* 0.29681AB* 0.29275137-0504-2 581 COUPLING BOX - FLAP MEC RAR I: 8000 FC MRB AMM 275137/4011 3.00 POST 01789681 SB 27-01011 3.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HALO TYPEPRE 04494UNIVERSAL JOINT POSITION 14(27-0164)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 20APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275137-0504-2 * * * * * C O N T I N U E * * * * *ACCESS: 581AB 581CB* 0.33681AB 681CB* 0.32275137-0504-3 581 COUPLING BOX MEC RAR I: 16000 FC MRB AMM 275137/4011 3.00 PRE 01789681 SB 27-01011 3.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPE SB 27-0159POST 04494UNIVERSAL JOINT POSITION 14.(27-0164)ACCESS: 581AB* 0.29681AB* 0.29275137-0504-4 581 COUPLING BOX MEC RAR I: 8000 FC MRB AMM 275137/4011 3.00 PRE 01789681 CN1 3.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPE 1983-147-055(B) PRE 04494UNIVERSAL JOINT POSITION 14. FAA AD 84-06-01 (27-0164)SB 27-0101ACCESS: 581AB SB 27-0159* 0.29681AB* 0.29275138-0502-1 571 BEARING-STEADY MEC DET I: 350 FH ISB ISB 27-00441 0.60 PRE 015016711 0.60 (57-0035)DETAILED INSPECTION OF FLAP TRANSMISSION NO.1PRE 01673BEARING AND SUPPORT BRACKETS FOR CRACKS.(57-0007)PRE 01798(27-0087)275138-0502-2 571 BEARING-STEADY MEC DET I: 2000 FH ISB ISB 27-00441 0.60 POST 015016711 0.60 (57-0035)DETAILED INSPECTION OF FLAP TRANSMISSION NO.1POST 01673BEARING AND SUPPORT BRACKETS FOR CRACKS.(57-0007)PRE 01798(27-0087)275153-0502-1 500 CARRIAGE-FLAP TRACK 1 TO 6 MEC DET I: 4 C MRB AMM 275100/6011 3.00 ALL600 AMM 275153/6011 3.00CHECK CARRIAGE FLAP TRACK NO.1 - 6:* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 21APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275153-0502-1 * * * * * C O N T I N U E * * * * *01. CHECK TRACKS AND ROLLERS FOR EVIDENCE OF WEARPARTICULARY AT SELECTED POSITIONS02. CHECK WEAR OF RUBBING PLATES (TRACK 1)03. DETAILED INSPECTION OF INNER FLAPHINGE FOR CONDITION AND SECURITY (TRACK 1)275154-0502-1 500 FRONT CARRIAGE - TRACK 2 MEC CHK I: 9000 FH MRB AMM 275100/6011 0.50 ALL6001 0.50CHECK CLEARANCE BETWEEN MAIN ROLLERS AND FLAPTRACK 2 AT SELECTED POSITION(LEAD A/C PER OPERATOR ONLY)275211-0503-1 147 CONTROL UNIT-FLAP ERI OPC I: 1 C MRB AMM 275400/5011 1.00 ALLCHECK JAMMING DETECTION ELECTRICAL CIRCUIT FORCORRECT OPERATIONACCESS: 147SZ 148SZ* 0.03275211-0504-1 147 CONTROL UNIT-FLAP ERI RAR I: 12000 FC MRB AMM 275211/4011 6.00 ALLREMOVE CONTROL UNIT FLAP FOR OVERHAULACCESS: 148SZ* 0.01275211-0505-1 147 CONTROL UNIT-FLAP ERI RPL I: 1 C MRB AMM 121327/0011 0.50 ALLCHECK CONTROL UNIT - FLAP FOR CORRECT OIL LEVEL:01. REMOVE OIL LEVEL FILLER PLUG02. FILL UP WITH OIL MIL-L-7808/G/2 TILL OIL OVER-FLOWS THROUGH OIL LEVEL PORT03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TORECOMMENDED VALUEACCESS: 148SZ* 0.01275400-0503-1 210 FLAP ASYMMETRY MEC OPC I: 1 A MRB ** AMM 275400/5011 0.10 ALL* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 22APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)275400-0503-1 * * * * * C O N T I N U E * * * * *OPERATIONAL TEST OF FLAP ASYMMETRY MONITORING CIRCUIT(INCL.SOLENOID OPERATION)275400-0503-2 210 FLAP-PRESSURE OFF BRAKE ERI OPC I: 1000 FH MRB ** AMM 275400/5011 0.50 ALLOPERATIONAL TEST OF PRESSURE-OFF BRAKE275421-0505-1 570 SCREWJACK NO.1 MEC LUB I: 5 A MPD AMM 122227/0011 0.20 POST 082386701 0.20 (57-0174)LUBRICATION OF INNER FLAP UPLOCK ROLLERNOTE: FLAPS TO BE EXTENDED275512-0502-1 147 FLAP INSTRUMENTATION UNIT ELO GVI I: 3 A MPD AMM 275512/6011 0.20 PRE 01871(24-0022)GENERAL VISUAL INSPECTION OF ELECTRICAL CONNECTORS ATFLAP INSTRUMENTATION UNIT FOR SATISFACTORY CONDITIONAND DETERIORATION BY FLUID.ACCESS: 148SZ* 0.01276100-0503-1 575 SPOILER & AIRBRAKE CABLES MEC FUC I: 3 C MRB AMM 276000/6011 0.50 ALL6751 0.50CHECK CONTROL CABLES OF SPOILER AND AIRBRAKESFOR CORRECT TENSION WITH TENSIOMETER IN ACCORDANCEWITH AMM CABLE TENSION ADJUSTMENT GRAPH.ACCESS: 575AB 575FB* 0.13675AB 675FB* 0.13276100-0503-2 210 ELECTRICAL & MECH.CONTROL ELO OPC I: WEEKLY MRB ** AMM 276100/5011 0.20 ALLOPERATIONAL TEST OF GROUND SPOILER ELECTRICAL CIRCUIT(ELECTRICAL AND MECHANICAL CONTROL AIRBRAKES ANDSPOILERS)SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 23APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)276114-0503-1 147 REGULATOR-CABLE TENSION MEC FUC I: 3 C MRB AMM 276000/5011 0.75 ALL01. CHECK (IN ACCORDANCE WITH THE RESPECTIVE AMMCABLE TENSION ADJUSTMENT GRAPH) SPEEDBRAKE ANDSPOILER CONTROL CABLES FOR CORRECT TENSIONNOTE: USE CABLE TENSIOMETER AND PLACE IT APPROX.ONE METER NEAR THE CABLE TENSION REGULATOR02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLETENSION REGULATOR IS WITHIN LIMITS03. CHECK REGULATOR FOR CLEANLINESS,WEAR,CORROSION,SECURITY OF ATTACHMENT AND INSTALLATIONACCESS: 147DZ 148DZ* 0.06276122-0503-1 581 DETENT-SPOILER & OUT.AIRBR. MEC FUC I: 6 C MRB AMM 276122/6011 3.00 ALL681 AMM 276129/6011 3.00CHECK DETENT SPRING CHARACTERISTICS AND ROLLER AMM 276132/601-CAM DISCONNECT FORCE (SPOILERS,INNER AND OUTERAIRBRAKES)ACCESS: 572CB 572GB 572LB 581EB 581FB 581GB* 0.41581HB 581JB672CB 672GB 672LB 681EB 681FB 681GB* 0.45681HB 681JB276161-0505-1 572 MICROSWITCH INNER SPEEDBR. INP LUB I: 1 C MPD AMM 122227/0011 0.25 ALL6721 0.25LUBRICATE CONTROL LINKAGE/MICROSWITCHES OFINNER SPEEDBRAKESACCESS: 572GB 572LB* 0.11672GB 672LB* 0.14278100-0503-1 210 SLAT RETRACTION INTERLOCK MEC OPC I: 1 A MRB ** AMM 278100/5011 0.10 ALLOPERATIONAL TEST OF SLAT RETRACTION INTERLOCK(MECHANICAL CONTROL)278112-0504-1 144 SHOCK ABSORBER SLAT MEC FUC I: 12000 FC MRB AMM 278112/4011 3.50 ALLCMM 270901CHECK SHOCK ABSORBER FOR CORRECT OIL LEVEL AND* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 24APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278112-0504-1 * * * * * C O N T I N U E * * * * *CARRY OUT FUNCTIONAL TEST.PREP.: REMOVE/INSTALL SHOCK ABSORBER, SLAT.ACCESS: 147GZ* 0.03278112-0505-1 144 SHOCK ABSORBER SLAT MEC RPL I: 3 C MRB AMM 121327/0011 0.50 ALLCHECK OIL LEVEL OF SHOCK ABSORBER:01. ALIGN OIL LEVEL OF SHOCK ABSORBER HORIZONTALLY02. REMOVE OIL LEVEL PLUG AND CHECK OIL LEVEL03. IF NECESSARY REMOVE VENT PLUG AND FILL SHOCK AB-SORBER WITH MATERIAL NO.03-006 (REFER TO AMM 20-31-00/13) UNTIL OIL OVERFLOWS THROUGH OIL LEVELPORT04. REPLACE SEALS,INSTALL PLUGS AND FULLY TIGHTEN OILLEVEL AND VENT PLUGACCESS: 147GZ* 0.03278113-0505-1 143 TEE GEARBOX-SLAT MEC RPL I: 1 C MRB AMM 121327/0011 1.00 ALLCHECK FOLLOWING ITEMS FOR CORRECT OIL LEVEL- TEE GEARBOX - SLAT- TORQUE LIMITER - SLAT (INCLUDING ZONE 144)01. REMOVE OIL LEVEL PLUG02.FILL UP WITH HYDR.FLUID MIL-H-5606/C/1 TILLFLUID OVERFLOWS THROUGH OIL LEVEL PORT03. REPLACE PLUG SEAL,INSTALL PLUG AND TORQUETO RECOMMENDED VALUEACCESS: 147GZ* 0.03278115-0505-1 512 GEARBOX BEVEL - SLAT MEC RPL I: 1 C MPD AMM 121327/0011 0.33 NON-KRUG.FLAP6121 0.33CHECK FOR CORRECT OIL LEVEL:01. REMOVE OIL LEVEL PLUG02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILLFLUID OVERFLOWS THROUGH OIL LEVEL PORT03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TO* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 25APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278115-0505-1 * * * * * C O N T I N U E * * * * *RECOMMENDED VALUEACCESS: 512BB* 0.23612BB* 0.23278116-0505-1 512 GEARBOX STEPBACK - SLAT MEC RPL I: 1 C MRB AMM 121327/0011 0.50 KRUEGER FLAP6121 0.50CHECK GEARBOX FOR CORRECT OIL LEVEL:01. REMOVE THE TWO OIL LEVEL/FILLER PLUGS (ONE PLUGFOR EACH GEARBOX)02. FILL UP WITH MATERIAL NO.02-001 TILL FLUID OVER-FLOWS THROUGH OIL LEVEL/FILLER PORT03. REPLACE PLUG SEALS, INSTALL PLUGS AND TIGHTEN TORECOMMENDED TORQUE VALUESACCESS: 512JB 512KB* 0.23612JB 612KB* 0.23278117-0504-1 523 STEADY BEARING - SLAT MEC RAR I: 12000 FC MRB AMM 278117/4011 6.00 POST 01789623 SB 27-01011 6.00 (27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HALO-TYPE SB 27-0158POST 04494UNIVERSAL JOINTS POSITION 20 AND 21.(27-0164)ACCESS: 512KB 512LB 523AB 523BB* 0.43612KB 612LB 623AB 623BB* 0.43278117-0504-2 523 STEADY BEARING - SLAT MEC RAR I: 3500 FC MRB AMM 278117/4011 6.00 POST 01789623 CN1 6.00 (27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HAL0-TYPE 1983-148-056(B) PRE 04494UNIVERSAL JOINT POSITION 20 AND 21. FAA AD 84-06-01 (27-0164)SB 27-0101ACCESS: 512KB 512LB 523AB 523BB SB 27-0158* 0.43612KB 612LB 623AB 623BB* 0.43278117-0504-3 523 STEADY BEARING - SLAT MEC RAR I: 12000 FC MRB AMM 278117/4011 6.00 PRE 01789623 SB 27-01011 6.00 (27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HOOKES-TYPEPOST 04494* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 26APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278117-0504-3 * * * * * C O N T I N U E * * * * *UNIVERSAL JOINTS POSITION 20 AND 21.(27-0164)ACCESS: 512KB 512LB 523AB 523BB* 0.43612KB 612LB 623AB 623BB* 0.43278117-0504-4 523 STEADY BEARING - SLAT MEC RAR I: 8000 FC MRB AMM 278117/4011 6.00 PRE 01789623 SB 27-01011 6.00 (27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HOOKESPRE 04494TYPE UNIVERSAL JOINTS POSITION 20 AND 21(27-0164)ACCESS: 512KB 512LB 523AB 523BB* 0.43612KB 612LB 623AB 623BB* 0.43278118-0504-1 512 COUPLING BOX - SLAT MEC RAR I: 16000 FC MRB AMM 278118/4011 2.00 POST 01789612 SB 27-01011 2.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HALO-TYPE SB 27-0158POST 04494UNIVERSAL JOINT POSITION 8(27-0164)ACCESS: 147GZ 512BB* 0.27148GZ 612BB* 0.27278118-0504-2 512 COUPLING BOX - SLAT MEC RAR I: 5000 FC MRB AMM 278118/4011 2.00 POST 01789612 CN1 2.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HALO-TYPE 1983-148-056(B) PRE 04494UNIVERSAL JOINT POSITION 8. FAA AD 84-06-01 (27-0164)SB 27-0101ACCESS: 147GZ 512BB SB 27-0158* 0.27148GZ 612BB* 0.27278118-0504-3 512 COUPLING BOX - SLAT MEC RAR I: 16000 FC MRB AMM 278118/4001 2.00 PRE 01789612 SB 27-01011 2.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPEPOST 04494UNIVERSAL JOINT POSITION 8.(27-0164)ACCESS: 147GZ 512BB* 0.27148GZ 612BB* 0.27SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 27APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278118-0504-4 512 COUPLING BOX - SLAT MEC RAR I: 8000 FC MRB AMM 278118/4011 2.00 PRE 01789612 CN1 2.00 (27-0084)REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPE 1983-148-056(B) PRE 04494UNIVERSAL JOINT POSITION 8. FAA AD 84-06-01 (27-0164)SB 27-0101ACCESS: 147GZ 512BB* 0.27148GZ 612BB* 0.27278119-0504-1 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 12000 FC MRB AMM 278119/4011 3.00 POST 01789600 SB 27-01011 3.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 9/10 FOR SB 27-0158POST 04494OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 9(27-0164)KRUG.FLAPACCESS: 512AB 512BB* 0.42612AB 612BB* 0.42278119-0504-2 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 3500 FC MRB AMM 278119/4011 3.00 POST 01789600 CN1 3.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 9/10 FOR 1983-148-056(B) PRE 04494OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 9 FAA AD 84-06-01 (27-0164)SB 27-0101KRUG.FLAPACCESS: 512AB 512BB SB 27-0158* 0.42612AB 612BB* 0.42278119-0504-3 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 12000 FC MRB AMM 278119/4011 3.00 PRE 01789600 SB 27-01011 3.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 9/10 FORPOST 04494OVERHAUL OF HOOKES TYPE UNIVERSAL JOINT POSITION 9(27-0164)KRUG.FLAPACCESS: 512AB 512BB* 0.42612AB 612BB* 0.42278119-0504-4 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4011 3.00 PRE 01789600 CN1 3.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 9/10 FOR 1983-148-056(B) PRE 04494OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 9 FAA AD 84-06-01 (27-0164)SB 27-0101ACCESS: 512AB 512BB* 0.42* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 28APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278119-0504-4 * * * * * C O N T I N U E * * * * *612AB 612BB* 0.42278119-0504-5 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4011 6.00 POST 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFTS POSITION 9/10 AND SB 27-0158POST 0449421/22 FOR OVERHAUL OF HALO-TYPE UNIVERSAL JOINTS(27-0164)POSITIONS 9 AND 22NON-KRUG.FLAPACCESS: 523CB 523EB* 0.32623CB 623EB* 0.32278119-0504-6 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4011 6.00 POST 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFTS POSITION 9/10 AND SB 27-0158PRE 0449421/22 FOR OVERHAUL OF HALO-TYPE UNIVERSAL JOINTS(27-0164)POSITIONS 9 AND 22NON-KRUG.FLAPACCESS: 523CB 523EB* 0.32623CB 623EB* 0.32278119-0504-7 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4011 6.00 PRE 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFTS POSITION 21/22 FORPOST 04494OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 22.(27-0164)NON-KRUG.FLAPACCESS: 523CB 523EB* 0.32623CB 623EB* 0.32278119-0504-8 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4011 6.00 PRE 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFTS POSITION 21/22 FORPRE 04494OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 22.(27-0164)ACCESS: 523CB 523EB* 0.32623CB 623EB* 0.32SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 29APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278120-0504-1 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4011 6.00 POST 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 11/12 AND SB 27-0158POST 0449421/22 FOR OVERHAUL OF HALO TYPE UNIVERSAL JOINTS(27-0164)POSITION 12 AND 22KRUG.FLAPACCESS: 523CB 523EB* 0.32623CB 623EB* 0.32278120-0504-2 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4011 6.00 POST 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFT POSITION 11/12 AND SB 27-0158PRE 0449421/22 FOR OVERHAUL OF HALO TYPE UNIVERSAL JOINTS(27-0164)POSITION 12 AND 22KRUG.FLAPACCESS: 523CB 523EB* 0.32623CB 623EB* 0.32278120-0504-3 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4011 6.00 PRE 01789600 SB 27-01011 6.00 (27-0084)REMOVE TRANSMISSION SHAFTS POSITION 11/12 FORPOST 04494OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 12.(27-0164)KRUG.FLAPACCESS: 512BB 523CB 523EB* 0.55612BB 623CB 623EB* 0.55278120-0504-4 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4011 6.00 PRE 01789600 CN 1983-148-056 1 6.00 (27-0084)REMOVE TRANSMISSION SHAFTS POSITION 11/12 FOR FAA AD 84-06-01 PRE 04494OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 12. SB 27-0101(27-0164)KRUG.FLAPACCESS: 512BB 523CB 523EB* 0.55612BB 623CB 623EB* 0.55278121-0504-1 143 STEADY BEARING - SLAT MEC RAR I: 16000 FC MRB AMM 278121/4011 2.00 POST 01789SB 27-0101(27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HAL0-TYPE SB 27-0158POST 04494UNIVERSAL JOINT POSITION 2.(27-0164)ACCESS: 147GZ 148GZ* 0.06SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 30APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278121-0504-2 143 STEADY BEARING - SLAT MEC RAR I: 8000 FC MRB AMM 278121/4011 2.00 POST 01789SB 27-0101(27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HAL0-TYPE SB 27-0158PRE 04494UNIVERSAL JOINT POSITION 2.(27-0164)ACCESS: 147GZ 148GZ* 0.06278121-0504-3 143 STEADY BEARING - SLAT MEC RAR I: 16000 FC MRB AMM 278121/4011 2.00 PRE 01789SB 27-0101(27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HOOKES-TYPEPOST 04494UNIVERSAL JOINT POSITION 2.(27-0164)ACCESS: 147GZ 148GZ* 0.06278121-0504-4 143 STEADY BEARING - SLAT MEC RAR I: 8000 FC MRB AMM 278121/4011 2.00 PRE 01789SB 27-0101(27-0084)REMOVE STEADY BEARING FOR OVERHAUL OF HOOKES-TYPEPRE 04494UNIVERSAL JOINT POSITION 2.(27-0164)ACCESS: 147GZ 148GZ* 0.06278124-0502-1 500 SCREW JACKS - SLAT MEC DET T: 12000 FC MRB AMM 278100/6011 10.50 ALL600 I: 2500 FC1 10.50CHECK PLAY OF JACK SCREW (BALL IN SCREW NUT)AND PERFORM DETAILED INSPECTION OF MOUNTINGTRUNNIONS FOR CONDITION AND SECURITY,JACK 1 TO 6278124-0505-1 500 SCREW JACKS - SLAT MEC RPL I: 1 C MPD AMM 121327/0011 3.00 POST 02628600 SIL 27-0811 3.00 (27-0136)CHECK SLAT SCREW JACK 1 TO 6 FOR CORRECT OIL LEVEL:ACCESS: 512CB 512GB 523DB 523KB 524DB 524JB* 0.38612CB 612GB 623DB 623KB 624DB 624JB* 0.40278124-0505-2 500 SCREW JACKS - SLAT MEC LUB I: 3 A MRB AMM 122227/0011 2.00 ALL6001 2.00LUBRICATION OF SLAT SCREWJACKS BALL NUTS (SCREWJACKNO.1 TO 6)ACCESS: 512CB 512GB 523DB 523KB 524DB 524JB* 0.38* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 31APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278124-0505-2 * * * * * C O N T I N U E * * * * *612CB 612GB 623DB 623KB 624DB 624JB* 0.40278124-0505-3 500 SCREW JACKS - SLAT MEC RPL I: 5 A MPD AMM 121327/0011 0.50 PRE 02628600 SIL 27-0811 0.50 (27-0136)CHECK SLAT SCREW JACK 1 TO 6 FOR CORRECT OILLEVEL.ACCESS: 512CB 512GB 523DB 523KB 524DB 524JB* 0.38612CB 612GB 623DB 623KB 624DB 624JB* 0.40278141-0502-1 500 SEALING SHUTTERS-SLAT TRACK MEC DET I: 1 C MPD SIL 27-0771 0.30 PRE 076026001 0.30 (57-0160)DETAILED INSPECTION AT TRACK POSITIONS 4 TO11, OF SHUTTER MECHANISM CAM BLOCKS AND VISIBLELENGTH OF FORWARD AND AFT DRESSING ANGLES FOR WEARAND/OR DAMAGE278147-0504-1 524 FRICTION BRAKE - SLAT MEC RAR I: 12000 FC MRB AMM 278147/4011 2.00 ALL6241 2.00REMOVE SLAT FRICTION BRAKE FOR OVERHAULACCESS: 524KB* 0.22624KB* 0.22278147-0505-1 524 FRICTION BRAKE - SLAT MEC RPL I: 1 C MRB AMM 121327/0011 0.50 ALL6241 0.50CHECK OIL LEVEL OF SLAT FRICTION BRAKE:01. REMOVE FILLER PLUG02. FILL UP WITH MATERIAL NO.03-004(REFER TO MM 20-31-00/12)TILL OIL OVERFLOWS03. DRAW OFF 25 C.C. OF MATERIAL NO.03-004 IN ORDERTO MAINTAIN A VOLUME OF AIR EQUAL TO 25 C.C. INTHE FRICTION BRAKE04. REPLACE PLUG SEAL,INSTALL PLUG AND TORQUE TORECOMMENDED VALUEACCESS: 524KB* 0.22624KB* 0.22SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 32APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278149-0504-1 513 MOVABLE VANE - KRUEGER FLAP MEC RAR I: 8 C MPD AMM 278149/4011 1.20 KRUEGER FLAP613 SIL SIL 27-1121 1.20REMOVE KRUEGER FLAP SPRING ROD FOR OVERHAUL.ACCESS: 513AT* 0.14613AT* 0.06278149-0505-1 513 MOVABLE VANE - KRUEGER FLAP MEC LUB I: 1 C MPD SIL 27-0201 0.50 PRE 02701613 SIL1 0.50 (27-0126)CLEAN AND LUBRICATE PISTON OF SPRING ROD (ATTACHED TOKRUG.FLAPMOVABLE VANE) AND CHECK OVERLAP AND CONDITION OFKRUEGER FLAP (FLAT)SEAL.PREP.: EXTEND KRUEGER FLAP TO HALF EXTENDED POSITION.278153-0504-1 512 STEPBACK GEARBOX - SLAT MEC RAR I: 12000 FC MRB AMM 278153/4011 3.00 POST 01789612 SB 27-01011 3.00 (27-0084)REMOVE STEPBACK GEARBOX FOR OVERHAUL OF SB 27-0158POST 04494HALO-TYPE UNIVERSAL JOINT POSITION 10(27-0164)KRUG.FLAPACCESS: 512BB* 0.23612BB* 0.23278153-0504-2 512 STEPBACK GEARBOX - SLAT MEC RAR I: 3500 FC MRB AMM 278153/4011 3.00 POST 01789612 CN1 3.00 (27-0084)REMOVE STEPBACK GEARBOX FOR OVERHAUL OF 1983-148-056(B) PRE 04494HALO-TYPE UNIVERSAL JOINT POSITION 10 FAA AD 84-06-01 (27-0164)SB 27-0101KRUG.FLAPACCESS: 512BB SB 27-0158* 0.23612BB* 0.23278153-0504-3 512 STEPBACK GEARBOX - SLAT MEC RAR I: 12000 FC MRB AMM 278153/4011 3.00 PRE 01789612 SB 27-01011 3.00 (27-0084)REMOVE STEPBACK GEARBOX FOR OVERHAUL OFPOST 04494HOOKES-TYPE UNIVERSAL JOINT POSITION 10(27-0164)KRUG.FLAPACCESS: 512BB* 0.23612BB* 0.23SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 33APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278153-0504-4 512 STEPBACK GEARBOX - SLAT MEC RAR I: 8000 FC MRB AMM 278153/4011 3.00 PRE 01789612 CN1 3.00 (27-0084)REMOVE STEPBACK GEARBOX FOR OVERHAUL OF 1983-148-056(B) PRE 04494HOOKES-TYPE UNIVERSAL JOINTS POSITION 10 AND 11 FAA AD 84-06-01 (27-0164)SB 27-0101KRUG.FLAPACCESS: 512BB* 0.23612BB* 0.23278153-0504-5 512 STEPBACK GEARBOX - SLAT MEC RAR I: 16000 FC MRB AMM 278153/4011 3.00 POST 01789612 SB 27-01011 3.00 (27-0084)REMOVE STEPBACK GEARBOX FOR OVERHAUL OF SB 27-0158POST 04494HALO-TYPE UNIVERSAL JOINT POSITION 11(27-0164)KRUG.FLAPACCESS: 512BB* 0.23612BB* 0.23278153-0504-6 512 STEPBACK GEARBOX - SLAT MEC RAR I: 8000 FC MRB AMM 278153/4011 3.00 POST 01789612 SB 27-01011 3.00 (27-0084)REMOVE STEPBACK GEARBOX FOR OVERHAUL OF SB 27-0158PRE 04494HALO-TYPE UNIVERSAL JOINT POSITION 11(27-0164)KRUG.FLAPACCESS: 512BB* 0.23612BB* 0.23278153-0504-7 512 STEPBACK GEARBOX - SLAT MEC RAR I: 16000 FC MRB AMM 278153/4011 3.00 PRE 01789612 CN1 3.00 (27-0084)REMOVE STEPBACK GEARBOX FOR OVERHAUL OF 1983-148-056(B) POST 04494HOOKES-TYPE UNIVERSAL JOINT POSITITION 11 FAA AD 84-06-01 (27-0164)SB 27-0101KRUG.FLAPACCESS: 512BB* 0.23612BB* 0.23278153-0505-1 512 STEPBACK GEARBOX - SLAT MEC RPL I: 1 C MPD AMM 121327/0011 0.50 KRUEGER FLAP6121 0.50CHECK FOR CORRECT OIL LEVEL:01. REMOVE OIL LEVEL PLUG02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILLFLUID OVERFLOWS THROUGH OIL LEVEL PORT03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TO* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 34APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278153-0505-1 * * * * * C O N T I N U E * * * * *RECOMMENDED VALUEACCESS: 512BB* 0.23612BB* 0.23278211-0503-1 147 CONTROL UNIT-SLAT ERI OPC I: 1 C MRB AMM 278300/5011 0.25 ALLCHECK JAMMING DETECTION ELECTRICAL CIRCUIT FORCORRECT OPERATION278211-0504-1 147 CONTROL UNIT-SLAT MEC RAR I: 12000 FC MRB AMM 278211/4011 6.00 ALLREMOVE CONTROL UNIT-SLAT FOR OVERHAULACCESS: 147CZ* 0.01278211-0505-1 147 CONTROL UNIT-SLAT MEC RPL I: 1 C MRB AMM 121327/0011 0.50 ALLCHECK CONTROL UNIT, SLAT FOR CORRECT OIL LEVEL:01. REMOVE OIL LEVEL FILLER PLUG02. FILL UP WITH OIL MIL-L-7808/G/2 TILL OIL OVER-FLOWS THROUGH OIL LEVEL PORT03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TORECOMMENDED VALUEACCESS: 147CZ* 0.01278300-0503-1 210 SLAT ASYMMETRY MEC OPC I: 1 A MRB ** AMM 278300/5011 0.20 ALLOPERATIONAL TEST OF SLAT ASYMMETRY MONITORING CIRCUIT278300-0503-2 210 SLAT - PRESSURE OFF BRAKE MEC OPC I: 1000 FH MRB ** AMM 278300/5011 0.50 ALLOPERATIONAL TEST OF PRESSURE-OFF BRAKESYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 35APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)278415-0503-1 210 IND.UNIT-KRUEGER&SLOT FLAP ELO OPC I: 1 C MRB ** AMM 278400/5011 0.10 KRUEGER FLAPOPERATIONAL TEST (BITE TEST) OF THE KRUEGER AND SLOTFLAP INDICATING UNIT* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION:2-27 PAGE 36APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)281100-0502-1 500 FUEL TANKS MEC GVI I: DY-TERM MRB AMM 121128/0011 0.20 ALL6001 0.20CHECK THAT DIPSTICKS ARE RETRACTED AND IN SECUREDPOSITION (LH AND RH WING) AND NO LEAKS ARE PRESENT281100-0502-2 500 FUEL TANKS MEC GVI I: 1 A MRB AMM 281100/6011 0.30 ALL6001 0.30CHECK FUEL TANK AREAS FOR FUEL LEAKS ESPECIALLYIN AREAS OF PYLON ATTACHMENT AND INBOARD OF RIB 1.281100-0503-1 140 FUEL TANKS MEC DET I: NOTE 5-2 MPD AMM 123228/0011 0.25 B4500 SIL SIL 28-0791 0.25 C4600 SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATION1 0.25 F4ANALYSIS281100-0503-2 500 FUEL TANKS MEC DET I: NOTE 5-2 MPD AMM 123228/0011 0.25 B2600 SIL SIL 28-0791 0.25SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATIONANALYSIS281100-0503-3 140 CENTER TANK MEC DRN I: WEEKLY MPD AMM 123228/0011 0.50 B4SIL SIL 28-079C4WATER DRAIN CHECKF4CENTER TANKNON-USAGE281100-0505-1 500 FUEL TANKS MEC CHK I: DY-TERM MPD AMM 123228/0011 0.20 ALL600 OR SIL SIL 28-0791 0.20CHECK WATER CONTENT OF ALL FUEL TANKS AT DRAIN NOTE 5-2VALVESNOTE: INTERVAL MAY BE INCREASED DEPENDINGON INDIVIDUAL OPERATORS OPERATINGINVIRONMENT281115-0503-1 500 VALVES-FLAP MEC OPC I: 4 YE MRB AMM 281115/4011 0.75 ALL6001 0.75VISUAL INSPECTION AND MANUAL OPERATION TO REVEAL ANYTENDENCY OF THE VALVE TO STICK AS FOLLOWS:* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)281115-0503-1 * * * * * C O N T I N U E * * * * *01. GAIN ACCESS TO VALVE THROUGH RELEVANT MANHOLES02. CHECK THAT FLAP VALVE WILL CLOSE WITH LIGHT PUSH03. CHECK FLAP VALVE FOR FREEDOM OF MOVEMENT OVERCOMPLETE RANGEACCESS: 541AB 542CB 550BB* 4.50641AB 642CB 650BB* 4.50281300-0503-1 140 WING CENT.BOX/TANK VENT.SYS MEC OPC I: 4 C MRB ** AMM 251300/5011 0.75 B2AMM 281312/601PRE 0269501. VISUAL INSPECTION OF WING CENTER BOX VENTILATION(28-0043)SYSTEM AIR INLET AND OUTLET SCREENS FOR CLEAN-INLESS02. OPERATIONAL TEST OF CHECK VALVEACCESS: 148AZ 148GZ 241ZF* 0.41281300-0503-2 140 WING CENT.BOX/TANK VENT.SYS MEC OPC I: 4 C MRB ** AMM 281312/6011 0.50 B4C401. INSPECT CENTER TANK VENTILATION SYSTEM AIR INLETF4SCREEN FOR CLEANLINESSPRE 0269502. PERFORM OPERATIONAL TEST OF CHECK VALVE(28-0043)ACCESS: 241ZF* 0.15281300-0503-3 140 WING CENT.BOX/TANK VENT SYS MEC OPC I: 4 C MRB ** AMM 281312/6011 0.50 POST 02695(28-0043)OPERATIONAL TEST OF CHECK VALVEACCESS: 241ZF* 0.15281800-0502-1 143 IGNITION PREVENTION MEC FUC I: 6 YE EUAD AMM 281800/5011 0.20 B4 C4 F4144 EUAD 2007-00941 0.20145 FUNCTIONAL CHECK OF CENTER TANK VAPOUR SEAL FAL 95A.1928/05 1 0.201461 0.20ACCESS: 147FZ 147GZ 147HZ* 0.09148GZ 148HZ* 0.05241AAF 241ABF 241ZF* 0.15* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)281800-0502-1 * * * * * C O N T I N U E * * * * *242VF 242WF* 0.28281800-0502-2 541 IGNITION PREVENTION MEC DET I: 12 YE MRB 9 AMM 281800/6011 0.20 B25421 0.20543 DETAILED INSPECTION OF THE WING TANK BONDING LEADS.1 0.205501 0.205601 0.206411 0.206421 0.206431 0.206501 0.206601 0.20R 281800-0502-3 141 IGNITION PREVENTION MEC DET I: 12 YE FAL AMM 281800/6011 0.20 B41421 0.20 C4541 DETAILED VISUAL INSPECTON OF WING AND CENTER TANK1 0.20 F4542 BONDING LEADS.1 0.205431 0.205501 0.205601 0.206411 0.206421 0.206431 0.206501 0.206601 0.20281800-0502-4 541 IGNITION PREVENTION MEC GVI I: 12 YE MRB 9 AMM 281800/6011 0.20 B25421 0.20543 GENERAL VISUAL INSPECTION OF INTERNAL WING TANK1 0.20550 WIRING AND PROBE ATTACHMENTS.1 0.205601 0.206411 0.206421 0.206431 0.206501 0.206601 0.20R 281800-0502-5 141 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6011 0.20 B41421 0.20 C4* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)281800-0502-5 * * * * * C O N T I N U E * * * * *541 GENERAL VISUAL INSPECTION OF INTERNAL WING AND1 0.20 F4542 CENTER TANK WIRING AND PROBE ATTACHMENTS.1 0.205431 0.205501 0.205601 0.206411 0.206421 0.206431 0.206501 0.206601 0.20R 281800-0502-6 130 IGNITION PREVENTION MEC GVI I: 6 YE FAL AMM 281800/6011 0.20 B4C4GENERAL VISUAL INSPECTION OF CENTER TANK FORWARDF4CARGO BAY INSULATION MATS.R 281800-0502-7 145 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6011 0.20 B41461 0.20 C4GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVEF4CENTER TANK.R 281800-0502-8 512 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6011 0.20 ALL5231 0.20524 GENERAL VISUAL INSPECTION OF WING LEADING - AND1 0.20572 TRAILING EDGE ELECTRICAL WIRING CONNECTIONS.1 0.205751 0.205811 0.205911 0.206121 0.206231 0.206241 0.206721 0.206751 0.206811 0.206911 0.20R 281800-0502-9 500 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6011 0.20 ALL6001 0.20GENERAL VISUAL INSPECTION OF WING FUEL PUMP* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)281800-0502-9 * * * * * C O N T I N U E * * * * *ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICALSUPPLY CABLE.281800-0503-1 143 IGNITION PREVENTION MEC FUC I: 6 YE EUAD AMM 281800/6011 0.30 B4 C4 F4144 EUAD 2007-00941 0.30147 DETAILED INSPECTION OF CENTER TANK VAPOUR SEAL. FAL 95A.1928/05 1 0.301481 0.30ACCESS: 147FZ 147GZ 147MZ* 0.13148GZ 148HZ* 0.05734* 0.10744* 0.10281800-0503-2 141 IGNITION PREVENTION MEC OPC I: NOTE EUAD AMM 281800/5011 0.30 ALL142 EUAD 2007-00941 0.30540 OPERATIONAL CHECK OF FUEL QUANTITY INDICATING AND FAL 95A.1928/05 1 0.30550 LEVEL SENSING FOR ELECTRICAL CONTINUITY.1 0.306401 0.30650 NOTE: TO BE CARRIED OUT IN ACCORDANCE WITH THE AD.1 0.30ACCESS: TANK ACCESS PANELSR 281801-0502-1 140 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6011 0.20 ALL5001 0.20600 GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS.1 0.20282100-0503-1 141 FUEL-CENTER TANK INSPECTION OF FUEL NDT SDI T: 19600 FC CN CN F-2005-1991 1.00 B4142 PUMPS AND PUMP CANISTERS I: 3000 FC FAA AD FAA AD1 1.00 C4ISB 2006-12-05F4REMOVE CENTRE FUEL TANK BOOSTER PUMPS FOR: . ISB 28-0084PRE 1304101. DETAILED INSPECTION.(28-0085)02. SPECIAL DETAILED INSPECTION OF THE BOOSTER PUMPCANISTERS.PREP.: INNER TANKS AND CENTER TANK TO BE DEFUELEDACCESS: 147AZ 147HZ 734* 0.34148AZ 148HZ 744* 0.34SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)282112-0503-1 500 PUMP BOOSTER ENG OPC I: ENG. CHG MRB AMM 710000/5011 0.40 ALL6001 0.40OPERATE ENGINE ON SUCTION FEED AND MONITORENGINE FUEL PRESSURE INDICATOR.(WITHOUT BOOSTERPUMPS)282116-0503-1 210 VALVES-ISOLATION (SHUT OFF) MEC OPC I: 1 C MRB ** AMM 282117/4012 0.25 B2OPERATIONAL TEST OF INBOARD,OUTBOARD TANK ISOLATIONSHUT-OFF VALVE AND ACTUATORS USING KNOB INDICATORLIGHTS TO VERIFY VALVE POSITIONACCESS: 575BB 675BB* 0.12282116-0503-2 210 VALVES-ISOLATION (SHUT OFF) MEC OPC I: 1 C MRB ** AMM 282117/4011 0.25 B4C4OPERATIONAL TEST OF INBOARD,OUTBOARD AND CENTER TANKF4ISOLATION SHUT OFF VALVES AND ACTUATORS USING KNOBINDICATOR LIGHTS TO VERIFY VALVE POSITIONACCESS: 575BB 675BB* 0.12282116-0503-3 210 VALVES - ISOLATION (S/O) MEC DET I: 500 FH CN AMM 282100/4011 0.20 PRE 04845FAA AD CN(28-0055)OPERATIONAL TEST OF ISOLATION VALVE AND CROSS-FEED 1991-173-126(B) PRE 08964VALVE CONTROL UNIT. FAA AD 97-07-09 (28-0061)282118-0503-1 500 LOW PRESSURE FUEL FIRE SHUT OFF VALVE MEC OPC I: ENG. CHG MRB ** AMM 282118/5012 0.25 ALL6002 0.25CHECK FOR LEAKAGE:01. BEFORE RECONNECTION OF FUEL LINE MAKE CERTAINTHAT LP FIRE SHUT OFF VALVES ARE CLOSED (BY USINGFIRE CONTROL HANDLE)02. START UP BOOSTER FUEL PUMPS (TANK 1 AND 2)03. LEAVE THE SYSTEM PRESSURIZATED FOR SEVERALMINUTES04. MAKE CERTAIN THAT THERE IS NO FUEL FLOW FROM ENDOF ENGINE PYLON FUEL LINE05. SHUT DOWN FUEL PUMPSSYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)282124-0503-1 550 JET PUMP-OUTBOARD TANKS MEC FUC I: 4 C MRB ** AMM 282124/5012 0.50 ALL6502 0.50FUNCTIONAL TEST OF JET PUMP OUTBOARD TANKS282125-0503-1 210 VALVE CROSSFEED ELO OPC I: 4000 FH MRB ** AMM 282100/5011 0.20 ALLOPERATIONAL TEST OF VALVE AND ACTUATOR CROSSFEED WITHEACH ACTUATOR INCLUSIVE POSITION INDICATORACCESS: 147DZ* 0.03282200-0503-1 144 VALVE - OVERFLOW MEC OPC I: DY-TERM MRB AMM 282200/0011 0.10 B4C4OPERATIONAL TEST OF OVERFLOW VALVE AT REFUELINGF4PANEL:- MANUALLY OPERATE THE HANDLE AND CHECK FOR FREEMOVEMENTACCESS: 144ER* 0.01282214-0502-1 523 COUPLING REFUEL/DEFUEL MEC GVI I: 6 C MRB AMM 282214/6011 0.30 ALL6231 0.30INSPECT REFUEL/DEFUEL COUPLING FOR EVIDENCE OFDEMAGE AND WEAR,CAP-ROLLERS FOR FREEDOM,CABLE ANDCHAIN FOR CHAFING.ENSURE SEAL SUPPORT PLATE CAN BEDEPRESSED AND RETURNED BY SPRINGACCESS: 523HB* 0.17623HB* 0.17282400-0502-1 310 APU FUEL DUCT DRAIN MAST MEC GVI I: 1 A MRB AMM 282400/6011 0.50 ALLCHECK APU FUEL DUCT DRAIN MAST HOLES (AT FRAME54) FOR OBSTRUCTION AND FOR FUEL LEAKAGE WITH TANK 1BOOSTER PUMP OPERATING282414-0502-1 313 VALVE-LP FUEL FIRE SHUT OFF ENG GVI I: 1 C MRB ** AMM 282400/5012 1.00 ALLINSPECT APU DRAIN VALVE,APU DIFFERENTIAL PRESSURE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)282414-0502-1 * * * * * C O N T I N U E * * * * *SWITCH AND APU FUEL FIRE SHUT OFF VALVE FORSATISFACTORY CONDITION AND EXTERNAL FUEL LEAKAGE,WITH BOOSTER PUMP (TANK NO.1) OPERATING,APU ISOLATION(SHUT OFF) AND APU FIRE SHUT-OFF VALVE OPEN.ACCESS: 313AL* 0.14282611-0502-1 147 VALVE-ECOLOGICAL DISCHARGE MEC GVI I: 1 C MRB AMM 282611/6011 0.10 GE1481 0.10 POST 01024CHECK THAT DISCHARGE VALVE DIFFERENTIAL(28-0010)PRESSURE INDICATOR IS NOT PROTRUDINGPOST 01351(73-0001)283100-0502-1 535 FUEL JETTISON - FLEX. HOSE MEC DET T: 4 C MPD AMM 275165/4011 0.10 B4635 I: 1 C1 0.10 C4DETAILED INSPECTION OF THE FUEL JETTISIONF4SYSTEM FLEXIBLE HOSE FOR PROPER INSTALLATION,EVIDENCE OF DAMAGE AND/OR LEAKAGE.NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY OFTASK 275126-0505-2ACCESS:-LH MOVABLE AND FIXED FLAP-TRACK FAIRING NO.5-RH MOVABLE AND FIXED FLAP-TRACK FAIRING NO.5283100-0503-1 535 FUEL JETTISON SYSTEM MEC OPC I: 3 C MRB ** AMM 283100/5012 1.20 B46352 1.20 C401. OPERATIONAL TEST OF JETTISON VALVEF4CONTROL AND INDICATING CIRCUITS02. OPERATIONAL TEST OF JETTISON VALVE03. FUNCTIONAL TEST OF FUEL JETTISON SYSTEM04. CHECK JETTISON PIPE BETWEEN WINGLOWER SKIN AND END OF FLAP TRACK FAIRINGFOR LEAKAGE283111-0503-1 542 CHECK VALVE-FUEL FEED MEC OPC I: 6 C MRB AMM 283111/5012 0.25 B46422 0.25 C4OPERATIONAL TEST OF CHECK VALVE - FUEL FEEDF4SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)283114-0502-1 535 NOZZLE JETTISON MEC GVI I: 1 A MRB1 0.25 B46351 0.25 C4CHECK JETTISON DISCHARGE NOZZLE (AT FLAP TRACKF4NO. 5) FOR GENERAL CONDITION284200-0503-1 210 CAPACITANCE QUANTITY INDIC. ERI FUC I: 4 C MRB AMM 284200/5013 15.00 B4C4FUNCTIONAL TEST OF FUEL QUANTITY AMPLIFIER ( 15QT )F4WITH TANKS DRYACCESS: 144ER 523JB 623JB* 0.16284200-0503-2 210 CAPACITANCE QUANTITY INDIC. ERI FUC I: 4 C MRB AMM 284200/5013 12.00 B2FUNCTIONAL TEST OF FUEL QUANTITY AMPLIFIER ( 15QT )WITH TANKS DRYACCESS: 144ER 523JB 623JB* 0.16284300-0503-1 210 FUEL LOW PRESSURE INDICAT. ERI OPC I: PRE-ACPT MRB AMM 331400/5011 0.10 ALLLIGHT TEST OF FUEL LOW PRESSURE INDICATORS.284600-0503-1 210 FUEL LOW LEVEL INDICATING ERI OPC I: 1 C MRB ** AMM 284600/5011 2.00 ALLOPERATIONAL TEST OF LOW LEVEL INDICATING SYSTEM.( ALTERNATIVE WITHOUT TEST EQUIPMENT: TRANSFER FUELFROM ONE TANK TO THE OTHER )* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION:2-28 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)290000-0502-1 570 HYDRAULIC POWER MEC DET T: 27000 FH ISB ISB 29-01221 2.00 PRE 13297670 OR1 2.00 PRE 13424DETAILED INSPECTION OF HYDRAULIC PIPES IN WING AREA 13500 FC(29-0121)LH/RH BETWEEN RIB 5A AND RIB 9. I: 24 MOACCESS: 575CB 575DB* 0.15675CB 675DB* 0.15291000-0502-1 147 MAIN SYSTEM - FILTERS MEC GVI I: WEEKLY MPD AMM 290000/3011 0.10 ALL5711 0.10671 CHECK THAT RETURN FILTER CLOGGING INDICATOR1 0.10BUTTONS ARE NOT PROTRUDING (GREEN,BLUE AND YELLOW)ACCESS: 147SZ* 0.02291000-0502-2 147 MAIN SYSTEM - FILTERS MEC GVI I: 1 A MPD AMM 290000/3011 0.25 ALLCHECK THAT CLOGGING INDICATORS OF GROUND SERVICE,HIGH PRESSURE, BRAKE FILTER AND RETURN FILTER ARENOT PROTRUDING.291000-0502-3 435 E.D.P. CASE DRAIN FILTER MEC GVI I: 1 A MRB AMM 290000/3011 0.10 ALL4451 0.10CHECK THAT EDP CASE DRAIN FILTERS CLOGGINGINDICATORS ARE NOT PROTRUDINGACCESS: 435AL* 0.01445AL* 0.01291000-0503-1 147 HYDRAULIC POWER MEC FUC I: 3 C MRB AMM 290000/6013 9.00 ALLCHECK AND MEASUREMENT OF HYDRAULIC COMPONENTSINTERNAL LEAKAGE AS FOLLOWS:MEASURE AND RECORD LEAKAGE RATE PER GROUP OF USERSERVICES IN GREEN,BLUE AND YELLOW SYSTEM AND COMPAREWITH "NOMINAL"FLOW RATE OF EACH GROUP (FOR MONITORINGPURPOSE)ACCESS: 147DZ* 0.03SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)291000-0503-2 210 HYDR.FLUID TEMP.INDICATING MEC OPC I: 1 A MRB ** AMM 293300/5011 0.30 ALLOPERATIONAL TEST OF HYDRAULIC FLUID TEMPERATUREOVERHEAT WARNING SYSTEM (PUSH TO TEST)291000-0503-3 210 HYDRAULIC QTY, INDICATING MEC FUC I: 3 C MRB AMM 293100/5012 1.50 ALLFUNCTIONAL TEST OF QUANTITY AND LOW LEVELWARNING.(MAIN AND AUXILARY SYSTEMS)ACCESS: 147SZ 148SZ* 0.03291000-0503-4 210 HYDRAULIC POWER MEC FUC I: 1 C MPD AMM 290000/6011 1.00 ALLINTERNAL LEAKAGE CHECK OF HYDRAULIC SYSTEM BY MEANSOF ELECTRIC PUMP PRESSURE291000-0503-5 147 HYDRAULIC SYSTEM FLUID SAMPLING MEC CHK I: 1 C SIL AMM 123229/0011 0.20 ALL148 SIL 29-0341 0.20SAMPLING OF HYDRAULIC FLUID. SIL 29-081ACCESS: 734* 0.10744* 0.10291000-0505-1 148 HYDRAULIC PRESSURE FILTERS MEC DET I: 1 C MRB AMM 291142/3011 5.00 ALLAMM 292117/301CHECK PRESSURE FILTER ELEMENTS FOR PARTICLES: AMM 292213/30101. REMOVE FILTER ELEMENTS (1048,1049,2048,3049,AND AMM 292412/3011079,2091,3084,3090)02. DETAILED INSPECTION FOR SATISFACTORYCONDITION AND METAL PARTICLES03. REINSTALL A NEW OR RECONDITIONED FILTER ELEMENTACCESS: 147LZ 147SZ 148LZ* 0.30291000-0505-2 148 RETURN MANIFOLD FILTERS (G) MEC CLN I: 3 C MPD AMM 291114/3011 1.50 POST 02352(32-0203)REMOVE,INSPECT AND CLEAN GREEN RETURN MANIFOLDPOST 02538FILTER ELEMENT (1066)(29-0061)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)291000-0505-2 * * * * * C O N T I N U E * * * * *ACCESS: 148SZ* 0.01291000-0505-3 147 RETURN FILTERS MEC RAR I: 3 C MRB AMM 291115/3011 0.75 ALL5711 0.75671 REPLACE RETURN FILTER ELEMENT AND CHECK FOR1 0.75PARTICLES (1002,2002,3002)ACCESS: 147BL* 0.01571EB* 0.02671EB* 0.02291000-0505-4 147 GROUND SERVICE FILTER MEC DET I: 4 C MRB AMM 291164/3011 0.75 ALLINSPECT GROUND SERVICE FILTER ELEMENT FORPARTICLES AS FOLLOWS:01. REMOVE FILTER ELEMENT02. DETAILED INSPECTION FOR SATISFACTORYCONDITION AND METAL PARTICLES.03. REINSTALL NEW OR RECONDITIONED FILTER ELEMENTACCESS: 147BL* 0.01291000-0505-5 671 RAM AIR TURBINE FILTER MEC DET I: 4 C MRB AMM 292535/3011 0.75 ALLINSPECT RAM AIR TURBINE FILTER ELEMENT FOR PARTICLES:01. REMOVE FILTER ELEMENT02. DETAILED INSPECTION FOR SATISFACTORYCONDITION AND METAL PARTICLES03. REINSTALL NEW OR RECONDITIONED FILTER ELEMENT291000-0505-6 430 E.D.P.SHAFT SEAL DRAINS MEC SER I: 5 A MPD AMM 290000/6011 0.20 GE4401 0.20DRAIN INDIVIDUAL COLLECTOR OF EACH E.D.P.SHAFTSEAL DRAIN,TO MONITOR SHAFT SEAL LEAKAGEACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)291000-0505-7 450 E.D.P.SHAFT SEAL DRAINS MEC SER I: 5 A MRB AMM 290000/6011 0.20 PW4601 0.20DRAIN INDIVIDUAL VALVE OF EACH E.D.P.SHAFT SEALDRAIN,ON GEARBOX SEAL DRAIN MANIFOLD ASSY,TO MONITORSHAFT SEAL LEAKAGEACCESS: 451AL 452AR* 0.02461AL 462AR* 0.02291000-0505-8 435 MAIN HYDRAULIC POWER MEC RAR I: EDP CHG MRB AMM 291136/3011 2.00 ALL445 ENG. CHG1 2.00REMOVE EDP CASE DRAIN FILTER ELEMENTS (GREEN, BLUE,YELLOW), INSPECT FILTER ELEMENTS FOR PARTICLES,INSTALL NEW FILTER ELEMENTS.ENSURE CLOGGING INDICATORIS NOT PROTRUDINGNOTE: AFTER ENGINE OR EDP CHANGEACCESS: 435AL* 0.01445AL* 0.01291111-0505-1 140 HYDR.QUANTITY INDICATING MEC RPL I: 1 A MRB AMM 121229/0011 0.30 ALLCHECK FLUID LEVEL OF HYDRAULIC TANKS (BLUE-GREEN-YELLOW).ACCESS: 147BL 147RZ 147SZ 147XZ 148RZ 148SZ* 0.07291132-0503-1 210 PUMP-ENGINE DRIVEN (G&B&Y) MEC OPC I: 1 A MRB AMM 291000/5011 0.20 ALLDEPRESSURATION OPERATIONAL TEST OF ENGINE DRIVENPUMPS (GREEN-BLUE-YELLOW)291133-0503-1 210 SHUT OFF VALVE-FIRE (G&B&Y) MEC FUC I: 4000 FH MRB ** AMM 291000/5011 0.10 ALLFUNCTIONAL TEST OF FIRE SHUT OFF VALVES.NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITYOF TASK 762000-0503-1 AND 762000-0503-2SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)291133-0503-3 210 SHUT OFF VALVE-FIRE (G&B&Y) MEC OPC I: 3 A MRB ** AMM 291000/5011 0.10 NON FWD-FACEOPERATIONAL TEST OF HYDRAULIC FIRE SHUT OFF VALVES -GREEN,BLUE,YELLOW - WITH INDIVIDUAL CONTROL SWITCHES(PUMP NOT RUNNING).291133-0503-4 210 SHUT OFF VALVE-FIRE (G&B&Y) MEC OPC I: 600 FH SIL SIL 29-0521 0.20 POST 10720(29-0105)OPERATIONAL TEST OF FIRE VALVES.PRE 11767(29-0112)ORPOST 10720(29-0105)PRE 11768(09-0113)291136-0502-1 450 EDP CASE DRAIN FILTER MEC DET I: 50 FH CN AMM 291136/3011 0.40 ABEX EDP460 CN F-1991-1481 0.40 P/N 65066-06REMOVE AND INSPECT EDP CASE DRAIN FILTER FOR EVIDENCES/N 242001 THRUOF STEEL PARTICLES.242082291156-0505-1 147 HYDR. ACCUMULATOR (G&B&Y) MEC RPL I: 1 A MRB AMM 121429/0011 0.25 ALLCHECK CHARGE PRESSURE OF HYDR.ACCUMULATORS(BLUE-GREEN-YELLOW) AND BRAKE ACCUMULATORACCESS: 147RZ 147SZ 148RZ 148XZ* 0.05291400-0502-1 571 TANK PRESSURATION FILTER MEC GVI I: 1 A MPD AMM 291400/3011 0.10 POST 3079ORCHECK BY-PASS OPENING INDICATOR ON PRESSURISATIONPOST 4152LINE FILTER OF "ENG I" AIR BLEED IS NOT PROTRUDING.(29-0080)291400-0505-1 450 HYDR.TANK PRESSURE FILTER MEC CLN I: ENG. CHG MPD AMM 291415/4011 0.10 POST 017864601 0.10 (29-0042)CLEAN PRESSURIZATION LINE FILTER SCREEN(BETWEEN RIB 5 AND 6 IN LOWER PYLON SECTION)NOTE: AFTER 1ST ENGINE RUN-UP.ACCESS: 435AL 455AL 456AR* 0.04* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)291400-0505-1 * * * * * C O N T I N U E * * * * *445AL 465AL 466AR* 0.04292000-0502-1 147 AUXILARY SYSTEM MEC GVI I: 1 A ISB ISB 29-00152 0.50 PRE 015721482 0.50 (29-0031)CHECK GREEN SYSTEM ELECTRIC PUMPS (ABEX MODEL PMP 09(ABEX MODELV01 P/N: 4007) AT PORT CAPS FOR LEAKS, WHEN PUMPS AREPMP 09 V01OPERATING.P/N 4007)CAUTION: PORT CAP LEAKAGE SHOULD NOT BE CONFUSED WITHDRAINAGE FROM DRAIN HOLE BETWEEN PUMP ANDMOTORACCESS: 147SZ* 0.02148SZ* 0.01292211-0503-1 210 POWER TRANSFER UNIT MEC OPC I: 2 A MRB AMM 292200/5011 0.25 ALLAMM 292300/501OPERATIONAL TEST OF POWER TRANSFER UNITS (GREEN/BLUEAND GREEN/YELLOW)292527-0503-1 210 TURBINE-RAM AIR MEC FUC I: 2 C MRB ** AMM 292500/3012 5.00 POST 01758AMM 292500/501(29-0039)FUNCTIONAL TEST OF TURBINE - RAM AIRPOST 02528(29-0060)POST 06054(29-0088)292527-0503-2 132 TURBINE-RAM AIR MEC FUC I: 3 C MRB AMM 292500/5011 0.50 ALLCHECK CABLES OF TURBINE - RAM AIR CONTROL WITHTENSIOMETER FOR CORRECT TENSION (REFER TO CABLETENSION ADJUSTMENT GRAPH IN THE RESP. AMM 292500/501)292527-0503-3 671 TURBINE - RAM AIR MEC FUC I: 600 FH CN AMM 292500/3012 5.00 PRE 01758OR FAA AD AMM 292500/501(29-0039)FUNCTIONAL TEST OF TURBINE - RAM AIR 6 MO CNPRE 025281985-146-IMP(B) (29-0060)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)292527-0503-3 * * * * * C O N T I N U E * * * * *ACCESS: 671BB 671CB FAA AD 90-23-11 * 0.85292527-0503-4 671 TURBINE - RAM AIR MEC FUC I: 3000 FH CN AMM 292500/3012 5.00 POST 01758OR FAA AD AMM 292500/501(29-0039)FUNCTIONAL TEST OF TURBINE - RAM AIR 1 YE CNPOST 02528NOTE 1985-146-IMP(B) (29-0060)NOTE: FOR INITIAL INSPECTION 9000 FH OR 3 YE FAA AD 90-23-11 PRE 06054SUBJECT TO A ONCE ONLY CHECK PER AIRCRAFT ISB 29-0087(29-0088)292527-0503-5 671 TURBINE - RAM AIR MEC RAR I: 20000 FH CN AMM 292527/4012 10.00 POST 01758OR FAA AD CN(29-0039)REMOVE RAM AIR TURBINE FOR OVERHAUL 10 YE 1985-146-IMP(B) POST 02528FAA AD 90-23-11 (29-0060)ACCESS: 671BB 671CB ISB 29-0087* 0.85 PRE 06054(29-0088)292527-0503-6 671 TURBINE - RAM AIR MEC DET I: 30 MO CN AMM 292500/5011 0.30 PRE 04803FAA AD CNPRE 08732DETAILED INSPECTION, CLEANING AND GREASING OF 1991-124-122(B) (29-0099)RAT EXTENSION CONTROL CABLES. FAA AD 92-19-03ISB 29-0097NOTE: TASK MAY BE ACCOMPLISHED DURING FUNCTIONALTEST OF RAT.ACCESS: 671BB 671CB* 0.85292527-0503-7 671 TURBINE - RAM AIR MEC FUC I: 10 MO CN AMM 292500/5011 0.50 PRE 11206FAA AD CN(29-0106)01. DEPLOY RAM AIR TURBINE 2000-259-315(B)02. CHECK FOR CORRECT ADJUSTMENT OF FAA ADRAM AIR TURBINE LOCKING ROD. 2001-01-06ISB 29-0101ACCESS: 671BB 671CB* 0.85292527-0503-8 671 TURBINE - RAM AIR MEC RAR I: 20 YE CN AMM 292527/4012 5.00 ALLFAA AD CN 2001-212(B)REMOVE RAM AIR TURBINE FOR OVERHAUL FAA AD2002-02-05* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)292527-0503-8 * * * * * C O N T I N U E * * * * *ACCESS: 671BB 671CB SB 29-0118* 0.85292527-0504-1 671 TURBINE-RAM AIR MEC RAR I: 30 MO CN AMM 292526/4011 10.00 PRE 11527FAA AD CN(29-0109)REMOVE THE LEVER ASSEMBLY OF THE RAT UPLOCK 1995-163-182(B)FEEDTHROUGH MECHANISM FOR STRIP INSPECTION FAA AD 98-21-32ISB 29-0108PREP.: RAT EXTENSIONACCESS: 671BB* 0.43292527-0505-1 671 TURBINE-RAM AIR MEC LUB I: 2 C MPD AMM 122229/0011 0.20 PRE 11206(29-0106)LUBRICATE RAM AIR TURBINE DOOR HINGES ANDEXTENSION JACK ROD END FITTING292527-0505-2 671 TURBINE-RAM AIR MEC LUB I: 2 C MPD AMM 122229/0011 0.20 POST 11206(29-0106)LUBRICATE RAM AIR TURBINE DOOR HINGES ANDEXTENSION JACK ROD END FITTING AND LOCKINGROD ASSEMBLY* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION:2-29 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)301100-0503-1 210 WING ICE PROTECTION ERI OPC I: 2 C MRB AMM 301100/5011 0.17 FWD-FACEOPERATIONAL TEST OF EMERGENCY IN FLIGHT ICEPROTECTION (APU SUPPLY) CONTROL AND INDICATINGCIRCUIT.301100-0503-2 140 UNDERPRESSURE SWITCH ERI FUC I: 3 C MRB AMM 301112/5012 3.00 FWD-FACEFUNCTIONAL TEST OF BOTH UNDERPRESSURE SWITCHES 137 DMAND 138 DMNOTE: ON A/C FUNCTIONAL TEST WITH PRESSURESWITCHES REMOVEDACCESS: 147FZ* 0.04301100-0503-3 210 WING ICE PROTECTION ERI OPC I: 2 C MPD AMM 301100/5011 0.20 PRE 02372NON-FWD FACEOPERATIONAL TEST OF OVERHEAT WARNING CIRCUITS301100-0503-4 210 WING ICE PROTECTION ERI OPC I: 2 A MRB ** AMM 301100/5011 0.33 POST 02372NON-FWD FACEON PANEL 38VU:01. OPERATIONAL TEST OF ANTI-ICE VALVES FAULTYPOSITION WARNING.02. OPERATIONAL TEST OF EMERGENCY ICE PROTECTION(APU SUPPLY) CONTROL AND INDICATING CIRCUIT.301100-0503-5 210 WING ICE PROTECTION ERI OPC I: 2 A MRB AMM 301100/5011 0.17 FWD-FACEON PANEL 426 VU:01. OPERATIONAL TEST OF "ALTERNATE" MODE02. OPERATIONAL TEST OF "FAULT" WARNING (EACH VALVEDISAGREE DETECTION)301100-0503-6 210 WING ICE PROTECTION ERI OPC I: 2 A MRB ** AMM 301100/5011 0.10 PRE 02372NON-FWD FACEON PANEL 38 VU01. OPERATIONAL GROUND TEST OF ICE PROTECTION UNDERPRESSURE AND EXCESSIVE PRESSURE WARNING CIRCUITS02. OPERATIONAL TEST OF UNDER TEMPERATURE WARNING* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ICE AND RAIN PROTECTION REV. DATE: APR 01/10 SECTION:2-30 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)301100-0503-6 * * * * * C O N T I N U E * * * * *INHIBITION WITH EMERGENCY INFLIGHT ICE PROTECTIONCONTROLLED BY APU301112-0503-1 512 SWITCH - UNDERPRESSURE ERI FUC I: 2 C MPD AMM 301112/5011 0.30 PRE 023726121 0.30 NON-FWD FACEFUNCTIONAL TEST OF UNDERPRESSURE SWITCH ANDASSOCIATED WARNING CIRCUITSACCESS: 512KB* 0.17612KB* 0.17301113-0503-1 512 SWITCH - EXCESSIVE PRESSURE ERI FUC I: 2 C MPD AMM 301113/5011 0.30 PRE 023726121 0.30 NON-FWD FACEFUNCTIONAL TEST OF EXESSIVE PRESSURE SWITCH ANDASSOCIATED CIRCUITSACCESS: 512KB* 0.17612KB* 0.17302100-0503-1 210 ENGINE AIR INTAKE ANTI-ICE ERI OPC I: 3 C MRB AMM 302100/5011 0.17 FWD-FACEOPERATIONAL TEST OF ENGINE ANTI ICE INDICATING SYSTEM302100-0503-2 430 ENGINE AIR INTAKE ANTI-ICE ERI FUC I: 3 C MRB AMM 302112/5011 0.25 PW4401 0.25 FWD FACEFUNCTIONAL TEST OF POD ANTI ICE PRESSURE SWITCHESACCESS: 436AR* 0.01302100-0503-3 210 ENGINE-AIR INTAKE ANTI-ICE ERI OPC I: DY-TERM MRB ** AMM 302100/5011 0.10 ALLOPERATIONAL TEST OF ENGINE ANTI-ICE SYSTEM303100-0503-1 210 SENSORS,PITOT PROBES/STATIC ERI OPC I: DY-TERM MRB ** AMM 303100/5011 0.10 ALL* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ICE AND RAIN PROTECTION REV. DATE: APR 01/10 SECTION:2-30 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)303100-0503-1 * * * * * C O N T I N U E * * * * *OPERATIONAL TEST OF PITOT PROBES AND STATIC PORTSHEATING SYSTEM304100-0502-1 210 WINDSHIELD RAIN REMOVAL SYS ERI GVI I: C MPD AMM 304100/6011 0.25 ALLNOTEGENERAL VISUAL INSPECTION OF WINDSHIELD WIPERS FORSATISFACTORY CONDITIONNOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITHOPERATIONAL ENVIRONMENT AND OPERATOR EXPERIENCE304100-0502-2 210 WINDSHIELD RAIN REMOVAL SYS ERI GVI I: DY-TERM MRB AMM 304151/4011 0.10 PRE 11480(30-0044)CHECK QUANTITY AND PRESSURE OF RAIN REPELLENTSYSTEM304200-0502-1 210 WINDSHIELD PANEL ANTI-ICE AND DE-FOGGING ERI DET T: 15000 FH ISB ISB 30-00471 2.50 ALLI: 1 CDETAILED INSPECTION OF PILOT AND COPILOT ORSLIDING WINDOWS ELECTRICAL HARNESS AND METALLIC 5000 FHCONDUIT304200-0503-1 210 WINDSHIELD ANTI ICE/DEFOG. ERI OPC I: 1 C MRB AMM 304200/5011 0.50 ALLAMM 304300/501OPERATIONAL TEST OF ANTI-ICING AND DE-FOGGINGOVERCURRENT PROTECTION307200-0503-1 136 WATER SERV.PANELS HEATING MEC OPC I: 1 C MPD AMM 307200/4011 0.20 POST 068832201 0.20 (38-0037)OPERATIONAL TEST OF THE WATER SERVICING PANEL HEATINGACCESS: 136BR* 0.01* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ICE AND RAIN PROTECTION REV. DATE: APR 01/10 SECTION:2-30 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)310000-0502-1 210 INDICATING/RECORDING SYSTEM MEC OPC I: PRE-ACPT MRB AMM 311500/0011 0.10 ALLCHECK ENGINE OIL, APU OIL AND HYDRAULIC TANK FLUIDFOR CORRECT LEVELS AT FLIGHT COMPARTMENT INDICATORS311500-0502-1 210 LATERAL PANEL ELO OPC I: PRE-ACPT MPD AMM 242100/0011 0.10 FWD-FACECHECK STATUS OF AC GENERATORS "BEARING RUB"LATCHING MAGNETIC INDICATORS311500-0502-2 210 LATERAL PANEL ELO OPC I: DY-TERM MRB AMM 311500/0011 0.10 FWD-FACEON LATERAL PANEL:01. SELECT ANNUNCIATOR LIGHTS SWITCH TO "READ" POSI-TION:- CHECK STATUS OF "OPEN / SHUT" INDICATINGLIGHTS (HYDRAULIC FIRE SHUT-OFF VALVES ANDAPU ISOLATING VALVE)- CHECK STATUS OF "DC BUS TIE CONTACTOR" INDI-CATING LIGHT02. CHECK STATUS OF ALL LATCHING MAGNETIC INDICATORS03. MAKE CERTAIN THAT ALL TEST ROTARY SELECTORS AREIN "NORMAL FLT" POSITIONTAKE APPROPRIATE ACTION ACCORDING TO FINDINGS313100-0503-1 171 DIGITAL FLIGHT DATA RECORD. ELO FUC I: NOTE 5-3 MRB AMM 313135/4011 7.50 ALLORDFDR TAPE READ OUT FOR AQUISITION CHECK OF MANDATORY 2 CPARAMETERS AS DEFINED BY OPERATORS AIRWORTHINESSAUTHORITYACCESS: 162AZ* 0.01313100-0503-2 171 UNDERWATER LOCATOR BEACON ELO FUC I: NOTE 5-1 MRB AMM 313100/4011 0.50 ALLNOTE 5-3FUNCTIONAL TEST OF UNDERWATER LOCATOR BEACON ANDREPLACE BATTERY IF NECESSARYACCESS: 162AZ* 0.01SYSTEMS AND POWERPLANT PROGRAM : INSTRUMENTS REV. DATE: APR 01/10 SECTION:2-31 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)313100-0504-1 171 DFDR - U.L.B. ELO RAR I: NOTE 5-1 MRB AMM 313100/4011 0.25 ALLDISCARD AND REPLACE BATTERY OF UNDERWATER LOCATORBEACON ATTACHED TO THE DIGITAL FLIGHT DATA RECORDERACCESS: 162AZ* 0.01314211-0503-1 210 COMPUTER - N1 LIMIT ELO OPC I: DY-TERM MRB AMM 314200/5011 0.10 GENON-FWD FACEOPERATIONAL TEST OF N1 LIMIT COMPUTER314211-0503-2 210 COMPUTER EPR LIMIT ELO OPC I: DY-TERM MRB AMM 314200/5011 0.10 PWNON-FWD FACEOPERATIONAL TEST OF EPR LIMIT COMPUTER314213-0503-1 122 FAN COOLING - N1 ELO OPC I: 3 C MRB AMM 314213/4011 0.17 GEPOST 01839OPERATIONAL TEST OF N1 LIMIT COMPUTER COOLING FANNON-FWD FACE(AURAL CHECK)314213-0503-2 122 FAN COOLING - EPR ELO OPC I: 3 C MRB AMM 314213/4011 0.17 PWNON-FWD FACEOPERATIONAL TEST OF EPR LIMIT COMPUTER COOLING FAN(AURAL CHECK)* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : INSTRUMENTS REV. DATE: APR 01/10 SECTION:2-31 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)321000-0502-1 731 MAIN GEAR AND DOORS MEC GVI I: WEEKLY MRB AMM 321000/6011 0.30 ALL7411 0.30CHECK ATTACHMENTS AND INSTALLATIONS FOR SECURITYAND DAMAGE.CHECK EXTERNAL LEAKAGE OF ALL COMPONENTS,DOOR UP-LOCK ASSY AND MAIN GEAR UP-LOCK ASSY(DOORS OPEN)321100-0502-1 730 MAIN GEAR MEC DET I: 4 YE ISB ISB 32-02332 24.00 PRE 010337402 24.00 (32-0040)DETAILED INSPECTION OF SHOCK ABSORBER LOWERMHB 322BEARING HOUSING FOR CORROSION321100-0502-2 731 MAIN GEAR MEC DET I: REFER CN CN CN2 2.00 PRE 01257741 FAA AD 1981-174-041(B) 2 2.00 MHB 224DETAILED CHECK OF MLG HINGE ARMS FAA AD 84-02-04(PIN C65381-2) IN THE VICINITY OF THE RETRACTION ISB 32-0328MECHANISM ATTACHING TRUNNIONS FOR CORROSION ANDCRACKS321100-0502-3 731 MAIN GEAR MEC GVI I: PRE-ACPT MRB AMM 321000/6011 0.20 ALL7411 0.20CHECK MAIN GEAR FOR GENERAL CONDITION,FLUIDLEAKAGE,TYRES FOR EVIDENCE OF UNDERINFLATION,ANDBRAKES FOR EXTERNAL LEAKAGE.(DOORS CLOSED) CHECK THATPITCH DAMPER DROOP INDICATOR IS NOT PROTRUDING(IF INSTALLED)321100-0502-4 731 MAIN GEAR MEC GVI I: DY-TERM MRB AMM 321000/6011 0.20 ALL741 AMM 324100/6011 0.20CHECK NORMAL EXTENSION AND GENERAL CONDITION OFSLIDING TUBE, WHEELS AND TYRES FOR DAMAGE, WEAR(DEFORMATION,CUTS,FLAT SPOTS) AND CORRECT PRESSURE,BRAKES FOR GENERAL CONDITION AND EXTERNAL LEAKS321100-0503-1 731 MLG - HINGE ARM MEC FUC I: ISB CN CN2 5.00 POST 01257741 32-356 FAA AD 1982-160-049(B) 2 5.00 MHB 224AT HINGE ARMS MEASURE SIDE PLAY OF BRONZE BUSH, CNPRE 04544LOCATED BETWEEN STIRRUP AND HINGE ARM TRUNNION 1983-051-050(B) (32-0348)AT ACTUATING CYLINDER SIDE. FAA AD 84-03-08 (32-0355)ISB 32-0356MHB 542/ 585* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)321100-0503-1 * * * * * C O N T I N U E * * * * *P/N C65381-4P/N C65381-6321100-0503-2 730 MLG - HINGE ARM NDT SDI T: REFER CN CN CN1 0.80 PRE 01257740 I: 400 FC FAA AD 1983-052-051(B) 1 0.80 MHB 485SPECIAL DETAILED INSPECTION (ULTRA SONIC) FAA AD 84-02-04-PROBE PARALLEL AND PROBE AT 45 DEGREES- ISB 32-0365P/N C65381-2ON THE LATERAL INBOARD TRUNNION OF HINGE ARM ON ISB 470-32-442P/N C65381-4ACTUATOR SIDE.321100-0503-3 730 MLG - HINGE ARM NDT SDI I: REFER CN CN CN2 0.50 B2740 FAA AD 1987-029-078(B) 2 0.50SPECIAL DETAILED INSPECTION (ULTRASONIC) ON THE TWO FAA AD 88-03-04LOWER FLANGE TIE RODS ON HINGE ARM. ISB 32-0369ISB 470-32-420321112-0502-1 731 MAIN LANDING GEAR ASSY MEC DET I: 1 C MRB ** AMM 321000/6011 4.00 ALL7411 4.00DETAILED INSPECTION OF MAIN LANDING GEARSTRUCTURE, RELATED COMPONENTS AND ATTACHMENTS(WITH DOORS OPEN)- SHOCK STRUT (OUTER CYLINDER), HINGE ARM (TRUNNION)AND BEARING, MULTIPLE CLEVIS ASSY, CROSS BRACE ANDUP-LOCK ROLLER, TORQUE LINKS, SLIDING TUBE,BOGIE BEAM(TRUCK BEAM),PITCH DAMPER,BRAKE BAR (BRAKE EQUALIZINGRODS), BRACE STRUT (SIDE STRUT), LOCK LINK ASSY,SPRINGS, BRACE STRUT HINGE POINT AT FRAME 50, SHAFT(VISIBLE PART ONLY) FOR:CLEANLINESS,CORROSION,PROTECTIVE PAINTWORK,SECURITYOF ATTACHMENT,LEAKAGE,IDENTIFICATION PLATES CORRECTLYATTACHED,BONDING JUMPERS FOR CORRECT CONDITION ANDFLAKED AREAS ON THE CHROMIUM PLATED RODS.321112-0502-2 731 MLG - UPLOCK ROLLERS MEC GVI I: 5 A MRB AMM 321000/6011 0.10 ALL7411 0.10CHECK UPLOCK ROLLERS OF STRUT ASSY FOR FREEROTATIONSYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)321112-0504-1 700 MAIN LANDING GEAR ASSY MEC RAR I: 12000 FC MRB ** AMM 321111/4013 35.00 ALLORREMOVE AND REPLACE FOLLOWING COMPONENTS FOR 8 YEOVERHAUL:- STRUT ASSY - MAIN GEAR SHOCK- ABSORBER MAIN GEAR SHOCK- BEAM ASSY - BOGIE- STRUT BRACE- LINK ASSY LOCK321112-0505-1 731 MAIN LANDING GEAR ASSY MEC LUB I: 3 A MRB AMM 122232/0011 2.00 ALL7411 2.00CLEAN AND LUBRICATE ALL POINTS OF MLG SUCH AS:- UPLOCK ASSY - MAIN GEAR DOOR- ACTUATING CYLINDER - MAIN GEAR- ACTUATING CYLINDER - BRACE STRUT NORMAL- MAIN GEAR - ATTACH FITTING- STRUT ASSY - MAIN GEAR SHOCK- LINK ASSY - LOCK- MECHANICAL INDICATOR (EXPOSED METAL PARTS OF CON-TROL SYSTEM)- HINGE ARM TRUNNION- DOOR - CENTER HINGE BEARING (POST 6480)- BRAKE UNIT BOGIE BEAM SIDENOTE: BRAKE UNIT ON WHEEL SIDE AT OPPORTUNITY OFWHEEL CHANGE321112-0505-2 731 MAIN LANDING GEAR ASSY MEC LUB I: 2 A MRB AMM 122232/0011 0.30 ALL7411 0.30CLEAN AND LUBRICATE FOLLOWING POINTS:- BOGIE BEAM ARTICULATION- PITCH DAMPER ATTACH POINTS- BRAKE BARS ATTACH POINTS321112-0505-3 731 MAIN LANDING GEAR ASSY MEC LUB I: 1 A SIL AMM 122232/0011 TBD ALL741 SIL 32-1111 TBDLUBRICATION OF LOWER BEARING - SHOCK STRUT(BARREL LOWER BEARING)SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)321113-0505-1 731 ABSORBER-MAIN GEAR SHOCK MEC RPL I: 1 C MRB AMM 121232/0011 0.50 ALL7411 0.50CHECK MLG SHOCK ABSORBER CHARGE PRESSURE321113-0505-2 731 ABSORBER-MAIN GEAR SHOCK MEC RPL I: 2 C MRB AMM 121232/0011 1.00 ALL7411 1.00CHECK MLG SHOCK ABSORBER FLUID LEVEL ANDCHARGE PRESSURE321114-0502-1 731 BOGIE BEAM ASSEMBLY MEC DET I: ISB CN AMM 321114/6011 0.30 PRE 01257741 32-394 FAA AD CN1 0.30 (32-0396)DETAILED INSPECTION OF THE INNER SIDE OF THE 1990-005-101(B) MHB SBBOGIE BEAM BETWEEN THE TWO AXLES. FAA AD 90-26-03 470-32-672ISB 32-0394SB MHB470-32-659321115-0505-1 731 DAMPER-PITCH MEC RPL I: 1 C MRB ** AMM 121232/0011 1.00 PRE 029497411 1.00 (32-0258)CHECK MLG PITCH DAMPER CHARGE PRESSUREPOST 03080(32-0268)321115-0505-2 731 DAMPER-PITCH MEC RPL I: 2 C MRB AMM 121232/0011 1.50 PRE 029497411 1.50 (32-0258)CHECK MLG PITCH DAMPER FLUID LEVELPOST 03080(32-0268)321115-0505-3 731 DAMPER - PITCH MEC RPL I: 1 C MRB AMM 121232/0011 1.50 PRE 029497411 1.50 (32-0258)CHECK MLG PITCH DAMPER FLUID LEVELPRE 03080(32-0268)321115-0505-4 731 DAMPER - PITCH MEC RPL I: 3 A MRB AMM 121232/0011 1.50 POST 029497411 1.50 (32-0258)CHECK MLG PITCH DAMPER FLUID LEVELPOST 03080(32-0268)SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)321118-0502-1 147 MULTIPLE CLEVIS ASSY MEC DET I: 1 C MRB ** AMM 321000/6011 0.50 ALL1481 0.50DETAILED INSPECTION OF MULTIPLE CLEVIS ASSY ATFRAME 50 FOR CRACKS AND CORROSION(IN SITU,AS FAR AS VISIBLE)321118-0504-1 147 MULTIPLE CLEVIS SHAFT FR.50 MEC RAR I: 12000 FC MRB ** AMM 321118/4012 4.00 ALL148 OR2 4.00REMOVE UPPER SHAFT OF MULTIPLE CLEVIS AT 8 YEFR.50 AND INSPECT FOR WEAR AND CORROSION321124-0504-1 700 FWD SPHERICAL BEARING HOUS. MEC RAR I: 12000 FC MPD AMM 321124/4011 1.00 PRE 06329OR SIL 32-038(32-0377)REMOVE SPHERICAL BEARING ASSY FROM FORWARD 8 YEPICK-UP AND INSPECT HOUSING AND SCREW THREADSNOTE: TO BE PERFORMED AT OPPORTUNITY OF LANDINGGEAR OVERHAUL321127-0502-1 731 TORQUE LINKS - MAIN GEAR MEC GVI I: 4 C MPD AMM 321127/4011 0.30 ALL7411 0.30CHECK TORQUE LINKS FOR EXESSIVE FREEPLAY322000-0502-1 711 NOSE GEAR AND DOORS MEC GVI I: WEEKLY MRB AMM 322000/6011 0.30 ALLCHECK NLG FOR SECURITY AND DAMAGE OF ATTACHM.INSTALLATIONS AND EXTERNAL LEAKAGE OF ALL COMPONENTS,DOORS UP-LOCK ASSY, DOORS STRUCTURE AND HINGES, NOSEGEAR UP-LOCK ASSY AND TAXI-LIGHTS FOR DAMAGE (WITHDOORS OPEN)322100-0502-1 711 NOSE GEAR MEC GVI I: PRE-ACPT MRB AMM 322000/0011 0.20 ALLAMM 324100/601CHECK NOSE LANDING GEAR FOR GENERAL CONDITION,FLUID LEAKAGE,TYRES FOR EVIDENCE OF UNDERINFLATION(DOORS CLOSED)322100-0502-2 711 NOSE GEAR MEC GVI I: DY-TERM MRB AMM 322000/0011 0.10 ALLAMM 324100/601* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)322100-0502-2 * * * * * C O N T I N U E * * * * *CHECK NORMAL EXTENSION AND GENERAL CONDITIONOF SLIDING TUBE,WHEELS AND TYRES FOR DAMAGE,WEAR(DEFORMATION,CUTS,FLAT SPOTS) AND CORRECT PRESSURE322112-0502-1 711 STRUT-NOSE- GEAR SHOCK MEC DET I: 1 C MRB ** AMM 322000/6011 3.00 ALLDETAILED INSPECTION OF NOSE LANDING GEARSTRUCTURE, RELATED COMPONENTS AND ATTACHMENTS (WITHDOORS OPEN) SUCH AS:- STRUT (OUTER CYLINDER) AND BEARINGS,ROTATING TUBE,SLIDING TUBE (INNER CYLINDER) TORQUE LINKS,AXLE(VISIBLE PART ONLY) FOR:CLEANLINESS,CORROSION,PROTECTIVE PAINTWORK,SECURITYOF ATTACHMENT,EXTERNAL LEAKAGE IDENTIFICATION PLATESCORRECTLY ATTACHED,BONDING JUMPERS FOR CORRECT CON-DITION AND FLAKED AREAS ON THE CHROMIUM PLATED RODS322112-0504-1 711 NOSE LANDING GEAR ASSY MEC RAR I: 12000 FC MRB ** AMM 322111/4013 20.00 ALLORREMOVE AND REPLACE FOLLOWING COMPONENTS FOR 8 YEOVERHAUL:- STRUT ASSY - NOSE GEAR SHOCK- ABSORBER - NOSE GEAR SHOCK- STRUT ASSY - NOSE GEAR TELESCOPIC DRAG322112-0504-2 711 NOSE LANDING GEAR ASSY. NDT SDI I: REFER CN CN CN1 0.50 PRE 01257MRB 1987-100-080(B) (32-0383)SPECIAL DETAILED INSPECTION (ULTRASONIC) OF NOSE GEAR ISB 32-0382MHB SBBARREL. SB MHB470-32-605470-32-604322112-0504-3 711 NOSE LANDING GEAR ASSY NDT SDI I: REFER CN CN CN2 3.00 PRE 01257FAA AD 1988-143-088(B) (32-0389) MHB SBSPECIAL DETAILED INSPECTION (ULTRASONIC) OF NOSE GEAR FAA AD 69-23-11 470-32-642LOWER BARREL AREA ISB 32-0388* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)322112-0504-3 * * * * * C O N T I N U E * * * * *SB MHB470-32-641322112-0505-1 710 STRUT-NOSE- GEAR SHOCK MEC LUB I: 3 A MRB AMM 122232/0011 2.00 ALLCLEAN AND LUBRICATE ALL POINTS OF NLG SUCH AS:- STRUT ASSY - NOSE GEAR SHOCK- ABSORBER - NOSE GEAR SHOCK- UPLOCK ASSY - NOSE GEAR DOOR- UPLOCK ASSY - NOSE GEAR- ACTUATING CYLINDER - NOSE GEAR- BRACE STRUT HINGE PIN322114-0505-1 710 ABSORBER-NOSE GEAR SHOCK MEC RPL I: 1 C MRB AMM 121232/0011 0.50 ALLCHECK OF NOSE LANDING GEAR SHOCK ABSORBER CHARGEPRESSURE.322114-0505-2 711 ABSORBER-NOSE GEAR SHOCK MEC RPL I: 2 C MRB AMM 121232/0011 1.00 ALLCHECK NOSE LANDING GEAR FLUID LEVEL AND CHARGEPRESSURE322114-0505-3 711 ABSORBER-NOSE GEAR SHOCK MEC RPL T: NOTE EASA AD EASA AD1 3.00 PRE 13212I: 3200 FC ISB 2008-0052(32-0453)NOSE LANDING GEAR ASSY SHOCK ABSORBER/BARREL OR ISB 32-0447ATTACHMENT BOLTS - INSPECTION 30 MONOTE: REFER TO EASA AD FOR APPLICABLE THRESHOLD322115-0502-1 711 TORQUE LINKS - NOSE GEAR MEC GVI I: 4 C MPD AMM 322115/8011 0.50 ALLCHECK TORQUE LINKS FOR EXESSIVE FREEPLAY322116-0502-1 123 UPLOCK/DRAG STRUT FITTING MEC DET I: 1 C MRB ** AMM 322000/6011 0.25 ALL1241 0.25IN SITU DETAILED INSPECTION OF NOSE GEAR:* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)322116-0502-1 * * * * * C O N T I N U E * * * * *- UPLOCK MECHANICAL LINK AND ATTACH BOLTS (REARATTACHMENT)- TELESCOPIC DRAG STRUT HINGE PINFOR CRACKS AND CORROSION322116-0504-1 120 UPLOCK/DRAG STRUT FITTING MEC RAR I: 12000 FC MRB ** AMM 323121/4011 2.00 ALLOR AMM 323124/401REMOVE FOLLOWING PARTS FROM NOSE GEAR: 8 YE- UPLOCK BOX MECHANICAL LINK AND ASSOCIATED ATTACHBOLTS (REAR ATTACHMENT)- TELESCOPIC DRAG STRUT HINGE PINAND INSPECT FOR WEAR AND CORROSION.NOTE: TASK SHOULD BE ACCOMPLISHED AT THE OPPORTUNITYOF LDG REMOVAL.322200-0502-1 123 NOSE GEAR DOORS MEC LUB I: 1 C MPD AMM 323000/5011 0.70 POST 02328124 SIL 32-0551 0.70 (32-0207)01. DISASSEMBLE, CLEAN AND LUBRICATE NOSE GEAR DOORPRE 11220GROUND OPENING MECHANISM(32-0416)02. LUBRICATE THE TORSION TUBE CENTRE BEARINGS03. REASSEMBLE NOSE GEAR DOOR GROUND OPENINGMECHANISM04. PERFORM GROUND DOOR OPENING AND CLOSING TESTACCESS: 713* 0.06714* 0.06322200-0505-1 123 NOSE GEAR DOORS MEC LUB I: 4 A MPD AMM 122232/0011 0.30 POST 02328124 SIL 32-0551 0.30 (32-0207)LUBRICATION OF THE MECHANICAL LINKAGE OF THEPOST 11220BELLCRANKS OF THE GROUND OPENING CONTROL MECHANISM.(32-0416)ACCESS: 713* 0.06714* 0.06323100-0503-1 210 NORMAL EXTENSION/RETRACTION MEC OPC I: 6400 FH MRB ** AMM 323000/5012 3.00 ALLOPERATIONAL TEST OF RETRACTION (FLIGHT MODE) AND* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)323100-0503-1 * * * * * C O N T I N U E * * * * *INHIBITION OF RETRACTION (GROUND MODE),BY ELECTRICALSYSTEM 1 AND 2,AS FOLLOWS:- GEAR RETRACTION INHIBITION WITH SHOCK ABSORBERSCOMPRESSED (AMM 323000/501 "D. SYSTEM TEST 4.D)- GEAR RETRACTION INHIBITION WITH NOSE WHEEL STEERINGLEFT OR RIGHT(AMM 323000/501 "D. SYSTEM TEST 4.E)- GEAR RETRACTION INHIBITION WITH MAIN GEAR BOGIE(TRUCK) BEAM NOT LEVELED (AMM 323000/501 "D.SYSTEMTEST 4.F)323100-0503-2 210 NORMAL EXTENSION/RETRACTION MEC OPC I: 3 C MRB ** AMM 323000/6011 1.00 ALLCHECK ELECTRIAL CIRCUITS ASSOCIATED WITH LANDINGGEAR NORMAL CONTROL (MICROSWITCH UNIT).323112-0503-1 210 ELECTROVALVE-LANDING GEAR ERI OPC I: 15000 FH MRB ** AMM 323112/6012 0.50 POST 02529ISB 32-0055(32-0228)OPERATIONAL TEST OF ELECTROVALVE LANDING GEARPOST 03083(32-0269)NOTE: ACCOMPLISHMENT OF THIS TASK SATISFIESREQUIREMENTS OF TASK 323112-0503-4323112-0503-2 210 ELECTROVALVE-LANDING GEAR ERI OPC I: 3000 FH MRB ** AMM 323112/6013 1.00 POST 02529ISB 32-0055(32-0228)OPERATIONAL TEST OF ELECTROVALVE LANDING GEARPRE 03083(32-0269)323112-0503-3 210 ELECTROVALVE-LANDING GEAR ERI OPC I: 1000 FH MRB ** AMM 323112/6013 0.50 PRE 02529ISB 32-0055(32-0228)OPERATIONAL TEST OF ELECTROVALVE LANDING GEARPRE 03083(32-0269)323112-0503-4 210 ELECTROVALVE LANDING-GEAR ERI OPC T: 32000 FC CN AMM 323112/6012 0.40 POST 02529I: 2800 FC FAA AD CN 2001-603(B)(32-0228)OPERATIONAL TEST OF ELECTROVALVE LANDING GEAR OR 18 MO FAA ADPOST 030832004-04-10(32-0269)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)323112-0503-4 * * * * * C O N T I N U E * * * * *NOTE: ACCOMPLISHMENT OF THIS TASK SATISFIESREQUIREMENTS OF TASK 323112-0503-1323112-0503-5 210 ELECTROVALVE LANDING-GEAR ERI OPC I: 32000 FC CN AMM 323112/6012 0.40 PRE 02529FAA AD CN 2001-603(B)(32-0228)DISCARD ELECTROVALVE LANDING GEAR FAA AD2004-04-10323114-0503-1 711 NLG - DOOR UPLOCKS MEC FUC T: 3000 LG ISB AMM 323114/6011 1.00 ALLI: 5 A SB MHBCHECK LOAD REQUIRED TO CLOSE UPLOCK HOOK 470-32-206USING DYNAMOMETER323118-0502-1 120 VALVE-NOSE GEAR-SEQUENCE MEC GVI I: 5 A MRB AMM 323118/8011 0.10 ALLCHECK FLEXIBLE DIAPHRAGM OF VALVE-NOSE GEARSEQUENCE (LH/RH) FOR RED WITNESS MARK323124-0502-1 120 NLG - DOWN LOCK INDICATING MEC GVI I: 2 A MRB ** AMM 326100/6011 0.10 ALLCHECK VISUAL INDICATOR FROM ELECTRONIC BAY FORCLEANLINESS,CORROSION,CORRECT INDICATION ANDCLEAN INDICATOR WINDOW323133-0503-1 147 MLG - DOOR UPLOCKS MEC FUC T: 3000 LG ISB AMM 323133/6011 0.30 ALL148 I: 1 C SB MHB1 0.30CHECK LOAD REQUIRED TO CLOSE UPLOCK HOOK 470-32-206USING DYNAMOMETER323200-0503-1 145 EMERGENCY EXTENSION MEC FUC I: 3 C MRB AMM 323200/6011 0.50 ALLCHECK EMERGENCY EXTENSION CONTROL CABLES FORCORRECT TENSION:01. CHECK CABLE TENSION WITH TENSIOMETER (ACCESS241AEF)02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLETENSION REGULATOR IS WITHIN LIMITS.SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)323200-0503-2 121 EMERGENCY EXTENSION MEC FUC I: 3 C MRB AMM 323226/4011 0.40 ALL122 AMM 324500/5011 0.40CHECK EMERGENCY EXTENSION,PARKING AND ULTIMATE AMM 324500/601EMERGENCY BRAKING AND STEERING CONTROL CABLES FOR AMM 325100/601CORRECT TENSION WITH TENSIOMETERACCESS: 132AZ* 0.01323200-0503-3 711 NLG - DOWNLOCK FRICT. CHECK MEC FUC I: 3 C ISB AMM 322100/6012 1.00 ALLISB 32-0353NOTEFRICTION CHECK OF NLG COMPONENTS WITH A/C ON JACKS OR SB MHBNOSE GEAR JACKED UP: 470-32-40901. MEASURE TOTAL FRICTION OF COMPONENTS02. MEASURE FRICTION OF TELESCOPIC STRUT03. MEASURE FRICTION OF NLG-ACTUATOR AND ATTACHEMENT04. PERFORM SWING TEST OF NLG HINGE POINTSNOTE: TASK CANCELLED AFTER EMBODIMENT OF ALLTHE FOLLOWING MODSMOD 1033 (S 6237)/MHB 606MOD 1033 (S 6384)/MHB 657MOD 1257 (S 4482)/MHB 457323200-0503-4 700 EMERGENCY EXTENSION MEC DET I: 1000 FH ISB ISB 32-02982 4.00 PRE 01257SB MHBMHB 384MEASUREMENT OF PRESSURE REQUIRED TO EXTENT THE MAIN 470-32-349GEAR BRACE STRUT ACTUATING CYLINDER ROD.323200-0503-5 210 EMERGENCY EXTENSION MEC FUC I: 2 C MPD AMM 323000/5013 5.00 PRE 01232(32-0072)FUNCTIONAL TEST OF LANDING GEAR EMERGENCY EXTENSIONR 323300-0503-1 210 FREE FALL EXTENSION MEC OPC I: 2000 FH ISB AMM 323000/5012 1.00 POST 02781MRB ** ISB 32-0335(32-0272)OPERATIONAL TEST OF FREE FALL EXTENSION LIMITED TOPRE 03433UNLOCKING OF LANDING GEAR DOORS AND GEAR UPLOCKS (A/CON WHEELS)323300-0503-2 210 FREE FALL EXTENSION MEC FUC I: 3 C MRB ** AMM 323000/5013 5.00 ALL* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)323300-0503-2 * * * * * C O N T I N U E * * * * *FUNCTIONAL TEST OF LANDING GEAR FREE FALL EXTENSIONNOTE: CARRY OUT TOGETHER WITH TASK 325000-0503-1R 323300-0503-4 210 FREE FALL EXTENSION MEC FUC I: 12 MO AOT AMM 323000/5013 0.50 PRE 04443CN AOT 32-14(32-0425)FUNCTIONAL TEST OF LANDING GEAR FREE FALL EXTENSION. FAA AD CN 1997-113-221 POST 02781FAA AD 99-25-15 (32-0272)PRE 03433324111-0504-1 730 WHEELS - MAIN LANDING GEAR MEC DET I: TIRE CHG MRB AMM 123732/0011 0.50 ALL740 SB MHB1 0.5001. DETAILED INSPECTION OF WHEEL HALVES AND 470-32-001TIE-BOLTS FOR GENERAL CONDITION,CRACKS,CORROSIONAND DAMAGE02. DETAILED INSPECTION OF BEARINGS FOR GEN-ERAL CONDITION AND EVIDENCE OF OVERHEATING03. LUBRICATION OF BEARINGS324111-0504-2 730 WHEELS - MAIN LANDING GEAR NDT SDI I: TIRE CHG MRB AMM 123732/0011 2.00 ALL740 SB MHB1 2.00SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF WHEEL 470-32-001HALVES AND MAGNAFLUX INSPECTION OF TIE-BOLTS INACCORDANCE WITH VENDOR RECOMMENDATIONS.324111-0504-4 730 WHEELS.- MAIN LANDING GEAR MEC DET I: 4 C MPD AMM 324227/4012 2.00 ALL7402 2.00DETAILED INSPECTION OF SLEEVE AND AXLE FORSATISFACTORY CONDITION.PREP.: REMOVE AXLE SLEEVES.324111-0504-5 730 WHEELS - MAIN LANDING GEAR MEC GVI I: BRAKE MPD AMM 324227/4011 0.10 ALL740 UNIT CHG1 0.10GENERAL VISUAL INSPECTION OF MAIN WHEEL AXLE SLEEVEFOR SHOCKS, CORROSION, CHROME PLATING DAMAGE ANDOVERHEATING.SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)324112-0504-1 710 WHEEL NOSE LANDING GEAR MEC DET I: TIRE CHG MRB AMM 123732/0011 0.20 ALLSB MHB01. DETAILED INSPECTION OF WHEEL HALVES AND 470-32-001TIE-BOLTS FOR GENERAL CONDITION,CRACKS,CORROSIONAND DAMAGE02. DETAILED INSPECTION OF BEARINGS FOR GEN-ERAL CONDITION AND EVIDENCE OF OVERHEATING03. LUBRICATION OF BEARINGS324112-0504-2 710 WHEEL-NOSE LANDING GEAR NDT SDI I: TIRE CHG MRB AMM 123732/0011 0.50 ALLSB MHBSPECIAL DETAILED INSPECTION (EDDY CURRENT) OF WHEEL 470-32-001HALVES AND MAGNAFLUX INSPECTION OF TIE-BOLTS INACCORDANCE WITH VENDOR RECOMMENDATIONS.324200-0503-1 210 STAND-BY BRAKING MEC OPC I: 1 C MRB ** AMM 324300/5012 0.50 POST 01033ISB 32-0373MHB 423OPERATIONAL TEST OF STAND-BY BRAKING SYSTEMNCE:324200-0503-2 210 NORMAL BRAKING MEC OPC I: 1 C MRB ** AMM 324200/5012 0.50 POST 01430(32-0143)OPERATIONAL TEST TO CHECK AUTOBRAKE MAX. MODEORENGAGEMENTPOST 02340(32-0415)324200-0503-3 210 STANDBY BRAKING MEC OPC I: 1 A MRB ** AMM 324300/5011 0.50 ALLOPERATIONAL TEST OF STANDBY BRAKING SYSTEM324200-0505-1 121 NORMAL BRAKING MEC RPL I: 2 A MRB AMM 121232/0011 0.25 ALLCHECK FLUID LEVEL IN BRAKE RESERVOIR ANDTOP-UP AS NECESSARYACCESS: 132AZ* 0.01SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)324200-0505-2 147 NORMAL BRAKING MEC CLN I: 3 C MRB AMM 324212/3011 1.00 ALLCHECK BRAKE SYSTEM FILTER ELEMENT 1298 (NORMALBRAKING SYSTEM-GREEN HYDRAULIC):- REMOVE FILTER ELEMENT AND INSPECT FOR SATISFACTORYCONDITION AND PARTICLES- INSTALL A NEW OR CLEAN FILTER ELEMENTACCESS: 147SZ* 0.02324227-0502-1 731 BRAKE UNIT MEC GVI I: WEEKLY MRB AMM 324227/6011 0.10 ALL7411 0.10CHECK BRAKES FOR WEAR324227-0504-1 730 BRAKE UNIT MEC DET I: BRAKE MRB AMM 324227/4011 0.50 ALL740 UNIT CHG AMM 324227/6011 0.50DETAILED INSPECTION OF WHEEL AXLE, BRAKEHOUSING AND TORQUE TUBES FOR SATISFACTORY CONDITION,CRACKS AND FOR EXTERNAL LEAKAGE.324247-0502-1 122 TRANSMIT-BRAKE PEDAL POSIT. MEC DET I: WEEKLY CN AMM 324200/6011 0.70 PRE 03101FAA AD CN(32-0267)DETAILED CHECK OF REAR ATTACHMENTS OF 1980-151-027(B)BRAKE PEDAL TRANSMITTER SUPPORT FOR CRACKS FAA AD 80-16-52ISB 32-0264ACCESS: 132AZ* 0.01324257-0503-1 700 ANTI-SKID TACH.GENERATORS MEC OPC I: 3 C MPD AMM 324200/5011 0.50 ALLOPERATIONAL TEST OF BRAKE ANTI-SKID SYSTEM.324272-0503-1 210 CONTROL BOX,BRAKE SYSTEM MEC OPC I: 1 A MRB AMM 324272/4011 0.10 ALLTEST OF ANTI-SKID SYSTEM 1 & 2SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)324314-0505-1 148 EMERGENCY BRAKE DISTRIBUTION - DUAL MEC SER I: 4 A CN AMM 324314/6011 0.20 POST 12012VALVE FAA AD CN(32-0429)1998-263-255(B)DRAIN WATER ACCUMULATION IN THE DRAIN TUBE OF THE FAA ADBRAKE DUAL DISTRIBUTION VALVE (BDDV). 2001-15-10324500-0503-1 210 PARK/ULTIMATE EMERGENCY BRAKING MEC OPC I: 1 C MRB ** AMM 324500/5012 0.50 ALLOPERATIONAL TEST OF PARKING AND ULTIMATE EMERGENCYBRAKING SYSTEM.325000-0503-1 210 STEERING MEC FUC I: 3 C MRB ** AMM 325100/5011 0.50 POST 02862(32-0336)FUNCTIONAL TEST OF ELECTRO/HYDRAULIC SELECTOR VALVEPOST 03070WITH ELECTRICAL POWER ALTERNATIVELY SUPPLIED THROUGH(32-0265)MICROSWITCHES ASSOCIATED WITH ENGINE 1 AND 2 HP FUELLEVERS (HP FUEL LEVERS ALTERNATIVELY SET TO "ON" THENTO "OFF" POSITION).NOTE: CARRY OUT TOGETHER WITH TASK 323300-0503-2325000-0503-2 210 STEERING MEC FUC I: 3 C MRB AMM 325100/5011 0.50 PRE 02862(32-0336)FUNCTIONAL TEST OF ELECTRO/HYDRAULIC SELECTOR VALVESPOST 03070(GREEN/YELLOW HYDRAULIC SYSTEM) WITH ELECTRICAL POWER(32-0265)ALTERNATIVELY SUPPLIED THROUGH MICROSWITCHESASSOCIATED WITH ENGINE 1 AND 2 HP FUEL LEVERS (HPFUEL LEVERS ALTERNATIVELY SET TO OFF POSITION) MOD3070 EMBODIED325000-0503-3 210 STEERING MEC FUC I: 6 C MPD AMM 325100/5011 0.50 PRE 02862(32-0336)FUNCTIONAL TEST OF ELECTRO/HYDRAULIC SELECTOR VALVESPRE 03070(GREEN/YELLOW HYDRAULIC SYSTEM)(32-0265)325100-0502-1 710 STEERING MEC GVI I: 4400 FH ISB ISB 27-01071 0.20 MACHINED PULLEYSGENERAL VISUAL INSPECTION OF MACHINED NOSE GEAREMERG/ULTIMATE EMERG. EXTENSION, PARKING BRAKE ANDNOSE GEAR WHEEL STEERING CONTROL PULLEYS FOR HYDR.* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)325100-0502-1 * * * * * C O N T I N U E * * * * *FLUID CONTAMINATION.326100-0503-1 210 INDICATING AND WARNING ERI OPC I: 2400 FH MRB ** AMM 326100/5011 0.20 ALLOPERATIONAL TEST OF AURAL WARNING MICROSWITCH ONSYSTEM 1 AND 2326112-0503-1 122 MODUL UNIT-PROX.DETECTOR ERI FUC I: 600 FH MRB ** AMM 320000/5011 0.50 ALLCONTINUITY TEST OF MODUL UNIT-PROXIMITY DETECTOR.ACCESS: 132AZ* 0.01* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION:2-32 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)331300-0503-1 210 INSTRUMENT AND PANEL INTEGRAL LIGHTING ERI OPC I: 700 FH EUAD AMM 331300/5011 0.20 POST 12513FAA AD EUAD 2006-0370(31-0077)OPERATIONAL CHECK OF STANDBY HORIZON INTEGRAL FAA ADLIGHTING LOGIC. 2005-20-06331500-0503-1 210 MASTER WARNING ERI OPC I: DY-TERM MRB ** AMM 331400/5011 0.20 ALLCHECK LIGHTS OF MASTER WARNING SYSTEM ANDANNOUNCIATOR PANEL331500-0503-2 210 MASTER WARNING ERI OPC I: 2 A MRB ** AMM 331500/5011 0.33 ALLOPERATIONAL TEST OF MASTER WARNING SYSTEM332100-0502-1 200 GENERAL ILLUMINATION ERI GVI I: 1 A MPD AMM 332600/5011 1.00 ALLCHECK ALL INTERNAL FLIGHT COMPARTMENT AND PASSENGERCOMPARTMENT LIGHTS (INCLUDING FASTEN SEAT BELT /NO SMOKING SIGNS) FOR BURNT OUT BULBS, MISSING SPAREBULBS AND FUSES (SPARE BOX)334000-0502-1 100 EXTERIOR LIGHTS ERI GVI I: WEEKLY MRB AMM 334300/6011 0.30 ALLAMM 334900/501CHECK RUNWAY TURNOFF LIGHTS AND WING/ENGINE SCANLIGHTS FOR DAMAGE, GENERAL CONDITION AND FOR BURNTOUT BULBS334000-0502-2 500 EXTERIOR LIGHTS ERI GVI I: WEEKLY MRB AMM 334100/6011 0.10 ALL600 AMM 334200/5011 0.10CHECK LANDING/TAKEOFF, NAVIGATION/TOWING LIGHTS AMM 334600/501FOR DAMAGE, GENERAL CONDITION AND FOR BURNT OUT BULBS334000-0502-3 300 EXTERIOR LIGHTS ERI GVI I: WEEKLY MRB AMM 334700/0011 0.10 ALLCHECK EXTERIOR LIGHTS OF AFT FUSELAGE FOR DAMAGE,GENERAL CONDITION AND FOR BURNT OUT BULBSSYSTEMS AND POWERPLANT PROGRAM : LIGHTS REV. DATE: APR 01/10 SECTION:2-33 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)335100-0502-1 200 PASS COMPT EMERGENCY LIGHT ERI GVI I: 1 C MRB AMM 335100/5011 0.75 ALLCHECK PASSENGER COMPARTMENT EMERGENCY LIGHTS FORFAILED BULBS335100-0503-1 200 PASS COMPT/EXT EMERG LIGHT ERI FUC I: 6 C MRB ** AMM 335100/5012 2.00 ALLFUNCTIONAL TEST OF ELECTRICAL CIRCUITS AND INVERSEBREAKDOWN CHARACTERISTICS OF DIODES335100-0503-2 200 PASS COMPT/EXT EMERG LIGHT ERI OPC I: WEEKLY MRB ** AMM 335100/5011 0.10 ALLOPERATIONAL TEST OF PASSENGER COMPARTMENT EMERGENCYLIGHTING (28V/6V).335100-0503-3 200 PASS COMP/EXT EMERG LIGHT ERI OPC I: 1 A MPD AMM 335100/5011 0.20 PRE (33-0113)EXCL. F4OPERATIONAL TEST OF EMERGENCY ESCAPE PATH MARKINGLIGHTING.335100-0504-1 200 PASS COMPT/EXT EMERG LIGHT ERI RAR I: 2 YE MRB ** AMM 335111/3011 5.00 ALLAMM 335114/401REMOVE PASSENGER CABIN EMERGENCY LIGHT BATTERIESFOR BENCH TEST AND CHECK CAPACITY.* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : LIGHTS REV. DATE: APR 01/10 SECTION:2-33 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)340000-0502-1 100 NAVIGATION-GENERAL ELO GVI I: DY-TERM MRB WDM 910004/0011 0.20 ALLCHECK ANTENNAS FOR DAMAGE (VHF 1, MARKER BEACON,DME, ATC, GLIDE, TCAS).341100-0502-1 100 AIR DATA-PRESSURE SYSTEM ELO GVI I: 1 A MRB AMM 273615/6011 0.33 ALLAMM 341115/601CHECK PITOT PROBES, STATIC PORTS, TEMPERATURE SENSORS AMM 341116/601AND ANGLE OF ATTACK SENSORS FOR SECURITY OF AMM 341218/601ATTACHMENT, SATISFACTORY CONDITION AND CLEAR APPEAR-ENCE OF MARKINGS AND PLACARDS341100-0503-1 100 AIR DATA-PRESSURE SYSTEM ELO FUC I: 1 C MRB AMM 122434/0011 4.00 ALLAMM 341110/501DRAIN AND LEAK TEST OF PITOT AND STATIC SYSTEM.ENSURE VALVE IS PROPERLY SEATED AFTER DRAINING.ACCESS: 133AL 133BL 133CL* 0.11341100-0505-1 100 AIR DATA-PRESSURE SYSTEM ELO CLN I: 2 C MRB AMM 341110/3012 2.50 ALLNOTE SIL 34-084FLUSHING OF PITOT AND STATIC SYSTEM(AFTER FLUSHING PERFORM LEAK TEST)NOTE: INTERVAL 2C-CHECK RECOMMENDED BUT CAN BEADJUSTED WITH EXPERIENCE TO SUIT OPERATINGENVIRONMENTACCESS: 133AL 133BL 133CL* 0.11341120-0503-1 210 AIR DATA-COMPUTATION ELO OPC I: 2 A MRB ** AMM 341120/5011 0.50 NON FWD-FACEBITE TEST OF AIR DATA COMPUTER, INDICATORS ANDOVERSPEED FUNCTION SYSTEM 1+2.341134-0503-1 120 AIR DATA COMPUTER ELO OPC I: 2 A MRB AMM 341800/5011 0.25 POST 02688FWD FACEBITE TEST OF HYBRID AIR DATA COMPUTER SYSTEM 1 AND 2TO COVER OPERATIONAL TEST OF FOLLOWING FUNCTIONS:* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION:2-34 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)341134-0503-1 * * * * * C O N T I N U E * * * * *- OVERSPEED- MACH AIRSPEED (NORMAL MASI)- VERTICAL SPEED (VSI)- TAS AND TAT/SAT- ALTITUDE (ALTIMETER MAIN)CHECK INDICATIONS, LIGHTS AND FLAGS ON RESPECTIVEINDICATORS342100-0503-1 210 MAGNETIC HEADING REFERENCE ELO OPC I: 2 C MRB AMM 342100/5011 0.50 NON FWD-FACEOPERATIONAL TEST OF COMPASS AND MAGNETIC HEADINGSYSTEM; INCLUSIVE COMPASS SWITCHING DEVICE.342122-0503-1 210 INDICATOR-HORIZONTAL SITU. ELO OPC I: 3 A MRB AMM 342100/5011 0.50 NON FWD-FACEOPERATIONAL TEST OF HSI MAGNETIC MODE AND MONITORING.342400-0503-1 210 SPEED REFERENCE SYSTEM ELO OPC I: 1 C MRB ** AMM 342400/5011 0.50 POST 01510(22-0017)OPERATIONAL TEST OF ALPHA-FLOOR PROTECTION.NON-FWD FACE342400-0503-2 210 SPEED REFERENCE SYSTEM ELO FUC I: 2 C MRB ** AMM 342400/5011 0.50 POST 01510(22-0017)FUNCTIONAL TEST OF SRS COMPUTER FOR CORRECT OPERATIONNON-FWD FACEOF SLAT INSTRUMENTATION UNIT, FLAP MICROSWITCHES ANDMAIN GEAR RELAYS342400-0503-3 210 SPEED REFERENCE SYSTEM ELO OPC I: DY-TERM MRB ** AMM 342400/5011 0.20 NON FWD-FACECHECK SPEED REFERENCE SYSTEM ENGAGEMENT342500-0503-1 210 ATTITUDE AND HEADING SYSTEM ELO OPC I: 5 A MRB AMM 342000/5011 0.20 POST 02688PRE 11862BITE TEST OF ATTITUDE AND HEADING REFERENCE SYSTEMS(34-0150)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION:2-34 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)342500-0503-1 * * * * * C O N T I N U E * * * * *(AHRS 1, 2 AND 3) TO COVER OPERATIONAL TEST OFFWD FACEFOLLOWING FUNCTIONS:- ATTITUDE (ADI)- HEADING (HSI AND RDMI)- GROUND SPEED (AHRS/ONS GROUND SPEED DISPLAY ONONS CONTROL DISPLAY UNIT)- VERTICAL SPEED (VSI)- INSTRUMENTS SWITCHING (SYS 3)CHECK INDICATIONS, LIGHTS AND FLAGS ON AHRU ANDRESPECTIVE INDICATORS.342500-0503-2 210 INERTIAL REFERENCE SYSTEM ELO OPC I: 1 C MRB AMM 342000/5011 0.50 POST 11862(34-0150)OPERATIONAL TEST OF "ATT" SWITCHING (DATA SUPPLY FROMIRS 3) THROUGH "ATT/SYS 3" PUSH BUTTONS ON CAPT ANDF/O SWITCHING PANEL.342500-0504-1 121 INERTIAL NAVIGATION UNIT ELO RAR I: 1 C MPD SIL 34-0551 0.10 DELCO UNIT01. REMOVE INERTIAL NAVIGATION UNITS02. CLEAN AIR FILTER OF EACH INU IN THE WORKSHOP03. INSTALL INERTIAL NAVIGATION UNITSACCESS: 132AZ* 0.01342523-0503-1 210 INDICATOR-ATTITUDE DIRECTOR ELO OPC I: WEEKLY MRB ** AMM 342523/4011 0.10 NON FWD-FACEBITE TEST OF ATTITUDE DIRECTOR INDICATOR.342538-0504-1 121 BATTERY - ISS/INS ELO RAR I: NOTE 5-1 MRB ** AMM 342538/4011 3.00 PRE 12009SIL 34-005(34-0159)REMOVE BATTERY FOR RESTORATION / CAPACITY CHECK (SHOPVISIT). CLEAN BATTERY UNIT SHELF.NOTE: INTERVAL SHOULD BE IN ACCORDANCE WITH THEVENDOR RECOMMENDATIONS.ACCESS: 132AZ* 0.01SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION:2-34 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)342723-0503-1 210 DIGITAL ATTITUDE DIRECTOR INDICATOR ELO OPC I: WEEKLY MPD AMM 342500/5011 0.10 POST 02688FWD FACETEST OF A.D.I. 1 AND 2 BY MEANS OF PUSH-TO-TESTBUTTON343600-0503-1 210 ILS (INSTR. LANDING SYSTEM) ELO OPC I: 2 A MRB ** AMM 343600/5011 0.30 NON FWD-FACEOPERATIONAL TEST OF INSTRUMENT LANDING SYSTEM BY BITE343600-0503-2 210 ILS (INSTR. LANDING SYSTEM) ELO OPC I: 2 A MRB AMM 343600/5011 0.30 POST 02688AMM 343636/401FWD FACEBITE TEST OF ILS 1 AND 2 TO COVER OPERATIONAL TEST OFFOLLOWING FUNCTIONS:- ILS RECEPTION AND INDICATION (ADI,HSI)- OPERATIONAL TEST OF DIGITAL/ANALOGIC CONVERTERFOR GPWS AND FDAU.CHECK INDICATIONS,LIGHTS AND FLAGS ON RECEIVERSAND RESPECTIVE INDICATORS.344200-0503-1 210 RADIO ALTIMETER ELO OPC I: 2 A MRB ** AMM 344200/5011 0.25 ALLSELF TEST OF SYSTEM 1 AND 2 USING THE TEST KNOB ONINDICATORS.N 344200-0503-2 150 RADIO ALTIMETER MEC CLN I: 6 MO SIL AMM 20-31-001 0.20 ALLPAGE1RADIO ALTIMETER ANTENNAS EXTERNAL SURFACE TO BE SIL 34-099CLEANED.344243-0503-1 152 FAN - RADIO ALTIMETER ELO OPC I: 1 C MRB AMM 344200/5011 0.17 POST 02066(34-0049)AURAL OPERATIONAL TEST OF RADIO ALTIMETER TRANSCEIVERCASE COOLING FAN344800-0503-1 210 GROUND PROXIMITY WARNING SYSTEM ELO FUC I: 1 C MPD AMM 344800/5011 0.20 PRE 10293(34-0121)FUNCTIONAL TEST OF GPWC MODESORPRE 10617* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION:2-34 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)344800-0503-1 * * * * * C O N T I N U E * * * * *(34-0126)344800-0503-2 210 GROUND PROX.WARNING SYSTEM ELO OPC I: 2 A MRB ** AMM 344800/5011 0.25 ALLOPERATIONAL TEST OF GPW SYSTEM BY BITE345100-0503-1 210 DME (DISTANCE MEASUR.EQUIP) ELO OPC I: 2 A MPD AMM 345100/5011 0.17 POST 02688FWD FACEBITE TEST OF DME 1 AND 2 TO COVER OPERATIONAL TEST OFFOLLOWING FUNCTIONS:- DME INTERROGATION AND INDICATION (RDMI,HSI)CHECK INDICATIONS,LIGHTS AND FLAGS ONTRANSCEIVERS AND INDICATORS.345233-0503-1 200 ATC TRANSPONDER ELO FUC I: 2 YE MPD AMM 345200/5011 0.50 FAAFUNCTIONAL TEST AS PER FAR 91.413NOTE: TASK APPLICABLE TO AIRCRAFT OPERATED UNDERFAA REQUIREMENTS345300-0503-1 210 ADF (AUTOMAT.DIRECT.FIND.) ELO OPC I: 2 A MRB ** AMM 345300/5011 0.25 NON FWD-FACEOPERATIONAL TEST OF ADF SYSTEM BY BITE345300-0503-2 210 ADF (AUTOMAT.DIRECT.FIND.) ELO OPC I: 2 A MRB AMM 345300/5011 0.17 POST 02688FWD FACEBITE TEST OF ADF 1 AND 2 TO COVER OPERATIONAL TEST OFFOLLOWING FUNCTIONS:- ADF RECEPTION AND INDICATION (HSI)CHECK INDICATIONS,LIGHTS AND FLAGS ON RECEIVERSAND INDICATORS.345500-0503-1 210 VOR (VHF OMNI RANGE) ELO OPC I: 2 A MRB ** AMM 345500/5011 0.50 NON FWD-FACE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION:2-34 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)345500-0503-1 * * * * * C O N T I N U E * * * * *OPERATIONAL TEST OF VOR SYSTEM BY BITE345500-0503-2 210 VOR (VHF OMNI RANGE) ELO OPC I: 2 A MRB AMM 345500/5011 0.17 POST 02688FWD FACEBITE TEST OF VOR 1 AND 2 TO COVER OPERATIONAL TEST OFFOLLOWING FUNCTIONS:-VOR RECEPTION AND INDICATION(RDMI,HSI COURSE POINTER)-MARKER BEACON MONITORINGCHECK INDICATIONS,LIGHTS AND FLAGS ONRECEIVERS AND INDICATORS.345600-0503-1 210 OMEGA NAVIGATION SYSTEM ELO OPC I: 2 A MPD AMM 345600/5011 0.17 POST 02139POST 03500TEST OF ONS 1 AND 2 USING THE TEST KNOB ON ONSPRE 11639CONTROL DISPLAY UNITS.(35-0143)* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION:2-34 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)351111-0502-1 132 CYLINDER - OXYGEN STORAGE INS GVI I: 1 A MRB AMM 351300/6011 0.33 ALLCHECK CREW OXYGEN BY COMPARING PRESSURE INDICATORWITH GAUGES ON OXYGEN CYLINDERS IN FWD CARGOCOMPARTMENT.351111-0504-1 132 CYLINDER - OXYGEN STORAGE INS RAR I: NOTE 5-3 MRB ** AMM 351111/4011 2.00 ALLORREMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST 3 YEACCESS: 132BZ* 0.10351200-0502-1 132 OXYGEN DISCHARGE DISCS INS GVI I: DY-TERM MRB AMM 351100/6011 0.10 ALLCHECK OXYGEN DISCHARGE DISCS ARE MAINTAINEDON INDICATORS351200-0503-1 132 OXYGEN DISTRIBUTION INS FUC I: 2 C MRB AMM 351000/5011 1.50 ALLLEAK TEST OF CREW OXYGEN SYSTEM:01. CLOSE OXYGEN CYLINDER VALVE (ZONE 132)02. MONITOR AT COCKPIT OXYGEN GAGES FOR CONSTANTPRESSURE (ZONE 210)03. OPEN OXYGEN CYLINDER VALVE (ZONE 132)ACCESS: 132BZ 132CZ* 0.20351241-0502-1 210 MASK ASSY-CREW OXYGEN INS GVI I: 1 C MRB AMM 351241/7011 0.30 ALLGENERAL VISUAL INSPECTION OF CREW OXYGEN MASK (MASKOUT OF THE BOX) FOR CLEANLINESS AND SATISFACTORYCONDITION351241-0502-2 210 MASK ASSY - CREW OXYGEN MEC GVI I: 6 MO ISB AMM 351241/4011 0.50 PRE 08762ISB 35-0009(35-0010)GENERAL VISUAL INSPECTION OF QUICK DONNING MASKREGULATORS FOR RETENTION OF MASK SHELL ON REGULATOR.PREP.: REMOVE CREW OXYGEN MASK ASSEMBLY BOXES.SYSTEMS AND POWERPLANT PROGRAM : OXYGEN REV. DATE: APR 01/10 SECTION:2-35 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)351241-0503-2 210 MASK ASSY-CREW OXYGEN INS OPC I: DY-TERM MRB ** AMM 351241/5011 0.10 ALL"IN SITU" OPERATIONAL TEST OF CREW OXYGEN MASKASSEMBLY351241-0504-1 210 MASK ASSY-CREW OXYGEN INS FUC I: 4 YE MRB AMM 351241/4011 0.42 ALLREMOVE QUICK DONNING OXYGEN MASKS AND PERFORMFUNCTIONAL TEST OF DEMAND REGULATOR ASSEMBLY(OFF AIRCRAFT)352000-0503-1 200 PASSENGER OXYGEN SYSTEM INS FUC I: 6 C MRB ** AMM 352100/5012 16.00 ALLU1. FUNCTIONAL TEST OT AUTOMATIC RELEASE OF PASSENGEROXYGEN MASKS02. DETAILED INSPECTION OF MASKS, GENERATORS(INCLUSIVE SENSITIVE TAPE) AND RELEASE CATCHESNOTE: TO BE ACCOMPLISHED WITH 352000-0503-2.352000-0503-2 200 PASSENGER OXYGEN SYSTEM INS OPC I: 2 C MRB ** AMM 352100/5011 3.00 ALLOPERATIONAL TEST OF PASSENGER MASK RELEASE:01. SET ALL DOOR STOPS OF EMERGENCY OXYGEN CONTAINERSTO THE "TEST" POSITION02. ON "PASSENGER OXYGEN PANEL" SET GUARDED SWITCHTO "MANUAL OVERRIDE" POSITION AND CHECK THATINDICATOR LIGHT "SYS.ACTUATED" COMES ON.03. CHECK THAT ALL DOORS OF EMERGENCY OXYGEN CONTAIN-ERS OPEN TO MAXIMUM PERMITTED BY DOOR STOPS04. ON "PASSENGER OXYGEN PANEL" PRESS "RESET" PUSHBUTTON AND CHECK THAT INDICATOR LIGHT GOES OFF.05. CLOSE DOORS OF ALL EMERGENCY OXYGEN CONTAINERSBY DEPRESSING THE SPRING LOADED LATCH WITH THEMANUAL RELEASE TOOLNOTE: TO BE ACCOMPLISHED WITH 352000-0503-1352000-0504-1 200 PASSENGER OXYGEN SYSTEM INS RAR I: NOTE 5-1 MRB ** AMM 352113/4012 30.00 ALLSIL 35-003REMOVE AND REPLACE OXYGEN GENERATORS* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : OXYGEN REV. DATE: APR 01/10 SECTION:2-35 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)352000-0504-1 * * * * * C O N T I N U E * * * * *353000-0502-1 200 PORTABLE OXYGEN INS GVI I: 1 C MRB AMM 353121/7011 1.17 ALLVISUAL INSPECTION OF FULL FACE SMOKE MASK FORSATISFACTORY CONDITION - CLEAN MASK AND CONTAINER IFNECESSARY353000-0502-2 200 PORTABLE OXYGEN INS GVI I: WEEKLY MRB AMM 353111/6011 0.10 ALLCHECK PRESSURE OF PORTABLE OXYGEN BOTTLES AT GAUGE(CORRECT PRESSURE IS 1850 PSI AT 20 DEGREES CELSIUS)353000-0503-1 200 PORTABLE OXYGEN INS OPC I: 3 C MRB ** AMM 353100/5011 1.84 ALLOPERATIONAL TEST OF PORTABLE OXYGEN SUPPLY ANDREGULATION:01. TURN REGULATOR "ON-OFF VALVE" TO "ON" POSITION02. CONNECT MASK TO THE DEMAND REGULATOR, PUT MASK ONAND BREATH IN TO ENSURE THAT REGULATOR OPERATESCORRECTLY03. DISCONNECT MASK AND STORE IN CONTAINER04. TURN REGULATOR "ON-OFF VALVE" TO "ON" POSITION353000-0504-1 200 PORTABLE OXYGEN INS RAR I: NOTE 5-3 MRB ** AMM 353111/6011 2.75 ALLORREMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST 5 YE* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : OXYGEN REV. DATE: APR 01/10 SECTION:2-35 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)361100-0503-1 210 ENGINE BLEED AIR - TEMP.HI. ERI OPC I: 2 C MRB AMM 361100/5011 0.17 NON FWD-FACEOPERATIONAL TEST OF TEMP HI WARNING CIRCUIT361100-0503-2 210 ENGINE BLEED AIR SUPPLY SYS ENG OPC I: 3 A MRB AMM 361100/5011 0.17 ALLOPERATIONAL TEST OF PNEUMATIC SYSTEM CONTROLLER BYBITE361100-0503-3 210 ENGINE BLEED AIR SUPPLY SYS ENG OPC I: 5 A MRB ** AMM 361100/5011 0.25 NON FWD-FACEOPERATIONAL TEST OF MANIFOLD FAULT WARNING WITH BLEEDVALVE CONTROL SWITCH IN AUTO POSITION361100-0503-4 210 ENGINE BLEED AIR SUPPLY SYS ERI OPC I: 5 A MRB ** AMM 361100/5011 0.25 FWD-FACEOPERATIONAL TEST OF MANIFOLD "LEAK" WARNING WITHBLEED VALVE IN "AUTO" CONTROL MODE361111-0503-1 210 VALVE ISOLATION ERI OPC I: 2 A MRB AMM 361100/5011 0.17 NON FWD-FACEOPERATIONAL TEST OF ENGINE BLEED AIR ISOLATION VALVE("X"-BLEED VALVE) IN "AUTO NORM" AND "AUTO ALT"POSITION361111-0503-2 210 VALVE ISOLATION ERI OPC I: 2 A MRB AMM 361100/5011 0.17 FWD-FACEOPERATIONAL TEST OF ENGINE BLEED AIR ISOLATION ANDCROSS BLEED VALVE ("X"-BLEED VALVE) IN "AUTO" AND"MAN" (MANUAL) CONTROL MODES361113-0504-1 410 LP CHECK VALVE MEC RAR I: 3000 FH MPD AMM 360000/4011 0.50 GARRETT420 SB GARRETT1 0.50 P/N 123894-1CHECK THE FLAPPER BUSHING/HINGE PIN FOR WEAR. 123894-36-1215123894-2SIL 36-026123940-1PREP.: VALVE TO BE REMOVED.SYSTEMS AND POWERPLANT PROGRAM : PNEUMATIC REV. DATE: APR 01/10 SECTION:2-36 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)361113-0504-2 410 LP CHECK VALVE MEC CHK T: ENG. CHG ISB AMM 360000/4011 0.30 GARRETT420 OR SB GARRETT1 0.30 P/N 123894-1CHK STOP TUBE FOR WEAR. 1200 HSN 123894-36-1215123894-2I: 3000 FH SIL 36-026123940-1(UP TO S/N1380)361115-0502-1 410 PRECOOLER - BLEED AIR MEC DET T: 8000 FH ISB AMM 361100/6012 2.50 PRE 10756420 I: 1 C ISB 36-00312 2.50 (36-0032)DETAILED INSPECTION OF THE PRECOOLER DUCTS.ACCESS: 413BL* 0.01423BL* 0.01361116-0502-1 450 VALVE-FAN AIR MEC DET T: 4 C MPD AMM 361116/6011 2.00 GE460 I: 1 C SIL 36-0231 2.00DETAILED INSPECTION OF VORTEX GENERATORASSEMBLY FOR INTEGRITY AND ABSENCE OF CRACKSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05361117-0503-1 413 VALVE-PNEUMA SYS OVERPRESS. ERI FUC I: 2 C MRB ** AMM 361117/5011 1.00 ALL4231 1.00FUNCTIONAL TEST OF PNEUMATIC SYSTEM OVERPRESSUREVALVEACCESS: 413FL 423FL* 0.77414CR 424CR* 0.80361119-0502-1 453 ENGINE BLEED PRESS.SEN.LINE MEC DET I: 2 A MPD AMM 361114/6011 0.30 GE4631 0.30 PRE 04770DETAILED INSPECTION OF ENGINE BLEED PRESSURE(36-0024)SENSING LINE FOR EVIDENCE OF CRACKS.NOTE: PAY PARTICULAR ATTENTION TO SLIGHT CONTOURVARIATIONS (WAVES) AND SURFACE (SCORES ANDSMALL FOLDS)ACCESS: 451AL* 0.01461AL* 0.01SYSTEMS AND POWERPLANT PROGRAM : PNEUMATIC REV. DATE: APR 01/10 SECTION:2-36 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)361121-0503-1 471 SENSOR-PNEUMA SYS TEMP CONT ERI FUC I: 4 C MRB AMM 361121/4011 1.00 ALL4821 1.0001. REMOVE TEMPERATURE CONTROL SENSOR.02. CLEAN SENSOR AND INSPECT FOR SATISFACTORYCONDITION.03. PERFORM FUNCTIONAL TEST.04. RE-INSTALL SENSOR.05. PERFORM BITE TEST OF PNEUMATIC SYSTEM CONTROLLER.ACCESS: 471AL* 0.35482AR* 0.35361200-0503-1 100 APU BLEED AIR SUPPLY SYSTEM ENG OPC I: 4 C MRB AMM 361200/6012 4.00 ALL300 AMM 361211/6012 4.0001. LEAK CHECK OF APU BLEED AIR SUPPLY DUCTING02. OPERATIONAL CHECK OF APU BLEED AIR LP-CHECK VALVEBY OPERATING MANUALLY THE FLAPPERS FOR FREEDOM OFMOVEMENT03. VISUAL INSPECTION OF COMPONENTS (CHECK-VALVES,DUCTS, COUPLINGS) FOR GENERAL CONDITION,CLEANLINESS AND SECURITY OF ATTACHMENTS.ACCESS: 147FZ 151MF 161AF* 0.41312AR 313AL 315AL 316AR* 0.20361311-0502-1 143 GROUND CONNECTOR-HP ENG DET I: 4 C MRB AMM 361300/6011 0.25 ALLDETAILED INSPECTION OF GROUND CONNECTOR WITHNIPPLE-CHECK VALVE ASSEMBLY FOR SATISFACTORYCONDITION, SECURITY OF CAP AND ATTACHMENT CHAIN ANDCLEANLINESS.ACCESS: 143FL* 0.01361415-0505-1 512 VALVE-LEADING EDGE VENT. MEC LUB I: 5 A MPD AMM 122257/0011 0.33 PRE 043076121 0.33 (36-0014)LUBRICATE SPRING STRUT PLUNGER OF VENTILATIONVALVEACCESS: 512EB* 0.05612EB* 0.05* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : PNEUMATIC REV. DATE: APR 01/10 SECTION:2-36 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)381100-0505-1 100 WATER STORAGE, DISTRIBUTION MEC RPL I: 2 A MRB AMM 381000/3011 1.50 ALLOR AMM 381200/50101. FLUSH, REFILL AND STERILIZE THE POTABLE WATER NOTE 5-3SYSTEM (INCLUDING WATER TAPS) AND- CLEAN WASTE WATER PIPES IF NECESSARY -02. PERFORM OPERATIONAL TEST OF POTABLEWATER SYSTEMACCESS: 122BR 172BR* 0.02383000-0503-1 200 WASTE DISPOSAL MEC CLN I: 2 C MPD AMM 383000/3011 2.00 ALLCLEAN TOILET VENT LINES OF ALLLAVATORIESACCESS: TOILET SHROUD383100-0502-1 200 TOILET SYSTEM MEC GVI I: 1 C SIL SIL 38-0131 0.30 RECIRCTOILETSVISUAL CHECK OF WASTE HOLDING TANK, LAVATORY FLOORAND WASTE LINE CONNECTION FOR SIGNS OF "BLUE FLUID"LEAKAGE AND CHECK OF ADJACENT UNDERFLOOR AREA.PREP: REMOVE TOILET SHROUDACCESS: 121DL 172AR* 0.01383100-0503-1 200 TOILET SYSTEM MEC OPC I: 2 A MRB AMM 383100/5011 0.20 ALLOROPERATIONAL TEST OF FLUSHING SYSTEM. NOTE 5-3ACCESS: 121DL 172AR* 0.01383200-0502-1 200 WATER WASTE DRAIN MEC GVI I: 3 A MRB AMM 383215/4011 0.80 ALLCHECK OVERFLOWS AND PAN DRAIN FOR OBSTRUCTIONAND CLEAN IF NECESSARY384100-0505-1 138 AIR SUPPLY FILTER MEC RAR I: 2 C MRB AMM 384112/3011 0.75 ALL* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : WATER/WASTE REV. DATE: APR 01/10 SECTION:2-38 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)384100-0505-1 * * * * * C O N T I N U E * * * * *REPLACE FILTER ELEMENT AND CHECK TANK-PRESSURIZATIONSYSTEM AND COMPONENTS FOR CLEANLINESS ANDSATISFACTORY CONDITIONACCESS: 131BZ 131CZ 132EZ* 0.39* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : WATER/WASTE REV. DATE: APR 01/10 SECTION:2-38 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)491200-0703-1 310 APU-MOUNTS ENG DET I: APU CHG MRB1 1.00 ALL01. DETAILED INSPECTION OF APU MOUNTS02. DETAILED INSPECTION OF APU ATTACH FITTINGSAND SUPPORT STRUCTURE AT FRAME 95, 97 AND 98(SSI NO.530905) INTERNAL IN ZONES 315 AND 31603. DETAILED INSPECTION OF FRAMES, STRINGERSAND SKIN IN APU COMPARTMENT AREA FROM FRAME 95TO 100 (SSI NO.530907) INTERNAL IN ZONES 315/316ACCESS: 315AL 315AZ 316AR 316AZ 316BZ* 0.12491600-0703-1 313 AIR INTAKE SYSTEM ENG DET I: APU CHG MRB AMM 491000/4011 0.25 ALL3141 0.25DETAILED INSPECTION OF APU AIR INTAKE AREA,DUCTS AND SUPPORTS FOR SATISFACTORY CONDITION,CRACKS, WEAR, CORROSION AND SECURITY OF ATTACHMENTS.ACCESS: 313AL* 0.14491600-0703-2 310 AIR INLET SCREEN ENG GVI I: 1000 AH MRB AMM 492000/7011 0.25 ALLVISUAL INSPECTION OF APU - AIR INLET SCREEN FORSATISFACTORY CONDITION AND CLEANLINESSACCESS: 313AL* 0.14491700-0702-1 316 ENGINE DRAIN SYSTEM ENG DRN I: 3 A MPD AMM 491700/6011 0.50 ALLDRAINAGE OF COLLECTOR SIGHT GLASSESACCESS: 315AL 316AR* 0.05492000-0703-1 315 APU COMPRESSOR, FIRST STAGE ENG DET I: 500 AH MRB AMM 492000/6011 1.50 ALL01. REMOVE THE AIR INTAKE DUCT OR REMOVE INSPECTIONPLUG FROM BOTTOM OF INLET CYLINDER02. DETAILED INSPECTION OF LP COMPRESSORFIRST STAGE ROTOR BLADES FOR CRACKS, CORROSIONAND FOD OR PERFORM BOROSCOPE INSPECTION OF LPCOMPRESSOR FIRST STAGE ROTOR BLADES* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION:2-49 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)492000-0703-1 * * * * * C O N T I N U E * * * * *03. CHECK LP COMPRESSOR WHEEL, STAGE 1 FOR FREEROTATION.ACCESS: 313AL 315AL 316AR* 0.19492000-0703-2 315 ENGINE - APU ENG DET I: 2000 FC CN CN1 0.50 PRE 02011FAA AD 1977-163-IMP(B) (49-0029)DETAILED INSPECTION OF 1 ST STAGE LP FAA AD 77-17-06COMPRESSOR DISK SB GTSCP700-49-A391ACCESS: 315AL 316AR 2* 0.05493000-0703-1 315 ENGINE FUEL AND CONTROL ENG GVI I: 500 AH MRB AMM 493114/3011 0.25 ALLCHECK THAT THE FUEL FILTER DIFFERENTIAL PRESSUREINDICATOR IS NOT PROTRUDING.ACCESS: 315AL 316AR* 0.05493000-0703-2 315 ENGINE FUEL AND CONTROL ENG RAR I: 1000 AH MRB AMM 493114/3011 1.00 ALL- REMOVE THE PRIMARY FUEL FILTER AND INSPECT FORSATISFACTORY CONDITION AND PARTICLES- INSTALL A NEW FILTER ELEMENTACCESS: 315AL 316AR* 0.05N 493000-0703-3 315 APU FUEL SHROUD LINE ENG FUC I: 10 YE SIL AMM 493100/5011 0.80 ALLSIL 49-056FUNCTIONAL CHECK (AIR PRESSURE CHECK) OF APU FUELSHROUD LINE494000-0702-4 315 IGNITION AND STARTING ENG OPC I: 3 A MPD AMM 494000/5012 0.30 POST 01721(49-0026)TEST OF "SELF TEST" CAPABILITY FOR APU STARTERCIRCUIT (USING TEST SWITCH 14 KA)ACCESS: 315AL 316AR* 0.05SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION:2-49 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)494000-0703-1 315 APU-IGNITER PLUGS ENG DET I: 500 AH MRB AMM 494212/2011 1.50 ALL01. REMOVE IGNITER PLUGS02. CLEAN PLUGS03. DETAILED INSPECTION OF IGNITER PLUGSFOR CERAMIC CRACKING AND ALUMINIUM SPRAY DEPOSITS04. INSPECT THREADS FOR CORROSION AND DAMAGE05. REINSTALL IGNITER PLUGS.ACCESS: 315AL 316AR* 0.05494000-0703-2 315 APU-ELECTRIC STARTER MOTOR ENG GVI I: 500 AH MRB AMM 494411/6011 2.00 ALLGENERAL VISUAL INSPECTION OF APU ELECTRICAL STARTERMOTOR BRUSHES AND BRUSH LEADS FOR SATISFACTORYCONDITION, WEAR, CORROSION AND DAMAGED LEADS.ACCESS: 315AL 316AR* 0.05494000-0703-3 315 APU STARTER MOTOR CLUTCH ENG DET I: 1000 AH MRB AMM 494412/6011 5.00 ALLDETAILED INSPECTION OF APU STARTER MOTORCLUTCH COMPONENTS AND PAWL STROKE.ACCESS: 315AL 316AR* 0.05495000-0703-1 316 AIR - BLEED ENG CLN I: 1000 AH MRB AMM 495114/3011 1.50 ALLREMOVE AIRFLOW SENSOR FOR CLEANING AND INSPECTFOR CRACKS AND OBVIOUS DAMAGEACCESS: 315AL 316AR* 0.05495000-0703-2 316 AIR ENG DET I: 600 FH ISB AMM 495116/6011 0.50 POST 01782ISB 49-0031(49-0025)DETAILED INSPECTION OF HOUSING (FLEXIBLEPRE 04770COUPLING) BETWEEN SURGE BLEED VALVE AND AIR DUCT(49-0046)SUPPORT STRUTS FOR WEARACCESS: 315AL 316AR* 0.05SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION:2-49 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)495000-0703-3 315 COOLING FAN ENG DET I: 500 AH MPD AMM 495211/6011 0.50 ALLDETAILED INSPECTION OF FAN IMPELLER FOR FODAND EVIDENCE OF OIL LEAKS.INSPECT INLET DUCT FOR GENERAL CONDITIONPREP.: REMOVE COOLING FAN INLET DUCTING.ACCESS: 315AL 316AR* 0.05495000-0703-4 315 APU COMPARTMENT ENG GVI I: 3 A MRB AMM 495200/6011 0.50 POST 01646(49-0019)VISUAL INSPECTION OF APU COMPARTMENT FOR GENERALCONDITION AND EXTERNAL LEAKS (DOOR OPEN)ACCESS: 315AL 316AR* 0.05495000-0703-5 315 AIR ENG GVI I: 2A ISB ISB 49-00171 1.10 PRE 01646OR(49-0019)REMOVE COOLING AIR INLET DUCT AND CHECK DUCT FOR APU CHGSATISFACTORY CONDITION AND CRACKS - COOLING FANFOR F.O.D. AND OIL LEAKSACCESS: 315AL 316AR* 0.05495000-0703-6 316 SURGE AIR VALVE FILTER ENG CLN I: 500 AH MRB AMM 495113/3011 1.50 ALLREMOVE,INSPECT AND CLEAN THE SURGE AIR VALVEFILTER AND FILTER SCREENACCESS: 315AL 316AR* 0.05498000-0703-1 310 EXHAUST DUCT AND MUFFLER ENG DET I: APU CHG MRB AMM 491000/4011 0.50 ALLDETAILED INSPECTION OF APU EXHAUST DUCTAND MUFFLER FOR SATISFACTORY CONDITION, CRACKS ANDCORROSION IN ZONES 315, 316, 317 AND 318ACCESS: 315AL 316AR 317AL* 0.06SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION:2-49 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)499000-0703-1 315 APU OIL QUANTITY INDICATION ENG DET I: APU CHG MPD AMM 499312/4011 0.30 ALLCOMPARE BY READING OF QUANTITY INDICATOR INFLIGHT COMPARTMENT AGAINST DIPSTICK THE CORRECTFUNCTIONING OF LIQUID QUANTITY TRANSMITTER(AFTER APU REPLACEMENT)ACCESS: 315AL 316AR* 0.05499000-0705-1 315 APU - OIL FILTER ENG RPL I: 500 AH MRB AMM 499112/3011 1.50 ALLAMM 499113/30101. REMOVE OIL FILTER FOR INSPECTION AND CHANGEFILTER ELEMENT02. REMOVE MAGNETIC PLUG/CHIP DETECTOR FOR CONTAMINA-TION CHECK OF OIL PER MAGNETIC PLUG FINDINGSNOTE: CHANGE OIL IF OIL IS FOUND CONTAMINATEDDETERIORATED OR IF OIL BRAND IS CHANGEDACCESS: 315AL 316AR* 0.05* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION:2-49 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)513000-0502-1 100 FUSELAGE DRAIN VALVES MEC GVI I: C MPD AMM 513041/6011 0.20 ALLOR SIL 53-060CHECK FUSELAGE DRAINAGE AT: NOTE- DRAIN RUBBER FLAP VALVE AT FR.11,- DRAIN MAST AT FR. 80,- APU DRAIN MAST AT FR. 95,- DRAIN PLUGS AND DRAIN PISTON VALVESBETWEEN FR. 19 AND FR. 65,FOR FREEDOM OF OBSTRUCTION ( FROM OUTSIDE ONLY )NOTE: INSPECTION MAY BE NEED TO BE PERFORMEDMORE FREQUENTLY IN CERTAIN OPERATINGCONDITIONS513000-0502-2 100 FUSELAGE DRAIN VALVES MEC DET I: 4 YE MPD AMM 513011/6011 1.50 ALLAMM 513021/601DETAILED INSPECTION OF FUSELAGE DRAIN VALVES AMM 513031/601(INCLUDING RUBBER SEALING FLAP) IN INTERNAL FUSELAGE AMM 513041/601BILGE AREA (ZONE: 121/122, 133/134, 135/136, 143/144,153/154, 164, 171/172, 311, 312).NOTE: INSPECTION TO BE DONE AT THE OPPORTUNITYOF ZONAL INSPECTIONS IN CORRESPONDINGZONES513000-0502-3 100 PRESSURE BULKHEADS DRAINS MEC GVI I: 1 C MPD AMM 513011/6011 0.30 ALLAMM 513041/601CHECK DRAIN HOLES AT THE:- LOWER AREA OF THE FORWARD PRESSURE BULKHEAD- LOWER AREA OF THE AFT PRESSURE BULKHEADFOR FREEDOM OF OBSTUCTION (FROM INSIDE)ACCESS: 132AZ 162AZ* 0.01513000-0502-4 311 FUSELAGE DRAIN MAST MEC OPC I: 4 MO SIL AMM 513041/6011 0.20 ALL312 OR SIL 53-0601 0.20CHECK FUSELAGE DRAINAGE AND DRAIN PATH AT DRAIN MAST NOTEAFT OF FR 80 FOR FREEDOM OF OBSTRUCTION ( FROMINSIDE)NOTE: INSPECTION MAY BE NEEDED TO BE PERFORMED MOREFREQUENTLY IN CERTAIN OPERATING CONDITIONS* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STRUCTURES REV. DATE: APR 01/10 SECTION:2-51 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)513000-0502-4 * * * * * C O N T I N U E * * * * *ACCESS: 312AR* 0.01518061-0502-1 400 PYLON DRAINAGE MEC CHK I: 1 C MPD AMM 513061/6011 0.20 ALLOITCHECK PYLON UPPER SPAR DRAIN INLETS ST/999.0108/92FOR BLOCKAGE518061-0502-2 400 PYLON DRAINAGE MEC BSI I: 2 C MPD AMM 513061/6011 0.50 ALLOITBOROSCOPE INSPECTION OF PYLON LOWER SPAR INLETS FOR ST/999.0108/92SIGNS OF CONTAMINATION* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STRUCTURES REV. DATE: APR 01/10 SECTION:2-51 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)520000-0502-1 800 DOORS AND PANELS MEC GVI I: 1 A MRB AMM 520000/6011 2.00 ALLAMM 522200/601CHECK FUSELAGE DOORS AND SERVICE PANELS FORSATISFACTORY CONDITION520000-0502-2 100 SERVICE PANELS MEC GVI I: 3 A MRB SIL 38-0131 1.50 ALLCHECK DRAIN AND FILLER CAPS ARE CORRECTLY INSTALLEDAND SEALS ARE SERVICEABLE.NOTE: ACCESS 134 BR IS OPTIONAL ACCORDING TO GALLEY/TOILETS CONFIGURATION.ACCESS: 121DL 134BR 136BR 172AR* 0.03521000-0502-1 831 PASSENGER/CREW DOOR MEC DET I: 36 MO CN CN1 1.00 B2832 1999-410-294(B) 1 1.00 B4833 DETAILED INSPECTION OF DOOR DAMPER/EMERGENCY FAA AD1 1.00 C4841 ACTUATOR STRIKER MECHANISM FOR CORROSION. 2003-03-041 1.00 PRE 12024842 ISB 52-01681 1.00 (52-0173)8431 1.00521000-0502-2 831 PASSENGER/CREW DOOR MEC DET I: 36 MO CN CN1 1.00 F4841 1999-410-294(B) 1 1.00 PRE 12024DETAILED INSPECTION OF DOOR DAMPER/EMERGENCY FAA AD(52-0173)ACTUATOR STRIKER MECHANISM FOR CORROSION. 2003-03-04ISB 52-0168521014-0504-1 830 CYLINDER - DOOR DAMPER MEC RAR I: 18 MO CN AMM 521014/4011 12.00 PRE 06240840 FAA AD CN1 12.00 (52-0132)REMOVE PERCUSSION MECHANISM FROM EACH DOOR DAMPER 1989-092-095(B)AND INSPECT FOR CORROSION FAA AD 90-17-16ISB 52-0130NOTE: DEPENDING ON DAMPER TYPE,DAMPER MAY HAVE TO BEREMOVED FROM DOOR FIRSTACCESS: UPPER SUPPORT ARM LININGSYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)521022-0505-1 800 MECHANISM SLIDE RELEASE MEC LUB I: NOTE 5-2 MPD SIL 52-0291 1.20 ALLAPPLY LPS 3 TO GIRT BAR SLIDERS AND FITTINGS521031-0502-2 830 PASSENGER/CREW DOORS MEC DET I: 3000 FH ISB ISB 52-00141 1.75 PRE 010948401 1.75 (53-0051)WEAR CHECK OF PAX/CREW DOOR STOPFITTINGS ON DOOR AND ON FUSELAGE.521031-0502-3 830 PASSENGER/CREW DOORS MEC DET T: 12000 FH ISB ISB 52-00141 1.75 POST 01094840 I: 9000 FH1 1.75 (53-0051)WEAR CHECK OF PAX/CREW DOOR STOPFITTINGS ON DOOR AND FUSELAGE STRUCTURE521114-0502-1 830 CYLINDER - DOOR DAMPER MEC GVI I: 1 A MRB ** AMM 521014/6011 0.10 ALL8401 0.10CHECK DOOR DAMPER / EMERGENCY CYLINDER FORCORRECT PRESSURECAUTION: WHEN REFILLING A BOTTLE DO NOT EXCEED THEMAXIMUM PRESSURE,INDICATED ON THE PLACARD521114-0505-1 830 CYLINDER - DOOR DAMPER INP LUB I: 1 C MPD AMM 122252/0011 0.30 ALL8401 0.30LUBRICATE DAMPER/TELESCOPIC RODS OFPASSENGER DOORS521121-0503-1 830 MECHANISM - DOOR LOCKING MEC FUC I: 6 C MRB AMM 521020/6011 25.00 ALL8401 25.00ON THE LOCKING MECHANISM OF THE PASSENGER/CREW DOORS:01. FUNCTIONAL TEST OF LOCKING MECHANISM ON DOORS02. DETAILED INSPECTION OF INTERNAL LOCKINGMECHANISM FOR SATISFACTORY CONDITION,CORROSION,WEAR AND SECURITY OF ATTACHMENTPREP.: REMOVE LININGS.521121-0505-1 830 MECHANISM - DOOR LOCKING MEC LUB I: 1 C MPD AMM 122252/0011 0.50 ALL8401 0.50* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)521121-0505-1 * * * * * C O N T I N U E * * * * *LUBRICATE THE EXTERIOR CONTROL HANDLES(PASSENGER/CREW DOORS)521122-0503-1 831 MECH.EMERG.ESCAPE SLIDE REL MEC FUC I: 2 C MRB ** AMM 521030/6011 1.00 ALL832 AMM 522222/6011 1.00833 01. REMOVE ESCAPE SLIDE AND DOOR LINING1 1.00834 02. PERFORM FUNCTIONAL TEST OF ESCAPE SLIDE RELEASE1 1.00841 MECHANISM1 1.00842 (FWD, MID, AFT PASSENGER/CREW DOORS AND1 1.00843 PASSENGER COMPARTMENT EMERGENCY EXIT1 1.00844 DOORS)1 1.0003. REINSTALL DOOR LINING AND ESCAPE SLIDE521131-0505-1 831 FWD PAX DOOR LATCHING LINK. MEC LUB I: 1 C MPD AMM 521022/4011 1.00 PRE 05262841 SIL 52-0301 1.00LUBRICATE LATCHING LINKAGE ASSEMBLY RODPREP.: REMOVE DOOR LININGS522221-0503-1 834 LOCKING MECHANISM,EMER.EXIT MEC FUC I: 6 C MRB AMM 522200/6011 8.00 B2844 AMM 522213/4011 8.00 B401. DO A FUNCTIONAL TEST OF LOCKING MECHANISM OF AMM 522221/601C4EMERGENCY EXIT DOORS.02. REMOVE ESCAPE SLIDES, LININGS AND INSULATION03. DO A DETAILED INSPECTION OF INTERNALLOCKING MECHANISM FOR SATISFACTORY CONDITION,CORROSION, WEAR AND SECURITY OF ATTACHMENT04. REINSTALL ESCAPE SLIDES, LININGS AND ISOLATION522231-0502-2 834 PASSENGER COMPARTMENT EMERGENCY EXIT MEC DET T: 12000 FH ISB ISB 52-00141 0.25 PRE 01094844 I: 6000 FH1 0.25 (53-0051)WEAR CHECK ON EMERGENCY EXIT DOOR STOP FITTINGS ONDOOR AND ON FUSELAGE.522231-0502-3 834 PASSENGER COMPARTMENT EMERGENCY EXIT MEC DET T: 12000 FH ISB ISB 52-00141 0.25 POST 01094844 I: 9000 FH1 0.25 (53-0051)WEAR CHECK ON EMERGENCY EXIT DOOR STOP FITTINGS ONDOOR AND FUSELAGE STRUCTURESYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523011-0502-1 811 CARGO COMPARTMENT DOORS MEC GVI I: 2400 FC ISB ISB 52-00481 2.50 PRE 026248121 2.50 (52-0098)REMOVE AND CHECK SHEAR BOLT OF ACTUATORATTACHMENT FITTING AT CARGO DOORS FOR CRACKS523011-0504-1 811 CARGO COMPARTMENT DOORS MEC RAR I: 4800 FC ISB ISB 52-00481 2.50 PRE 026248121 2.50 (52-0098)REPLACE SHEAR BOLT OF ACTUATOR ATTACHMENT FITTINGAT CARGO DOOR523100-0505-1 811 FWD CARGO COMPARTMENT DOOR MEC LUB I: 1 C MPD AMM 122252/0011 1.20 ALLLUBRICATE THE FOLLOWING CARGO COMPARTMENT DOORCOMPONENTS:- STRUCTURAL SUPPORT HINGES (DOOR/FUSELAGE)- LOCKING ROLLERS AT LOWER DOOR FRAME (FUSELAGE)- BOLTS OF LOCKING HOOK, ATTACHMENT OF SPRING,LOCKING MECHANISM (LOWER DOOR SECTION)- DOOR HANDLE LOWER ATTACH BOLT AND HANDLE LATCH(DOOR OPERATING HANDLE)ACCESS: 132AR 811AR 811CR 811DR* 0.98523121-0503-1 811 LOCK.MECHANM.FWD CARGO DOOR MEC FUC I: 3 C MRB ** AMM 523021/6011 3.50 ALL- FUNCTIONAL TEST OF LOCKING MECHANISM- VISUAL INSPECTION OF INTERNAL DOOR LOCKINGMECHANISMACCESS: 811AR 811BR 811CR 811DR* 0.61523200-0505-1 812 AFT CARGO COMPARTMENT DOOR MEC LUB I: 1 C MPD AMM 122252/0011 1.20 ALLLUBRICATE THE FOLLOWING CARGO COMPARTMENT DOORCOMPONENTS:- STRUCTURAL SUPPORT HINGES (DOOR/FUSELAGE)- LOCKING ROLLERS AT LOWER DOOR FRAME (FUSELAGE)- BOLTS OF LOCKING HOOK, ATTACHMENT OF SPRING,LOCKING MECHANISM (LOWER DOOR SECTION)- DOOR HANDLE LOWER ATTACH BOLT AND HANDLE LATCH(DOOR OPERATING HANDLE)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523200-0505-1 * * * * * C O N T I N U E * * * * *ACCESS: 152BR 812AR 812CR 812DR* 0.82523221-0503-1 812 LOCK.MECHANM.AFT CARGO DOOR MEC FUC I: 3 C MRB ** AMM 523021/6011 4.00 ALL- FUNCTIONAL TEST OF LOCKING MECHANISM- VISUAL INSPECTION OF INTERNAL DOOR LOCKINGMECHANISMACCESS: 812AR 812BR 812CR 812DR* 0.57523307-0502-1 811 ACTUATOR ATTACHMENT FITTING CARGO DOOR NDT SDI I: ISB ISB ISB 52-01011 2.30 PRE 0229552-101PRE 03054DETAILED CHECK AND SPECIAL DETAILED INSPECTION(52-0104)OF FORWARD CARGO COMPARTMENT DOOR ACTUATOR ATTACH.FITTING FOR CRACKS.523316-0503-1 811 CARGO DOOR SEQUENCE VALVE MEC OPC I: 1 C MPD AMM 523300/6011 0.40 POST 044398121 0.40 (52-0121)OPERATIONAL TEST OF CARGO DOOR SEQUENCE VALVE523351-0502-1 835 ACTUATOR - DOOR, UDC COMPARTMENT MEC GVI I: 5 A MRB ** AMM 523600/5011 0.30 C4IN CARGO CONFIG01. PERFORM GAP-CHECK OF HOOKF402. CHECK THAT THE HYDRAULIC PRESSURE HOLDS THE DOORIN SELECTED POSITIONS BY VISUAL OBSERVATION523351-0503-1 835 ACTUATOR - DOOR, UDC COMPARTMENT MEC OPC I: 1 C MRB ** AMM 523600/5011 0.50 C4IN CARGO CONFIGCHECK FOR CORRECT OPERATION OF DETENT HOOK INF4SELECTED POSITIONS (70 DEG. AND 145 DEG.) WITHBYPASS CHECK VALVE MANUALLY OPENED.523400-0502-1 813 BULK CARGO COMPARTMENT DOOR MEC GVI I: 6 C MPD AMM 523441/6011 0.50 ALLON THE BALANCE MECHANISM:01. INSPECT MECHANISM FOR CORROSION AND GENERALCONDITION* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523400-0502-1 * * * * * C O N T I N U E * * * * *02. CHECK FORCE REQUIRED TO OPERATE MECHANISM523400-0505-1 813 BULK CARGO COMPARTMENT DOOR MEC LUB I: 1 C MPD AMM 122252/0011 1.00 ALLLUBRICATE THE FOLLOWING CARGO COMPARTMENT DOORCOMPONENTS:- ROD EYE END BOLTS,UNIVERSAL JOINT AND FLANGEASSEMBLY BEARING AT MAIN SHAFT OF LOCKING MECHA-NISM- DOOR OPERATING HANDLE MECHANISM- SPRING HOOK/BOX ASSEMBLYPREP.: REMOVE DOOR LININGS523500-0503-1 200 ELECTR. CONTR. SYST. DOORS MEC OPC I: WEEKLY MRB AMM 527111/5011 0.10 ALLOPERATIONAL TEST OF MONITORING SYSTEM (DOOR TESTSWITCH) OF THE ELECTRICAL CONTROL AND DOORWARNINGSYSTEM523500-0503-2 835 ELEC.CONT.SYS.(UDC-DOOR) ERI OPC I: 5 A MRB AMM 523600/5011 0.20 C4IN CARGO CONFIGUDC-COMPARTMENT DOOR - ELECTRICAL CONTROL AND DOORWARNING SYSTEM- CHECK ELECTRICAL CUT-OFF FROM THE UDC-DOOR TO MIDPASSENGER/CREW DOORCAUTION: TO AVOID DAMAGE TO UDC-COMPARTMENT DOORAND LH MID PASS./CREW DOOR, DO NOT FULLYOPEN LH MID PASS./CREW DOOR.523600-0502-1 835 MAIN DECK CARGO DOOR MEC DET I: 500 FH AOT AOT 52-111 0.50 C4F4DETAILED INSPECTION OF MAIN DECK CARGO DOOR- SLEEVES AT DOOR ACTUATOR ATTACHMENT POINTS FORPRE 11361DENTS(52-0165)- ROD EYE ENDS FOR CRACKS AND DENTS.SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523600-0505-1 835 UDC - COMPARTMENT DOOR MEC LUB I: 5 A MPD AMM 122252/0011 1.50 C4IN CARGO CONFIGLUBRICATE THE FOLLOWING UDC-COMPARTMENT DOORF4COMPONENTS:- STRUCTURAL PIANO HINGES (DOOR/FUSELAGE)- DOOR ACTUATOR (OPENING/CLOSING), RODS ETC.(9 LUBR. POINTS)- BOLTS OF LOCKING HOOK, LOCKING MECHANISM(LOWER DOOR SECTION)- DOOR SAFETY LEVER AND SAFETY MECHANISM(LOWER DOOR SECTION)ACCESS: 835AR 835BR 835CR 835DR 835ER 835FR* 0.88835GR523619-0503-1 835 LOCKING MECHANISM - UDC DOOR MEC OPC I: 5 A MRB AMM 523600/5011 0.25 C4IN CARGO CONFIGOPERATIONAL TEST OF SAFETY LEVER AND DOORF4LOCKING/UNLOCKING MECHANISM TO ENSURE PROPEROPERATION OF DECOMPRESSION FLAP AND VISUAL (RED) DOORLOCKING INDICATOR BUTTONS523619-0503-2 835 LOCKING MECHANISM - UDC DOOR MEC FUC I: 3 C MRB AMM 523600/5011 2.50 C4IN CARGO CONFIGFUNCTIONAL TEST OF DOOR LOCKING/ UNLOCKING MECHANISMF4524200-0505-1 121 FWD TOIL.SERVICE PANEL MEC LUB I: 3 A MPD AMM 122252/0011 0.10 ALLLUBRICATE SPRING DEVICE (HOLD OPEN MECHANISM)OF PANEL 121DLACCESS: 121DL* 0.01524215-0502-1 120 FWD CARGO COMPT DOOR CONTL NDT SDI I: 500 FC ISB ISB 52-01511 2.20 POST 02709PRE 08854SPECIAL DETAILED INSPECTION OF ACCESS PANEL HINGES OF(52-0152)FWD CARGO DOOR CONTROL PANEL FOR CRACKS.ACCESS: 122DR* 0.10SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)527300-0503-1 800 EMERG ESCAPE SLIDE WARNING ELO OPC I: 1 C MPD AMM 527300/5011 0.30 ALLOPERATIONAL TEST OF ESCAPE SLIDE RELEASE WARNINGSYSTEM (FLASHING WARNING LIGHT AND BUZZER TONE)IN ZONE 831/841, 832/842, 834/844 AND 833/843.ACCESS: 831* 0.10527300-0503-2 800 RESIDUAL PRESSURE WARNING ELO FUC I: 1 C SIL AMM 527300/5012 1.50 POST 08357SIL 52-043(52-0148)01. OPERATIONAL TEST OF RESIDUAL CABINPRESSURE WARNING.02. FUNCTIONAL TEST OF ASSOCIATEDPRESSURE SWITCH.IN ZONE 831/841, 832/842, 834/844,833/843 AND 100.ACCESS: 131AZ 811 811CR 812CR 831* 0.61527300-0503-3 121 RESIDUAL PRESSURE WARNING ELO FUC I: 4 A SIL AMM 527300/5011 3.00 POST 08357SIL 52-043(52-0148)01. CAPACITY TEST OF AUTONOMOUSSTANDBY SUPPLY UNIT.02. BITE TEST OF AUTONOMOUS STANDBYPOWER SUPPLY UNIT.ACCESS: 131AZ 811* 0.16528212-0503-1 715 SECONDARY NOSE LANDING GEAR DOORS NDT SDI T: 8000 FC CN NTM 5282111 1.00 NLG DOOR716 I: 700 FC FAA AD PART 61 1.00 ASSY P/NSPECIAL DETAILED INSPECTION (EDDY CURRENT) OF NLG OR CNA52810648000DOOR HINGE FITTINGS. NOTE 1995-011-174(B) NLG DOOR FITTINGFAA AD 95-12-09 P/NNOTE: AS AN ALTERNATIVE COMPLIANCE, REMOVE AND ISB 52-0161A52810629200/REPLACE NLG DOOR FITTINGS AT INTERVAL 8000 FC.201ACCESS: 713* 0.06714* 0.06* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:2-52 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)530000-0502-1 100 FUSELAGE GENERAL MEC GVI I: PRE-ACPT MRB1 0.20 ALLVISUAL INSPECTION OF FORWARD AND AFT FUSELAGE FROMGROUND FOR GENERAL CONDITION AND POSITIVE LOCKING OFFORWARD, AFT AND REAR CARGO COMPARTMENT DOORS, EXTER=NAL SERVICING PANELS AND ACCESS DOORS (DOORS CLOSED)530000-0502-2 300 AFT FUSELAGE AND EMPENNAGE MEC GVI I: PRE-ACPT MRB1 0.20 ALLVISUAL INSPECTION OF EXTERNAL APU AREA, HORIZONTALSTABILIZER (INCLUDING ELEVATORS AND RUDDER) FROMGROUND FOR GENERAL CONDITION, VISIBLE DAMAGE, LEAKSAND APU BAY DOORS CLOSED. CHECK TAIL SKID NOT DAMAGED530000-0502-3 100 FUSELAGE GENERAL MEC GVI I: DY-TERM MRB: 1 0.20 ALLVISUAL INSPECTION OF EXTERIOR FUSELAGE, INLETS/OUTLETS, TEMPERATURE AND ANGLE OF ATTACK SENSORSAND PITOT PROBES/STATIC PORTS FOR GENERAL CONDITIONAND DAMAGE.531300-0502-1 220 FUSELAGE FORWARD SECTION MEC GVI T: 3 YE ISB ISB 53-01551 6.00 PRE 02899230 I: 3 YE1 6.00VISUAL INSPECTION OF FORWARD PASSENGER/CREW DOORFRAME AT FRAME 14 AND 16A AND MID PASSENGER/CREW DOORFRAME AT FRAME 28A AND 30A FOR CORROSION.532411-0502-1 120 EXTENDING LADDER MEC FUC I: 1050 FH CN CN1 0.20 PRE 10929FAA AD 1994-187-163(B) (24-0086)1. FUNCTIONAL CHECK OF LADDER FOR INTERFERENCE. FAA AD 95-10-142. DETAILED INSPECTION OF LADDER SUPPORT ISB 24-0087SHAFT AND ATTACHMENT RIVETS.NOTE: THIS TASK IS RELATED TO INSPECTION OF 104 VUPANEL ELECTRICAL INSTALLATION REF TASK240000-0503-1.ACCESS: 121BL* 0.01SYSTEMS AND POWERPLANT PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:2-53 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534212-0502-1 230 MID/PAX DOOR ATTACH FITTG. MEC GVI T: 4000 FC ISB ISB 53-01651 0.20 PRE 03556I: 2000 FC(53-0168)DETAILED INSPECTION OF THE GUIDE ARM SUPPORTFITTINGS AT THE UPPER DOOR FRAME OF THE MID/PASSENGERCREW DOOR534600-0505-1 319 HORIZ. STAB. ATTACH FITTING MEC LUB I: 1 C MPD AMM 122253/0011 0.33 ALLLUBRICATE HORIZONTAL STABILIZER HINGE BEARINGSUPPORT FITTINGSACCESS: 313AL* 0.14534700-0502-1 311 TAIL CONE ATTACH FITTING MEC GVI I: 2 YE MPD SIL 53-0431 0.50 ALL01. CHECK FOR CLEANLINESS OF DRAIN HOLE AT FRAME 91.02. APPLY CORROSION INHIBITOR AND WATER REPELLENTON CENTERING FITTINGS.535100-0502-1 110 RADOME MEC GVI I: PRE-ACPT MRB1 0.10 ALLVISUAL INSPECTION OF RADOME FOR DAMAGE535112-0505-1 110 LATCH-RADOME ADJUST. HOOK MEC LUB I: 1 C MPD AMM 122253/0011 0.25 ALLLUBRICATE CABLE ASSY AND LOCKING MECHANISMMOVING PARTS (ENSURE NO PAINT ON LOCKING HOOK)ACCESS: 110AL* 0.01535300-0502-2 311 THS APRON TRAVEL AREA MEC GVI T: 1600 FH ISB ISB 53-00681 0.25 PRE 02021312 I: 400 FH1 0.25 (53-0089)313 GENERAL VISUAL CHECK OF TRIMMABLE HORIZONTAL1 0.25314 STABILIZER APRON TRAVEL AREA FOR GENERAL CONDITION,1 0.25SCRATCHES AND DAMAGE* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:2-53 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540000-0502-1 470 NACELLE/PYLON MEC DET I: 1 C ISB ISB 54-00291 2.00 PRE 022984801 2.00 (54-0030)DETAILED INSPECTION OF PIPES, CLAMPS ANDSUPPORTS FOR DAMAGE AND SECURITY OF ATTACHMENTACCESS: 413AL 413BL 413EL 413FL 414BR 435AL* 1.91475AL 475BL 475CL 475DL 476AR 476BR423AL 423BL 423EL 423FL 424BR 445AL* 1.91485AL 485BL 485CL 485DL 486AR 486BR540000-0502-2 470 LOWER AFT PYLON ENG GVI I: 1 A MRB AMM 543000/6011 0.50 ALL4801 0.50CHECK LOWER AFT PYLON FOR CORROSION, CRACKS,FUEL LEAKS, SECURITY OF FASTENERS AND DETERIORATIONOF TREATMENT541000-0502-1 470 ENGINE PYLON MEC GVI I: 3000 FH ISB ISB 54-00421 3.00 PRE 041254801 3.00 (54-0057)VISUAL INSPECTION OF SPIGOT BALL JOINT TO MAKECERTAIN THAT THE AIR-FLON LINER IS IN PLACEACCESS: 471AL 472AR 473AL* 0.63481AL 482AR 484AR* 0.63* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:2-54 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551100-0505-1 319 HORIZ.STABILIZER HINGE PINS MEC LUB I: 1 C MPD AMM 122255/0011 0.50 ALLLUBRICATE HINGE PINS OF TRIMMABLE HORIZONTALSTABILIZERACCESS: 313AL* 0.14552111-0504-1 334 ELEVATOR SERVO CONTROLS MEC RAR I: 6000 FH ISB ISB 55-00321 3.00 ALL3441 3.00REPLACE ABRASION WASHERS AND BUSHES OFELEVATOR SERVO CONTROLS AT ELEVATOR HINGE FITTINGSACCESS: 334BB 335BB* 0.50344BB 345BB* 0.50553645-0505-1 326 RUDDER HINGE BEARING NO.4 MEC LUB I: 1 C MPD AMM 122227/0011 0.10 POST 04242SIL 55-019LUBRICATE RUDDER HINGE BEARING NO.4ACCESS: 325DL 326DL* 0.51555100-0503-1 334 ELEVATOR HINGE ARMS MEC OPC I: 4 C MPD AMM 555000/6011 1.00 ALL344 SIL 55-0231 1.00CHECK PLAY AT EACH BEARING LOCATION AT TRAILING EDGEOF TRIMMABLE HORIZONTAL STABILIZER.ACCESS: 334BT 334DT 334FT 334HT 334KT* 1.70344BT 344DT 344FT 344HT 344KT* 1.70555200-0503-1 335 ELEVATOR ATTACH FITTINGS MEC OPC I: 4 C MPD AMM 555000/6011 1.00 ALL345 SIL 55-0231 1.00CHECK PLAY AT EACH BEARING LOCATION AT LEADING EDGEOF ELEVATOR.ACCESS: 334AB 334BB 334CB 334DB 334EB* 0.76344AB 344BB 344CB 344DB 344EB* 0.75555300-0503-1 325 RUDDER HINGE ARMS MEC OPC I: 4 C MPD AMM 555000/6011 1.00 ALLSIL 55-023CHECK PLAY AT EACH BEARING LOCATION AT TRAILING EDGE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:2-55 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)555300-0503-1 * * * * * C O N T I N U E * * * * *OF VERTICAL STABILIZER.ACCESS: 325BL 325DL 325FL 325HL 325KL* 1.21555400-0503-1 326 RUDDER ATTACH FITTINGS MEC OPC I: 4 C MPD AMM 555000/6011 1.00 ALLSIL 55-023CHECK PLAY AT EACH BEARING LOCATION AT LEADING EDGEOF RUDDER.ACCESS: 326AL 326AR 326BL 326BR 326CL 326CR* 3.08326DL 326DR 326EL 326ER* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:2-55 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)561000-0502-1 210 COCKPIT WINDOWS MEC DET I: 1 A MRB AMM 561111/6011 0.30 ALLSIL AMM 561112/601DETAILED INSPECTION OF ALL COCKPIT WINDOWS AMM 561211/601FROM INSIDE SIL 56-017561100-0502-1 210 COCKPIT FIXED SIDE WINDOWS MEC DET I: 1 C MPD AMM 561112/6011 0.30 PRE 07864SIL 56-011DETAILED INSPECTION OF COCKPIT SIDE WINDOWS INAREA OF BUS BARSNOTE: FROM INSIDE COCKPIT561100-0502-2 210 COCKPIT FIXED SIDE WINDOWS MEC DET I: 7 DAYS CN AMM 561112/6011 0.40 ALLFAA AD CNNOTEDETAILED INSPECTION OF COCKPIT FIXED SIDE ISB 1994-104-160(B)WINDOWS FOR EVIDENCE OF ELECTRICAL ARCING. FAA AD 94-10-51ISB 56-0008NOTE: 01. EFFECTIVITY DEPENDS ON P/N OF INSTALLED SIL 56-011WINDOWS, REFER CN 94-104-160(B).02. TASK TO BE ACCOMPLISHED FROM OUTSIDE.561100-0502-3 210 COCKPIT WINDOWS MEC DET I: 1 C MPD SIL 56-0171 0.30 ALLSILDETAILED INSPECTION OF ALL COCKPIT WINDOWSFROM OUTSIDE561200-0502-1 210 COCKPIT SLIDING WINDOWS MEC DET I: 2 C SIL SIL 56-0171 0.10 ALLDETAILED INSPECTION OF WINDOW SEALS.561200-0505-1 210 COCKPIT SLIDING WINDOWS MEC LUB I: 4 A MPD AMM 122256/0011 2.00 ALLSIL 56-009CLEANING AND LUBRICATION OF COCKPIT SLIDING WINDOWMECHANISM AND TRACKSACCESS: SLIDING WINDOW OPENEDSYSTEMS AND POWERPLANT PROGRAM : WINDOWS REV. DATE: APR 01/10 SECTION:2-56 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)562100-0502-1 200 PASS. COMPARTMENT WINDOWS MEC GVI I: 1 C ISB ISB 56-00021 2.60 PRE 01661PRE 02378VISUAL INSPECTION OF CABIN WINDOWS IN PASSENGER(53-0003)COMPARTMENT AND ALL DOORSPOST 04580(ZONE 800) FOR BULGING, CRAZING AND SCRATCHES.562100-0502-2 200 PASS. COMPARTMENT WINDOWS MEC GVI I: 1000 FH ISB ISB 56-00071 2.60 POST 01661POST 02378VISUAL INSPECTION OF CABIN WINDOWS IN PASSENGER(53-0003)COMPARTMENT AND ALL DOORSPRE 04580(ZONE 800) FOR BULGING, CRAZING AND SCRATCHES.* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : WINDOWS REV. DATE: APR 01/10 SECTION:2-56 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)570000-0502-1 500 WING MEC GVI I: PRE-ACPT MRB1 0.20 ALL6001 0.2001. CHECK LOWER SURFACE FROM GROUND AND UPPER SURFACETHROUGH CABIN WINDOWS OF WING EXTERIOR ANDLEADING EDGE SLATS FOR GENERAL CONDITION AND FUELLEAKAGE02. CHECK WING TRAILING EDGE, AILERONS, SPOILERS,AIRBRAKES, FLAPS AND FLAP TRACK FAIRINGS FORGENERAL CONDITION, DAMAGE AND SIGNS OF LEAKS570000-0502-2 513 WING MEC GVI I: PRE-ACPT MRB1 0.10 KRUEGER FLAP6131 0.10CHECK KRUEGER FLAP AND SLOT FLAP FOR GENERALCONDITION570000-0502-3 500 WING MEC GVI I: 3 A MRB AMM 570000/6011 0.75 ALL6001 0.75CHECK WING EXTERIOR FOR DAMAGE, GENERAL CONDITION,VORTEX GENERATORS, SLAT SEALS AND SHUTTERS FORCOMPLETENESS (SLATS EXTENDED).571119-0504-1 571 MLG-PICK UP AT RIB 5 MEC DET I: AT LDG. MRB AMM 574211/6011 0.25 ALL671 GEAR CHG1 0.25CLEAN AREA AND CARRY OUT DETAILED INSPECTIONOF MAIN LANDING GEAR PICK-UP AT RIB 5.571121-0504-1 571 MLG-RETRACT.ROD ATT. RIB 5 MEC DET I: AT LDG. MRB AMM 574211/6011 0.25 ALL671 GEAR CHG1 0.25CLEAN AREA AND CARRY OUT DETAILED INSPECTIONOF MAIN LANDING GEAR RETRACTION ROD ATTACHMENTS ANDLINKS AT RIB 5.571127-0504-1 571 MLG-PICK UP AT REAR SPAR MEC DET I: AT LDG. MRB AMM 574211/6011 0.25 ALL671 GEAR CHG1 0.25CLEAN AREA AND CARRY OUT DETAILED INSPECTIONOF MAIN LANDING GEAR PICK-UP ON REAR SPAR.571138-0504-1 571 MLG PIVOT PICK UP AT RIB 5 MEC DET I: AT LDG. MRB AMM 574211/6011 0.25 ALL671 GEAR CHG1 0.25* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:2-57 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571138-0504-1 * * * * * C O N T I N U E * * * * *CLEAN AREA AND CARRY OUT DETAILED INSPECTIONOF MAIN GEAR PIVOT PICK-UP LUGS AT RIB 5, AFT OFREAR SPAR.572030-0502-1 731 MAIN LANDING GEAR ATTACHMENT MEC DET T: 9 YE ISB ISB 57-02121 2.00 ALL741 I: 5 YE1 2.00DETAILED INSPECTION OF THE FORWARD AND AFTFACES OF:- MAIN LANDING GEAR ATTACHMENT LUGS- FORWARD CROSS BRACE ATTACHMENT LUG- AFT CROSS BRACE ATTACHMENT LUGPREP.:MAIN LANDING GEAR REMOVED.572500-0502-2 500 FLAP TRACK BEAMS MEC DET I: 2400 FC ISB ISB 57-01221 70.00 PRE 044006001 70.00 (57-0123)CHECK BOLTS AT FLAP TRACK BEAM NO. 2, 3, 4, 5 AND 6FORWARD ATTACHMENT BRACKETS FOR LOOSENESS ANDRETIGHTEN AS NECESSARYACCESS: MOVABLE AND FIXED FARINGS572500-0505-1 500 FLAP TRACK BEAM NO. 1 TO 6 MEC LUB I: 5 A MPD AMM 572511/7011 3.00 ALL6001 3.0001. CLEAN CHANNELS WITH LINT-FREE CLOTH02. CHECK FOR CORROSION03. RE-APPLY GREASE MIL-G-23827NOTE: IN CASE OF CORROSION PITS WITHINALLOWABLE LIMITS, ARDOX 3302 MUST BEAPPLIED ON CORROSION PITS BEFOREGREASING, AS TEMPORARY PROTECTIONBEFORE REPAIR572512-0502-1 532 FLAP TRACK BEAM NO.2 TO 6 MEC DET T: REFER CN CN CN1 3.80 PRE 06891632 I: 700 FC FAA AD 1987-121-081(B) 1 3.80 (57-0145)DETAILED INSPECTION OF BOLTING AT THE AFT FAA AD 88-22-08ATTACHMENT OF FLAP TRACK BEAMS 2 TO 6. ISB 57-0150SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:2-57 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)573100-0505-1 500 ACCESS DOORS MEC LUB I: 1 C MPD AMM 122257/0011 0.50 ALL6001 0.50LUBRICATION OF PIANO HINGES OF ACCESS DOORS ANDSPRING STRUT PLUNGER (INNER DEFLECTORS FLAP).NOTE: -FLAP TO BE EXTENDED TO GAIN ACCESS TOPIANO HINGES-ACCESS TO INNER FLAP DEFLECTOR SPRINGSTRUT PLUNGER IF GAINED THROUGH ACCESSPANELS LOCATED IN MLG WHEEL ON REARFALSE BARACCESS: 572FB 572KB 572PB* 0.13672FB 672KB 672PB* 0.13573111-0503-1 500 DOOR-ACCESS-WING SKIN,LH/RH MEC FUC I: 10000 FH MRB AMM 281114/5011 3.01 B4600 OR ISB 57-00891 3.01 C4BONDING CHECK OF NON-LOAD CARRYING FUEL TANK MANHOLE 5 YEF4COVERSPOST 02300(57-0083)573111-0503-2 500 DOOR ACCESS WING SKIN,LH/RH MEC FUC I: 6300 FH ISB AMM 281114/5011 0.50 B4600 OR ISB 57-00891 0.50 C4BONDING CHECK OF NON-LOAD CARRING FUEL TANK MANHOLE 3 YEF4COVERSPRE 02300(57-0083)574413-0505-1 500 ALL SPEED AILERON HINGES MEC LUB I: 5 A MPD AMM 122227/0011 0.50 ALL6001 0.50LUBRICATION OF ALL HINGE BEARINGS OF ALL SPEEDAILERON AND SERVO CONTROL ATTACHMENT POINTSACCESS: 575CB 575GB* 0.18675CB 675GB* 0.18574414-0502-1 582 ATTACHMENT OUTER AIRBRAKE LH/RH MEC GVI I: 3 A ISB ISB 57-00521 0.20 PRE 016985831 0.20 (57-0053)682 GENERAL VISUAL CHECK OF OUTER AIRBRAKE1 0.20 PRE 01872683 INNERMOST OUTER HINGE BRACKETS FOR CRACKS1 0.20 (57-0064)SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:2-57 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)574600-0505-1 520 ATTACHMENT-FLIGHT SURFACES MEC LUB I: 3 A MRB AMM 122227/0011 1.87 ALL6201 1.87CLEAN, INSPECT AND LUBRICATE:- SLAT TRACK ROLLERS (BRUSH APPLICATION)- SLAT TRACKS- SLAT TRACK ROLLER PINSACCESS: 512CB 523DB 523KB 524DB 524JB* 0.29612CB 623DB 623KB 624DB 624JB* 0.32574600-0505-2 500 ATTACHMENT-FLIGHT SURFACES MEC LUB I: 1 C MPD AMM 122257/0011 0.55 ALL6001 0.55LUBRICATION OF THE SLAT TO TRACK ATTACHMENT BOLTSACCESS: SLAT EXTENDED574600-0505-3 500 ATTACHMENT-FLIGHT SURFACES MEC LUB I: 1 C MPD AMM 122227/0011 0.60 PRE 033736001 0.60 (57-0099)LUBRICATION OF CLOSING PLATE SPRING STRUT PLUNGERACCESS: 512FB* 0.17612FB* 0.17575000-0502-1 500 FLIGHT SURFACES MEC GVI I: 1 A ISB ISB 57-00761 0.50 PRE 16446001 0.50CHECK TAPE AT SLAT LEADING EDGE SKIN SPLICESFOR PRESENCE575900-0505-1 500 FLAP DEFLECTORS MEC LUB I: 3 A MPD AMM 122257/0011 1.00 ALL6001 1.00LUBRICATION OF PIANO HINGES ON:- FLAPS DEFLECTOR DOORS AT INBOARD, INTERMEDIATE ANDOUTER POSITION. (FLAPS MUST BE EXTENDED)* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:2-57 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)711000-0802-1 450 COWLINGS ENG DET I: NOTE MPD AMM 711300/3011 0.50 GE4601 0.5001. CHECK CORRECT OPERATION AND TENSION OF FANAND THRUST REVERSER COWL LATCHES02. DETAILED INSPECTION OF HINGED AND SLIDINGCOWLS FOR SECURITY OF ATTACHMENT, SEALS FORSCRAPES, BINDING, FLUID STREAKING03. INSPECT COWL DOORS INNER AREA FOR EVIDENCE OFCRACKS, HOT SPOTS AND DISTORTIONNOTE: TASK DUE AT ENGINE CHANGE OR ONE YEAROR 2000 FH WHICHEVER OCCURS FIRSTACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07711000-0802-2 430 COWLINGS ENG FUC I: 1 C MPD AMM 711300/3012 0.50 GE4402 0.50FAN COWL LATCH TENSION CHECKACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02711000-0812-1 450 COWLINGS ENG DET I: ENG. CHG MPD AMM 711300/3011 0.50 PW460 OR NOTE1 0.5001. CHECK CORRECT OPERATION AND TENSION OF FANAND THRUST REVERSER COWL LATCHES02. DETAILED INSPECTION OF HINGED AND SLIDINGCOWLS FOR SECURITY OF ATTACHMENT, SEALS FORSCRAPES, BINDING, FLUID STREAKING03. INSPECT COWL DOORS INNER AREA FOR EVIDENCE OFCRACKS, HOT SPOTS AND DISTORTIONNOTE: TASK DUE AT ENGINE CHANGE OR ONE YEAROR 2000 FH WHICHEVER OCCURS FIRSTACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05711000-0812-2 430 COWLINGS ENG FUC I: 1 C MPD AMM 711305/5012 0.50 PW4402 0.50FAN COWL LATCH TENSION CHECK* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : POWER PLANT REV. DATE: APR 01/10 SECTION:2-71 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)711000-0812-2 * * * * * C O N T I N U E * * * * *ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02711100-0802-1 430 NOSE COWL ENG GVI I: WEEKLY MPD AMM 711100/6011 0.10 GE4401 0.10VISUAL INSPECTION OF NOSE COWL FOR LIP SKIN CRACKSAND SATISFACTORY CONDITION711100-0812-1 430 NOSE COWL ENG GVI I: WEEKLY MPD AMM 711100/6011 0.10 PW4401 0.10VISUAL INSPECTION OF NOSE COWL FOR LIP SKIN CRACKSAND SATISFACTORY CONDITION711300-0802-1 430 COWL DOORS ENG GVI I: PRE-ACPT MRB1 0.10 GE4401 0.10CHECK ALL R/H AND L/H ENGINE COWLS CLOSED ANDLATCHED711300-0805-1 450 COWL DOORS ENG LUB I: 1 C MPD AMM 122271/0011 1.00 GE4601 1.00CLEAN AND LUBRICATE LATCHES OF:- FAN COWL DOORS- THRUST REVERSER DOORS- CORE COWL DOORS- PRESSURE RELIEF DOORSACCESS: 435AL 435CL 436AR 451AL 451CL 452AR* 0.17455AL 455BL 456AR 456BR445AL 445CL 446AR 461AL 461CL 462AR* 0.16465AL 465BL 466AR 466BR711300-0812-1 430 COWL DOORS ENG GVI I: PRE-ACPT MRB1 0.10 PW4401 0.10CHECK ALL R/H AND L/H ENGINE COWLS CLOSED ANDLATCHEDSYSTEMS AND POWERPLANT PROGRAM : POWER PLANT REV. DATE: APR 01/10 SECTION:2-71 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)711300-0815-1 450 COWL DOORS ENG LUB I: 1 C MPD AMM 122271/0011 0.80 PW4601 0.80CLEAN AND LUBRICATE LATCHES OF- FAN COWL DOORS- THRUST REVERSER DOORS- PRESSURE RELIEF DOORSACCESS: 435AL 436AR 436DR 451AL 451CL 452AR* 0.09445AL 446AR 446DR 452AR 461AL 461CL* 0.08711301-0802-1 430 COWL CORE ENG GVI I: DY-TERM CN AMM 711300/5011 0.10 GE440 FAA AD CN1 0.10 PRE (71-0053)CHECK CORE COWL DOOR LATCHES 1987-132-082(B)FAA AD88-11-10R1ISB 71-0054712000-0802-1 450 MOUNTS-ENGINE ENG DET I: C MRB AMM 712000/6011 1.00 GE460 OR AMM 722300/6011 1.00DETAILED INSPECTION OF: ENG. CHG- THE FWD MOUNT, THE FRONT FLANGE OF THE HPCOMPRESSOR STATOR AND THE FAN FRAME ASSY FORSATISFACTORY CONDITION, SECURITY OF ATTACHMENTSAND CORROSION- THE AFT MOUNT, ATTACHMENT FITTINGS ON THE TURBINEMID FRAME FOR SATISFACTORY CONDITION, SECURITYOF ATTACHMENTS AND CORROSIONACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07712000-0802-2 450 MOUNTS-ENGINE ENG NDT I: ENG. CHG MRB AMM 710000/4011 2.00 GE460 CMM 712013/3011 2.00NDT INSPECTION OF FORWARD AND AFT ENGINE MOUNT BOLTSAND RUNNING CHECK ON NUTS712000-0812-1 450 MOUNTS-ENGINE ENG DET I: C MRB AMM 712002/4011 1.00 PW460 OR AMM 712003/4011 1.00DETAILED INSPECTION OF: ENG. CHG- THE FWD MOUNT, THE FRONT FLANGE OF THE HP* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : POWER PLANT REV. DATE: APR 01/10 SECTION:2-71 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)712000-0812-1 * * * * * C O N T I N U E * * * * *COMPRESSOR STATOR AND THE FAN FRAME ASSY FORSATISFACTORY CONDITION, SECURITY OF ATTACHMENTSAND CORROSION.- THE AFT MOUNT, ATTACHMENT FITTINGS ON THE ENGINEFLANGES OF THE EXHAUST CASE FOR SATISFACTORYCONDITION, SECURITY OF ATTACHMENTS AND CORROSION.712000-0812-2 450 MOUNTS-ENGINE ENG NDT I: ENG. CHG MPD AMM 710000/4011 2.00 PW460 CMM 712013/3001 2.00NDT INSPECTION OF FORWARD AND AFT ENGINE MOUNT BOLTS.( 4 BOLTS ATTACHING THE ENGINE FWD MOUNT TO THEPYRAMID AND 4 BOLTS ATTACHING THE ENGINE AFT MOUNT TOTHE PYLON BEAM. )712000-0812-3 450 MOUNTS ENGINE ENG FUC I: ENG. CHG MPD AMM 710000/4011 0.10 PW4601 0.10RUNNING CHECK TORQUE OF FWD AND AFT ENGINE MOUNTBOLTS AND NUTS712003-0802-1 430 MOUNT - FORWARD ENG DET I: 750 FH CN CN1 0.25 GE NOTE440 OR FAA AD 1995-225-IMP(B) 1 0.25DETAILED INSPECTION OF ENGINE FORWARD MOUNT 350 FC MPD FAA AD 95-17-15SIDE LINKS. SB GE 72-1092NOTE: TASK NOT REQUIRED IF SIDE LINKS REFURBISHEDWITH SERMETAL IN ACCORDANCE WITHCF6-50 SB 72-1092 (SHOP MANUAL ESM 72-23-11)ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : POWER PLANT REV. DATE: APR 01/10 SECTION:2-71 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)720000-0801-2 400 ENGINE PRIMARY FLOW CLEAN. ENG CLN I: NOTE 5-2 MPD AMM 720000/7014 1.00 GEGASPATH WATER WASH720000-0802-1 430 ENGINE ENG GVI I: PRE-ACPT MRB1 0.20 GE4401 0.20GENERAL VISUAL INSPECTION OF THE FOLLOWING AREAS FORCONDITION AND EVIDENCE OF FOREIGN OBJECT DAMAGE:(COWLINGS CLOSED)01. ENGINE INLET- AIR INTAKE- FAN ROTOR BLADES AND SPINNER (AND CHECK FREEROTATION BY HAND)- N1 SPEED SENSOR AND AREA- LOW PRESSURE COMPRESSOR INLET VANES- ACOUSTIC PANELS- ABRADABLE SHROUDS02. FAN REVERSER- DUCTS AND OUTLET GUIDE VANES03. ENGINE OUTLET- EXIT VANES- ACOUSTIC PANELS- EXHAUST DUCTS FOR FREEDOM OF FOREIGN OBJECT720000-0802-2 450 ENGINE ENG GVI I: DY-TERM MRB1 0.20 GE4601 0.20VISUAL INSPECTION OF THE FOLLOWING AREAS (COWLINGCLOSED)01. COWLING INLET FOR GENERAL CONDITION02. DRAIN MAST FOR OBSTRUCTION OR EVIDENCE OFLEAKAGE03. HYDRAULIC PUMPS SHAFT SEAL DRAIN OUTLET FOREVIDENCE OF LEAKAGE04. COWLING OUTLET FOR GENERAL CONDITION05. EXHAUST AREA FOR EVIDENCE OF OIL LEAKAGE06. TAIL PIPE FOR METAL DEPOSIT07. LAST LP TURBINE STAGE BLADES FOR GENERALCONDITION720000-0802-3 430 ENGINE ENG GVI I: 3 A MRB CE: 1 1.00 GE4401 1.00VISUAL INSPECTION OF ENGINE COMPONENTS IN FOLLOWING* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)720000-0802-3 * * * * * C O N T I N U E * * * * *SYSTEMS:- FUEL FEED- ENGINE CONTROL AND INDICATING- ENGINE VANE AND ENGINE BLEED AIR- BLEED AIR AND PNEUMATIC (INCLUDING STARTERAIR SUPPLY)- OIL- IGNITION- HYDRAULIC POWER- ELECTRICAL POWER- THRUST REVERSER DRIVE AND AIR SUPPLYFOR SECURITY OF ATTACHMENT, GENERAL CONDITION, DAMAGEAND FREEDOM FROM FUEL, OIL AND AIR LEAKSACCESS: 435AL 455AL 456AR* 0.04445AL 465AL 466AR* 0.04720000-0803-1 400 ENGINE ENG FUC I: AT SHOP MRB AMM 710000/4011 1.00 GEVISITFUNCTIONAL BENCH TEST IN LIEU OF DISASSEMBLY FOR THEFOLLOWING ENGINE ITEMS:- MAIN FUEL PUMP- MAIN ENGINE CONTROL- PNEUMATIC DRIVE UNIT AND CONTROL- OIL AND SCAVENGE PUMPNOTE: REFER TO RULES 1 AND 2 (SECTION 8 INTRUDUCTION)720000-0803-2 400 ENGINE ENG GVI I: AT SHOP MRB AMM 710000/4011 2.50 GEVISITOPPORTUNITY INSPECTION AT SHOP DISASSEMBLY FORFOLLOWING POWER PLANT ITEMS:- FAN MODULES- FAN ROTOR- FAN STATOR- FAN FRAME & CASE- FAN MID SHAFT- COMPRESSOR MODULES- COMPRESSOR ROTOR- COMPRESSOR FRONT STATOR- COMPRESSOR REAR STATOR* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)720000-0803-2 * * * * * C O N T I N U E * * * * *- COMPRESSOR REAR FRAME- COMBUSTION SECTION- COMBUSTION LINER- TURBINE MODULES- HPT STAGE 1 NOZZLE- HPT STAGE 2 NOZZLE- HPT ROTOR- TURBINE MID FRAME- LPT STAGE 1 NOZZLE- LPT STATOR- LPT ROTOR- TURBINE REAR FRAME- ACCESSORY DRIVE MODULES- INLET GEARBOX- RADIAL DRIVE SHAFT- TRANSFER GEARBOX- HORIZONTAL DRIVE SHAFT- ACCESSORY GEARBOXNOTE: REFER TO RULES 1 AND 2 (SECTION 8 INTRODUCTION)720000-0811-1 400 ENGINE PRIMARY FLOW CLEAN. ENG CLN I: NOTE 5-2 MPD AMM 720000/7014 1.00 PWGASPATH WATER WASH720000-0812-1 430 ENGINE ENG GVI I: PRE-ACPT MRB1 0.20 PW4401 0.20GENERAL VISUAL INSPECTION OF THE FOLLOWING AREAS FORCONDITION AND EVIDENCE OF FOREIGN OBJECT DAMAGE:(COWLINGS CLOSED)01. ENGINE INLET- AIR INTAKE- FAN ROTOR BLADES AND SPINNER (AND CHECK FREEROTATION BY HAND)- N1 SPEED SENSOR AND AREA- LOW PRESSURE COMPRESSOR INLET VANES- ACOUSTIC PANELS- ABRADABLE SHROUDS02. FAN REVERSER- DUCTS AND OUTLET GUIDE VANES03. ENGINE OUTLET* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)720000-0812-1 * * * * * C O N T I N U E * * * * *- EXIT VANES- ACOUSTIC PANELS- EXHAUST DUCTS FOR FREEDOM OF FOREIGN OBJECT720000-0812-2 450 ENGINE ENG GVI I: DY-TERM MRB1 0.20 PW4601 0.20VISUAL INSPECTION OF THE FOLLOWING AREAS (COWLINGCLOSED)01. COWLING INLET FOR GENERAL CONDITION02. DRAIN MAST FOR OBSTRUCTION OR EVIDENCE OFLEAKAGE03. HYDRAULIC PUMPS SHAFT SEAL DRAIN OUTLET FOREVIDENCE OF LEAKAGE04. COWLING OUTLET FOR GENERAL CONDITION05. EXHAUST AREA FOR EVIDENCE OF OIL LEAKAGE06. TAIL PIPE FOR METAL DEPOSIT07. LAST LP TURBINE STAGE BLADES FOR GENERALCONDITION720000-0812-3 430 ENGINE ENG GVI I: 3 A MRB: 1 1.00 PW4401 1.00VISUAL INSPECTION OF ENGINE COMPONENTS IN FOLLOWINGSYSTEMS:- FUEL FEED- ENGINE CONTROL AND INDICATING- ENGINE VANE AND ENGINE BLEED AIR- BLEED AIR AND PNEUMATIC (INCLUDING STARTERAIR SUPPLY)- OIL- IGNITION- HYDRAULIC POWER- ELECTRICAL POWER- THRUST REVERSER DRIVE AND AIR SUPPLYFOR SECURITY OF ATTACHMENT, GENERAL CONDITION, DAMAGEAND FREEDOM FROM FUEL, OIL AND AIR LEAKSACCESS: 435AL 455AL 456AR* 0.04445AL 465AL 466AR* 0.04SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)720000-0813-1 400 ENGINE ENG FUC I: AT SHOP MRB AMM 710000/4011 1.00 PWVISITFUNCTIONAL - BENCH TEST IN LIEU OF DISASSEMBLY FORFOLLOWING ENGINE ITEMS:- MAIN FUEL PUMP- FUEL CONTROL UNIT- ENGINE VANE AND BLEED CONTROL- PNEUMATIC DRIVE UNIT & CONTROLNOTE: REFER TO RULES 1 AND 2 (SECTION 8 INTRODUCTION)720000-0813-2 400 ENGINE ENG GVI I: AT SHOP MRB AMM 710000/4011 4.00 PWVISITOPPORTUNITY INSPECTION AT SHOP DISASSEMBLY FORFOLLOWING POWER PLANT ITEMS:- INLET CONE/FAN ROTOR ASSY- FRONT COMPRESSOR ROTOR AND STATOR ASSY- FAN CASE ASSY- INTERMEDIATE CASE ASSY- REAR COMPRESSOR ROTOR AND STATOR ASSY- TURBINE SHAFT COUPLING ASSY- DIFFUSER CASE ASSY- COMBUSTION CHAMBER AND 1. STAGE TURBINE NOZZLEGUIDE VANE ASSY- REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY- FRONT COMPRESSOR DRIVE TURBINE ROTOR AND STATORASSY- TURBINE EXHAUST CASE- MAIN GEAR BOX AND DRIVE SHAFT ASSYNOTE: REFER TO RULES 1 AND 2 (SECTION 8 INTRODUCTION)722100-0802-1 430 FAN ROTOR ASSEMBLY MEC NDT T: REFER AD CN CN1 3.00 GE440 I: REFER AD FAA AD 1991-053-IMP(B) 1 3.00AN ULTRASONIC AND FLUORESCENT PENETRANT (FPI) FAA AD 91-01-04INSPECTION OF THE STAGE 1 FAN DISK DOVETAIL POST. SB GE 72-999722100-0802-2 430 FAN AND LP COMPRESSOR SECT. ENG DET I: 1 A MRB AMM 722100/6011 0.50 GE440 AMM 722200/6011 0.50DETAILED INSPECTION OF:- FAN ROTOR BLADES (WITH PARTICULAR ATTENTION TOBLADES LEADING AND TRAILING EDGES, TIPS AND MIDSPAN SHROUDS) FOR DAMAGE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)722100-0802-2 * * * * * C O N T I N U E * * * * *- LOW PRESSURE COMPRESSOR I.G.V.722100-0805-1 430 FAN ROTOR ASSEMBLY MEC LUB I: 1000 FC CESM AMM 722100/6012 6.00 GE440 GE-CESM 76 REV2 6.0001. DETAILED INSPECTION OF FAN BLADES 9AND FAN DISK02. RELUBE DOVETAILS AND MIDSPAN SHROUDS WITH SPRAYLUBE- MOLYBDENUM DISULFIDE C02-004PREP.: FAN SPINNER AND BLADES REMOVE722100-0812-1 430 FAN AND LP COMPRESSOR SECTION MEC DET I: 1 A MRB AMM 722105/6011 0.50 PW440 AMM 723102/6011 0.50DETAILED INSPECTION OF:- FAN ROTOR BLADES (WITH PARTICULAR ATTENTION TOBLADES LEADING AND TRAILING EDGES,TIPS AND MIDSPAN SHROUDS) FOR DAMAGE.- LOW PRESSURE COMPRESSOR I.G.V.722100-0812-2 430 FAN AND LP COMPRESSOR SECT. ENG GVI I: 3 A MRB AMM 720000/2011 0.30 PW4401 0.30VISUAL CHECK OF PIPES AND WIRINGS OF FUELHEATER, IGV ANTI-ICING TURBINE CASE COOLING FOR SECU-RITY AND DAMAGE OF ATTACHMENTS INSTALLATIONS EXTERNALLEAKAGE AND SIGNS OF OVERHEATINGACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07722100-0815-1 430 FAN ROTOR ASSEMBLY ENG LUB I: 1 A MPD AMM 722103/2011 0.50 PW4401 0.5001. CLEAN BOTH SIDES OF PART SPAN SHROUDS02. APPLY LUBRICANT ON BOTH SIDES OF ALLPART SPAN SHROUDS722300-0802-1 430 FAN FRAME ASSEMBLY ENG GVI I: C MPD AMM 722300/6011 0.30 GE440 OR1 0.30* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)722300-0802-1 * * * * * C O N T I N U E * * * * *GENERAL VISUAL INSPECTION OF ENGINE FAN SECTION SHOP VIS(FAN FRAME AND CASING) FOR CONDITION AND EVIDENCEOF DAMAGEACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05722300-0812-1 430 FAN FRAME ASSEMBLY ENG GVI I: C MPD AMM 722000/0011 0.30 PW440 OR1 0.30GENERAL VISUAL INSPECTION OF ENGINE FAN SECTION SHOP VIS(FAN FRAME AND CASING) FOR CONDITION AND EVIDENCEOF DAMAGEACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723000-0802-1 430 ENGINE COMPRESSOR SECTION ENG DET I: C MPD AMM 723100/0011 0.50 GE440 OR1 0.50DETAILED INSPECTION OF ENGINE COMPRESSOR SHOP VISSECTION FOR SATISFACTORY CONDITION, CRACKS, DENTS,INSTALLATION FOR SECURITY OF ATTACHMENT, HOT SPOTSAND MISSING, LOOSEN OR BROKEN BOLTSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723000-0812-1 430 ENGINE COMPRESSOR SECTION ENG DET I: C MPD AMM 723200/2011 0.50 PW440 OR1 0.50DETAILED INSPECTION OF ENGINE COMPRESSOR SHOP VISSECTION FOR SATISFACTORY CONDITION, CRACKS, DENTS,INSTALLATION FOR SECURITY OF ATTACHMENT, HOT SPOTSAND MISSING, LOOSEN OR BROKEN BOLTSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723100-0802-2 450 COMPRESSOR ROTOR BLADES ENG BSI T: NOTE CESM AMM 723100/2012 2.00 GE460 I: 450 FC NTM GE 7230002 2.00 PREBOROSCOPE INSPECTION OF COMPRESSOR ROTOR BLADES STAGE PART 7SB GE 72-877* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)723100-0802-2 * * * * * C O N T I N U E * * * * *14 FOR DOMESTIC OBJECT DAMAGE GE-CESM 76 REV9NOTE:1 IF T/E DAMAGE IS FOUND INSPECT FOR POSSIBLESTG.14 JOINT BOLT FAILURENOTE:2 TH= 750 FC PRE 72-724TH= 300 FC POST 72-724ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723100-0802-3 450 COMPRESSOR ROTOR BLADES ENG BSI I: 1000 FC CESM AMM 723100/2011 0.50 GE460 NTM 7230001 0.50 PREBOROSCOPE INSPECTION OF STAGE 1 HPC BLADES FOR PART 7SB GE 72-743MIDSPAN COATING WEAR. GE-CESM 76 REVOR9PRENOTE: FIRST INSPECTION SINCE NEW : 2400 CY IFSB GE 72-842OPERATING IN A HOSTILE ENVIRONMENTACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723100-0804-1 450 COMPRESSOR ROTOR MEC NDT I: NOTE CN CN1 1.50 GE460 FAA AD 1991-135IMP(B)1 1.50A FLUORESCENT PENETRANT INSPECTION ON THE HPC REAR FAA ADSHAFT. 91-10-03R1NOTE: INITIAL AND SUBSEQUENT INSPECTIONS AS PERAD 91-10-03R1 / CN 1991-135-IMP(B).ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723100-0813-1 450 COMPRESSOR ROTOR ENG NDT T: 7500 FC AOW AOW PW JT9/2 12.00 PW460 I: 4000 FC 72-35/PSE:LEF:2 12.00 P/N -78991401. REMOVE ENGINE NOTE 2 8-4-25-1-79011402. SHOP DISASSEMBLY FOR INSPECTION OF THE 14TH STAGE SB PW A5806-791214COMPRESSOR DISK REAR FLANGE03. REINSTALL ENGINE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)723100-0813-1 * * * * * C O N T I N U E * * * * *NOTE 1:TASK BE PERFORMED AT THE OPPORTUNITY OF ANENGINE CHANGENOTE 2:THE CYCLES QUOTED ARE PART CYCLES723200-0802-1 450 COMPRESSOR VARIABLE STATOR ENG DET I: 5 A MPD AMM 723200/2011 0.50 GE4601 0.50 PRE SBDETAILED INSPECTION OF VSV ACTUATING SYSTEMGE 72-548WITH PARTICULAR ATTENTION TO VSV LEVERS FOR BENDINGAND LOOSENESS (STAGE 3 TO 6)723200-0802-2 450 COMPRESSOR VANES ENG BSI T: 650 FC CESM AMM 723100/2011 4.00 GE460 I: 450 FC NTM 7230001 4.00BOROSCOPE INSPECTION COMPLETE CIRCUMFERENCE PART 7( PORTS B1-6 AND B1-7 ) OF HPC. GE-CESM REV 9VANES STAGE 6 AND 7 TRAILING EDGE ROOT FOR NOTCHES.NOTE : INSPECTION NOT REQUIRED IF NO EROSION PROBLEMEXIST OR IF SHOP WORKSHOP ENTAILS PEVENTIONPLANACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723200-0802-3 450 COMPRESSOR VARIABLE STATOR ENG DET T: 1500 FC MPD AMM 723200/2011 0.50 GE460 I: 1500 FC1 0.50 POST SBDETAILED INSPECTION OF VSV ACTUATING SYSTEMGE 72-548WITH PARTICULAR ATTENTION TO VSV LEVERS FOR BENDINGAND LOOSENESS (STAGE 3 TO 6)723200-0812-1 430 COMPRESSOR VARIABLE STATOR ASSEMBLY MEC GVI I: 1 C EMP PW JT9D EMP1 0.50 PW4401 0.50GENERAL VISUAL INSPECTION OF VARIABLE VANE ARMS FORENTRAPPED FOREIGN MATERIAL, BENT, DISTORTED ORDETACHED VANE ARMS.ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)723300-0802-1 450 COMPRESSOR REAR STATOR ASSY ENG DET I: SB SB AMM 723300/2011 0.50 GE460 GE-CESM 76 REV1 0.50DETAILED INSPECTION OF REAR COMPRESSOR CASE 9AFT FLANGE BOLT HOLES AND HORIZONTAL FLANGE WELD SB GE 72-898JOINT FOR CRACKING.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723300-0802-2 450 COMPRESSOR REAR STATOR ASSY ENG DET I: 250 FC SB AMM 723300/2011 0.20 GE460 GE-CESM 76 REV1 0.20 PRE SBDETAILED INSPECTION OF REAR COMPRESSOR CASE 9GE 72-861HORIZONTAL FLANGE WELD JOINT FOR CRACKING. SB GE 72-861ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723300-0802-3 450 COMPRESSOR REAR STATOR ASSY ENG GVI T: 1200 CSN SB SB GE 72-0991 0.30 GE460 I: 250 FC1 0.30 PRE SBVISUAL INSPECTION OF CIRCUMFERENTIAL RIB OF HPCGE 72-099CASE FOR CRACKS, NICKS, DENTS, GOUGES AND SCRATCHESACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723300-0802-4 450 COMPRESSOR REAR STATOR ASSY. MEC GVI I: 600 FH MRB AMM 723300/2011 1.20 GE460 OR1 1.20VISUAL INSPECTION OF REAR COMPRESSOR CASE FLANGES AND 400 FCWELD JOINTS FOR CRACKINGACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723400-0802-2 450 COMPRESSOR REAR FRAME ASSEMBLY NDT SDI T: SB 72-839 SB NTM 7230001 0.75 GE460 I: SB 72-839 PART 61 0.75EDDY CURRENT/FLUORESCENT PENETRANT INSPECTION OF CRF SB GE 72-839IGNITER PORTS AND FUEL NOZZLE PADS FOR CRACKINGNOTE: APPLICABLE ON FRAMES AFFECTED BY SB 72-839SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)723400-0802-3 450 COMPRESSOR REAR FRAME ASSEMBLY NDT SDI T: 5000 CSN CESM AMM 723400/6011 1.00 GE460 I: 1000 FC NTM 7230001 1.00ULTRASONIC/FLUORESCENT PENETRANT/ EDDY CURRENT PART 4/6INSPECTION OF CRF MID FLANGE SB GE 72-780SB GE 72-837NOTE : FOR POST SB GE 72-0853 AND SB GE 72-0820,FIRST INSPECTION IS NOT REQUIRED UNTIL8500 CSN.ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07723400-0802-4 450 COMPRESSOR REAR FRAME ENG DET T: 1750 CSN SB AMM 723400/6011 0.20 GE460 I: 250 FC SB GE 72-7501 0.20 PREVISUAL INSPECTION OF:04685(71-0050)- FIRE WALL AND SEAL FOR GENERAL CONDITIONSB GE 72-750ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723400-0802-5 450 COMPRESSOR REAR FRAME ASSY. MEC DET T: NOTE SB GE-CESM 76 REV1 1.00 GE460 I: 450 FC 91 1.00DETAILED INSPECTION OF COMPRESSOR REAR FRAME SB GE 72-758FORWARD FLANGES (WITHOUT DOUBLERS INSTALLED) FORCRACKSNOTE: FIRST INSPECTION: 1750 CSN (PRE SB GE 72-876)3500 CSN (POST SB GE 72-876)ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05723400-0802-6 450 COMPRESSOR REAR FRAME ASSY. MEC DET I: SB SB GE-CESM 76 REV1 1.00 GE460 91 1.00DETAILED INSPECTION OF COMPRESSOR REAR FRAME SB GE 72-758FORWARD FLANGES (WITH DOUBLERS INSTALLED) FOR CRACKS.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)724000-0812-1 430 DIFFUSER CASE ASSY ENG NDT I: PW SB CN AMM 724103/6011 2.00 PW440 5749 FAA AD CN1 2.00NDT INSPECTION OF DIFFUSER CASE REAR RAIL FOR CRACKS 1999-292-IMP(B)FAA AD 99-11-09ACCESS: 435AL 436AR 451AL 452AR SB PW 5749* 0.05445AL 446AR 461AL 462AR* 0.05724000-0812-2 430 DIFFUSER CASE ASSY ENG GVI I: C MRB AMM 724103/6011 0.50 PW440 OR1 0.50VISUAL INSPECTION OF DIFFUSER CASE ASSY (WITH SHOP VISPARTICULAR ATTENTION TO CIRCUMFERENTIAL FLANGES) FORDAMAGE, WELD CRACKS SCORES AND SCRATCHES CHECK FIREWALL AND SEAL FOR GENERAL CONDITIONACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05724100-0802-1 450 COMBUSTION LINER ASSEMBLY INP BSI T: 900 CSI CESM AMM 724100/6011 2.00 GE460 I: 450 FC MRB NTM GE 7240001 2.00BOROSCOPE INSPECTION OF COMBUSTION LINER ASSEMBLY AND PART 7DOME AREAS IN ACCORDANCE WITH GE NTM. GE-CESM 76 REV9ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07724100-0802-2 450 COMBUSTION LINER ASSEMBLY INP BSI T: 75 HSN CESM NTM GE 7251001 3.00 GE460 I: 450 FC PART 71 3.00 PREBOROSCOPE INSPECTION OF COMBUSTION LINER FOR GE-CESM 76 REVSB GE 72-717INDICATION OF "FISHMOUTH SEAL" FAILURE (INNER). 9PREINSPECT HPT NOZZLE VANE LEADING EDGE AT 5-7 O ́CLOCK SB GE 72-688SB GE 72-688POSITION FOR INDICATION OF DISCOLORATION AND BURNING.ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07724100-0802-4 450 COMBUSTION LINER ASSEMBLY MEC GVI I: 450 FC CESM AMM 724100/6012 TBD GE460 GE-CESM 76 REV2 TBDVISUAL INSPECTION OF COMBUSTOR MOUNTING PINS FOR WEAR 9ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)724100-0802-4 * * * * * C O N T I N U E * * * * *445AL 446AR 461AL 462AR 465AL 466AR* 0.07724400-0812-1 450 COMBUSTION CHAMBER INP BSI T: 1000 HSN MRB AMM 720000/6011 2.00 PW460 OR1 2.00 POST SB PW 5195BOROSCOPE INSPECTION OF COMBUSTION CHAMBER 750 CSNPOST SB PW 5189I: 600 FHNOTE: INSPECTION TO BE CARRIED OUT TOGETHER WITH ORREFER TO 725100-0812-1 400 FCACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05724400-0812-2 450 COMBUSTION CHAMBER INP BSI I: 125 FC MPD AMM 720000/6011 1.50 PW4601 1.50 PRE SB PW 5195BOROSCOPE INSPECTION OF COMBUSTION CHAMBERPRE SB PW 5189ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05725000-0812-1 450 TURBINE SECTION MEC NDT I: PW SB CN CN 1994-213(B)1 3.00 PW460 5979 FAA AD FAA AD 94-10-09 1 3.00 PRE SB PW 5847AN EDDY CURRENT INSPECTION OF THE TURBINE 6TH STAGE SB PW 5979ORAIRSEAL KNIFE EDGES.PRE SB PW 6054725000-0812-2 450 TURBINE SECTION MEC NDT I: REFER CN CN CN1 3.00 PW460 FAA AD 1991-070-IMP(B) 1 3.00NDT INSPECTION OF THE HPT FIRST STAGE DISK COOLING FAA AD 91-04-10AIR HOLES.725000-0812-3 450 TURBINE SECTION MEC NDT I: PW SB CN CN 1994-213(B)1 2.00 PW460 5978 FAA AD FAA AD 94-10-09 1 2.00 PRE SB PW 6054A BORESCOPE AND EDDY CURRENT INSPECTION OF THE SB PW 5978TURBINE 6TH STAGE AIRSEAL RETAINING WING.725000-0814-1 450 TURBINE SECTION ENG NDT I: 2000 FC MPD AMM 710000/4012 12.00 PW460 SB PW SB 56682 12.00 PRE SB PW 5416- REMOVE ENGINE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)725000-0814-1 * * * * * C O N T I N U E * * * * *- SHOP VISIT FOR HPT MODULE DISASSEMBLY- PERFORM EDDY CURRENT CRACK INSPECTION OF THE 2NDSTAGE TURBINE AIRSEAL (LENTICULAR AIRSEAL)IN ACCORDANCE WITH PW SB 5668- REINSTALL HPT MODULE ASSEMBLY- REINSTALL ENGINEACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05725000-0814-2 450 TURBINE SECTION ENG NDT I: 3000 FC MPD AMM 710000/4012 12.00 PW460 SB PW SB 57862 12.00 POST SB PW 5416- REMOVE ENGINE- SHOP VISIT FOR HPT MODULE DISASSEMBLY- PERFORM EDDY CURRENT CRACK INSPECTION OF THE 2NDSTAGE TURBINE AIRSEAL (LENTICULAR AIRSEAL)IN ACCORDANCE WITH PW SB 5786- REINSTALL HPT MODULE ASSEMBLY- REINSTALL ENGINEACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05725100-0802-1 450 HP-TURBINE STAGE 1 INP BSI I: 450 FC CESM AMM 725100/6011 2.00 GE460 MRB NTM GE 7251001 2.00BOROSCOPE INSPECTION OF HPT NOZZLE STAGE 1 (HPTN-1) PART 7VIA COMBUSTION PORTS AND PORTS BETWEEN 5 AND 7 GE-CESM 76O ́CLOCK POSITIONACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07725100-0812-1 450 HP-TURBINE, STAGE 1 INP BSI I: 600 FH MRB AMM 720000/6011 2.00 PW460 OR1 2.00BOROSCOPE INSPECTION OF HPT NOZZLE GUIDE VANES STAGE 400 FC1 (NGV-1) VIA COMBUSTION PORTSNOTE: INSPECTION TO BE CARRIED OUT TOGETHER WITHCOMBUSTION CHAMBER INSPECTION, REFER TO724400-0812-1SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)725200-0812-1 450 2ND STAGE HP-TUR.STAT.VANES ENG BSI T: REFER AD CN AMM 720000/6011 2.00 PW460 I: 1000 FH FAA AD CN1 2.00BORESCOPE INSPECTION OF SECOND STAGE HP TURBINE VANES 1993-159-IMP(B)FAA AD 93-14-20ACCESS: 435AL 436AR 451AL 452AR SB PW 5667* 0.05445AL 446AR 461AL 462AR* 0.05725300-0802-1 450 HP-TURBINE ASSY. INP BSI T: NOTE CESM AMM 725300/2011 2.00 GE460 I: 450 FC MRB NTM GE 7253001 2.00BOROSCOPE INSPECTION OF HP TURBINE ROTOR BLADES PART 7STAGE 1 GE-CESM 76NOTE: FIRST INSPECTION- 4500 TSN/800 CSN FOR BLADES CONFIGURATION2 AND 3 (POST GE SB 72-466 OR 72-247)- 5000 TSN/1200 CSN FOR BLADES CONFIGURATION 4(POST GE SB 72-757)ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07725300-0802-3 450 HP-TURBINE ASSY. INP BSI T: 1200 CSN CESM AMM 725300/2011 1.00 GE460 I: 450 FC NTM GE 7253001 1.00BOROSCOPE INSPECTION OF HP TURBINE ROTOR BLADES STAGE PART 72.PAY PARTICULAR ATTENTION TO BLADE LEADING EDGE FOR GE-CESM 76 REVDAMAGE INDICATING POSSIBLE STAGE 2 NOZZLE DEFECTS 9SUCH AS BENDING OR TORSION OR SAG(REPAIRED STG 2 NOZZLE ASSEMBLIES.)ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07725300-0802-4 450 HP TURBINE ASSY NDT SDI I: 400 FC CN CN2 1.00 GE460 NOTE FAA AD 1991-232-IMP(B) 2 1.00 PRENDT (EDDY CURRENT) OF THE HPTR THERMAL SHIELD FAA AD 91-15-16 SB GE 72-0885GE-CESM 109NOTE: INSPECTION IS NOT REQUIRED IF THE THERMAL SB GE 72-879SHIELD IS INSTALLED WITH PIP INTERSTAGE SEALSOR HAS NEVER BEEN INSTALLED WITH PRE-PIPINTERSTAGE SEALS OR THE THERMAL SHIELD IS A"STEP TOOTH" DESIGN* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)725300-0802-4 * * * * * C O N T I N U E * * * * *ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07725300-0803-1 450 HP TURBINE ASSY NDT SDI I: NOTE CN CN1 1.00 GE460 FAA AD 1983-011-IMP(B) 1 1.00FLUORESENT PENETRANT INSPECTION OF HPT FAA AD 82-25-08SPACER/IMPELLER SB GE 72-748NOTE: INITIAL AND SUBSEQUENT INSPECTION AS PERAD 82-25-08/CN 1983-011-IMP(B)ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07725300-0812-1 450 HP-TURBINE ASSY. INP BSI T: 1000 HSN MRB AMM 720000/6011 2.00 PW460 OR1 2.00BOROSCOPE INSPECTION OF HP TURBINE ROTOR BLADES 750 CSNSTAGE 1 I: 600 FHORACCESS: 451AL 452AR 400 FC* 0.02461AL 462AR* 0.02725300-0812-2 450 HP TURBINE ASSY ENG GVI I: 1500 FC MPD SB PW 55511 1.00 PW460 NOTE1 1.00INSPECT NO.4 OIL PRESSURE TUBE, P/N 738535 OR 785544FOR EVIDENCE OF COKING AND CLEAN AS NECESSARYNOTE: IF LITTLE OR NO COKING IS FOUND INSPECTIONINTERVAL CAN BE EXTENDED TO 2500 CY.725400-0802-2 450 TURBINE MID-FRAME ASSEMBLY ENG NDT I: REFER AD CN CN1 1.00 GE460 FAA AD 1991-019-IMP(B) 1 1.00VISUAL AND ULTRASONIC INSPECTION OF TURBINE MID-FRAME FAA AD 90-23-15AFT FLANGE FOR CRACKS SB GE 72-957NOTE: INITIAL AND SUBSEQUENT INSPECTIONS AS PERAD 90-23-15/CN 1991-019-IMP(B).SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)725400-0802-3 450 ENGINE TURBINE MID FRAME ENG GVI T: NOTE CESM AMM 725400/2011 2.00 GE460 I: NOTE GE-CESM 76 REV1 2.00VISUAL INSPECTION OF THE ENGINE TURBINE MID FRAME 9(TMF): SB GE 72-658- LINER FOR CLOCKING- HAT SECTION AND T/C BOSS FOR CRACKINGNOTE: -FOR LINER CLOCKING PRE GE SB 72-658FIRST INSPECTION : 1500 CSNI : 750 FC-FOR OUTER CASE CRACKING (HAT SECTIONS, INSTRU-MENTATION BOSSES,SKIN WELDS):FIRST INSPECTION : 1500 CSNI : 450 FCACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07725600-0802-1 450 LOW PRESSURE TURBINE STATOR ENG GVI I: 750 FH CN CN1 TBD GE460 FAA AD 2001-108-IMP(B) 1 TBD PREGENERAL VISUAL INSPECTION OF LPT NOZZLE LOCKS FAA ADSB GE 72-A12012001-04-16SB GE 72-A1197725700-0802-1 430 LP TURBINE ROTOR BLADES ENG DET I: 1 A MRB AMM 725700/2011 0.50 GE4401 0.50DETAILED INSPECTION OF LP TURBINE ROTOR BLADESFOR DAMAGE (LAST STAGE)725700-0802-2 450 LOW PRESSURE TURBINE ROTOR ENG BSI I: 150 FC CESM AMM 725700/2012 2.00 GE460 NTM GE 7257002 2.00 PREBORESCOPE/VISUAL INSPECTION OF STAGE 4 BLADES/TIP PART 7SB GE 72-0675INTERLOCK WEAR. GE-CESM 76 REV9ACCESS: 435AL 436AR 455AL 456AR SB GE 72-227* 0.05445AL 446AR 465AL 466AR* 0.05725700-0802-3 450 LOW PRESSURE TURBINE ROTOR ENG BSI I: 450 FC CESM AMM 725700/2012 2.00 GE460 NTM GE 7257002 2.00 POSTBORESCOPE/DETAILED INSPECTION OF STAGE 4 BLADE PART 7SB GE 72-0675* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)725700-0802-3 * * * * * C O N T I N U E * * * * *TIP INTERLOCKS FOR WEAR GE-CESM 76 REV9ACCESS: 435AL 436AR 455AL 456AR SB GE 72-675* 0.05445AL 446AR 465AL 466AR* 0.05725700-0802-4 450 LOW PRESSURE TURBINE ROTOR ENG BSI I: NOTE SB GE-CESM 76 REV2 2.00 GE460 92 2.00 PREBORESCOPE INSPECTION OF LOW PRESSURE TURBINE STAGE 1 SB GE 72-1251SB GE 72-1239BLADES/DISK FOR RUBS FROM TMF STRUT STUD FAILURENOTE: INTERVAL IN ACCORDANCE WITH VENDORRECOMMENDATIONSACCESS: 435AL 436AR 455AL 456AR* 0.05445AL 446AR 465AL 466AR* 0.05725700-0812-1 430 LP TURBINE ROTOR BLADES MEC DET I: 1 A MRB AMM 725000/6011 0.50 PW4401 0.50DETAILED INSPECTION OF LP TURBINE ROTOR BLADESFOR DAMAGE (LAST STAGE)725800-0812-1 450 TURBINE EXHAUST CASE ASSY ENG GVI I: C MPD AMM 725800/6011 0.50 PW460 OR1 0.50GENERAL VISUAL INSPECTION OF TURBINE EXHAUST CASE FOR SHOP VISCONDITION, HOT SPOTS AND CRACKSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05726000-0802-1 450 ACCESSORY DRIVE SECTION ENG GVI I: 1000 FH MRB AMM 726500/6011 0.20 GE4601 0.20VISUAL INSPECTION OF ENGINE ACCESSORY DRIVE SECTIONFOR SATISFACTORY CONDITIONS, CRACKS, FREEDOM FROMLEAKAGE (WITH PARTICULAR ATTENTION TO MOUNTING LUGSAND BRACKETS).ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)726000-0802-2 450 ACCESSORY DRIVE SECTION ENG GVI I: 450 FC CESM AMM 726500/6011 0.50 GE460 GE-CESM 76 REV1 0.50VISUAL INSPECTION OF LH LINK MOUNT SPHERICAL BEARING 9FOR EVIDENCE OF WEAR AND MOUNT BRACKET FOR CRACKINGACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05726000-0812-1 450 ACCESSORY DRIVE SECTION ENG GVI I: C MRB AMM 726500/0011 0.20 PW460 OR1 0.20VISUAL INSPECTION OF ENGINE ACCESSORY DRIVE SECTION SHOP VISFOR SATISFACTORY CONDITIONS, CRACKS, FREEDOM FROMLEAKAGE (WITH PARTICULAR ATTENTION TO MOUNTING LUGSAND BRACKETS).ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05726300-0802-1 450 TRANSFER GEARBOX ENG GVI I: 150 FC CESM AMM 726300/6011 0.20 GE460 GE-CESM 76 REV1 0.20CHECK FLUID FITTING (ROZAN INSERTS) FOR LOOSENESS/ 9LEAKAGE.ACCESS: 435AL 436AR 451AL 455AL* 0.05445AL 446AR 461AL 465AL* 0.05* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION:2-72 PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)731000-0802-1 430 ENGINE FUEL AND CONTROL ENG GVI I: SB 73-007 CN CN1 1.00 GE440 FAA AD 1985-165-071(B) 1 1.00 PRE 05912INSPECT ENGINE FUEL FLOWMETER INLET TUBE ASSEMBLY. FAA AD 85-16-06 (73-0007)ISB 73-0007ACCESS: 435AL* 0.01445AL* 0.01731200-0801-1 430 FUEL FILTER (ENGINE) ENG RAR T: NOTE MRB AMM 731203/6011 1.00 GE440 I: 1000 FH SIL SIL 73-0111 1.00DISCARD FUEL FILTER ELEMENT AND INSTALL A NEW ONE.NOTE: REPLACE FILTER ELEMENT AT 150 FH AND 450 FHAFTER A/C DELIVERY OR MAJOR TANK REPAIRACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05731200-0802-1 430 FUEL PUMP ENG CLN T: NOTE CESM AMM 731201/6011 0.75 GE440 I: 1500 FC GE-CESM 76 REV1 0.75INSPECTION AND CLEANING OF FUEL PUMP CARTRIDGE 9STRAINER ELEMENTNOTE: AFTER FUEL TANK MAINTENANCE OR A/C DELIVERYTHE TASK SHOULD BE PERFORMED WITHIN 50 FC.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05731200-0811-1 430 FUEL FILTER (ENGINE) ENG RAR T: NOTE MPD SIL 73-0071 1.00 PW440 I: 1 C SIL1 1.00REMOVE, INSPECT AND REPLACE FUEL PUMP FILTER ELEMENTNOTE: REPLACE FILTER ELEMENT AT 150 FH AND 450 FHAFTER A/C DELIVERY OR MAJOR TANK REPAIRACCESS: 435AL* 0.01445AL* 0.01731201-0802-1 430 ENGINE FUEL PUMP - QAD ENG FUC I: 1500 FC CESM AMM 731201/2011 0.10 GE440 GE-CESM 76 REV1 0.10CHECK ENGINE FUEL PUMP/CONTROL PACKAGE QUICK 9* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE FUEL AND CONTROL REV. DATE: APR 01/10 SECTION:2-73 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)731201-0802-1 * * * * * C O N T I N U E * * * * *ATTACH (QAD) RING FOR PLAY AND LOCK BOLT FOR TORQUEACCESS: 435AL* 0.01445AL* 0.01731201-0812-1 430 ENGINE FUEL PUMP ENG FUC I: 4 A MPD AMM 731201/4011 0.30 PW4401 0.30CHECK ENGINE FUEL PUMP QUICK DISCONNECT NUTASSEMBLY FOR PLAY AND LOCK BOLT FOR TORQUE731301-0811-1 450 FUEL NOZZLE ENG CLN I: 3 A MPD AMM 731300/0011 1.50 PW4601 1.50 PRE SB PW 5195CLEAN FUEL NOZZLEACCESS: 451AL 452AR* 0.02461AL 462AR* 0.02731500-0812-1 436 FUEL HEATER ENG GVI I: PRE-ACPT MPD AMM 731500/0011 0.20 PW4461 0.20CHECK FUEL HEATER AIR OVERBOARD FOR EVIDENCEOF FUEL SPRAY732100-0812-1 450 FUEL CONTROL SYSTEM ENG GVI I: DY-TERM MPD AMM 732100/0011 0.20 PW4601 0.20GENERAL VISUAL INSPECTION OF TT-2 SENSORS FORCONDITION AND CLEANLINESS733000-0802-1 430 FUEL INDICATING ENG GVI I: C MRB AMM 733000/6011 0.50 GE440 OR1 0.50GENERAL VISUAL INSPECTION OF: SHOP VIS- FUEL FLOW TRANSMITTER, CONNECTOR AND HARNESS;- FUEL PRESSURE TRANSMITTER, CONNECTOR AND HARNESS;- FUEL FILTER DIFFERENTIAL SWITCH, CONNECTOR ANDHARNESS;FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,CORROSION, OVERHEATING, DETERIORATION AND FREEDOMFROM LEAKS* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE FUEL AND CONTROL REV. DATE: APR 01/10 SECTION:2-73 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)733000-0802-1 * * * * * C O N T I N U E * * * * *ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05733000-0812-1 450 FUEL INDICATING ENG GVI I: C MRB AMM 733300/0011 0.80 PW460 OR AMM 733400/0011 0.80GENERAL VISUAL INSPECTION OF: SHOP VIS- FUEL FLOW TRANSMITTER, CONNECTOR AND HARNESS;- FUEL PRESSURE TRANSMITTER, CONNECTOR AND HARNESS;- FUEL FILTER DIFFERENTIAL SWITCH, CONNECTOR ANDHARNESS;FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,CORROSION, OVERHEATING, DETERIORATION AND FREEDOMFROM LEAKSACCESS: 436AR 452AR* 0.02446AR 462AR* 0.02733400-0801-1 435 FUEL INDICATING SYSTEM ENG FUC I: ENG. CHG MRB AMM 733411/4012 1.50 GE4452 1.50FUNCTIONAL TEST OF FUEL FILTER DIFFERENTIALPRESSURE INDICATING SYSTEM.733400-0811-1 435 FUEL INDICATING SYSTEM ENG FUC I: 2 C MRB AMM 733400/5012 1.50 PW4452 1.50FUNCTIONAL TEST OF FUEL FILTER DIFFERENTIALPRESSURE INDICATING SYSTEM.733600-0811-1 210 FUEL HEATING SYSTEM ENG OPC I: ENG. CHG MRB AMM 733500/0011 0.10 PWFWD FACEOPERATIONAL TEST OF FUEL HEATING MANUAL CONTROL WITHENGINE RUNNING733600-0811-2 210 FUEL HEATING SYSTEM ENG OPC I: 1 A MRB AMM 733600/0011 0.10 PWFWD FACEOPERATIONAL TEST OF FUEL HEATING AUTOMATIC CONTROLWARNING CIRCUIT USING THE "FUEL HEATER HI TEMP TEST"PUSH BUTTON* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE FUEL AND CONTROL REV. DATE: APR 01/10 SECTION:2-73 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)740000-0802-1 430 IGNITION SYSTEM ENG GVI I: C MRB AMM 740000/2011 0.50 GE440 OR1 0.50VISUAL INSPECTION OF IGNITION EXCITERS, LEADS AND SHOP VISCOMPONENTS FOR SATISFACTORY CONDITIONACCESS: 436AR 452AR 456AR* 0.04446AR 462AR 466AR* 0.04740000-0812-1 430 IGNITION SYSTEM ENG GVI I: C MRB AMM 741101/4011 0.50 PW440 OR AMM 742101/4011 0.50VISUAL INSPECTION OF IGNITION EXCITERS, LEADS AND SHOP VISCOMPONENTS FOR SATISFACTORY CONDITIONACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05742102-0802-1 436 IGNITER PLUGS - ENGINE ENG DET I: 2 A MRB AMM 742102/4011 2.00 GE4461 2.0001. DETAILED INSPECTION OF IGNITER PLUGS FORCLEANLINESS, BURNS AND EROSION02. DEPENDING OF CONDITION OF PLUGS ROTATE PLUGS( TYPE 3 ONLY ) SO THAT PORTION OF PLUG WITHMOST EROSION IS LOCATED IN ONE OF THE LOWERQUADRANTS OF THE IGNITER PORT OR REPLACE.03. AURAL CHECK OF CONTINUOUS IGNITION SYSTEM(A AND B) AFTER IGNITER RE-INSTALLATIONACCESS: 436AR 452AR 456AR* 0.04446AR 462AR 466AR* 0.04742102-0812-1 436 IGNITER PLUGS - ENGINE ENG DET I: 2 A MRB AMM 742102/4011 2.00 PW446 AMM 742102/6011 2.0001. DETAILED INSPECTION OF IGNITER PLUGS(OR REPLACEMENT AS NECESSARY)02. AURAL CHECK OF CONTINUOUS IGNITION SYSTEM (A ANDB POSITION) AFTER RE-INSTALLATIONACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : IGNITION REV. DATE: APR 01/10 SECTION:2-74 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)750000-0802-1 450 AIR - GENERAL MEC DET I: GE SB CESM AMM 752600/6011 1.00 GE460 75-064 GE-CESM 76 REV1 1.00 PREDETAILED INSPECTION OF STAGE 8 AND 14 9SB GE 75-0077MANIFOLDS FOR CRACKS SB GE 75-064ORSB GE 75-070PREACCESS: 435AL 436AR 451AL 452AR* 0.05 SB GE 75-0078445AL 446AR 461AL 462AR* 0.05751000-0802-1 450 ANTI-ICING TUBE ENG GVI I: 150 FC CESM AMM 752201/6011 0.75 GE460 GE-CESM 76 REV1 0.75 PRECHECK 10TH STAGE ANTI-ICING TUBE FOR CRACKING 9SB GE 75-0051ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05752400-0813-1 450 ACCESSORY COOLING - TURBINE CASE COOLING ENG DET I: 1 A EMP PW JT9D EMP1 0.30 PW4601 0.30 PRE SB 6035DETAILED INSPECTION OF UPPER AND LOWER RIGHTREAR TCA TUBES AND BRACKETS FOR CRACKING,DEFORMATION, WEAR AND SECURITY OF ATTACHMENT.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05753100-0811-1 450 VSV FEEDBACK SYSTEM ENG FUC I: 2 A MPD AMM 753101/5011 0.20 PW4601 0.20FRICTION TEST OF VARIABLE STATOR VANEFEED BACK CABLEACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05753104-0812-1 450 CONTROL-ENG.VANE AND BLEED ENG DET I: 1400 FH MAN MAN1 0.20 PW460 MAN-JT9-3-921 0.20DETAILED INSPECTION OF THE ENGINE VANE ANDBLEED CONTROL (EVBC) WATER TRAP.ACCESS: 435AL* 0.01445AL* 0.01SYSTEMS AND POWERPLANT PROGRAM : ENGINE - AIR REV. DATE: APR 01/10 SECTION:2-75 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)753104-0812-2 450 CONTROL - ENGINE VANE AND BLEED ENG CHK I: 1 C EMP PW JT9D EMP1 2.50 PW4601 2.50CHECK EVC AND EVBC TRIMMING.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05753105-0811-1 450 FILTER ELEMENT-FUEL/EVBC ENG CLN T: NOTE MPD AMM 753105/5011 0.20 PW460 I: 5 A1 0.20REMOVE AND INSPECT (PH) FILTER ELEMENT OF ENGINE VANEAND BLEED CONTROL FOR FOREIGN MATTER AND/OR DAMAGESCREEN. INSTALL A NEW FILTER ELEMENT.NOTE: FIRST INSPECTION AT 3 MO AFTERENGINE OR FUEL PUMP INSTALLATION.ACCESS: 435AL* 0.01445AL* 0.01753400-0802-1 450 VBV SYSTEM FEED BACK CABLE ENG GVI I: 2 A MPD AMM 753401/2011 0.10 GE4601 0.10VISUAL INSPECTION OF VARIABLE BLEED VALVES ACTUATINGSYSTEM AND FEEDBACK MECHANISMACCESS: 435AL 451AL* 0.02445AL 461AL* 0.02753400-0812-1 450 VBV SYSTEM FEEDBACK CABLE ENG GVI I: 2 A MPD AMM 753400/4011 0.10 PW4601 0.10VISUAL INSPECTION OF 3.0 MODULATING BLEED VALVESACTUATING SYSTEM AND FEEDBACK MECHANISMACCESS: 435AL 451AL* 0.02445AL 461AL* 0.02754300-0802-2 450 LOW PRESSURE TURBINE COOLING AIR ENG DET I: 250 FC FAA AD CN1 TBD GE460 MANIFOLD 1986-003-IMP(B) 1 TBDFAA AD 85-25-56DETAILED INSPECTION OF RELATED STAGE 7 GE-CESM 76 REVCOOLING TUBES AND ATTACHING HARDWARE. 9SB GE 75-0058* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE - AIR REV. DATE: APR 01/10 SECTION:2-75 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)754300-0802-2 * * * * * C O N T I N U E * * * * *ACCESS: 435AL 436AR 451AL 452AR SB GE 75-0063* 0.05445AL 446AR 461AL 462AR* 0.05754300-0811-1 450 TURBINE CASE COOLING SYSTEM ENG FUC I: 5 A MRB AMM 752400/5011 0.10 PW4601 0.10FUNCTIONAL CHECK OF TURBINE CASE COOLING SYSTEM. (TCCINDICATING SYSTEM AND 13TH STAGE AIR SHUT OFF VALVE)ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE - AIR REV. DATE: APR 01/10 SECTION:2-75 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)760000-0503-1 510 ENGINE CONTROLS ENG FUC I: 3 C MRB AMM 761100/5011 1.00 NON FWD-FACE610 AMM 762100/5011 1.00CABLE TENSION CHECK OF THROTTLE, THRUST REVERSER AND AMM 783000/501EMERGENCY SHUT DOWN SYSTEMS WITH TENSIOMETER(INCLUDING ZONE 130)ACCESS: 131AZ 131CZ 132AZ 132EZ* 0.27760000-0503-2 510 ENGINE CONTROLS ENG FUC I: 3 C MRB AMM 761100/5011 1.00 FWD-FACE610 AMM 783000/5011 1.00CABLE TENSION CHECK OF THROTTLE AND THRUST REVERSERSYSTEMS WITH TENSIOMETER (INCLUDING ZONE 130)ACCESS: 131AZ 131CZ 132AZ 132EZ* 0.27761000-0802-1 430 POWER CONTROLS ENG GVI I: C MRB AMM 761100/0011 1.00 GE440 OR AMM 761200/0011 1.00VISUAL INSPECTION OF THROTTLE AND THRUST REVERSER SHOP VIS AMM 783100/201CONTROLS (ENGINE PORTION) FOR SATISFACTORY CONDITION,SECURITY OF ATTACHMENT, WEAR, CHAFING AND CORROSION.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05761000-0812-1 450 POWER CONTROLS ENG GVI I: C MRB AMM 761100/5011 0.50 PW460 OR1 0.50VISUAL INSPECTION OF THROTTLE AND THRUST REVERSER SHOP VISCONTROLS (ENGINE PORTION) FOR SATISFACTORY CONDITION,SECURITY OF ATTACHMENT, WEAR, CHAFING AND CORROSION.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05761131-0802-1 410 TRANSMISSION - SECONDARY MEC DET I: 1 C MPD AMM 761131/6011 0.50 GE420 SIL SIL 76-0151 0.5001. DETAILED INSPECTION OF ADJUSTABLELEVER FOR SECURITY.02. CHECK THE LOCKBOLT AND LOCKWASHER FOREVIDENCE OF LOOSENESS.ACCESS: 415AL 416AR* 0.13* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE CONTROLS REV. DATE: APR 01/10 SECTION:2-76 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)761131-0802-1 * * * * * C O N T I N U E * * * * *425AL 426AR* 0.13761131-0812-1 410 TRANSMISSION - SECONDARY MEC DET I: 1 C MPD AMM 761131/6011 0.50 PW4201 0.5001. DETAILED INSPECTION OF ADJUSTABLELEVER FOR SECURITY.02. CHECK THE LOCKBOLT AND LOCKWASHER FOREVIDENCE OF LOOSENESS.ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13762000-0503-1 210 EMERGENCY SHUT DOWN SYSTEM ENG OPC I: ENG. CHG MRB ** AMM 762100/5011 2.00 NON FWD-FACEOPERATIONAL CHECK OF THE EMERGENCY SHUT DOWN SYSTEMINCLUDING:- FUEL LP FIRE SHUT-OFF VALVES CLOSING- PACK SHUT OFF VALVES AUTOMATIC CLOSING- HP BLEED VALVE AND X-BLEED VALVE AUTOMATICCLOSINGNOTE: HYDRAULIC FIRE SHUT-OFF VALVE CLOSINGIS COVERED BY TASK 291133-0503-1762000-0503-2 210 EMERGENCY SHUT DOWN SYSTEM ENG OPC I: ENG. CHG MRB ** AMM 282100/5011 2.00 FWD-FACEAMM 762100/501OPERATIONAL TEST OF THE EMERGENCY SHUT DOWN SYSTEM(FIRE CONTROL HANDLES OPERATION) INCLUDING:- FUEL LOW PRESSURE FIRE SHUT OFF VALVES ELECTRICALACTUATORS USING EACH MOTOR IN TURN (MSI 28.21.18)- PACK SHUT OFF VALVES AUTOMATIC CLOSING-HP VALVE, BLEED VALVE AND X FEED VALVE AUTOMATICCLOSINGNOTE: HYDRAULIC FIRE SHUT OFF VALVESCLOSING IS COVERED BY TASK 291133-0503-1* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE CONTROLS REV. DATE: APR 01/10 SECTION:2-76 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)770000-0802-1 430 RPM INDICATING SYSTEM ENG GVI I: C MPD AMM 770000/6011 0.80 GE440 OR1 0.80GENERAL VISUAL INSPECTION OF: SHOP VIS- FAN SPEED (N1) SENSORS, CONNECTORS AND HARNESS- CORE SPEED (N2) SENSORS, CONNECTORS AND HARNESS- TOTAL PRESSURE PROBE AND LINE (PT 5-4)FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,CORROSION, CLEANLINESS AND CHAFING.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05770000-0812-1 430 RPM INDICATING SYSTEM ENG GVI I: C MPD AMM 771100/0011 0.80 PW440 OR AMM 771200/0011 0.80GENERAL VISUAL INSPECTION OF: SHOP VIS AMM 771500/001- FAN SPEED (N1) SENSORS, CONNECTORS AND HARNESS- CORE SPEED (N2) SENSORS, CONNECTORS AND HARNESS- TOTAL PRESSURE PROBE AND LINE (PT-2, PT-7)FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,CORROSION, CLEANLINESS AND CHAFINGACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05771100-0801-1 210 N1 RPM INDICATING SYSTEM ENG OPC I: 1 C MRB ** AMM 771112/4011 0.20 GEBITE CHECK OF THE N1 RPM INDICATING SYSTEM FOR THEL/H AND R/H ENGINE771500-0811-1 210 ENGINE PRESSURE RATIO ENG OPC I: 1 C MRB ** AMM 771500/0011 0.20 PWBITE TEST OF EPR INDICATORS771500-0812-1 450 ENGINE PRESSURE RATIO ENG GVI I: DY-TERM MPD AMM 771500/0011 0.60 PW4601 0.60GENERAL VISUAL INSPECTION OF PT-2 AND PT-7 PROBES FORCONDITION AND CLEANLINESSSYSTEMS AND POWERPLANT PROGRAM : ENGINE INDICATING REV. DATE: APR 01/10 SECTION:2-77 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)771500-0812-2 450 ENGINE PRESSURE RATIO ENG GVI I: 3 A MRB AMM 771500/0011 1.00 PW4601 1.00VISUAL INSPECTION OF PT-2 AND PT-7 PROBES FOR DAMAGE,CRACKS AND BLOCKAGE(AS FAR AS VISIBLE WITHOUT PROBE REMOVAL).772000-0812-1 450 TEMPERATURE ENG GVI I: DY-TERM MPD AMM 771500/0011 0.20 PW4601 0.20GENERAL VISUAL INSPECTION OF PT-7 PROBES FORCONDITION772100-0802-1 430 EGT TEMPERATURE SYSTEM ENG GVI I: C MPD AMM 772101/2011 0.50 GE440 OR1 0.50VISUAL INSPECTION OF THERMOCOUPLE HARNESSES AND LEADS SHOP VISFOR SATISFACTORY CONDITION AND SECURITY OFATTACHMENT.ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07772100-0812-1 450 EGT TEMPERATURE SYSTEM ENG GVI I: C MPD AMM 772100/0011 0.50 PW460 OR1 0.50VISUAL INSPECTION OF THERMOCOUPLE HARNESSES AND LEADS SHOP VISFOR SATISFACTORY CONDITION AND SECURITY OFATTACHMENT.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05772100-0812-2 210 EGT INDICATING SYSTEM ENG CHK I: 1 C EMP PW JT9D EMP1 2.50 PWEGT SYSTEM RESISTANCE CHECK FOR INSULATION GROUNDFAULTS.773200-0802-1 430 ENGINE VIBRATION INDICATING ENG GVI I: C MPD AMM 773200/4011 0.50 GE440 OR1 0.50GENERAL VISUAL INSPECTION OF: SHOP VIS- AFT VIBRATION TRANSDUCER AND HARNESS- INTERNAL FAN BEARING VIBRATION TRANSDUCER HARNESSFOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE INDICATING REV. DATE: APR 01/10 SECTION:2-77 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)773200-0802-1 * * * * * C O N T I N U E * * * * *CORROSION, CRACKS, DENTS AND BENDSACCESS: 435AL 436AR 451AL 455AL* 0.05445AL 446AR 461AL 465AL* 0.05773200-0812-1 450 ENGINE VIBRATION INDICATING ENG GVI I: C MPD AMM 773200/0011 0.50 PW460 OR1 0.50GENERAL VISUAL INSPECTION OF: SHOP VIS- AFT VIBRATION TRANSDUCER AND HARNESS- FORWARD VIBRATION TRANSDUCER AND HARNESSFOR SATSFACTORY CONDITION, SECURITY OF ATTACHMENT.ACCESS: 436AR 452AR* 0.02446AR 462AR* 0.02* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE INDICATING REV. DATE: APR 01/10 SECTION:2-77 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)781100-0802-1 450 CORE EXHAUST NOZZLE ASSEMBLY ENG DET I: 1500 FC CESM AMM 781100/6011 0.20 GE460 GE-CESM 761 0.20VISUAL CHECK FOR LOOSE OR MISSING BOLTS/NUTS/STUDSAT FORWARD CENTERBODY TO TURBINE REAR FRAMEATTACHMENT AND AT FORWARD TO AFT CENTERBODY JOINT.CHECK FOR CORRODED OR DAMAGED NUTPLATES IN AFTCENTERBODY. CHECK FOR SKIN CRACKS IN CENTERBODY,OUTER COWLING AND INNER LINERS.ACCESS: 455AL 456AR* 0.02465AL 466AR* 0.02781100-0802-2 450 LONG CORE EXHAUST NOZZLE ENG GVI I: 1500 FC CESM AMM 781100/6011 0.50 GE460 GE-CESM 76 REV1 0.50GENERAL VISUAL INSPECTION OF LONG FIXED-CORE EXHAUST 9NOZZLE FOR CRACKS IN THE "C" CHANNEL SUPPORTACCESS: 455AL 456AR* 0.02465AL 466AR* 0.02781100-0802-4 450 LONG CORE EXHAUST NOZZLE ENG GVI I: 1500 FC CESM AMM 781100/6011 0.20 GE460 GE-CESM 76 REV1 0.20CHECK FOR MISSING BOLTS/NUTS/STUDS AT FWD 9CENTERBODY TO TRF ATTACH POINTSNOTE: DO NOT REMOVE AFT CENTERBODY FOR THIS CHECK.ACCESS: 455AL 456AR* 0.02465AL 466AR* 0.02783100-0801-2 430 THRUST REVERSER SYSTEM CONTROL ENG FUC I: 1500 FC CESM AMM 783100/2011 1.50 GE440 GE-CESM 76 REV1 1.50PARTIALLY DEPLOY AND STOW EACH REVERSER HALF 9BY DRIVING THROUGH THE CENTER GEAR BOX REDUNDANT PADAND CHECK RUNNING TORQUE WHILE DEPLOYING AND STOWINGTHRUST REVERSERACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783100-0801-5 450 THRUST REVERSER SYSTEM CONTROL ENG RAR I: 7200 FC CESM AMM 783102/2011 3.00 GE460 AMM 783103/2011 3.00REMOVE FAN REVERSER ACTUATOR GEARBOXES AND GE-CESM 76 REVRETURN TO OVERHAUL FACILITY FOR GREASE PACKING 9ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783100-0801-6 210 THRUST REVERSER SYS. CONTR. ENG OPC I: 1500 FC CESM AMM 783100/2011 0.10 GEGE-CESM 76 REVOPERATIONAL CHECK OF THRUST REVERSER COCKPIT 9INDICATING LIGHTS783100-0801-7 450 THRUST REVERSER SYSTEM ENG CHK I: NOTE CN CN2 3.00 GE460 EUAD 1999-422-IMP(B) 2 3.00FAN REVERSER HEALTH CHECKS. FAA AD EUAD AD2008-02-17NOTE : INTERVAL IN ACCORDANCE WITH VENDOR FAA AD 99-18-20RECOMMENDATIONS SB GESBA78-3001ACCESS: 435AL 436AR 455AL 456AR* 0.05445AL 446AR 465AL 466AR* 0.05783100-0801-9 450 THRUST REVERSER SYSTEM CONTROL ENG DET I: 8000 FH CN CN F-2005-2081 5.00 GE460 ISB ISB 78-00251 5.00DETAILED INSPECTION OF THE THRUST REVERSERDIRECTIONAL PILOTING VALVE (DPV) AND ITS ASSOCIATEDCONTROL MECHANISM.ACCESS: 435AL 436AR 455AL 456AR* 0.05445AL 446AR 465AL 466AR* 0.05783100-0802-1 450 PNEUMATIC DRIVE MOTOR FILTER ENG RAR I: 1500 FC CESM AMM 783101/2011 0.75 GE460 GE-CESM 76 REV1 0.75REMOVE AND REPLACE INLET FILTER SCREEN OF 9PNEUMATIC DRIVE MOTORACCESS: 436AR 452AR 456AR* 0.04446AR 462AR 466AR* 0.04SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783100-0802-2 450 THRUST REVERSER STRUCTURE ENG DET I: 1500 FC CESM AMM 783100/2011 0.50 GE460 GE-CESM 76 REV1 0.50DETAILED INSPECTION OF FAN REVERSER STRUCTURE 9ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07783100-0802-3 430 THRUST REVERSER SYS. CONTR. ENG GVI I: 1500 FC CESM GE-CESM 76 REV1 0.10 GE440 91 0.10VISUAL INSPECTION OF PRESSURE REGULATOR FLANGE FORLOOSENED BOLTSACCESS: 436AR 452AR 456AR* 0.04446AR 462AR 466AR* 0.04783100-0802-4 450 PNEUM. DRIVE MOTOR MEC GVI I: 500 FC CESM AMM 783100/2011 1.00 GE460 GE-CESM 76 REV1 1.00GENERAL VISUAL INSPECTION OF: 9- REVERSER DRIVE CABLES FOR CONDITION.- SHAFT SEALS FOR LEAKAGE.ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783100-0802-5 450 PNEUM. DRIVE MOTOR MEC GVI I: 500 FC CESM AMM 783101/2011 0.50 GE460 GE-CESM 76 REV1 0.50CHECK DRIVE MOTOR TEMPERATURE DECAL FOR 9OVERTEMPERATURE.ACCESS: 436AR 452AR* 0.02446AR 462AR* 0.02783100-0802-6 430 THRUST REVERSER SYSTEM CONTROL ENG FUC I: 1500 FC CESM AMM 783100/2011 2.50 GE440 GE-CESM 76 REV1 2.50GAP CHECK BETWEEN TRANSLATING COWL AND SUPPORT 9ASSEMBLY (IF NOT WITHIN SPECIFIED LIMITS, ADJUST RODEND BEARINGS ON BALL SCREW ACTUATOR TO OBTAIN CORRECTGAP) SERVICE FLEXIBLE SHAFTS AND PERFORM RIGGING IFREQUIREDACCESS: 435AL 436AR 455AL 456AR* 0.05* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783100-0802-6 * * * * * C O N T I N U E * * * * *445AL 446AR 465AL 466AR* 0.05783100-0802-7 430 FAN REVERSER FEEDBACK MECHANISM ENG GVI I: 1500 FC MRB AMM 783100/2011 0.30 GE440 GE-CESM 76 REV1 0.30VISUAL INSPECTION OF PNEUMATIC VALVES AND ELECTRICAL 9SWITCHES CAM FOLLOWERS FOR WEAR AND FREE ROTATION BYHANDACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02783100-0802-8 430 THRUST REVERSER SYSTEM CONTROL ENG DET I: 1500 FC CESM AMM 783112/2012 4.00 GE440 GE-CESM 76 REV2 4.0001. REMOVE MAIN AND INTERCONNECTING DRIVE CABLES 902. PERFORM DRIVE CABLE CASING CHECK. PULL ALL CORESAND INSPECT FOR BROKEN WIRES, DEFORMATIONLOCAL BOWING AND WEAR. LUBRICATE EXTERIOR OFCORES AFTER WIPING WITH A LINT FREE CLOTH DAM-PENED WITH SOLVENT03. REINSTALL DRIVE CABLES AND PERFORM GAP CHECKAND RIGGINGACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783100-0802-9 450 THRUST REVERSER SYS. CONTR. ENG DET I: 1500 FC CESM AMM 783100/2011 0.50 GE460 GE-CESM 761 0.50CHECK TORQUE OF V-BAND CLAMPS IN THE REVERSERAIR SYSTEMACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07783100-0803-1 450 THRUST REVERSER SYS. CONTR. ENG CLN I: 1 C MRB AMM 783105/2011 0.30 GE4601 0.30REMOVE, INSPECT AND CLEAN PRESSURE REGULATORFILTERACCESS: 436AR 452AR* 0.02* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783100-0803-1 * * * * * C O N T I N U E * * * * *446AR 462AR* 0.02783100-0805-2 450 FAN REVERSER BALL SCREW MEC LUB I: 1000 FC MRB AMM 122271/0011 0.40 GE460 GE-CESM 76 REV1 0.40LUBRICATION OF FAN REVERSER BALL SCREW ACTUATORS. 9ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783100-0805-3 450 PNEUM. DRIVE MOTOR MEC RPL I: 500 FC CESM AMM 783101/2011 0.20 GE460 GE-CESM 76 REV1 0.20CHECK PNEUM. DRIVE MOTOR OIL LEVEL, 9REPLENISH IF NECESSARY.ACCESS: 436AR 452AR* 0.02446AR 462AR* 0.02783100-0805-5 450 THRUST REVERSER SYSTEM CONTROL ENG RPL I: 1500 FC CESM AMM 783101/2011 0.80 GE460 GE-CESM 76 REV1 0.80DRAIN AND FLUSH DRIVE MOTOR. REFILL WITH 9110 CC OF OILACCESS: 436AR 452AR* 0.02446AR 462AR* 0.02783100-0811-1 450 THRUST REVERSER SYS. CONTR. ENG OPC I: 3 C MRB ** AMM 783100/5011 1.50 PW4601 1.50OPERATIONAL TEST OF THRUST REVERSER DEPLOYMENTINHIBITIONACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783100-0811-2 430 THRUST REVERSER SYS. CONTR. ENG GVI I: 5 A MPD AMM 783115/2011 0.10 PW4401 0.10WITH THRUST REVERSER IN STOWED POSITION, CHECK THATTRANSLATING SLEEVES ARE RESTING ON THE RUBBER RINGAGAINST THE SUPPORT ASSEMBLY. (IN CASE OF EXESSIVE* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783100-0811-2 * * * * * C O N T I N U E * * * * *GAP,ADJUST AS REQUIRED)783100-0811-3 430 THRUST REVERSER SYS. CONTR. ENG OPC I: 1 C MPD AMM 783211/2011 1.50 PW4401 1.50CHECK SMOOTH OPERATION OF THRUST REVERSER WHILEDEPLOYING AND STOWING TRANSLATING SLEEVES BYACTUATING THE SYSTEM THROUGH DRIVE PAD ON EITHERLOWER SLAVE ACTUATOR.ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02783100-0811-6 450 THRUST REVERSER SYS. CONTR. ENG RAR I: 3 C MPD AMM 783100/4011 3.00 PW4601 3.00REMOVE FAN REVERSER ACTUATOR GEARBOXES ANDRETURN TO OVERHAUL FACILITY FOR GREASE PACKINGACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02783100-0812-2 430 THRUST REVERSER SYS. CONTR. ENG CHK I: 1 C MPD AMM 783112/4011 3.50 PW4401 3.5001. REMOVE MAIN AND INTERCONNECTING DRIVE CABLES02. PERFORM DRIVE CABLE CASING CHECK. PULL ALL CORESAND INSPECT FOR BROKEN WIRES, DEFORMATIONLOCAL BOWING AND WEAR. LUBRICATE EXTERIOR OFCORES AFTER WIPING WITH A LINT FREE CLOTH DAM-PENED WITH SOLVENT03. REINSTALL DRIVE CABLES AND PERFORM GAP CHECKAND RIGGINGACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783100-0812-3 430 THRUST REVERSER SYS. CONTR. ENG GVI I: 1 C MRB AMM 783100/0011 0.20 PW4401 0.20GENERAL VISUAL INSPECTION OF ELECTRICAL SWITCHES FORCONDITION AND WEAR OF CAMS AND PLUNGERS* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783100-0812-3 * * * * * C O N T I N U E * * * * *ACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783100-0815-1 450 FAN REVERSER BALL SCREW ENG LUB I: 800 FC MRB AMM 122278/0011 0.40 PW4601 0.40CLEAN AND LUBRICATE FAN REVERSER BALL SCREWACTUATOR BALL NUTSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783200-0802-1 450 FAN THRUST REVERSER BLOCKER DOORS ENG GVI I: 1500 FC CESM AMM 783200/6011 0.25 GE460 GE-CESM 76 REV1 0.25CHECK HINGE LUG BEARINGS OF FAN THRUST REVERSER 9BLOCKER DOORS FOR CONDITIONACCESS: 436AR 452AR 456AR* 0.04446AR 462AR 466AR* 0.04783200-0805-1 450 FAN REVERSER FEEDBACK MECH. ENG LUB I: 800 FC MRB GE-CESM 76 REV1 0.50 GE460 91 0.50LUBRICATE ALL MOVING PARTS OF FAN REVERSERFEED BACK MECHANISMACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02783200-0815-1 450 FAN REV. STOW LATCHES ENG LUB I: 5 A MRB AMM 122271/0011 0.50 PW4601 0.50CLEAN AND LUBRICATE THRUST REVERSER STOW LATCHESAND ROD END OF INTERLOCK PUSH-PULL CABLEACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02783300-0802-1 450 FIXED CORE EXHAUST NOZZLE ENG DET I: 3 C MPD AMM 781200/6011 1.50 GE4601 1.50 POST 01201DETAILED INSPECTION OF FIXED NOZZLE FOR(78-0006)* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783300-0802-1 * * * * * C O N T I N U E * * * * *SATISFACTORY CONDITION, SECURITY OF ATTACHMENT ANDCRACKSACCESS: 435AL 436AR 452AR 455AL 456AR* 0.06445AL 446AR 462AR 465AL 466AR* 0.06783300-0812-1 450 FIXED CORE EXHAUST NOZZLE ENG DET I: 3 C MPD AMM 781000/0011 1.50 PW4601 1.50DETAILED INSPECTION OF FIXED NOZZLE FORSATISFACTORY CONDITION, SECURITY OF ATTACHMENT ANDCRACKSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783600-0801-2 430 FAN REVERSER DOOR OPENING SYSTEM MEC OPC I: 1500 FC CESM AMM 783100/2011 0.50 GE440 GE-CESM 76 REV1 0.50OPERATIONAL CHECK OF FAN REVERSER DOOR POWER-OPENING 9SYSTEM.783600-0802-1 450 FAN REVERSER COWL DOOR SYS. ENG GVI I: 1500 FC CESM AMM 783100/2011 0.80 GE460 AMM 783600/2011 0.8001. VISUAL INSPECTION OF ACTUATOR MOUNT CUP AND GE-CESM 76 REVBRACKET FOR CRACKS 902. CHECK ALL CONNECTIONS AND FITTINGS IN SYSTEMFOR LEAKSACCESS: 435AL 436AR 451AL 452AR 455AL 456AR* 0.07445AL 446AR 461AL 462AR 465AL 466AR* 0.07783600-0812-1 430 FAN REV. DOORS OPEN. SYSTEM ENG OPC I: 3 A MPD AMM 711300/3001 0.50 PW440 AMM 783100/5011 0.5001. VISUAL INSPECTION FOR CRACKS OF MOUNTING FLANGEAND FORK OF THRUST REVERSER DOOR OPENING ACTU-ATORS02. CHECK SMOOTH OPERATION DURING CLOSINGACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)783600-0815-1 450 FAN REV. DOORS OPEN. SYSTEM ENG LUB I: 1 C MPD AMM 122278/0011 0.30 PW4601 0.30CLEAN AND LUBRICATE THRUST REVERSER DOOR JACKSCREWSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05783605-0802-1 450 THRUST REVERSER HOLD OPEN RODS ENG DET I: 3000 FH MPD SB GE 78-2281 1.00 GE4601 1.00DETAILED INSPECTION OF HOLD OPEN ROD ASSEMBLY* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION:2-78 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)790000-0805-2 430 ENGINE OIL SYSTEM ENG RPL I: 150 FC CESM AMM 121379/0011 0.10 GE440 GE-CESM 76 REV1 0.10CHECK ENGINE OIL LEVEL BY DIPSTICK AND PERFORM 9SNIFF SMELL CHECKNOTE: OBSERVE COLOR OF OIL,VERY DARK OIL COULDINDICATE CONTAMINATION OR BEARING DISTRESSACCESS: 436DR* 0.02446DR* 0.02790000-0805-3 430 OIL-GENERAL MEC DET I: 150 FC CESM AMM 123279/0011 0.20 GE440 GE-CESM 1111 0.20 PRETAKE OIL SAMPLE FROM ENGINE OIL TANK FOR GE-CESM 76 REVSB GE 72-0935SOAP-INSPECTION. 9ORPRENOTE: OIL SAMPLE SHOULD BE TAKEN WITHIN 45 MINSB GE 72-0977AFTER ENGINE SHUT-DOWN.ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02790000-0815-1 430 ENGINE OIL SYSTEM ENG RPL I: DY-TERM MRB AMM 121379/0011 0.10 PW4401 0.10CHECK ENGINE OIL LEVEL AT TANK FILLER NECKNOTE:-WHEN SERVICING OIL TANK SMELL FOR PRESENCE OFFUEL IN OIL-OBSERVE COLOR OF OIL.VERY DARK OIL COULDINDICATE CONTAMINATION OR BEARING DISTRESSACCESS: 436CR* 0.01446CR* 0.01791100-0815-1 430 LUBRICATION SYSTEM ENG RPL I: NOTE 5-2 MPD AMM 123279/0011 0.25 PW4401 0.25OIL SAMPLE EVALUATION FOR S.O.A.P.NOTE: SAMPLE SHALL BE TAKEN FROM THE MIDDLEOF THE ENGINE OIL TANK WITHIN 30 MIN. AFTERENGINE SHUT-DOWN PRIOR TO ANY OIL REFILLING* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE - OIL REV. DATE: APR 01/10 SECTION:2-79 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)791100-0815-1 * * * * * C O N T I N U E * * * * *ACCESS: 436AR* 0.01446AR* 0.01792100-0812-1 435 MAIN (SUPPLY) OIL FILTER ENG RAR T: NOTE MPD AMM 792103/4011 0.30 PW445 I: 5 A1 0.30REMOVE AND INSPECT (FOR PARTICLES) THE MAIN (SUPPLY)OIL FILTER. INSTALL A NEW FILTER ELEMENT.NOTE: FIRST INSPECTION 3 MO AFTERENGINE INSTALLATION.ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02792101-0802-1 435 PUMP-LUBE AND SCAVENGE ENG CLN T: 150 CSN CESM AMM 792101/3011 0.50 GE445 I: 1500 FC GE-CESM 76 REV1 0.50REMOVE AND INSPECT FOR PARTICLES BEFORE CLEANING 9THE LUBE SUPPLY OIL FILTER ELEMENT ASSEMBLY AND LUBEPUMP SUPPLY INLET SCREENACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02792101-0802-2 435 PUMP-LUBE AND SCAVENGE ENG CLN T: 150 CSN CESM AMM 792101/3011 0.80 GE445 I: 600 FC GE-CESM 76 REV1 0.80REMOVE AND INSPECT FOR PARTICLES BEFORE CLEANING 9THE LUBE SCAVENGE PUMP INLET SCREEN.ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02792201-0802-1 435 SCAVENGE OIL FILTER ENG CLN T: 150 CSN CESM AMM 792201/3011 0.80 GE445 I: 1500 FC CESM1 0.80REPLACE LUBE SCAVENGE FILTER CESM 76 REV 9ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02SYSTEMS AND POWERPLANT PROGRAM : ENGINE - OIL REV. DATE: APR 01/10 SECTION:2-79 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)792203-0802-1 435 OIL MAGNETIC CHIP DETECTOR ENG GVI I: 150 FC MRB AMM 792203/3011 0.30 GE445 GE-CESM 76 REV1 0.30REMOVE AND INSPECT BEFORE CLEANING MASTER 9MAGNETIC CHIP DETECTOR FOR METAL PARTICLESACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02792203-0812-1 435 OIL MAGNETIC CHIP DETECTOR ENG GVI I: 250 FH MRB AMM 792203/3011 0.30 PW445 SB PW 58901 0.3001. REMOVE THE FOLLOWING MAGNETIC PLUGS TO CHECKFOR METAL DEPOSITS BEFORE CLEANING :- NO. 1 & 2 BEARING SCAVENCE PLUG- NO. 3 BEARING SCAVENGE PLUG- NO. 4 SCAVENGE PLUG02. REINSTALLACCESS: 435AL* 0.01445AL* 0.01792204-0802-1 435 LUBE SCAVENGE PUMP ENG CLN I: NOTE CESM AMM 792101/3011 1.00 GE445 GE-CESM 76 REV1 1.00REMOVE AND INSPECT FOR PARTICLES BEFORE CLEANING 9THE LUBE SCAVENGE PUMPS SCREEN (5 OFF) AND - IFINSTALLED - INSPECT FOR CHIPS THE SCAVENGE ISOLATION-MAGNETIC PLUGS (5 OFF)NOTE: - SCAVENGE PUMP SCREENS : FIRST INSPECTION500FH/150CY AFTER ENGINE INSTALLATION THERE-AFTER EVERY 2000FH/600CY- ISOLATION MAGNETIC PLUGS INSPECT EVERY500FH/150CYACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02793000-0802-1 430 OIL INDICATION SYSTEM ENG GVI I: C MRB AMM 793000/6011 1.00 GE440 OR1 1.00GENERAL VISUAL INSPECTION OF: SHOP VIS- OIL QUANTITY TRANSMITTER, CONNECTOR AND HARNESS- OIL TEMPERATURE SENSOR, CONNECTOR AND HARNESS* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE - OIL REV. DATE: APR 01/10 SECTION:2-79 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)793000-0802-1 * * * * * C O N T I N U E * * * * *- OIL PRESSURE TRANSMITTER, CONNECTOR AND HARNESS- LOW OIL PRESSURE SWITCH, CONNECTOR AND HARNESS- OIL FILTER CLOGGING SWITCH, CONNECTOR AND HARNESSFOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,CORROSION, DETERIORATION, CRACKS, DENTS AND FREEDOMFROM LEAKSACCESS: 435AL 436AR 451AL 452AR* 0.05445AL 446AR 461AL 462AR* 0.05793000-0812-1 430 OIL INDICATION SYSTEM ENG GVI I: C MRB AMM 793000/0011 0.80 PW440 OR1 0.80GENERAL VISUAL INSPECTION OF: SHOP VIS- OIL QUANTITY TRANSMITTER, CONNECTOR AND HARNESS- OIL TEMPERATURE SENSOR, CONNECTOR AND HARNESS- OIL PRESSURE TRANSMITTER, CONNECTOR AND HARNESS- LOW OIL PRESSURE SWITCH, CONNECTOR AND HARNESS- OIL FILTER CLOGGING SWITCH, CONNECTOR AND HARNESSFOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,CORROSION, DETERIORATION, CRACKS, DENTS AND FREEDOMFROM LEAKSACCESS: 436AR* 0.01446AR* 0.01793500-0801-1 435 OIL FILTER CLOGGING INDICATING ENG FUC I: ENG. CHG MRB AMM 793511/4012 1.00 GE4452 1.00 POST 01654TEST OF MAIN OIL FILTER CLOGGING INDICATING SYSTEM(77-0007)793500-0801-2 212 OIL FILTER CLOGGING INDICATING ENG OPC I: ENG. CHG MPD AMM 793500/0011 0.10 GEPRE 01654BITE TEST OF SCAVENGE OIL FILTER MAGNETIC INDICATOR(77-0007)793500-0811-1 435 OIL FILTER CLOGG. INDICAT. ENG FUC I: ENG. CHG MRB AMM 793511/4012 1.00 PW4452 1.00 POST 1654TEST OF MAIN OIL FILTER CLOGGING INDICATING SYSTEM* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE - OIL REV. DATE: APR 01/10 SECTION:2-79 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)801300-0802-1 430 PNEUMATIC STARTER AND VALVE MEC DET I: 1500 FC CESM AMM 801302/2011 0.50 GE440 GE-CESM 76 REV1 0.50REMOVE ENGINE STARTER VALVE FILTER, INSPECT, CLEAN 9AND REINSTALL.ACCESS: 436AR* 0.01446AR* 0.01801300-0811-1 430 AIR FILTER (ENGINE) ENG CLN I: 1 C MPD AMM 801307/4011 0.50 PW4401 0.50CLEAN AIR FILTER OF PNEUMATIC STARTER VALVEACCESS: 436AR* 0.01446AR* 0.01801301-0805-1 430 PNEUMATIC STARTER ENG RPL I: 300 FC CESM AMM 121380/0011 0.50 GE440 GE-CESM 76 REV1 0.50OIL CHANGE OF PNEUMATIC STARTER 9ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02801301-0805-2 430 PNEUMATIC STARTER ENG RPL I: 150 FC CESM AMM 121380/0011 0.50 GE440 MRB AMM 801301/2001 0.50CHECK AND TOP UP OIL LEVEL OF PNEUMATIC STARTER AND GE-CESM 76 REVCHECK MAGNETIC PLUG FOR METAL PARTICLES 9ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02801301-0815-1 430 PNEUMATIC STARTER ENG RPL I: 3 A MPD AMM 121380/0011 0.50 PW4401 0.50OIL CHANGE OF PNEUMATIC STARTERACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02801301-0815-2 430 PNEUMATIC STARTER ENG RPL I: 1 A MRB AMM 121380/0011 0.50 PW440 AMM 801301/2011 0.50CHECK AND TOP UP OIL LEVEL OF PNEUMATIC STARTER* * * * * C O N T I N U E D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE - STARTING REV. DATE: APR 01/10 SECTION:2-80 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)801301-0815-2 * * * * * C O N T I N U E * * * * *AND CHECK MAGNETIC PLUG FOR METAL PARTICLES.:ACCESS: 435AL 436AR* 0.02445AL 446AR* 0.02* * * * * E N D * * * * *SYSTEMS AND POWERPLANT PROGRAM : ENGINE - STARTING REV. DATE: APR 01/10 SECTION:2-80 PAGE 2

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 STRUCTURE Page 1 

# INTRODUCTION

1. GENERAL

The purpose of this program is to maintain the continuous airworthiness of the aircraft structure and to

control corrosion to Level 1 or better.

Advantage is taken from the maintenance tasks performed by the Zonal Program.

2. STRUCTURE RULES

1. The Maintenance tasks are to be carried out 'at or before' the limits stated for threshold and

interval.

NOTE:

For maintenance tasks where a Fatigue Rating is given the figures for threshold and interval may

have to be adjusted iaw. paragraph 3, “Adjustment for Range”.

2. The thresholds and intervals quoted in calendar time in this program include aircraft time in and out

of service.

3. It is assumed that the structure to be inspected is in a state of cleanliness which allows a

satisfactory inspection to be carried out at the required inspection level.

Where existing Temporary Protection System (TPS) permits unobscured assessment of the

condition of the structure, then that Temporary Protection may remain in place for the inspection.

4. If damage is found or suspected (such as bulging skin) then the full extent of any damage must be

clearly identified using appropriate inspection techniques and/or disassembly where necessary.

All damage is to be evaluated and repaired in accordance with documentation acceptable to the

relevant Airworthiness Authority.

5. If inspections indicate evidence of deterioration, appropriate further actions must be taken to

prevent similar deteriorations from occurring in the operators fleet.

For corrosion findings refer to paragraph 5 “Corrosion Prevention and Control Program”.

6. The following applies only to maintenance tasks where re-application of Temporary Protection

System (TPS) is required:

Prior to application of TPS perform the required inspection.

NOTE:

Type III TPS (AIMS 09-08-003) is an alternative material that may be used as a replacement for the

combined Type I and Type II. In addition, Type III TPS may also be used in place of Type I or Type

II, except for movable parts, for which only Type I Grade 2 is permitted.

7. Ensure wet insulation blankets are dried prior to re-installation, or replaced with new.

8. Ensure that all drain holes and drainage paths are clear from obstruction.

9. The condition of the paint system should be verified during the inspections. Re-protection should be

applied where necessary.

10. The requirements stated in years were determined for an aircraft operated in a moderate humidity

environment and not subjected to corrosive products.

# MAINTENANCE PLANNING DOCUMENT

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# Any operator who routinely operates in humid or marine environments and/or carries corrosive

cargo such as seafood, may find that the calendar time maintenance tasks stated in this program

are not sufficient to control corrosion to Level 1 or better. Operators in this category should take

appropriate further actions.

11. Operators shall report inspection results to the manufacturer in accordance with the Structure

Program Reporting System. Refer to para. 7 Reporting System.

12. Based on reports made through the Structure Program Reporting System, Airbus will:

– Inform all the operators of the significant discrepancies discovered on the A300 fleet.

– Make the appropriate recommendations.

13. "Touch and Go" Cycles can be neglected if they are less than 5% of the total number of Flight

Cycles up to threshold inspection or between two consecutive inspections.

Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold

inspection or between two consecutive inspections.

14. Additional information concerning inspections is provided in the following Airbus supporting

publications:

– Aircraft Maintenance Manual (AMM)

– Non-Destructive Testing Manual (NTM)

– Structural Repair Manual (SRM)

3. ADJUSTMENT FOR RANGE

1. General

Inspection requirements are defined considering a Basic Flight Time (BFT) of

- 1.08 FH/FC for A300 B2 series

- 1.33 FH/FC for A300 B4 100 series

- 2.08 FH/FC for A300 B4 200, A300 C4 & F4 series

Maintenance tasks that have a Fatigue Rating (FR) may have to be adjusted considering the

individual utilization of concerned A/C. Actual thresholds/ intervals are calculated by multiplying the

stated MPD values by the relevant Adjustment Factor (AF).

The criteria whether an adjustment will be required is the Average Flight Time (AFT) of the A/C in

question, ie. where the AFT is longer than the BFT of the same A/C type the figures for

threshold/interval of concerned maintenance tasks must be adjusted. On the contrary where the

AFT is shorter than the BFT of the same A/C series the figures for threshold/interval may be

adjusted to benefit from longer intervals.

NOTE:

The A300 ALI, Section B, may be consulted for examples and background information to the

Adjustment for Range requirement.

# MAINTENANCE PLANNING DOCUMENT

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# 2. Aircraft Operated With Longer Flight Time.

For all A/C for which the Average Flight Time (AFT) up to threshold and/or between consecutive

inspections is higher than the associated Basic Flight Time (BFT) all maintenance requirements that

have a Fatigue Rating (FR) must be adjusted for threshold and repeat. The application of the

following adjustment formula will lead to reduced values for threshold and interval:

AF = 1 - (AFT - BFT) x FR

The Adjustment Factor (AF) has to be multiplied with the given figure for threshold and interval to

get the value applicable for a particular A/C for threshold and interval.

NOTE:

The reduction of threshold/interval figures can be significant, e.g. where a B4-200 is operated at

3.08 FH/FC on average the figures for threshold/interval may have to be reduced by 30%.

Therefore, when planning tasks with a Fatigue Rating (FR), sufficient lead-time must be considered.

3. Aircraft Operated With Shorter Flight Time.

For all A/C for which the Average Flight Time (AFT) up to threshold and/or between consecutive

inspections is lower than the associated Basic Flight Time (BFT) all maintenance requirements that

have a Fatigue Rating (FR) may be adjusted for threshold and repeat to benefit from the extended

values by application of the following adjustment formula:

AF = 1 - (AFT - BFT) x FR

The Adjustment Factor (AF) has to be multiplied with the given figure for threshold and interval to

get the value applicable for a particular A/C for threshold and interval.

NOTE:

The AFT in the above mentioned formula must not be lower than the following values even if the

actual flight times are lower:

- 0.54 FH/FC for A300 B2 series

- 0.67 FH/FC for A300 B4 100 series

- 1.04 FH/FC for A300 B4 200, A300 C4 & F4 series

4. Tolerance On AFT Values.

Since the calculation of the adjusted values for threshold and interval has to be performed with

predicted figures for the A/C utilization, a tolerance of 10% is given on the AFT. If for instance an

adjustment calculation has been performed by using an AFT of 2.82 FH/FC the calculated values

remain valid providing the actual AFT at the inspection date is not exceeding 3.1 FH/FC.

NOTE:

The fatigue rating (FR) is only provided for inspection tasks with source MRB S. For inspection

tasks with source ALI (former SSID tasks) refer to explanation provided in chapter 4 of this

introduction.

# MAINTENANCE PLANNING DOCUMENT

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# 4. AIRWORTHINESS LIMITATION ITEMS (ALI)

1. General

The requirements stated in the A300 ALI document issue 3 supersede the previously issued A300

SSID requirements.

The ALI document provides the requirements to comply with DGAC/SFACT/TC 53652, FAA AC 91-

56, CAA Airworthiness Notice n° 89 and NPA 20-10 for A300 B2, B4-100, B4-200, C4 and F4

airplanes for the baseline structure or structure modified as per Airbus.

It contains the fatigue related structural inspections arising from the Widespread Fatigue Damage

(WFD) evaluation.

Its objective is to maintain continuous airworthiness of the airplanes based on a reassessment of

the structure using the damage tolerance concept.

2. Organisation of the A300 ALI

The A300 ALI is the reference document that is mandated by the certification airworthiness

authorities, the following provides an overview of the organisation of this document with regard to

the requirements:

- Section A

provides the introduction of the ALI and explanation of the applicability and limit of validity.

- Section B

provides explanation of the program rules.

- Section C

provides the list of ALIs for which modifications must be embodied at the stated embodiment times.

This requirements are not listed in this MPD, because these are non repetive inspection

requirements.

- Section D

provides all standard ALI inspection requirements.

- Section E

provides alternative short range requirements for tasks of section C, where applicable.

- Section F

provides alternative adjustment for range requirements for tasks of section D, where applicable.

- Section G

provides illustrations for all inspection requirements listed in section D.

NOTE:

The inspection requirements listed in Section D 'Alternative Short Range Requirements' and listed

in Section E 'Alternative Adjustment for Range Requirements' can only be used as alternative

requirements and therefore these ta sks are not integrated in the structure program section of this

MPD. These alternative inspection requirements are listed in the A300 ALI document.

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# 5. CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

A. General

The Structures Program includes requirements to control corrosion to Level 1 or better.

These requirements are developed for the A3OO CPCP and they are either consolidated in the

Zonal Program or they are consolidated with other structural requirements. However reference to

the relevant CPCP requirement is always provided in the reference column.

NOTE: CPCP tasks consolidated with other requirements are still under the CPCP rules.

B. Corrosion Level Definitions

The severity of the corrosion damage is categorised into three 'Levels' as follows:

Level 1 Corrosion

Corrosion occurring between successive inspections that can be reworked / blended out within

allowable limits as defined by the manufacturer (SRM, SB, etc.)

or,

Corrosion damage that exceeds allowable limits but can be attributed to an event not typical of

operator's usage of other aircraft in the same fleet (e.g. mercury spillage).

or,

Operator experience has demonstrated only light corrosion between each successive inspection

but the latest inspection and cumulative blend out now exceeds the allowable limits.

Level 2 Corrosion

Corrosion occurring between successive inspections that requires a single rework/blend-out, which

exceeds allowable limits as defined by the manufacturer (SRM, SB, etc.), requiring a

repair/reinforcement or complete or partial replacement of applicable structure.

Level 3 Corrosion

Corrosion found during first or subsequent inspection(s), which is determined (normally by the

operator) to be an urgent airworthiness concern requiring expeditious action.

C. CPCP Rules

The effectiveness of the Corrosion Prevention and Control Program is determined by following the

rules listed below which are applicable individually for each tasks:

No Corrosion Findings

Should inspections consistently reveal no corrosion findings for a given area during repeat

inspections on particular aircraft operated in similar conditions, then the repeat interval for the

concerned task may be escalated.

Level 1 Corrosion Findings

Should inspections consistently reveal corrosion Level 1 findings for a given area during repeat

inspections on particular aircraft operated in similar conditions, then the existing program is

considered effective for the concerned area, and no change to the program is necessary.

Level 2 Corrosion Findings

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# Should inspections reveal that corrosion is Level 2 for a given area during repeat inspections, then

the existing program is not effective for the concerned area of the particular fleet.

NOTE: Reporting of any Level 2 corrosion findings is mandatory, refer to CN90-196-117.

In order to control corrosion to Level 1 or better, consideration should be given to one or more of

the following corrective actions:

– Decreasing the inspection threshold/interval

– Considering a higher inspection level

– Re considering the Program Concept

– Application/More frequent application of Temporary Protection System

– Embodiment of preventive modifications, where applicable

– Installation of parts with improved protection standard, where applicable

In this way, the program is self-regulating and will adjust itself to the optimum program.

Level 3 Corrosion Findings

Should inspections reveal that corrosion is Level 3 in a given area, then the existing program is not

effective for the concerned area.

NOTE: Reporting of any Level 3 corrosion findings is mandatory, refer to CN90-196-117.

In addition to the considerations given for Level 2 corrosion, an action plan ca lling for a one-time

inspection of the concerned area should be expeditiously agreed with the local Aviation Authority

and carried out on all aircraft of a similar age or older.

Airbus may be consulted to determine whether or not the airworthiness is affected. In this case all

details of findings are to be promptly reported for detailed evaluation and the assistance required

clearly expressed.

6. SAMPLING PROGRAM/CONVERSION OF SAMPLING PROGRAM

1. General

The Structure Program of the A300 MRB Document contains a number of SSIs controlled under a

sampling concept. Airbus however has performed a study to convert the concerned sampling

requirements into 100% requirements for an easier consolidation.

Since the sampling program and the converted 100% requirements are equivalent with regard to

safety protection of the A/C, each operator may take their own criteria to decide whether or not a

conversion is beneficial for them. The following paragraphs will provide guidance for the realisation

of the preferred solution.

2. Continuation of the Sampling Concept

In case it is intended to continue the sampling concept for a certain time or indefinitely all tasks of

this MPD Section where the four digits for MPD Section and task code are 0604 (i.e. all tasks which

are XXXXXX-0604-X) may be replaced by the corresponding requirement given in MPD Volume 3,

Section 16.

NOTE 1:

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# To facilitate the finding of the corresponding task In MPD Appendix 5 , i.e. task XXXXXX-0604-X in

this section becomes XXXXXX-060S-X in MPD Appendix 5.

NOTE 2:

The corresponding task in MPD Appendix 5 continue to reflect the sampling requirements given by

the MRB Document, however tasks for which in-service experience does not allow the continuation

of sampling have been/will be deleted from MPD Appendix 5 and the repeat interval in Section 16

have been/will be amended accordingly.

3. Conversion of Sampling Concept to 100% Concept

In case where an operator wishes to benefit from the increased intervals for tasks where the four

digits for MPD Section and task code are 0604 (i.e. for all tasks which are XXXXXX-0604-1) all A/C

must be inspected at all intervals (i.e. 100% concept).

The date for the conversion of the sampling concept to the 100% concept can be any time

convenient to the concerned operator. Once this date has been defined all A/C are due for

inspections at intervals not exceeding the intervals required by this section (this includes the

Adjustment for Range).

NOTE:

The interval for the next inspection for any particular A/C counts always from the last time where

this A/C has been inspected. An exception to this rule is where an A/C currently controlled under

the sampling concept and has not been inspected during the interval stated in this section, in this

case the next inspection is due at the FC status of the A/C of the fleet concerned where the

conversion date is fixed. The diagram shown on the next page illustrates this rule.

For this example refer to task 531817–0604–1:

Sampling requirement:

Sample Threshold : 20000 FH

Sample Interval : 6000FH

Sample Rate : 1/5

100% requirement:

100% interval : 17700 FH

Typical Operator with 4 A/C

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# 7. REPORTING SYSTEM

The Structural Inspection Report form provided below may be used by operators/maintenance

organizations to report structural inspection results to Airbus. However investigations are in progress to

develop a means to transmit the required data electronically.

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# The following rules apply to the reporting:

1. A completed Structural Inspection Report is required any time a structurally significant defect

occurs.

2. The responsibility for reporting rests with the operator.

3. The reports should be sent to Airbus via the Resident Customer support Manager or directly to

Airbus at the following address:

AIRBUS

Customer Service Directorate

Attn.: Department Manager Maintenance Engineering

1, Rond Point Maurice Bellonte

F-31707 Blagnac Cedex

FRANCE

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# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)510000-0603-1 000 STRUCTURES - GENERAL MEC GVI I: SEE ISB ISB ISB 20-00071 TBD ALLGENERAL VISUAL INSPECTION OF ALL EXPOSED UNPAINTEDCADMIUM PLATED PARTS FOR CORROSION.* * * * * E N D * * * * *STRUCTURE PROGRAM : STRUCTURES REV. DATE: APR 01/10 SECTION:3-51 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)521101-0602-1 831 FWD PASSENGER/CREW DOORS MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 TBD ALL841 MRB S1 TBD EXCL. F4GENERAL VISUAL INSPECTION OF FORWARD PASSENGER/CREW 521101-C602-1DOOR EXTERNAL STRUCTURE521110-0602-1 831 FWD PASSENGER/CREW DOORS MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 TBD F4841 MRB S1 TBDGENERAL VISUAL INSPECTION OF FORWARD PASSENGER/CREW 521110-C602-1DOOR EXTERNAL STRUCTURE521202-0602-1 831 FORWARD PASSENGER/CREW DOORS MEC DET I: 8500 FC MRB S AMM SSI 5212021 0.10 ALL8411 0.10DETAILED INSPECTION OF FWD PASSENGER/CREWDOOR EXTERNAL STRUCTURE.521202-0603-1 831 FORWARD PASSENGER/CREW DOORS MEC DET I: 5 YE CPCP AMM SSI 5212021 5.00 ALL841 MRB S1 5.00DETAILED INSPECTION OF FORWARD PASSENGER/CREW MRB REFERENCE:DOOR INTERNAL STRUCTURE.521202-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 ,G2 OR G3 AFTER INSPECTIONPREP.: ESCAPE SLIDE/RAFT, DOOR LINING AND INSULATIONREMOVED521210-0602-1 832 MID PASSENGER/CREW DOORS MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 TBD ALL842 MRB S1 TBD EXCL. F4GENERAL VISUAL INSPECTION OF MID PASSENGER/CREW 521210-C602-1DOOR EXTERNAL STRUCTURE521403-0603-1 832 MID PASSENGER/CREW DOORS MEC DET I: 5 YE CPCP AMM SSI 5214031 5.00 ALL842 MRB S1 5.00DETAILED INSPECTION OF MID PASSENGER/CREW DOOR MRB REFERENCE:INTERNAL STRUCTURE.521403-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2OR G3 AFTER INSPECTIONPREP.: ESCAPE SLIDE/RAFT, DOOR LINING AND INSULATION* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)521403-0603-1 * * * * * C O N T I N U E * * * * *REMOVED521409-0602-1 832 SKIN OF MID PASS/CREW DOOR MEC DET I: 7000 FC MRB S AMM SSI 5214091 0.20 ALL8421 0.20DETAILED INSPECTION OF EXTERNALSKIN AND RIVETS OF MID PASSENGER/CREW DOOR.521801-0602-1 833 AFT PASSENGER/CREW DOORS MEC GVI I: 5 YE SSI1 TBD ALL8431 TBD EXCL. F4GENERAL VISUAL INSPECTION OF AFT PASSENGER/CREWDOOR EXTERNAL STRUCTURE521803-0602-1 833 AFT PASSENGER/CREW DOORS MEC DET I: 8500 FC MRB S AMM SSI 5218031 0.20 ALL8431 0.20DETAILED INSPECTION OF EXTERNAL STRUCTUREOF AFT PASSENGER/CREW DOOR.521803-0603-1 833 AFT PASSENGER/CREW DOORS MEC DET I: 5 YE CPCP AMM SSI 5218031 5.00 ALL843 MRB S1 5.00DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR MRB REFERENCE:INTERNAL STRUCTURE.521803-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2OR G3 AFTER INSPECTIONPREP.: ESCAPE SLIDE/RAFT, DOOR LINING AND INSULATIONREMOVED522201-0602-1 834 STRUCTURE OF EMERGENCY EXITS MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 TBD ALL844 MRB S1 TBDGENERAL VISUAL INSPECTION OF EMERGENCY EXIT 522201-C602-1EXTERNAL STRUCTURE522601-0603-1 834 STRUCTURE OF EMERG.EXITS MEC DET I: 5 YE CPCP AMM SSI 5226011 5.00 ALL844 MRB S1 5.00DETAILED INSPECTION OF EMERGENCY EXITSINTERNAL STRUCTURE.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)522601-0603-1 * * * * * C O N T I N U E * * * * *522601-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2OR G3 AFTER INSPECTIONPREP.: ESCAPE SLIDE/RAFT, DOOR LINING AND INSULATIONREMOVED522605-0602-1 834 SKIN OF EMERGENCY EXITS MEC DET I: 7000 FC MRB S AMM SSI 5226051 0.20 ALL8441 0.20DETAILED INSPECTION OF EXTERNAL SKIN OFEMERGENCY EXIT.523301-0602-1 811 HINGE END OF FWD CARGO DOOR MEC DET T: 23300 FC ALI AMM SSI 5233011 0.50 PRE 02295I: 3500 FC MRB S CN 2006-0071(B) FROM 0 FC/FHDETAILED INSPECTION OF HINGE END OF FWD FAA AD 96-13-11 TO LOVCARGO COMPARTMENT DOOR AT FRAMES 20B TO 24A(9 PLACES) (AS FAR AS VISIBLE) ALI REFERENCE:523301-01-1ACCESS: 132AR* 0.38523301-0602-2 811 HINGE END OF FWD CARGO DOOR MEC DET T: 14000 FC ALI AMM SSI 5233011 0.50 POST 02295I: 3500 FC MRB S CN 2006-0071(B) FROM 0 FC/FHDETAILED INSPECTION OF HINGE END OF FWD FAA AD 96-13-11 TO LOVCARGO COMPARTMENT DOOR AT FRAMES 20B TO 25, ASFAR AS VISIBLE. ALI REFERENCE:523301-01-1ACCESS: 132AR* 0.38523303-0603-1 811 LOCK MECHAN.ATTACH.FITTINGS MEC DET T: 12600 FC ALI AMM SSI 5233031 1.00 ALLI: 9500 FC MRB S CN 2006-0071(B) FROM 0 FC/FHDETAILED INSPECTION OF INTERNAL LOCK MECHANISM FAA AD 96-13-11 TO LOVATTACH FITTINGS AND SUPPORT STRUCTURE OF FWD CARGOCOMPARTMENT DOOR AT ALL FRAMES LONGERON 4 TO 5 ALI REFERENCE:523303-01-1ACCESS: 811AR* 0.25* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523303-0603-1 * * * * * C O N T I N U E * * * * *523307-0603-1 811 ACTUATOR ATTACH FITTING ON DOOR NDT SDI I: 6000 FC ISB NTM 5232041 0.50 POST 01202PART 6(52-0078)SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH NTM 523300ORFITTING OF FORWARD CARGO COMPARTMENT DOOR AT FRAME PART 6POST 0305422A. ISB 52-0136(52-0104)NOTE: FORWARD CARGO COMPARTMENT DOORLINING TO BE REMOVED523309-0602-1 811 SKIN OF FORWARD CARGO DOOR MEC DET T: 5 YE CPCP AMM SSI 5233091 0.50 ALLI: 7000 FC MRB SDETAILED INSPECTION OF EXTERNAL FWD CARGO 30 MO MRB REFERENCE:COMPARTMENT DOOR SKIN AND RIVETS523101-C602-1523315-0603-1 835 UDC-DOOR LOCKING-HOOKS MEC DET T: 12400 FC ALI AMM SSI 5233151 2.50 C4I: 6200 FC MRB S AMM 523600/600F4DETAILED INSPECTION OF INTERNAL UDC-DOOR CN 2006-0071(B) FROM 0 FC/FHLOCKING-HOOKS AT FRAMES 20B TO 26A FAA AD 96-13-11 TO LOV( 8 PLACES )ALI REFERENCE:ACCESS: 835 835BR 835CR 835DR 523315-01-1* 0.50523316-0603-1 835 UDC-DOOR LOCKING PLATES MEC DET I: 6000 FC MPD1 0.20 POST 06208MSN 256DETAILED INSPECTION OF UDC-DOOR LOCKINGPLATES AT FRAMES 20B TO 26A (8 PLACES).ACCESS: 835 835BR 835CR 835DR* 0.50523317-0603-1 835 ATTACH FITTING OF UDC-DOOR MEC DET T: 12200 FC ALI AMM SSI 5233171 2.50 C4I: 6100 FC MRB S AMM 523600/600F4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523317-0603-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF INTERNAL LOCKING CN 2006-0071(B) FROM 0 FC/FHMECHANISM ATTACH FITTINGS AND SUPPORT STRUCTURE OF FAA AD 96-13-11 TO LOVUDC-DOOR AT ALL FRAMES, BETWEEN STRINGER 27 ANDSTRINGER 30 AND BETWEEN LONGERON 8 AND 9. ALI REFERENCE:523317-01-1PREP.: DOOR LINING TO BE REMOVED.ACCESS: 835 835BR 835CR 835DR* 0.50523317-0603-2 835 ATTACH FITTING OF UDC-DOOR MEC DET T: 12200 FC ALI AMM SSI 5233171 2.50 POST 06208I: 6100 FC MRB S CN 2006-0071(B) MSN 256DETAILED INSPECTION OF INTERNAL LOCKING FAA AD 96-13-11 FROM 0 FC/FHMECHANISM ATTACH FITTINGS AND SUPPORT STRUCTURE OFTO LOVUDC-DOOR AT ALL FRAMES, BETWEEN STRINGER 27 AND ALI REFERENCE:STRINGER 30 AND BETWEEN LONGERON 8 AND 9. 523317-01-1PREP.: DOOR LINING TO BE REMOVED.ACCESS: 835 835BR 835CR 835DR* 0.50523319-0603-1 835 ACTUATOR ATTACH FITTING, UDC DOOR MEC DET I: 6000 FC MRB S AMM SSI 5233191 2.50 C4AMM 523600/600F4DETAILED INSPECTION OF INTERNAL ACTUATORATTACH FITTINGS OF UDC DOORPREP.: DOOR LININGS AND INSULATION REMOVEDACCESS: 835* 0.05523321-0603-1 835 MECH. LINKAGE OF UDC DOOR ACTUATOR MEC DET I: 6000 FC MRB S AMM SSI 5233211 2.50 C4AMM 523600/600F4DETAILED INSPECTION OF INTERNAL MECHANICALLINKAGE OF UDC DOOR ACTUATOR UNIT CONSISTING OFLEVER, BRACES, YOKE AND DOOR BOLTS.PREP.: DOOR LININGS REMOVEDACCESS: 835* 0.05STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523601-0602-1 835 UPPER (MAIN) DECK CARGO (UDC) DOOR MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 TBD C4MRB SF4GENERAL VISUAL INSPECTION OF UPPER (MAIN) DECK CARGO 523601-C602-1MSN 256(UDC) DOOR EXTERNAL SURFACE.523701-0602-1 812 HINGE END OF AFT CARGO DOOR MEC DET T: 12000 FC ALI AMM SSI 5237011 0.50 ALLI: 3000 FC MRB S NTM 523200FROM 0 FC/FHDETAILED INSPECTION OF EXTERNAL HINGE END PART 7TO 40000 FCOF AFT CARGO COMPARTMENT DOOR AT FRAMES 60 TO 63 CN 2006-0071(B)7 PLACES) ESPECIALLY IN FLANGE RADII ADJACENT TO FAA AD 96-13-11OUTER SKIN, CHECK WITH MAGNIFYING GLASSALI REFERENCE:ACCESS: 812AR 523701-01-1* 0.20523701-0602-2 812 HINGE END OF AFT CARGO DOOR MEC DET I: 1000 FC ALI NTM 5232001 0.50 ALLMRB S PART 7FROM 40000 FCDETAILED INSPECTION OF EXTERNAL HINGE END CN 2006-0071(B) TO LOVOF AFT CARGO COMPARTMENT DOOR AT FRAMES 60 TO 63 FAA AD 96-13-117 PLACES) ESPECIALLY IN FLANGE RADII ADJACENT TOOUTER SKIN, CHECK WITH MAGNIFYING GLASS ALI REFERENCE:523701-01-2ACCESS: 812AR* 0.20523707-0603-1 812 ACTUATOR ATTACH FITTING ON DOOR NDT SDI I: 6000 FC ISB NTM 5232041 0.50 POST 01202PART 6(52-0078)SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH ISB 52-136FITTING OF AFT CARGO COMPARTMENT DOOR AT FRAME 61A.NOTE: AFT CARGO COMPARTMENT DOORLINING TO BE REMOVED523715-0602-1 812 AFT CARGO COMPARTMENT DOOR MEC DET T: 5 YE SSI1 0.50 ALLI: 11200 FCDETAILED INSPECTION OF EXTERNAL 30 MOAFT CARGO COMPARTMENT DOOR SKIN AND RIVETSSTRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)523717-0602-1 813 SKIN OF BULK CARGO DOOR MEC DET T: 5 YE CPCP AMM SSI 5237171 0.20 ALLI: 7000 FC MRB SDETAILED INSPECTION OF EXTERNAL 30 MO MRB REFERENCE:BULK CARGO COMPARTMENT DOOR SKIN AND RIVETS523401-C602-1523719-0602-1 813 BULK CARGO DOOR STOPS MEC DET T: 13300 FC ALI AMM SSI 5237191 0.50 ALLI: 6000 FC MRB S CN 2006-0071(B) FROM 0 FC/FHDETAILED INSPECTION OF DOOR STOPS ON BULK FAA AD 96-13-11 TO 40000 FCCARGO COMPARTMENT DOOR AT FRAME 67 AND 69.ALI REFERENCE:ACCESS: 813 523719-01-1* 0.01523719-0602-2 813 BULK CARGO DOOR STOPS MEC DET I: 1000 FC ALI ALI REFERENCE: 1 0.50 ALLMRB S 523719-01-1FROM 40000 FCDETAILED INSPECTION OF DOOR STOPS ON BULKTO LOVCARGO COMPARTMENT DOOR AT FRAME 67 AND 69.ACCESS: 813* 0.01526101-0602-1 120 AVIONICS COMPARTMENT ACCESS DOOR MEC DET T: 40000 FC ALI CN 2006-0071(B) 1 TBD B2I: 24000 FC FAA AD 96-13-11 PRE 05134DETAILED INSPECTION OF AVIONICS COMPARTMENTFROM 0 FC/FHACCESS DOOR INTERNAL STRUCTURE. ALI REFERENCE: TO LOV526101-01-1PREP : FLOOR PANELS AND DOOR TO BE REMOVED.ACCESS: 212BL* 0.14526101-0602-2 120 AVIONICS COMPARTMENT ACCESS DOOR MEC DET T: 40000 FC ALI CN 2006-0071(B) 1 TBD B4I: 24000 FC FAA AD 96-13-11 C4DETAILED INSPECTION OF AVIONICS COMPARTMENTF4ACCESS DOOR INTERNAL STRUCTURE. ALI REFERENCE: PRE 05134526101-01-1FROM 0 FC/FHPREP : FLOOR PANEL AND DOOR TO BE REMOVEDTO LOVACCESS: 212BL* 0.14STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)526305-0606-1 835 UPPER (MAIN) DECK CARGO DOOR HINGE MEC DET ST: 12000 FC ALI NTM 5333001 2.00 B4-2CSI: 11200 FC PART 6POST 6208DETAILED INTERNAL AND EXTERNAL INSPECTION T: 12000 FC CN 2006-0071(B) C4OF HINGES OF UPPER DECK CARGO DOOR INCLUDING I: 11200 FC FAA AD 96-13-11 F4ADJACENT STRUCTURE BETWEEN DOOR STRS. 1 AND 3.FROM 0 FC/FHALI REFERENCE: TO 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-01-1526305-0606-3PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOORLINING AND INSULATION TO BE REMOVEDPASSENGER CONFIGURATION : UPPER DECK CARGODOOR LINING, CEILING, INSULATION AND HATRACKSTO BE REMOVEDACCESS: 835* 0.05526305-0606-2 835 UPPER (MAIN) DECK CARGO DOOR HINGE MEC DET I: 11200 FC ALI NTM 5333001 2.00 B4-2CPART 6POST 6208DETAILED INTERNAL AND EXTERNAL INSPECTION CN 2006-0071(B) C4OF HINGES OF UPPER DECK CARGO DOOR INCLUDING FAA AD 96-13-11 F4ADJACENT STRUCTURE BETWEEN DOOR STRS. 1 AND 3.FROM 34000 FCALI REFERENCE: TO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-01-2526305-0606-3PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOORLINING AND INSULATION TO BE REMOVEDPASSENGER CONFIGURATION : UPPER DECK CARGODOOR LINING, CEILING, INSULATION AND HATRACKSTO BE REMOVEDACCESS: 835* 0.05526305-0606-3 835 UPPER (MAIN) DECK CARGO DOOR HINGE NDT SDI ST: 12000 FC ALI NTM 5333001 2.00 B4-2CSI: 11200 FC PART 6POST 6208SPECIAL DETAILED INSPECTION OF HINGES OF UPPER DECK CN 2006-0071(B) C4CARGO DOOR (UDC) INCLUDING ADJACENT STRUCTURE BETWEEN FAA AD 96-13-11 F4DOOR STRINGER 1 AND 3.FROM 0 FC/FHALI REFERENCE: TO 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-02-1526305-0606-1* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)526305-0606-3 * * * * * C O N T I N U E * * * * *PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOORLINING AND INSULATION TO BE REMOVEDPASSENGER CONFIGURATION : UPPER DECK CARGODOOR LINING, CEILING, INSULATION AND HATRACKSTO BE REMOVEDACCESS: 835* 0.05526305-0606-4 835 UPPER (MAIN) DECK CARGO DOOR HINGE NDT SDI I: 11200 FC ALI NTM 5333001 2.00 B4-2CPART 6POST 6208SPECIAL DETAILED INSPECTION OF HINGES OF UPPER DECK CN 2006-0071(B) C4CARGO DOOR (UDC) INCLUDING ADJACENT STRUCTURE BETWEEN FAA AD 96-13-11 F4DOOR STRINGER 1 AND 3.FROM 34000 FCALI REFERENCE: TO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-02-2526305-0606-2PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOORLINING AND INSULATION TO BE REMOVEDPASSENGER CONFIGURATION : UPPER DECK CARGODOOR LINING, CEILING, INSULATION AND HATRACKSTO BE REMOVEDACCESS: 835* 0.05528021-0603-1 811 CARGO COMPARTMENT DOORS MEC DET I: 5 YE CPCP AMM SSI 5237031 1.00 ALL812 MRB S AMM SSI 5237111 1.00813 DETAILED INSPECTION OF FORWARD, AFT AND REAR1 0.50CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE. MRB REFERENCE:NOTE: 01. DOOR LINING AND INSULATION TO BE REMOVED. 528021-C603-102. APPLY TEMPORARY PROTECTION SYSTEM TYPE 1,G2 OR G3 AFTER INSPECTION.ACCESS: 811AR* 0.25812AR* 0.20528023-0603-1 835 UDC DOOR MEC DET I: 5 YE CPCP MRB REFERENCE: 1 15.00 C4528023-C603-1F401. DETAILED INSPECTION OF INTERNAL STRUCTUREMSN 256* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)528023-0603-1 * * * * * C O N T I N U E * * * * *OF UPPER (MAIN)DECK CARGO (UDC) DOOR02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2OR G3 AFTER INSPECTION.PREP.: DOOR LINING AND INSULATION REMOVED.ACCESS: 835AR 835BR 835CR 835DR 835ER 835FR* 0.88835GR528203-0602-1 710 NOSE GEAR DOOR HINGES MEC SDI I: 8500 FC MRB S AMM SSI 5282031 0.50 ALLNTM 528211DETAILED OR SPECIAL DETAILED INSPECTION OF EXTERNAL PART 4 AND 6NOSE GEAR DOOR HINGES, ZONE 713,714,715,716NOTE: FOR REARMOST HINGE, ONLY VISUAL INSPECTION ORHF-EC INSPECTION IS REQUIRED IN ACCORDANCE WITHILLUSTRATION IN SECTION 13, OR IN ACCORDANCEWITH NTM 52-82-11 PART 6, RESPECTIVELY528503-0602-1 734 MAIN GEAR DOOR HINGES MEC SDI I: 8500 FC MRB S AMM SSI 5285031 0.50 ALL744 NTM 5281121 0.50DETAILED OR SPECIAL DETAILED INSPECTION OF EXTERNAL PART 6MAIN GEAR DOOR HINGES528505-0602-1 734 MLG-DOOR ACT.ATTACH.FITTING MEC SDI I: 8500 FC MRB S AMM SSI 5285051 0.50 ALL744 NTM 5281121 0.50DETAILED OR SPECIAL DETAILED INSPECTION OF EXTERNAL PART 4 AND 6MAIN GEAR DOOR ACTUATING CYLINDER ATTACH FITTING529003-0603-2 831 DOORS MEC DET T: 36 MO ISB CN1 2.00 PRE 12024832 I: 36 MO 1999-410-294(B) 1 2.00 (52-0173)833 DETAILED INSPECTION OF THE PAX DOOR EMERGENCY FAA AD1 2.00841 CYLINDER STRIKER MECHANISM. 2003-03-041 2.00842 ISB 52-1681 2.00843 ACCESS : OPEN THE DOOR1 2.00* * * * * E N D * * * * *STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION:3-52 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)530407-0603-1 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET T: 17700 FC ALI CN 2006-0071(B) 1 8.00 B2132 I: 9000 FC FAA AD 96-13-11 1 8.00 FROM 0 FC/FHDETAILED INSPECTION OF ATTACHMENT FITTINGS FORTO 48000 FCFORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENCE:TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-1STRINGERS 40 AND 41, LH AND RHPREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TOTO BE REMOVED.530407-0603-2 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET I: 4500 FC ALI CN 2006-0071(B) 1 8.00 B2132 FAA AD 96-13-11 1 8.00 FROM 48000 FCDETAILED INSPECTION OF ATTACHMENT FITTINGS FORTO LOVFORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENCE:TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-2STRINGERS 40 AND 41, LH AND RHPREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TOTO BE REMOVED.530407-0603-3 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET I: 4500 FC ALI CN 2006-0071(B) 1 8.00 B4-100132 FAA AD 96-13-11 1 8.00 FROM 40000 FCDETAILED INSPECTION OF ATTACHMENT FITTINGS FORTO LOVFORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENCE:TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-3STRINGERS 40 AND 41, LH AND RHPREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TOTO BE REMOVED.530407-0603-4 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET T: 17700 FC ALI CN 2006-0071(B) 1 8.00 B4-100132 I: 9000 FC FAA AD 96-13-11 1 8.00 FROM 0 FC/FHDETAILED INSPECTION OF ATTACHMENT FITTINGS FORTO 40000 FCFORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENCE:TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-5STRINGERS 40 AND 41, LH AND RHPREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TOTO BE REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)530407-0603-5 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET I: 4500 FC ALI CN 2006-0071(B) 1 8.00 B4-200132 FAA AD 96-13-11 1 8.00 C4DETAILED INSPECTION OF ATTACHMENT FITTINGS FORF4FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENCE: FROM 34000 FCTO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-4TO LOVSTRINGERS 40 AND 41, LH AND RHPREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TOTO BE REMOVED.530407-0603-6 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET T: 17700 FC ALI CN 2006-0071(B) 1 8.00 B4-200132 I: 9000 FC FAA AD 96-13-11 1 8.00 C4DETAILED INSPECTION OF ATTACHMENT FITTINGS FORF4FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENCE: FROM 0 FC/FHTO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-6TO 34000 FCSTRINGERS 40 AND 41, LH AND RHPREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TOTO BE REMOVED.530503-0603-1 147 KEEL BEAM INTERNAL STRUCT. MEC DET I: 9000 FH ISB CN1 1.00 PRE 01208148 1979-125-018(B) 1 1.00DETAILED INSPECTION OF KEEL BEAM CENTER ISB 53-0096AND SIDE WEBS AT FR. 47A AND FR. 53A (STRINGER 53LH,RH AND STRG. 57) FOR CRACKSACCESS: 147AF 147SZ 147TZ* 0.06148AF 148SZ 148TZ* 0.06530505-0602-1 577 FLAP TRACK NO.1 ATT.FITTING MEC DET I: 5700 FC MRB S AMM SSI 5305051 0.33 ALL6771 0.33DETAILED INSPECTION OF ATTACHMENT FITTINGS ATFLAP TRACK NO.1 TO FUSELAGE AT FRAME 51.NOTE: AS ALTERNATE TO TASK 530505-0602-1NDT INSPECTION OF FLAP TRACK NO.1ATTACHMENT FITTINGS TO FUSELAGE ATFRAME 51 INSIDE ZONE 577/677 CAN BEPERFORMED ACCORDING TO NTM 531500 PART 6.THIS INSPECTION REQUIRES REMOVAL OF FLAPTRACKSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)530505-0604-1 147 FLAP TRACK NO.1 ATT.FITTING MEC DET I: 27300 FC MRB S AMM SSI 5305051 0.40 ALL1481 0.40DETAILED INSPECTION OF FLAP TRACK NO.1ATTACHMENT FITTINGS TO FUSELAGE AT FRAME 51.ACCESS: 147PZ 147QZ* 0.03148PZ 148QZ* 0.03530601-0604-1 577 SUPPORT STRUCTURE FRAM 54.1 MEC DET I: 8400 FC MRB S AMM SSI 5306011 3.00 B26771 3.00DETAILED INSPECTION OF SUPPORT STRUCTURE INAREA OF WING FLAP ATTACH FITTINGS ON FUSELAGE BETWEENFRAMES NO. 54.1 AND 54.2 AND BETWEEN STRINGERS 30 AND35.ACCESS: 577BB 677BB* 0.75530601-0604-2 577 SUPPORT STRUCTURE FRAM 54.1 MEC DET I: 8400 FC MRB S AMM SSI 5306011 3.00 B4-1006771 3.00DETAILED INSPECTION OF SUPPORT STRUCTURE INAREA OF WING FLAP ATTACH FITTINGS ON FUSELAGE BETWEENFRAMES NO. 54.1 AND 54.2 AND BETWEEN STRINGERS 30 AND35.ACCESS: 577BB 677BB* 0.75530601-0604-3 577 SUPPORT STRUCTURE FRAM 54.1 MEC DET I: 8400 FC MRB S AMM SSI 5306011 3.00 B4-2006771 3.00 C4DETAILED INSPECTION OF SUPPORT STRUCTURE INF4AREA OF WING FLAP ATTACH FITTINGS ON FUSELAGE BETWEENFRAMES NO. 54.1 AND 54.2 AND BETWEEN STRINGERS 30 AND35.ACCESS: 577BB 677BB* 0.75531000-0602-2 100 FUSELAGE SKIN - SCUFF PLATE AREA MEC DET I: 30 MO MPD1 0.10 ALL2001 0.10DETAILED INSPECTION OF FUSELAGE SKIN AT EDGESOF PAX CREW DOOR SCUFF PLATES (AND CARGO DOOR SCUFFPLATES IF INSTALLED) FOR CORROSION AND SCUFF PLATEEXTERNAL SURFACES FOR BULGING.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531000-0602-3 100 FUSELAGE JOINTS MEC DET I: ISB ISB ISB 53-01541 3.00 MSN 003-156200 53-1541 3.00 PRE 02727DETAILED INSPECTION OF LONGITUDINAL ANDCIRCUMFERENTIAL SKIN JOINTS FOR SEALING CONDITION ANDEXTERNAL SURFACE CORROSION.NOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0154531000-0602-4 100 FUSELAGE JOINTS MEC DET I: ISB ISB CN2 26.00 MSN 003-156200 53-178 1984-140-064(B) 2 26.00 NOTEDETAILED EXTERNAL INSPECTION OF BONDED FAA ADLONGITUDINAL AND CIRCUMFERENTIAL JOINTS FOR CORROSION 2000-16-07ISB 53-0178NOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0178531000-0603-1 100 FUSELAGE JOINTS NDT SDI I: ISB ISB NTM 5330104 >99.9 MSN 003-156200 53-148 PART 4 AND 64 >99.9 NOTESPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP NTM 533020JOINTS AND CIRCUMFERENCIAL JOINTS FOR BONDING PART 4 AND 6DELAMINATION. NTM 533030PART 5NOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0148 CN1984-140-064(B)FAA AD2000-16-07ISB 53-0148531000-0603-2 100 FUSELAGE STRINGERS/DOUBLERS NDT SDI I: ISB ISB NTM 5310104 96.00 MSN 003-156200 53-149 PART 4, 54 96.00 NOTESPECIAL DETAILED INSPECTION OF BONDED STRINGERS AND NTM 533050DOUBLERS FOR BONDING DELAMINATION. PART 5CNNOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0149 1984-140-064(B)FAA AD2000-16-07ISB 53-0149531000-0603-5 100 FUSELAGE LAP JOINTS NDT SDI T: 24000 FC ISB NTM 5330102 2.50 MSN 003-156200 NOTE NTM 5330102 2.50 PRE 02611SPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP I: 6000 FC PART 4POST 01421JOINTS IN SECTION 14, 16 AND 17 AT SPECIAL AREAS NOTE(53-0033)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531000-0603-5 * * * * * C O N T I N U E * * * * *NTM 533010RETROFITNOTE: FOR THRESHOLD AND FOLLOW UP INTERVALS OF PART 6POST 07085REPAIRED AREAS REFER TO ISB 53-0211 CATEGORY 3. CN(53-0223)1989-061-092(B) ORFAA AD 90-01-10 POST 01421ISB 53-0211SERIAL531000-0603-6 100 FUSELAGE LAP JOINTS NDT SDI T: 32000 FC ISB NTM 5330101 20.00 MSN 003-156200 NOTE PART 4 CONFIG1 1 20.00 PRE 02611SPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP I: 6000 FC PART 6PRE 02525JOINTS IN SECTION 13 THRU 18 AT STANDARD AREAS NOTE CONFIG 1 TO 3(53-0126)CNPOST 01421NOTE: 01. FOLLOW-UP INTERVAL FOR LAP JOINTS WITH 1989-061-092(B) (53-0033)BONDED DOUBLERS 6000 FC FAA AD 90-01-10 RETROFITISB 53-211POST 0708502. FOLLOW-UP INTERVAL FOR LAP JOINTS WITHOUT(53-0223)BONDED DOUBLERS 8000 FC.ORPOST 0142103. FOR THRESHOLD AND FOLLOW-UP INTERVALS OFSERIALREPAIRED AREAS REFER TO ISB 53-0211 CATE-GORY 3.ACCESS: 577AB 577AT 577BB 577BT 577CT 577DT* 7.36577ET 577GT 677AB 677AT 677BB 677BT677CT 677DT 677ET 677GT531000-0603-7 100 FUSELAGE LAP JOINTS NDT SDI T: NOTE ISB NTM 5330101 20.00 MSN 003-156200 I: 5000 FC PART 4 CONFIG1 1 20.00 PRE 2611SPECIAL DETAILED INSPECTION MODIFIED LONGITUDINAL LAP PART 6JOINTS IN SECTION 13/14 AND 18 CONFIG 1 TO 3CNNOTE: 01. THRESHOLD 32000 FC FOR LAP JOINTS WITH 1989-061-092(B)CUT OUT, SB 53-206 OR SB 53-209 FAA AD 90-01-1002. THRESHOLD 32000 FC FOR LOWER SHELL (4 PANEL ISB 53-0211SOLUTION), SB 53-21503. THRESHOLD 32000 FC FOR LOWER SHELL (3 PANELSOLUTION), SB 52-21604. THRESHOLD 42000 FC FOR LAP JOINTS WITHOUTCUT OUT, SB 53-20905. THRESHOLD 42000 FC FOR LAP JOINTS SB 53-22306. THRESHOLD 34000 FC AND RI 12000 FC FOR LAP* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531000-0603-7 * * * * * C O N T I N U E * * * * *JOINTS, SB 53-306531001-0603-1 230 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 5330104 25.00 PRE 02727240 OR PART 64 25.00 MSN 003-103SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 15 YE NTM 533040OF LONGITUDINAL LAP JOINTS, IN SECTION 13 AND 14, I: 12000 FC PART 5ABOVE AND INCLUDING STR 22 LH/RH EXCEPT STR 22 RH IN OR CNSECTION 13. 7 YE 1989-061-092(B)FAA AD 90-01-10NOTE: 01. MSN 102, 103 ONLY SECTION 14 EFFECTED ISB 53-022902. LINING, HATRACKS AND INSULATION TO BEREMOVED AS REQUIRED.531001-0603-2 130 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 5330104 20.00 PRE 02727140 OR PART 64 20.00 MSN 003-156240 SPECIAL DETAILED INSPECTION BONDED INNER DOUBLERS OF 15 YE NTM 5330404 20.00250 LONGITUDINAL LAP JOINTS, IN SECTION 15 THRU 18 EXCEPT I: 12000 FC PART 54 20.00260 STR 31 LH/RH AND SECTION 13 AND 14, BELOW STR 22, OR CN4 20.00(INCLUDING ZONE 140, 240, 250 AND 260). 102 MO 1989-061-092(B)FAA AD 90-01-10NOTE: LININGS, HATRACKS AND INSULATION TO BE ISB 53-0229REMOVED AS REQUIRED.531001-0603-3 150 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 5330104 7.50 PRE 02727160 OR PART 64 7.50 MSN 003-156SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 12 YE NTM 533040OF LONGITUDINAL LAP JOINTS, IN SECTION 16 AND 17, STR I: 12000 FC PART 531 (INCLUDING ZONE 160). OR CN7 YE 1989-061-092(B)NOTE: INSULATION TO BE REMOVED AS REQUIRED FAA AD 90-01-10ISB 53-0229531001-0603-5 130 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 5330108 4.00 PRE 02727OR PART 6MSN 105SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 15 YE NTM 533040LONGITUDINAL LAP JOINTS, IN SECTION 14 AT STR. 47 LH I: 12000 FC PART 5AND STR. 49 RH BETWEE FR. 26 AND FR. 38.1. OR CN7 YE 1989-061-092(B)NOTE: INSULATION TO BE REMOVED AS REQUIRED FAA AD 90-01-10* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531001-0603-5 * * * * * C O N T I N U E * * * * *ISB 53-0229531001-0603-6 130 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 5330104 7.50 PRE 02727240 OR PART 64 7.50 MSN 107SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 15 YE NTM 533040LONGITUDINAL LAP JOINTS, IN SECTION 14 I: 12000 FC PART 5- AT STR. 22 LH AND AT STR. 31 LH, BETWEEN FRAME 16 OR CNAND FRAME 39 7 YE 1989-061-092(B)- AT STR. 47 LH AND AT STR. 49 RH BETWEEN FRAME 26 FAA AD 90-01-10AND FRAME 38.1 ISB 53-0229PREP.: LININGS AND INSULATION TO BE REMOVEDAS REQUIRED.531001-0603-7 230 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 5330104 2.00 PRE 02727240 OR PART 64 2.00 MSN 109SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLER 15 YE NTM 533040OF LONGITUDINAL LAP JOINTS, IN SECTION 14 AT STR. 5 I: 12000 FC PART 5LH BETWEEN FR. 26 AND FR 38.1 (INCLUDING ZONE 240). OR CN7 YE 1989-061-092(B)PREP.: INSULATION TO BE REMOVED FAA AD 90-01-10ISB 53-0229531101-0602-1 211 SECTION OF FRAMES 2 TO 6 MEC DET I: 7000 FC MRB S AMM SSI 5311011 0.20 ALL2121 0.20DETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS IN AREA OF FRAMES 2 TO 6 EXTENDING FROM WIND-SHIELD TO FLIGHT COMPARTMENT FLOOR531105-0602-1 121 FRAMES 2 TO 9 MEC DET I: 8500 FC MRB S AMM SSI 5311051 0.20 ALL1221 0.20DETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS BETWEEN FRAMES 2 AND 9 BELOW AVIONICS COMPART-MENT FLOOR.531107-0602-1 110 FWD PRESSURE BULKHEAD MEC DET I: 9200 FC ALI CN 2006-0071(B) 1 0.33 B2FAA AD 96-13-11 FROM 45000 FCDETAILED INSPECTION OF FWD PRESSURETO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531107-0602-1 * * * * * C O N T I N U E * * * * *BULKHEAD FRONT FACE SURROUNDING FRAME 1 AND FUSELAGE ALI REFERENCE:SKIN AT ATTACHMENT WITH FRAME 1. 531107-01-1ACCESS: 110AL* 0.01531107-0602-2 110 FWD PRESSURE BULKHEAD MEC DET I: 9200 FC ALI CN 2006-0071(B) 1 0.33 B4-100FAA AD 96-13-11 FROM 40000 FCDETAILED INSPECTION OF FWD PRESSURETO LOVBULKHEAD FRONT FACE SURROUNDING FRAME 1 AND FUSELAGE ALI REFERENCE:SKIN AT ATTACHMENT WITH FRAME 1. 531107-01-2ACCESS: 110AL* 0.01531107-0602-3 110 FWD PRESSURE BULKHEAD MEC DET I: 9200 FC ALI CN 2006-0071(B) 1 0.33 B4-200FAA AD 96-13-11 C4DETAILED INSPECTION OF FWD PRESSUREF4BULKHEAD FRONT FACE SURROUNDING FRAME 1 AND FUSELAGE ALI REFERENCE: FROM 34000 FCSKIN AT ATTACHMENT WITH FRAME 1. 531107-01-3TO LOVACCESS: 110AL* 0.01531115-0602-1 211 FRAME 7 ABOVE WINDSHIELD MEC DET I: 8500 FC MRB S AMM SSI 5311151 0.10 ALL2121 0.10DETAILED INSPECTION OF EXTERNAL STRUCTURE INAREA OF FRAME 7 ABOVE WINDSHIELD.531120-0602-1 211 WINDSHIELD CENTER POST MEC DET I: 7000 FC MRB S AMM SSI 5311201 0.10 ALL2121 0.10DETAILED INSPECTION OF EXTERNAL WINDSHIELDCENTER POST.531120-0604-1 211 WINDSHIELD CENTER POST MEC DET I: 27300 FC MRB S AMM SSI 5311201 1.50 ALLNTM 531100DETAILED INSPECTION OF INTERNAL WINDSHIELD PART 2CENTER POST-NDT INSPECTION, CAN BE CARRIED OUT AS ALTERNATE TOVISUAL INSPECTION WITHOUT LINING REMOVAL ACCORDINGTO NTM 531100 PART 2 -* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531120-0604-1 * * * * * C O N T I N U E * * * * *NOTE: LINING REMOVED531121-0602-1 211 WINDSHIELD SIDE POST FRAME 7 MEC DET I: 5700 FC ALI CN 2006-0071(B) 1 0.20 ALL212 FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF EXTERNAL WINDSHIELDTO LOVSIDE POST AT FRAME 7. ALI REFERENCE:531121-01-1531121-0604-1 211 WINDSHIELD SIDE POST FR. 7 MEC DET I: 27300 FC MRB S AMM SSI 5311211 1.00 ALLNTM 531100DETAILED INSPECTION OF INTERNAL WINDSHIELD PART 6SIDE POST AT FRAME 7-NDT INSPECTION CAN BE CARRIED OUT AS ALTERNATE TOVISUAL INSPECTION, WITHOUT LINING REMOVAL ACCORDINGTO NTM 531100 PART 6NOTE: LINING REMOVED531125-0602-1 211 SIDE WINDOWS STRUCTURE MEC DET I: 7500 FC ALI CN 2006-0071(B) 1 0.33 ALL212 FAA AD 96-13-11 1 0.33 FROM 0 FC/FHDETAILED INSPECTION OF EXTERNALTO LOVSTRUCTURE IN AREA OF SIDE WINDOWS UPPER ALI REFERENCE:AND LOWER SECTIONS BETWEEN FRAMES 2 AND 10, 531125-01-1ESPECIALLY THE LOWER CORNER ADJOINING FRAME 10531125-0604-1 211 SIDE WINDOWS STRUCTURE MEC DET I: 27300 FC MRB S AMM SSI 5311251 5.00 ALLNTM 531100DETAILED INSPECTION OF INTERNAL SIDE WINDOWS, PART 2UPPER AND LOWER STRUCTURE BETWEEN FRAME 2 AND 10, NTM 531100ESPECIALLY THE LOWER CORNER ADJOINING FRAME 10 PART 6-NDT INSPECTION CAN BE CARRIED OUT AS ALTERNATE OFVISUAL INSPECTION OF LOWER CORNER AT FRAME 10NOTE: LINING REMOVED531129-0602-1 211 WINDSHIELD CENTER POST MEC DET I: 7000 FC MRB S AMM SSI 5311291 0.10 ALL2121 0.10* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531129-0602-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF EXTERNAL WINDSHIELDCENTER POST LOWER ATTACHMENT.531129-0604-1 211 WINDSHIELD CENTER POST NDT SDI I: 27300 FC MRB S AMM SSI 5311291 4.00 ALL212 NTM 5311001 4.00DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 4WINDSHIELD CENTER POST LOWER ATTACHMENT,(INCLUDING ZONE 212).NOTE: LH 3VU, RH 5VU, LINING BELOW 13VU INSULATIONREMOVED531131-0602-1 211 WINDSHIELD CENTER POST MEC DET I: 7000 FC MRB S AMM SSI 5311311 0.10 ALL2121 0.10DETAILED INSPECTION OF EXTERNAL WINDSHIELDCENTER POST UPPER ATTACHMENT.531131-0604-1 211 WINDSHIELD CENTER POST NDT SDI I: 27300 FC MRB S AMM SSI 5311311 4.00 ALL212 NTM 5311001 4.00DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 2WINDSHIELD CENTER POST UPPER ATTACHMENT.NOTE: LINING BELOW 20VU AND INSULATION REMOVED531133-0604-1 211 JUNCTION AT FRAMES 6 AND 7 NDT SDI I: 27300 FC MRB S AMM SSI 5311331 2.50 ALL212 NTM 5311001 2.50DETAILED AND SPECIAL DETAILED INSPECTION OF JUNCTIONS PART 6BETWEEN FRAMES 6 ́AND 7 AND WINDSHIELD FRAME LOWERSECTION.NOTE: 1VU, 7VU, LINING AND INSULATION REMOVED531135-0604-1 211 WINDSHIELD SIDE POST NDT SDI I: 27300 FC MRB S AMM SSI 5311351 2.50 ALL212 NTM 5311001 2.50DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 6WINDSHIELD SIDE POST UPPER ATTACHMENT AT FRAME 7.NOTE: LINING REMOVEDSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531137-0602-1 211 CLOSING PANEL AT FRAME 4 MEC DET I: 7500 FC ALI CN 2006-0071(B) 1 0.10 ALL212 FAA AD 96-13-11 1 0.10 FROM 0 FC/FHDETAILED INSPECTION OF JUNCTION OF CLOSINGTO LOVPANEL TO FRAME 4, JUNCTION OF WINDSHIELD FRAME LOWER ALI REFERENCE:SECTION WITH FRAMES 2, 3 AND 4 AND JUNCTION AREA 531137-01-1BETWEEN TRIM PANEL, FRAMES 4 AND 2 AND WINDSHIELDFRAME LOWER SECTION. JUNCTION OF FRAME 4 WITHWINDSHIELD SIDE POST AND TWO RIVETS FOR ATTACHMENT OFFRAME 2 TO SKIN.531137-0604-1 211 CLOSING PANEL AT FRAME 4 NDT SDI I: 27300 FC MRB S AMM SSI 5311371 4.00 ALL212 NTM 5311001 4.00DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 2JUNCTION OF CLOSING PANEL TO FRAME 4, JUNCTION OF NTM 531100WINDSHIELD FRAME LOWER SECTION WITH FRAMES 2, 3 AND PART 6JUNCTION AREA BETWEEN TRIM PANEL, FRAMES 4 AND 2 ANDWINDSHIELD FRAME LOWER SECTION JUNCTION OF FRAME 4WITH WINDSHIELD SIDE POST AND TWO RIVETS FORATTACHMENT OF FRAME 2 TO SKIN.NOTE: 2VU, 6VU, 13VU, LINING REMOVED531150-0603-1 121 FUSELAGE STRUCTURE FROM FRAME 1 TO FRAME MEC GVI T: 15 YE CPCP MRB REFERENCE: 1 TBD ALL122 20 I: 9 YE MRB S1 TBD531150-C603-1GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE FROM FRAME 1 TO FRAME 20 BELOW CABINFLOOR LEVEL INCLUDING REAR FACE OF FORWARDPRESSURE BULKHEAD.PREP.: INSULATION TO BE LIFTED ENOUGH TO INSPECT THESTRUCTURE WITHOUT REMOVAL OF ELECTRICALDEVICES.ACCESS: 131AZ* 0.01132AZ 811* 0.16531200-0603-1 200 FUSELAGE FWD DOOR FRAME MEC DET I: 5 YE SIL SIL 53-0301 0.20 ALLDETAILED INSPECTION OF FUSELAGE FWD PASS/CREWDOOR FRAMES IN AREA OF FITTINGS* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531200-0603-1 * * * * * C O N T I N U E * * * * *NOTE: LININGS TO BE REMOVED531208-0602-1 221 INSPECTION OF FRAME 12A STIFFENERS NDT SDI T: 20400 FC ALI NTM 5130001 0.10 B2222 I: 13300 FC PART 11 0.10 POST 12662SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERSORAT UPPER HORIZONTAL FLANGE (LH/RH). ALI REFERENCE: B4-100531208-01-1POST 12662PREP : FLOOR PANELS, INSULATION AND IF INSTALLEDORCABIN ATTENDANT SEAT, LAVATORY AND GALLEYB4-200TO BE REMOVEDPOST 12662FROM 0 FC/FHTO LOV531208-0602-2 221 INSPECTION OF FRAME 12A STIFFENERS NDT SDI T: 16100 FC ALI NTM 5130001 0.10 C4222 I: 10700 FC PART 11 0.10 POST 12662SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERSORAT UPPER HORIZONTAL FLANGE (LH/RH). ALI REFERENCE: F4-100531208-01-2POST 12662PREP : FLOOR PANELS, INSULATION AND IF INSTALLEDFROM 0 FC/FHCABIN ATTENDANT SEAT, LAVATORY AND GALLEYTO LOVTO BE REMOVED531208-0603-1 121 MAIN FRAME - FUSELAGE NOSE SECTION NDT SDI T: 19300 FC CN NTM 5131051 2.00 B2122 I: 11450 FC FAA AD PART 11 2.00 B4-100SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERS ISB CN F-2005-084B4-200AT UPPER HORIZONTAL FLANGE LH AND RH. FAA ADPRE 126622005-25-19(53-0364)NOTE: FLOOR PANELS, INSULATION AND IF INSTALLED ISB 53-0365CABIN ATTENDENT SEAT, LAVATORY AND GALLEY.ACCESS: 831* 0.10841* 0.10531208-0603-2 121 MAIN FRAME - FUSELAGE NOSE SECTION NDT SDI T: 15500 FC CN NTM 5131051 2.00 C4-203122 I: 9200 FC FAA AD PART 11 2.00 F4-203SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERS ISB CN F-2005-084PRE 12662AT UPPER HORIZONTAL FLANGE LH AND RH. FAA AD(53-0364)2005-25-19NOTE: FLOOR PANELS, INSULATION AND IF INSTALLED ISB 53-0365* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531208-0603-2 * * * * * C O N T I N U E * * * * *CABIN ATTENDENT SEAT, LAVATORY AND GALLEY.ACCESS: 831* 0.10841* 0.10531214-0602-1 211 INSPECTION OF FRAME 10 TO 12 MEC DET T: 27800 FC ALI EASA AD1 0.10 ALL212 I: 8700 FC FAA AD 2006-00711 0.10 FROM 0 FC/FH221 DETAILED INSPECTION OF FRAME 10 TO 12 AT EACH FAA AD1 0.10 TO LOV222 INTERSECTION OF STRINGER FROM CABIN FLOOR TO STR 9. 2007-04-111 0.10PREP : LINING, INSULATION, 15VU, 50VU, LH TOILET ALI REFERENCE:TO BE REMOVED. 531214-01-1531215-0602-1 223 SKIN PANELS FRAMES 10 TO 18 MEC DET T: 11400 FC ALI CN 2006-0071(B) 1 0.25 ALL224 I: 5700 FC FAA AD 96-13-11 1 0.25 FROM 0 FC/FHDETAILED INSPECTION OF EXTERNAL SKINTO LOVPANELS BETWEEN FRAMES 10 AND 18 AND BETWEEN ALI REFERENCE:SRINGERS 9 RH AND 9 LH. 531215-01-1531216-0602-1 121 FRAMES 10 TO 18 MEC DET I: 7000 FC MRB S AMM SSI 5312161 0.20 ALL122 NOTE 6-11 0.20DETAILED INSPECTION OF EXTERNAL SKINAND RIVETS FROM FRAME 10 TO 18 AND FROM CABIN FLOORAREA TO 30 CM DOWN.531216-0604-1 121 FRAMES 10 TO 18 MEC DET I: 27300 FC MRB S AMM SSI 5312161 2.00 ALL1221 2.00DETAILED INSPECTION OF FRAMES 10 TO 18INCLUSIVE EXCEPT FRAMES 14 AND 16A FROM CABIN FLOOR30 CM DOWN, PARTICULARY AT ATTACHMENTS OF FLOOR BEAMSTO FRAMES.NOTE: LINING AND INSULATION REMOVEDACCESS: 221DF 221EF 221KF 222DF 222EF 222JF* 2.22531219-0604-1 121 FRAMES 14 AND 16A MEC DET I: 27300 FC MRB S AMM SSI 5312191 1.00 ALL1221 1.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531219-0604-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF FRAMES 14 TO 16A,BETWEEN CABIN FLOOR AND STRINGER 30.NOTE: INSULATION REMOVED531220-0603-1 221 STRUCTURE AROUND FORWARD PAX DOOR MEC DET T: 9 YE CPCP AMM SSI 5312201 6.00 ALL222 I: 5 YE MRB S1 6.00DETAILED INSPECTION OF INTERNAL STRUCTURE MRB REFERENCE:AROUND FORWARD PASSENGER/CREW DOOR ABOVE CABIN FLOORBETWEEN FRAMES 13A AND 17 AND BETWEEN STRINGER 9 AND 531220-C603-A26. 531220-C603-BNOTE: 01. FURNISHINGS, LINING AND INSULATION INFLOOR AREA REMOVED02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.531221-0602-1 121 NOSE GEAR BAY ARCHES MEC DET I: 8500 FC MRB S AMM SSI 5312211 0.20 ALL1221 0.20DETAILED INSPECTION OF NOSE GEAR BAY ARCHESBETWEEN FRAMES 11A AND 16A, UPPER CORNERS, INCLUDINGBRACE STRUT ATTACH FITTING LUGS.ACCESS: 131AZ 132AZ* 0.01531223-0604-1 121 NOSE GEAR BAY ARCHES MEC DET I: 27300 FC MRB S AMM SSI 5312231 0.25 ALL1221 0.25DETAILED INSPECTION OF NOSE GEAR BAY ARCHESBETWEEN FRAMES 11 AND 16A LOWER CORNERS.ACCESS: 121KF 121MF 121NF 121PF 121QF 122EF* 1.98122GF 122HF 122JF 122KF531225-0604-1 121 NOSE GEAR BAY ARCHES MEC DET I: 27300 FC MRB S AMM SSI 5312251 0.50 ALL1221 0.50DETAILED INSPECTION OF NOSE GEAR BAY ARCHESATTACHMENTS TO FRAMES AT STRINGER 44, BETWEEN FRAMES11A AND 16A INCLUSIVE.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531225-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 121LF 121MF 121NF 121PF 121QF 122FF* 1.95122GF 122HF 122JF 122KF531227-0602-1 123 NOSE GEAR BAY TOP PANEL MEC DET I: 5 YE MRB S AMM SSI 5312271 0.10 ALL1241 0.10DETAILED INSPECTION OF TOP PANEL INNOSE GEAR BAY.531237-0604-1 121 FRAME 17 MEC DET I: 27300 FC MRB S AMM SSI 5312371 0.25 ALL1221 0.25DETAILED INSPECTION OF FRAME 17 AT STRINGERS43, 48 AND 51.ACCESS: 121TF 121UF 121VF 122LF 122MF 131AZ* 0.63531249-0603-1 120 NLG DOOR ACTUATOR ATTACHMENT FITTING NDT SDI T: 7500 FC ISB NTM 5130101 1.00 PRE 07191I: 2400 FC PART 1PRE 07587SPECIAL DETAILED INSPECTION OF FASTENER HOLES OF LH ISB 53-0248PRE 08492FITTING, NOSE GEAR WELL ROOF AND CROSSBEAM FRAME 14(53-0263)AND DETAILED VISUAL INSPECTION OF LH FITTING LUGS.NOTE : IF FASTENER HOLES ARE FITTED WITH BUSHES,REMOVE THE BUSHES FOR THE NDT INSPECTION.ACCESS: 132AZ* 0.01531249-0603-2 120 NLG DOOR ATTACHMENT FITTING MEC SDI T: 7000 FC ISB NTM 5312521 1.00 PRE 07191I: 1500 FC PART 4PRE 07587SPECIAL DETAILED INSPECTION OF NLG DOOR ACTUATOR ISB 53-0248PRE 08492UPPER SUPPORT ATTACHMENT FITTING, AND DETAILED(53-0263)INSPECTION OF FITTING FASTENERS AND CROSSBEAM AT FR14,RH.ACCESS: 132AZ* 0.01531249-0603-3 120 NLG DOOR ACTUATOR UPPER SUPPORT FITTING NDT SDI T: 16000 FC ISB NTM 5312521 1.00 POST 07191I: 2200 FC PART 4POST 07587SPECIAL DETAILED INSPECTION OF RH FITTING LUGS, FRAME ISB 53-0248POST 08492* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531249-0603-3 * * * * * C O N T I N U E * * * * *14.(53-0263)ACCESS: 132AZ* 0.01531249-0603-4 120 NLG DOOR ACTUATOR UPPER SUPPORT FITTING MEC DET T: 7000 FC ISB ISB 53-02481 0.20 PRE 07191I: 1500 FCPRE 07587DETAILED INSPECTION OF CROSSBEAM, FRAME 14.PRE 08492(53-0263)ACCESS: 132AZ* 0.01 POST 11421(53-0326)531251-0604-1 121 NOSE GEAR BAY SIDE LONGERON MEC DET I: 27300 FC MRB S AMM SSI 5312511 0.50 ALL1221 0.50DETAILED INSPECTION OF INTERNAL NOSE GEAR BAYSIDE LONGERON AT STRINGER 49 BETWEEN FRAMES 10 AND 11AND BETWEEN FRAMES 17 AND 19.ACCESS: 121JF 121TF 122CF 122DF 131AZ* 0.64N 531253-0604-1 121 FUSELAGE NOSE SECTION MEC DET T: 6600 FC EASA AD EASA AD1 2.30 ALL122 I: NOTE ISB 2009-01651 2.30DETAILED INSPECTION OF THE CROSSBEAM ON NLG FR 15A ISB 53-0327WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FITTINGNOTE: REFER TO ISB 53-0388 FOR INTERVALACCESS: 121BL* 0.01531303-0604-1 232 LONGERON CAB.FLOOR SUPPORT MEC DET I: 27300 FC MRB S AMM SSI 5313031 0.50 B2PRE 02295DETAILED INSPECTION OF LONGERON FOR CABINFLOOR PANEL SUPPORT FROM FRAME 20B TO 24A RH.PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTINGPANELS REMOVED.531303-0604-2 232 LONGERON CAB. FLOOR SUPPORT MEC DET I: 27300 FC MRB S AMM SSI 5313031 0.50 B2POST 02295* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531303-0604-2 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF LONGERON FOR CABINFLOOR PANEL SUPPORT FROM FRAME 20B TO 25 RH.PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTINGPANELS REMOVED.531303-0604-3 232 LONGERON CAB.FLOOR SUPPORT MEC DET I: 22600 FC MRB S AMM SSI 5313031 0.50 B4-100PRE 02295DETAILED INSPECTION OF LONGERON FOR CABINFLOOR PANEL SUPPORT FROM FRAME 20B TO 24A RH.PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTINGPANELS REMOVED.531303-0604-4 232 LONGERON CAB. FLOOR SUPPORT MEC DET I: 22600 FC MRB S AMM SSI 5313031 0.50 B4-100POST 02295DETAILED INSPECTION OF LONGERON FOR CABINFLOOR PANEL SUPPORT FROM FRAME 20B TO 25 RH.PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTINGPANELS REMOVED.531303-0604-5 232 LONGERON CAB.FLOOR SUPPORT MEC DET I: 19200 FC MRB S AMM SSI 5313031 0.50 B4-200C4DETAILED INSPECTION OF LONGERON FOR CABINF4FLOOR PANEL SUPPORT FROM FRAME 20B TO 24A RH.PRE 02295PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTINGPANELS REMOVED.531303-0604-6 232 LONGERON CAB. FLOOR SUPPORT MEC DET I: 19200 FC MRB S AMM SSI 5313031 0.50 B4-200C4DETAILED INSPECTION OF LONGERON FOR CABINF4FLOOR PANEL SUPPORT FROM FRAME 20B TO 25 RH.POST 02295PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTINGPANELS REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531309-0602-1 232 CARGO COMPARTM. DOOR FRAME MEC DET I: 7000 FC MRB S AMM SSI 5313091 0.20 ALLDETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS AT ATTACHMENT AREA OF STRINGER 24R TO FRAME 20AT UPPER FORWARD CORNER OF FWD CARGO COMPARTMENT DOORFRAME531309-0604-1 232 CARGO COMPARTM. DOOR FRAME MEC DET I: 27300 FC MRB S AMM SSI 5313091 1.00 B2DETAILED INSPECTION OF ATTACHMENT AREA OFSTRINGER 24R TO FRAME 20 AT UPPER FORWARD CORNER OFFWD CARGO COMPARTMENT DOOR FRAME.PREP.: CABIN SIDE LINING AND INSULATION REMOVED531309-0604-2 232 CARGO COMPARTM. DOOR FRAME MEC DET I: 22600 FC MRB S AMM SSI 5313091 1.00 B4-100DETAILED INSPECTION OF ATTACHMENT AREA OFSTRINGER 24R TO FRAME 20 AT UPPER FORWARD CORNER OFFWD CARGO COMPARTMENT DOOR FRAME.PREP.: CABIN SIDE LINING AND INSULATION REMOVED531309-0604-3 232 CARGO COMPARTM. DOOR FRAME MEC DET I: 19200 FC MRB S AMM SSI 5313091 1.00 B4-200C4DETAILED INSPECTION OF ATTACHMENT AREA OFF4STRINGER 24R TO FRAME 20 AT UPPER FORWARD CORNER OFFWD CARGO COMPARTMENT DOOR FRAME.PREP.: CABIN SIDE LINING AND INSULATION REMOVED531313-0603-1 134 FWD CARGO DOOR SILL BEAM MEC DET I: 5 YE CPCP AMM SSI 5313071 2.00 ALLMRB S AMM SSI 531313DETAILED INSPECTION OF FWD CARGO COMPARTMENTDOOR SILL BEAM FROM FRAME 19 TO FRAME 26, INCLUDING MRB REFERENCE:TORSION BOX AND ATTACHMENT AREAS.531313-C603-1NOTE: 01. DOOR SILL LATCHES AND GUIDES, BALLMATS,ROLLER TRACK AND INSULATION TO BE REMOVED02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531314-0604-1 100 FRAME BETWEEN 18 AND 40 NDT SDI T: SEE SB ISB NTM 51-70-001 1.50 B2K-3CI: SEE SB PART 1B4-103FSPECIAL DETAILED INSPECTION OF BONDED DOUBLERS IN THE NTM 53-30-00B4-120AREA OF LON LONGITUDINAL LAP JOINTS BETWEEN FR18 AND PART 5B4-203FR 40 NTM 53-30-50B4-203FPART 5B4-2CNOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 ISB 53-0378FOR APPLICABILITY DETAILS REFER TO SB 53-0378531314-0604-2 100 FRAME BETWEEN 26 AND 40 NDT SDI T: SEE SB ISB NTM 51-70-001 1.50 B2K-3CI: SEE SB PART 1B4-103FSPECIAL DETAILED INSPECTION OF BONDED DOUBLERS IN THE NTM 53-30-00B4-120CIRCUMFERENTIAL JOINT AREA BETWEEN FR 26 AND FR 40 PART 5B4-203NTM 53-30-10B4-203FNOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 PART 4 ORB4-2CFOR APPLICABILITY DETAILS REFER TO SB 53-0378 PART 6NTM 53-30-16PART 6NTM 53-30-20PART 4 ORPART 6NTM 53-30-50PART 5ISB 53-0378531314-0604-3 100 FRAME BETWEEN 34 AND 39 LH/RH NDT SDI T: SEE SB ISB NTM 51-70-001 1.50 B2K-3CI: SEE SB PART 1B4-103FSPECIAL DETAILED INSPECTION OF BONDED WING DOUBLERS NTM 53-30-00B4-120BETWEEN FR.34 AND FR.39, STGR 22 AND STGR 43 LH/RH PART 5B4-203NTM 53-30-10B4-203FNOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 PART 4 ORB4-2CFOR APPLICABILITY DETAILS REFER TO SB 53-0378 PART 6NTM 53-30-16PART 6NTM 53-30-20PART 4 ORPART 6NTM 53-30-50PART 5ISB 53-0378STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531314-0604-4 100 MANHOLE AREA BETWEEN FR 23 RH AND 24 RH NDT SDI T: SEE SB ISB NTM 51-70-001 1.50 B2K-3CAND BETWEEN FR 38.1 AND FR 38.2 I: SEE SB PART 1B4-103FNTM 53-30-00B4-120SPECIAL DETAILED INSPECTION OF BONDED DOUBLERS IN PART 5B4-203THE MANHOLE AREA BETWEEN FR 23 RH AND 24 RH AND NTM 53-30-10B4-203FBETWEEN FR 38.1 AND FR 38.2 PART 4 ORB4-2CPART 6NOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 NTM 53-30-16FOR APPLICABILITY DETAILS REFER TO SB 53-0378 PART 6NTM 53-30-20PART 4 ORPART 6NTM 53-30-50PART 5ISB 53-0378531315-0604-1 132 FRAME 25 MEC DET I: 27300 FC MRB S AMM SSI 5313151 0.50 B2PRE 02295DETAILED INSPECTION OF FRAME 25, BETWEENSTRINGERS 35R AND 37R.PREP.: SIDE LINING AND INSULATION REMOVED.531315-0604-2 132 FRAME 26 MEC DET I: 27300 FC MRB S AMM SSI 5313151 0.50 B2POST 02295DETAILED INSPECTION OF FRAME 26 BETWEENSTRINGERS 35R AND 37R.PREP.: SIDE LINING AND INSULATION REMOVED.531315-0604-3 132 FRAME 25 MEC DET I: 22600 FC MRB S AMM SSI 5313151 0.50 B4-100PRE 02295DETAILED INSPECTION OF FRAME 25, BETWEENSTRINGERS 35R AND 37R.PREP.: SIDE LINING AND INSULATION REMOVED.531315-0604-4 132 FRAME 26 MEC DET I: 22600 FC MRB S AMM SSI 5313151 0.50 B4-100POST 02295DETAILED INSPECTION OF FRAME 26 BETWEENSTRINGERS 35R AND 37R.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 20APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531315-0604-4 * * * * * C O N T I N U E * * * * *PREP.: SIDE LINING AND INSULATION REMOVED.531315-0604-5 132 FRAME 25 MEC DET I: 19200 FC MRB S AMM SSI 5313151 0.50 B4-200C4DETAILED INSPECTION OF FRAME 25, BETWEENF4STRINGERS 35R AND 37R.PRE 02295PREP.: SIDE LINING AND INSULATION REMOVED.531315-0604-6 132 FRAME 26 MEC DET I: 19200 FC MRB S AMM SSI 5313151 0.50 B4-200C4DETAILED INSPECTION OF FRAME 26 BETWEENF4STRINGERS 35R AND 37R.POST 02295PREP.: SIDE LINING AND INSULATION REMOVED.531317-0604-1 132 FRAME 20 MEC DET I: 27300 FC MRB S AMM SSI 5313171 0.50 B2DETAILED INSPECTION OF FRAME 20, BETWEEN EFERENCE:STRINGERS 35R AND 37R.PREP.: SIDE LINING AND INSULATION REMOVED.531317-0604-2 132 FRAME 20 MEC DET I: 22600 FC MRB S AMM SSI 5313171 0.50 B4-100DETAILED INSPECTION OF FRAME 20, BETWEENSTRINGERS 35R AND 37R.PREP.: SIDE LINING AND INSULATION REMOVED.531317-0604-3 132 FRAME 20 MEC DET I: 19200 FC MRB S AMM SSI 5313171 0.50 B4-200C4DETAILED INSPECTION OF FRAME 20, BETWEENF4STRINGERS 35R AND 37R.PREP.: SIDE LINING AND INSULATION REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 21APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531319-0602-1 232 FORMED FRAMES 21 TO 24 MEC DET I: 3500 FC MRB S AMM SSI 5313191 0.20 PRE 02295DETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS IN AREA OF FRAMES 21 TO 24 (4 PLACES) BETWEENSTRINGERS 21R AND 22R.531319-0602-2 232 FORMED FRAMES 21 TO 25 MEC DET I: 3500 FC MRB S AMM SSI 5313191 0.20 POST 02295DETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS IN AREA OF FRAME 21 TO 25 BETWEEN STRINGERS21RH AND 22RH.531319-0604-1 232 FORMED FRAMES 21 TO 24 MEC DET I: 27300 FC MRB S AMM SSI 5313191 2.50 B2PRE 02295DETAILED INTERNAL INSPECTION OF HINGE FITTINGSFITTINGS OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE ATATTACHMENT AREAS OF FORMED FRAMES 21 TO 24 (4 PLACES)TO HINGE FITTINGS BETWEEN STRINGERS 21R AND 22R.PREP.: SIDE LINING AND INSULATION REMOVED531319-0604-2 232 FORMED FRAMES 21 TO 25 MEC DET I: 27300 FC MRB S AMM SSI 5313191 2.50 B2POST 02295DETAILED INTERNAL INSPECTION OF HINGE FITTINGSOF FWD CARGO COMPARTMENT DOOR IN FUSELAGE ATATTACHMENT AREAS OF FORMED FRAMES 21 TO 25 BETWEENSTRINGERS 21RH AND 22RH.PREP.: SIDE LINING AND INSULATION REMOVED.531319-0604-3 232 FORMED FRAMES 21 TO 24 MEC DET I: 22600 FC MRB S AMM SSI 5313191 2.50 B4-100PRE 02295DETAILED INTERNAL INSPECTION OF HINGE FITTINGSFITTINGS OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE ATATTACHMENT AREAS OF FORMED FRAMES 21 TO 24 (4 PLACES)TO HINGE FITTINGS BETWEEN STRINGERS 21R AND 22R.PREP.: SIDE LINING AND INSULATION REMOVEDSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 22APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531319-0604-4 232 FORMED FRAMES 21 TO 25 MEC DET I: 22600 FC MRB S AMM SSI 5313191 2.50 B4-100POST 02295DETAILED INTERNAL INSPECTION OF HINGE FITTINGSOF FWD CARGO COMPARTMENT DOOR IN FUSELAGE ATATTACHMENT AREAS OF FORMED FRAMES 21 TO 25 BETWEENSTRINGERS 21RH AND 22RH.PREP.: SIDE LINING AND INSULATION REMOVED.531319-0604-5 232 FORMED FRAMES 21 TO 24 MEC DET I: 19200 FC MRB S AMM SSI 5313191 2.50 B4-200C4DETAILED INTERNAL INSPECTION OF HINGE FITTINGSF4FITTINGS OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE ATPRE 02295ATTACHMENT AREAS OF FORMED FRAMES 21 TO 24 (4 PLACES)TO HINGE FITTINGS BETWEEN STRINGERS 21R AND 22R.PREP.: SIDE LINING AND INSULATION REMOVED531319-0604-6 232 FORMED FRAMES 21 TO 25 MEC DET I: 19200 FC MRB S AMM SSI 5313191 2.50 B4-200C4DETAILED INTERNAL INSPECTION OF HINGE FITTINGSF4OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE ATPOST 02295ATTACHMENT AREAS OF FORMED FRAMES 21 TO 25 BETWEENSTRINGERS 21RH AND 22RH.PREP.: SIDE LINING AND INSULATION REMOVED.531321-0602-1 100 INSPECTION AT CIRCUMFERENTIAL SKIN NDT SDI T: 30000 FC ALI NTM 5313211 1.25 B2200 SPLICE AT FR 26 OR PART 61 1.25 FROM 0 FC/FH34200 FHTO 42500 FCSPECIAL DETAILED INSPECTION AT SPLICE PLATE AT I: 3700 FC ALI REFERENCE:CIRCUMFERENTIAL SKIN SPLICE AT FR26, FROM STR13 TO OR 531321-01-1CROWN CENTERLINE, LH/RH AREA 1. 4200 FH531321-0602-2 100 INSPECTION AT CIRCUMFERENTIAL SKIN NDT SDI T: 30000 FC ALI NTM 5313211 1.25 B4-100200 SPLICE AT FR 26 OR PART 61 1.25 FROM 0 FC/FH41700 FHTO 42500 FCSPECIAL DETAILED INSPECTION AT SPLICE PLATE AT I: 3100 FC ALI REFERENCE:CIRCUMFERENTIAL SKIN SPLICE AT FR26, FROM STR13 TO OR 531321-01-2CROWN CENTERLINE, LH/RH. 4300 FHSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 23APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531321-0602-3 100 INSPECTION AT CIRCUMFERENTIAL SKIN NDT SDI T: 30000 FC ALI NTM 5313211 1.25 B4-200200 SPLICE AT FR 26 OR PART 61 1.25 C469600 FH EASA ADF4SPECIAL DETAILED INSPECTION AT SPLICE PLATE AT I: 4100 FC 2006-0071FROM 0 FC/FHCIRCUMFERENTIAL SKIN SPLICE AT FR26, FROM STR13 TO OR FAA ADTO 42500 FCCROWN CENTERLINE, LH/RH. 9500 FH 2007-04-11ALI REFERENCE:531321-01-3531400-0602-1 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 7400 FC ISB ISB 53-01621 1.50 B2I: 2400 FCPRE 03275DETAILED INSPECTION OF THE FRONT LOWERPRE 05724REINFORCEMENT AT FR.40.(53-0161)PRE 11045(53-0315)531400-0602-2 231 MID.PASS/CREW DOOR FRAME MEC DET T: 30000 FC ISB CN1 0.20 PRE 02611232 I: 2000 FC 1983-102-053(B) 1 0.20DETAILED INSPECTION OF WEB- PLATE BETWEEN NOTE FAA AD 98-20-36FR.30A AND FR.32 AT STRINGER 18 AND 22 ISB 53-0182(LH & RH) FOR CRACKS (IF NECESSARY USE LIQUID PENE-TRANT METHODS).NOTE: FOR INTERVALS REFER ALSO TO ISB 53-0182.531400-0602-3 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 6000 FC ISB ISB 53-01621 1.50 B4-100I: 2000 FCPRE 03275DETAILED INSPECTION OF THE FRONT LOWERPRE 05724REINFORCEMENT AT FR.40.(53-0161)PRE 11045(53-0315)531400-0602-4 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 4500 FC ISB ISB 53-01621 1.50 B4-200I: 1400 FCC4DETAILED INSPECTION OF THE FRONT LOWERF4REINFORCEMENT AT FR.40.PRE 03275PRE 05724(53-0161)PRE 11045(53-0315)STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 24APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531400-0602-5 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 10000 FC ISB ISB 53-01621 1.50 B2NOTEPOST 03275DETAILED INSPECTION OF THE FRONT LOWER I: 4800 FCORREINFORCEMENT AT FR.40.POST 05724(53-0161)NOTE : THRESHOLD IS APPLICABLE STARTING FROM LASTPRE 11045EMBODYMENT OF SB 53-0161.(53-0315)531400-0602-6 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 8100 FC ISB ISB 53-01621 1.50 B4-100NOTEPOST 03275DETAILED INSPECTION OF THE FRONT LOWER I: 3900 FCORREINFORCEMENT AT FR.40.POST 05724(53-0161)NOTE : THRESHOLD IS APPLICABLE STARTING FROM LASTPRE 11045EMBODYMENT OF SB 53-0161.(53-0315)531400-0602-7 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 6200 FC ISB ISB 53-01621 1.50 B4-200NOTEC4DETAILED INSPECTION OF THE FRONT LOWER I: 3000 FCF4REINFORCEMENT AT FR.40.POST 03275ORNOTE : THRESHOLD IS APPLICABLE STARTING FROM LASTPOST 05724EMBODYMENT OF SB53-0161.(53-0161)PRE 11045(53-0315)531409-0603-1 231 FUSELAGE FRAME 28A AND 30A NDT SDI T: 10 YE ISB NTM 5314021 11.00 PRE 03185232 I: 5 YE PART 61 11.00 PRE SRM 531400SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 28A AND ISB 53-027430A, DOOR FRAME AREA.PREP.: MID DOOR FRAME LINING TO BE REMOVED.UPPER CARGO COMPARTMENT SIDEWALL PANELSTO BE REMOVED.531411-0603-1 230 STRUCTURE AROUND MID PAX/CREW DOOR MEC DET I: 5 YE AD AD 2007-04-111 2.00 ALL240 ALI EUAD 2006-00711 2.00DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND CPCPMID PASSENGER/CREW DOOR ABOVE CABIN FLOOR BETWEEN EUAD ALI REFERENCE:FRAMES 27 AND 32 AND BETWEEN STRINGERS 9 AND 26. MRB S 531411-01-1* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 25APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531411-0603-1 * * * * * C O N T I N U E * * * * *PREP.: - FURNISHING, LINING AND INSULATION IN FLOOR MRB REFERENCE:AND FURNISHING, LINING AND INSULATION IN SSI 531411DOOR REMOVED 531411-C603-A531411-C603-B- APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.531411-0604-1 231 STRUCTURE AROUND MID PAX/CREW DOOR NDT SDI I: 9000 FC ALI NTM 5314001 0.25 ALL232 PART 2,61 0.25 FROM 0 FC/FHDETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL EASA ADTO LOVSTRUCTURE AROUND MID PASSENGER/CREW DOOR ABOVE CABIN 2006-0071FLOOR BETWEEN FR27 AND FR32 AND BETWEEN STR9 AND FAA ADSTR26. 2007-04-11PREP : FURNISHING, LINING AND INSULATION IN DOOR ALI REFERENCE:AREA TO BE REMOVED 531411-01-1531411-02-1531501-0604-1 130 FRAME NO. 39 MEC DET I: 27300 FC MRB S AMM SSI 5315011 1.25 ALL2401 1.25DETAILED INSPECTION OF FRAME 39 BETWEENSTRINGERS 20 AND 30.PREP.: LOWER SIDE WALL PANEL AND DECOMPRESSION PANEL,CABIN AND CARGO SIDE LINING AND INSULATIONREMOVED.ACCESS: 241TF 241YF 242QF 242UF* 1.53531503-0604-1 143 WING CENTER BOX ATTACHMENT MEC DET I: 27300 FC MRB S AMM SSI 5315031 0.50 B21441 0.50DETAILED INSPECTION OF LOWER ATTACHMENTS OFCENTER WING BOX FRONT SPAR TO FRAME FITTINGS ATFRAME 40.ACCESS: 147GZ 148GZ* 0.06531503-0604-2 143 WING CENTER BOX ATTACHMENT MEC DET I: 22600 FC MRB S AMM SSI 5315031 0.50 B4-1001441 0.50* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 26APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531503-0604-2 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF LOWER ATTACHMENTS OFCENTER WING BOX FRONT SPAR TO FRAME FITTINGS ATFRAME 40.ACCESS: 147GZ 148GZ* 0.06531503-0604-3 143 WING CENTER BOX ATTACHMENT MEC DET I: 19200 FC MRB S AMM SSI 5315031 0.50 B4-2001441 0.50 C4DETAILED INSPECTION OF LOWER ATTACHMENTS OFF4CENTER WING BOX FRONT SPAR TO FRAME FITTINGS ATFRAME 40.ACCESS: 147GZ 148GZ* 0.06531505-0604-1 145 WING CENTER BOX ATTACHMENTS MEC DET I: 27300 FC MRB S AMM SSI 5315051 0.50 B21461 0.50DETAILED INSPECTION OF UPPER ATTACHMENTS OFCENTER WING BOX FRONT SPAR TO FRAME FITTINGS ATFRAME 40.ACCESS: 241VF* 0.31531505-0604-2 145 WING CENTER BOX ATTACHMENTS MEC DET I: 22600 FC MRB S AMM SSI 5315051 0.50 B4-1001461 0.50DETAILED INSPECTION OF UPPER ATTACHMENTS OFCENTER WING BOX FRONT SPAR TO FRAME FITTINGS ATFRAME 40.ACCESS: 241VF* 0.31531505-0604-3 145 WING CENTER BOX ATTACHMENTS MEC DET I: 19200 FC MRB S AMM SSI 5315051 0.50 B4-2001461 0.50 C4DETAILED INSPECTION OF UPPER ATTACHMENTS OFF4CENTER WING BOX FRONT SPAR TO FRAME FITTINGS ATFRAME 40.ACCESS: 241VF* 0.31STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 27APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531508-0604-1 140 FRAMES 40 TO 53 MEC DET I: 27300 FC MRB S AMM SSI 5315081 5.00 B22401 5.00DETAILED INSPECTION OF FRAMES 40 TO 53,BETWEENPRESSURIZED FLOOR AND STRINGERS 18 ́LH,RH.PREP.: SIDE LININGS AND INSULATION REMOVED.ACCESS: 241AC 241AD 241AH 241AJ 241AN 241AP* 2.90241AT 241AU 241AV 242AB 242AC 242AF242AG 242AK 242AL 242AM 242XF 242YF531508-0604-2 140 FRAMES 40 TO 53 MEC DET I: 22600 FC MRB S AMM SSI 5315081 5.00 B4-1002401 5.00DETAILED INSPECTION OF FRAMES 40 TO 53,BETWEENPRESSURIZED FLOOR AND STRINGERS 18 ́LH,RH.PREP.: SIDE LININGS AND INSULATION REMOVED.ACCESS: 241AC 241AD 241AH 241AJ 241AN 241AP* 2.90241AT 241AU 241AV 242AB 242AC 242AF242AG 242AK 242AL 242AM 242XF 242YF531508-0604-3 140 FRAMES 40 TO 53 MEC DET I: 19200 FC MRB S AMM SSI 5315081 5.00 B4-2002401 5.00 C4DETAILED INSPECTION OF FRAMES 40 TO 53,BETWEENF4PRESSURIZED FLOOR AND STRINGERS 18 ́LH,RH.PREP.: SIDE LININGS AND INSULATION REMOVED.ACCESS: 241AC 241AD 241AH 241AJ 241AN 241AP* 2.90241AT 241AU 241AV 242AB 242AC 242AF242AG 242AK 242AL 242AM 242XF 242YF531513-0602-1 240 FRAME 47 MEC DET T: 12000 FC MRB S1 0.25 B4-100I: 4300 FCPOST 3039DETAILED INSPECTION AT FR47 FROM STR 13 TO STR 22,ORLH/RH, EXTERNAL SURFACEB4-200POST 3039ORF4POST 3039FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 28APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531513-0602-1 * * * * * C O N T I N U E * * * * *TO LOV531514-0602-1 140 SPLICE AT FRAME 54 MEC DET I: 5500 FC MRB S AMM SSI 5315141 0.25 B21501 0.25DETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS AT STRINGER TO SKIN PICK UP SPLICE AT FRAME 54BETWEEN STRINGERS 42, L/H AND R/H.531514-0602-2 140 SPLICE AT FRAME 54 MEC DET I: 4500 FC MRB S AMM SSI 5315141 0.25 B4-1001501 0.25DETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS AT STRINGER TO SKIN PICK UP SPLICE AT FRAME 54BETWEEN STRINGERS 42, L/H AND R/H.531514-0602-3 140 SPLICE AT FRAME 54 MEC DET I: 3800 FC MRB S AMM SSI 5315141 0.25 B4-2001501 0.25 C4DETAILED INSPECTION OF EXTERNAL SKIN ANDF4RIVETS AT STRINGER TO SKIN PICK UP SPLICE AT FRAME 54BETWEEN STRINGERS 42, L/H AND R/H.531514-0604-1 140 SPLICE AT FRAME 54 MEC DET I: 27300 FC MRB S AMM SSI 5315141 1.50 B21501 1.50DETAILED INSPECTION OF INTERNAL STRINGER TOSKIN PICK-UP SPLICE AT FRAME 54 BETWEEN STRINGERS 42,LH AND RH.ACCESS: 147SZ 147TZ 148SZ 148TZ* 0.09151AF 151BF 151CF 152AF 152BF* 0.83531514-0604-2 140 SPLICE AT FRAME 54 MEC DET I: 22600 FC MRB S AMM SSI 5315141 1.50 B4-1001501 1.50DETAILED INSPECTION OF INTERNAL STRINGER TOSKIN PICK-UP SPLICE AT FRAME 54 BETWEEN STRINGERS 42,LH AND RH.ACCESS: 147SZ 147TZ 148SZ 148TZ* 0.09151AF 151BF 151CF 152AF 152BF* 0.83STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 29APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531514-0604-3 140 SPLICE AT FRAME 54 MEC DET I: 19200 FC MRB S AMM SSI 5315141 1.50 B4-2001501 1.50 C4DETAILED INSPECTION OF INTERNAL STRINGER TOF4SKIN PICK-UP SPLICE AT FRAME 54 BETWEEN STRINGERS 42,LH AND RH.ACCESS: 147SZ 147TZ 148SZ 148TZ* 0.09151AF 151BF 151CF 152AF 152BF* 0.83531518-0604-1 143 WING CENTER BOX LOWER PANEL MEC DET I: 27300 FC MRB S AMM SSI 5315181 12.50 B21441 12.50DETAILED INSPECTION OF WING CENTER BOX LOWERPANEL OUTER SURFACE FROM FRAME NO.45 TO FRAME NO.47.ACCESS: 147FZ 147GZ* 0.07531518-0604-2 143 WING CENTER BOX LOWER PANEL MEC DET I: 22600 FC MRB S AMM SSI 5315181 12.50 B4-1001441 12.50DETAILED INSPECTION OF WING CENTER BOX LOWERPANEL OUTER SURFACE FROM FRAME NO.45 TO FRAME NO.47.PREP.: VAPOR SEAL REMOVEDACCESS: 147FZ 147GZ* 0.07531518-0604-3 143 WING CENTER BOX LOWER PANEL MEC DET I: 19200 FC MRB S AMM SSI 5315181 12.50 B4-2001441 12.50 C4DETAILED INSPECTION OF WING CENTER BOX LOWERF4PANEL OUTER SURFACE FROM FRAME NO.45 TO FRAME NO.47.PREP.: VAPOR SEAL REMOVEDACCESS: 147FZ 147GZ* 0.07531525-0604-1 150 FRAME 54 MEC DET I: 27300 FC MRB S AMM SSI 5315251 1.00 ALL2401 1.00DETAILED INSPECTION OF FRAME NO.54 BETWEENSTRINGERS 25 AND 30, RH AND LH.PREP.: LININGS AND INSULATION REMOVED* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 30APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531525-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 241AU 241AV 241AZ 241BA 242AL 242AM* 1.28242AQ 242AR531531-0602-1 147 BRACE STRUT HINGE FITTING MEC DET T: 18800 FC ALI CN 2006-0071(B) 1 0.17 B2148 OR FAA AD 96-13-11 1 0.17 FROM 0 FC/FHDETAILED INSPECTION OF BRACE STRUT 21200 FHTO LOVHINGE FITTING IN MAIN GEAR BAY AND ATTACHMENTS TO I: 8500 FC ALI REFERENCE:CANTED FRAMES. OR 531531-01-19600 FHACCESS: 734* 0.10744* 0.10531531-0602-2 147 BRACE STRUT HINGE FITTING MEC DET T: 18800 FC ALI CN 2006-0071(B) 1 0.17 B4-100148 OR FAA AD 96-13-11 1 0.17 FROM 0 FC/FHDETAILED INSPECTION OF BRACE STRUT 25700 FHTO LOVHINGE FITTING IN MAIN GEAR BAY AND ATTACHMENTS TO I: 8500 FC ALI REFERENCE:CANTED FRAMES. OR 531531-01-211600 FHACCESS: 734* 0.10744* 0.10531531-0602-3 147 BRACE STRUT HINGE FITTING MEC DET T: 18800 FC ALI CN 2006-0071(B) 1 0.17 B4-200148 OR FAA AD 96-13-11 1 0.17 C4DETAILED INSPECTION OF BRACE STRUT 42700 FHF4HINGE FITTING IN MAIN GEAR BAY AND ATTACHMENTS TO I: 8500 FC ALI REFERENCE: FROM 0 FC/FHCANTED FRAMES. OR 531531-01-3TO LOV19300 FHACCESS: 734* 0.10744* 0.10531533-0604-1 143 WING CENTER BOX FRONT SPAR MEC DET I: 27300 FC MRB S AMM SSI 5315331 0.25 B21441 0.25DETAILED INSPECTION OF ATTACHMENT OF WINGCENTER BOX FRONT SPAR TO LOWER SKIN PANEL IN AREA OFAIRCRAFT CENTER LINE.ACCESS: 147GZ* 0.03148GZ* 0.03STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 31APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531533-0604-2 143 WING CENTER BOX FRONT SPAR MEC DET I: 22600 FC MRB S AMM SSI 5315331 0.25 B4-1001441 0.25DETAILED INSPECTION OF ATTACHMENT OF WINGCENTER BOX FRONT SPAR TO LOWER SKIN PANEL IN AREA OFAIRCRAFT CENTER LINE.PREP.: REMOVE/INSTALL VAPOR SEAL.ACCESS: 147GZ* 0.03148GZ* 0.03531533-0604-3 143 WING CENTER BOX FRONT SPAR MEC DET I: 19200 FC MRB S AMM SSI 5315331 0.25 B4-2001441 0.25 C4DETAILED INSPECTION OF ATTACHMENT OF WINGF4CENTER BOX FRONT SPAR TO LOWER SKIN PANEL IN AREA OFAIRCRAFT CENTER LINE.PREP.: REMOVE/INSTALL VAPOR SEAL.ACCESS: 147GZ* 0.03148GZ* 0.03531537-0604-1 141 WING CENTER SPAR MEC DET I: 27300 FC MRB S AMM SSI 5315371 0.20 B2142 NTM 5315001 0.20DETAILED OR NDT INSPECTION OF CORNERS OF PART 6TRIANGULAR CUTOUTS IN WING CENTER SPAR.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531537-0604-2 141 WING CENTER SPAR MEC SDI I: 22600 FC MRB S AMM SSI 5315371 0.20 B4-100142 NTM 5315001 0.20DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6TRIANGULAR CUTOUTS IN WING CENTER SPAR.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531537-0604-3 141 WING CENTER SPAR MEC DET I: 19200 FC MRB S AMM SSI 5315371 0.20 B4-200142 NTM 5315001 0.20 C4DETAILED NDT INSPECTION OF CORNERS OF PART 6F4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 32APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531537-0604-3 * * * * * C O N T I N U E * * * * *TRIANGULAR CUTOUTS IN WING CENTER SPAR.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531539-0604-1 147 WING REAR SPAR MEC SDI I: 27300 FC MRB S AMM SSI 5315391 0.20 B2148 NTM 5315001 0.20DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6TRIANGULAR CUTOUTS IN WING REAR SPAR.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531539-0604-2 147 WING REAR SPAR MEC SDI I: 22600 FC MRB S AMM SSI 5315391 0.20 B4-100148 NTM 5315001 0.20DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6TRIANGULAR CUTOUTS IN WING REAR SPAR.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531539-0604-3 147 WING REAR SPAR MEC SDI I: 19200 FC MRB S AMM SSI 5315391 0.20 B4-200148 NTM 5315001 0.20 C4DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6F4TRIANGULAR CUTOUTS IN WING REAR SPAR.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531540-0603-1 145 FRAME 47 NDT SDI I: 6000 FC ISB ISB 53-01951 4.00 B21461 4.00 PRE 02373SPECIAL DETAILED INSPECTION OF FLANGES OF FRAME 47LH/RH BETWEEN STRINGERS 23 AND 26NOTE: 1. TASK NOT APPLICABLE AFTER SHOT PEENING2. LINING AND INSULATION TO BE REMOVEDSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 33APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531540-0603-2 241 FUSELAGE FRAME 47 NDT SDI T: 6000 FC ISB CN1 4.00 B2242 I: 6000 FC 1984-117-062(B) 1 4.00 PRE 05760SPECIAL DETAILED INSPECTION OF TWO FASTENER HOLES ON CN(53-0198)FR 47 IN ACCORDANCE WITH ISB 53-0194 FOR FIRST 1990-222-116(B)INSPECTION AND WITH ISB 53-0196 FOR SUBSEQUENT FAA ADINSPECTION. 2000-10-01FAA AD 87-04-12NOTE : LINING AND INSULATION TO BE REMOVED FAA AD 96-08-08ISB 53-0194ISB 53-0196531540-0604-1 145 FRAME 47 NDT SDI I: 27300 FC MRB S AMM SSI 5315401 0.80 B2146 NTM 5315001 0.80147 DETAILED AND SPECIAL DETAILED INSPECTION OF FRAME 47 PART 21 0.80148 MACHINED AREAS AND ATTACHMENT TO ADJOINING PARTS1 0.80241 (INCLUDING ZONES 146, 147/148, 241/242).1 0.802421 0.80PREP.: LINING AND INSULATION REMOVED.ACCESS: 241AKF 241ALF 241AMF 241ANF* 0.50242ADF 242AEF 242AFF* 0.38531540-0604-2 145 FRAME 47 NDT SDI I: 22600 FC MRB S AMM SSI 5315401 0.80 B4-100146 NTM 5315001 0.80147 DETAILED AND SPECIAL DETAILED INSPECTION OF FRAME 47 PART 21 0.80148 MACHINED AREAS AND ATTACHMENT TO ADJOINING PARTS.1 0.802411 0.80242 PREP.: LINING AND INSULATION REMOVED.1 0.80ACCESS: 241AKF 241ALF 241AMF 241ANF* 0.50242ADF 242AEF 242AFF* 0.38531540-0604-3 145 FRAME 47 NDT SDI I: 19200 FC MRB S AMM SSI 5315401 0.80 B4-200146 NTM 5315001 0.80 C4147 DETAILED AND SPECIAL DETAILED INSPECTION OF FRAME 47 PART 21 0.80 F4148 MACHINED AREAS AND ATTACHMENT TO ADJOINING PARTS.1 0.802411 0.80242 PREP.: LINING AND INSULATION REMOVED.1 0.80ACCESS: 241AKF 241ALF 241AMF 241ANF* 0.50242ADF 242AEF 242AFF* 0.38STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 34APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531543-0604-1 141 CENTER WING BOX MEC DET I: 27300 FC MRB S AMM SSI 5315431 0.10 B21421 0.10DETAILED INSPECTION OF INNER FACE OF LOWERSKIN PANEL OF CENTER WING BOX BETWEEN FRAMES NO.44AND 46 AT AIRCRAFT CENTER LINE.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531543-0604-2 141 CENTER WING BOX MEC DET I: 22600 FC MRB S AMM SSI 5315431 0.10 B4-1001421 0.10DETAILED INSPECTION OF INNER FACE OF LOWERSKIN PANEL OF CENTER WING BOX BETWEEN FRAMES NO.44AND 46 AT AIRCRAFT CENTER LINE.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531543-0604-3 141 CENTER WING BOX MEC DET I: 19200 FC MRB S AMM SSI 5315431 0.10 B4-2001421 0.10 C4DETAILED INSPECTION OF INNER FACE OF LOWERF4SKIN PANEL OF CENTER WING BOX BETWEEN FRAMES NO.44AND 46 AT AIRCRAFT CENTER LINE.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531547-0604-1 141 WING CENTER BOX - INBOARD NDT SDI I: 27300 FC MRB S AMM SSI 5315471 2.50 B2142 NTM 5315001 2.50DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2CENTER BOX LOWER SKIN SPLICE WITH RIB 1 INBOARD.ACCESS: 147AZ 147DZ 541AB 542CB* 3.25148AZ 148DZ 641AB 642CB* 3.25531547-0604-2 141 WING CENTER BOX - INBOARD NDT SDI I: 22600 FC MRB S AMM SSI 5315471 2.50 B4-100142 NTM 5315001 2.50DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2CENTER BOX LOWER SKIN SPLICE WITH RIB 1 INBOARD,ACCESS: 147AZ 147DZ 541AB 542CB* 3.25* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 35APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531547-0604-2 * * * * * C O N T I N U E * * * * *148AZ 148DZ 641AB 642CB* 3.25531547-0604-3 141 WING CENTER BOX - INBOARD NDT SDI I: 19200 FC MRB S AMM SSI 5315471 2.50 B4-200142 NTM 5315001 2.50 C4DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2F4CENTER BOX LOWER SKIN SPLICE WITH RIB 1 INBOARD.ACCESS: 147AZ 147DZ 541AB 542CB* 3.25148AZ 148DZ 641AB 642CB* 3.25531548-0603-1 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 26300 FC ALI NTM 5315481 1.50 B2542 OR PART 41 1.50 FROM 0 FC/FH641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 28400 FH EASA AD1 1.50 TO LOV642 ATTACHMENT (WING SIDE). I: 3800 FC 2006-00711 1.50OR FAA AD4100 FH 2007-04-11ALI REFERENCE:531548-01-1531548-0603-2 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 30300 FC ALI NTM 5315481 1.50 B4-100542 OR PART 41 1.50 FROM 0 FC/FH641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 40300 FH EASA AD1 1.50 TO LOV642 ATTACHMENT (WING SIDE). I: 4500 FC 2006-00711 1.50OR FAA AD9400 FH 2007-04-11ALI REFERENCE:531548-01-2531548-0603-3 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 31100 FC ALI NTM 5315481 1.50 B4-200542 OR PART 41 1.50 C4641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 64700 FH EASA AD1 1.50 F4642 ATTACHMENT (WING SIDE). I: 4500 FC 2006-00711 1.50 FROM 0 FC/FHOR FAA ADTO LOV9400 FH 2007-04-11ALI REFERENCE:531548-01-3STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 36APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531548-0603-4 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 31100 FC ALI NTM 5315481 1.50 B2542 OR PART 21 1.50 FROM 0 FC/FH641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 64700 FH EASA AD1 1.50 TO LOV642 ATTACHMENT (WING SIDE). I: 4500 FC 2006-00711 1.50OR FAA ADACCESS: 541AB 9400 FH 2007-04-11* 1.50542CB* 1.50641AB ALI REFERENCE: * 1.50642CB 531548-02-1* 1.50531548-0603-5 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 35100 FC ALI NTM 5315481 1.50 B4-100542 OR PART 21 1.50 FROM 0 FC/FH641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 46700 FH EASA AD1 1.50 TO LOV642 ATTACHMENT (WING SIDE). I: 2300 FC 2006-00711 1.50OR FAA ADACCESS: 541AB 3100 FH 2007-04-11* 1.50542CB* 1.50641AB ALI REFERENCE: * 1.50642CB 531548-02-2* 1.50531548-0603-6 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 31100 FC ALI NTM 5315481 1.50 B4-200542 OR PART 21 1.50 C4641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 64700 FH EASA AD1 1.50 F4642 ATTACHMENT (WING SIDE). I: 2200 FC 2006-00711 1.50 FROM 0 FC/FHOR FAA ADTO LOVACCESS: 541AB 4500 FH 2007-04-11* 1.50542CB* 1.50641AB ALI REFERENCE: * 1.50642CB 531548-02-3* 1.50531548-0604-1 540 LOWER SKIN SPLICE RIB 1 NDT SDI I: 27300 FC MRB S AMM SSI 5315481 5.00 B2640 NTM 5315001 5.00DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2CENTER BOX LOWER SKIN SPLICE WITH RIB 1 (IN SITU ASFAR AS VISIBLE).ACCESS: 541AB 542CB* 3.00641AB 642CB* 3.00531548-0604-2 540 LOWER SKIN SPLICE RIB 1 NDT SDI I: 22600 FC MRB S AMM SSI 5315481 5.00 B4-1006401 5.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 37APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531548-0604-2 * * * * * C O N T I N U E * * * * *DETAILED AND SPECIAL DETAILED INSPECTION OF WING NTM 531500CENTER BOX LOWER SKIN SPLICE WITH RIB 1 (IN SITU AS PART 2FAR AS VISIBLE).ACCESS: 541AB 542CB* 3.00641AB 642CB* 3.00531548-0604-3 540 LOWER SKIN SPLICE RIB 1 NDT SDI I: 19200 FC MRB S AMM SSI 5315481 5.00 B4-200640 NTM 5315001 5.00 C4DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2F4CENTER BOX LOWER SKIN SPLICE WITH RIB 1 (IN SITU ASFAR AS VISIBLE).ACCESS: 541AB 542CB* 3.00641AB 642CB* 3.00531549-0602-1 140 WING SPAR BOX MEC DET I: 3800 FC MRB S AMM SSI 5315491 0.33 B4-200C4DETAILED INSPECTION OF EXTERNALF4WING SPAR BOX LOWER SKIN PANEL AREA BETWEENFRAME 43 AND 46 AT THE END OF THE REINFORCINGMEMBERS (3 LAST BOLTS).531549-0602-2 140 WING SPAR BOX MEC DET I: 6000 FH MRB S AMM SSI 5315491 0.33 POST 06208MSN 256DETAILED INSPECTION OF EXTERNALWING SPAR BOX LOWER SKIN PANEL AREA BETWEENFRAME 43 AND 46 AT THE END OF THE REINFORCINGMEMBERS (3 LAST BOLTS).531549-0604-1 140 WING SPAR BOX NDT SDI I: 19200 FC MRB S AMM SSI 5315491 25.00 B4-200NTM 531500C4SPECIAL DETAILED INSPECTION OF WING CENTER BOX LOWER PART 2F4SKIN PANEL AREA BETWEEN FRAME 43 AND 46 AT THE END OFTHE REINFORCING MEMBERS (3 LAST BOLTS).ACCESS: 147AZ 148AZ* 0.45STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 38APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531549-0604-2 140 WING SPAR BOX NDT SDI I: 27300 FC MRB S AMM SSI 5315491 25.00 POST 06208NTM 531500MSN 256SPECIAL DETAILED INSPECTION OF WING CENTER BOX LOWER PART 2SKIN PANEL AREA BETWEEN FRAME 43 AND 46 AT THE END OFTHE REINFORCING MEMBERS (3 LAST BOLTS).ACCESS: 147AZ 147DZ 148AZ 148DZ* 0.51531553-0604-1 141 WEB PLATE MEC DET I: 27300 FC MRB S AMM SSI 5315531 0.25 B21421 0.25DETAILED INSPECTION OF WEB PLATE AROUND FUELPIPE CUTOUT IN RIB 1.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531553-0604-2 141 WEB PLATE MEC DET I: 22600 FC MRB S AMM SSI 5315531 0.25 B4-1001421 0.25DETAILED INSPECTION OF WEB PLATE AROUND FUELPIPE CUTOUT IN RIB 1.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531553-0604-3 141 WEB PLATE MEC DET I: 19200 FC MRB S AMM SSI 5315531 0.25 B4-2001421 0.25 C4DETAILED INSPECTION OF WEB PLATE AROUND FUELF4PIPE CUTOUT IN RIB 1.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531555-0604-1 147 MACHINED PART OF PRESSURE FLOOR MEC DET I: 27300 FC MRB S AMM SSI 5315551 0.25 ALL1481 0.25DETAILED INSPECTION OF MACHINED PART OFPRESSURE FLOOR LH AND RH BETWEEN FRAMES 51 AND 52.ACCESS: 147PZ* 0.02STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 39APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531557-0602-1 147 PRESSURIZED FLOOR MEC DET I: 5700 FC MRB S AMM SSI 5315571 0.33 PRE 03378(29-0077)DETAILED INSPECTION OF PRESSURIZEDFLOOR SEALED WEB L/H SIDE BETWEEN FRAMES 48 AND 49 -CUTOUT IN MACHINED SECTIONNOTE: QUICK RELEASE BOOT REMOVEDACCESS: 147KZ* 0.01531557-0602-2 147 PRESSURIZED FLOOR MEC DET I: 5700 FC MRB S AMM SSI 5315571 1.00 POST 03378(29-0077)DETAILED INSPECTION OF PRESSURIZED FLOORSEALED WEB LH SIDE BETWEEN FRAMES 48 AND 49 CUTOUTIN MACHINED SECTION531559-0604-1 147 VERTICAL STIFFENERS MEC DET I: 27300 FC MRB S AMM SSI 5315591 0.25 ALL1481 0.25DETAILED INSPECTION OF VERTICAL STIFFENERS ATY = 420 (LH,RH) AND UPPER SECTIONS OF THE 7 OTHERVERTICAL STIFFENERS AT MAIN GEAR BAY REAR BULKHEAD.ACCESS: 147LZ 147MZ* 0.11148LZ 148MZ* 0.28531561-0604-1 147 PRESSURIZED FLOOR MEC DET I: 27300 FC MRB S AMM SSI 5315611 0.25 ALL1481 0.25DETAILED INSPECTION OF ATTACHMENT OF WEB TOHORIZONTAL BEAMS LH AND RH BETWEEN FRAMES NO.47AND 54.ACCESS: 147LZ 147MZ 147NZ* 0.14148LZ 148MZ 148NZ* 0.31531563-0602-1 147 FRAMES 48 TO 53A MEC DET I: 8500 FC MRB S AMM SSI 5315631 0.25 POST 014441481 0.25 (53-0078)DETAILED INSPECTION OF FRAMES 48 TO 53A BELOWPRESSURIZED FLOOR SEALED WEB, INCLUDING Y-FITTINGCONNECTING THE REAR OBLIQUE FRAME TO FRAME 53A.FRAME 50 EXCEPTED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 40APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531563-0602-2 147 FRAME 53A MEC GVI I: 5700 FC ISB ISB 53-01291 0.75 PRE 014441481 0.75 (53-0078)GENERAL VISUAL INSPECTION OF Y-FITTINGCONNECTING THE REAR OBLIQUE FRAME TO FRAME 53A FORDAMAGE.NOTE: 6000 F/H (PLUS-MINUS 1500 F/H)531568-0604-1 145 HINGE SEAT RAILS MEC DET I: 19200 FC MRB S AMM SSI 5315681 0.50 C41461 0.50 F4DETAILED INSPECTION OF HINGE SEAT RAILS NO. 1,2, 3, 4 LH AND RH AT FRAMES 40 AND 54.PREP.: FLOOR PANELS REMOVED531568-0604-2 145 HINGE SEAT RAILS MEC DET I: 22600 FC MRB S AMM SSI 5315681 1.00 POST 062081461 1.00 MSN 256DETAILED INSPECTION OF HINGE SEAT RAILS NO. 1,2, 3, 4 LH AND RH AT FRAMES 40 AND 54.PREP.: FLOOR PANELS REMOVED531569-0604-1 145 FLOOR CROSS MEMBERS MEC DET I: 19200 FC MRB S AMM SSI 5315691 0.25 C41461 0.25 F4DETAILED INSPECTION OF FLOOR CROSS MEMBERSBETWEEN SEAT RAILS NO.2 AND 3 LH AND RH BETWEENFRAMES 40 AND 54.PREP.: FLOOR PANELS REMOVED.531569-0604-2 145 FLOOR CROSS MEMBERS MEC DET I: 22600 FC MRB S AMM SSI 5315691 0.25 POST 062081461 0.25 MSN 256DETAILED INSPECTION OF FLOOR CROSS MEMBERSBETWEEN SEAT RAILS NO.2 AND 3 LH AND RH BETWEENFRAMES 40 AND 54.PREP.: FLOOR PANELS REMOVED.531570-0603-1 141 MAIN FRAME - FUSELAGE CENTER SECTION MEC DET T: 9750 FC SB SB 53-03371 2.00 B2142 I: 8100 FC1 2.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 41APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531570-0603-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF THE FRAME BASE FITTINGSBETWEEN FRAME 41 AND FRAME 46.ACCESS: 147FZ 734* 0.14744* 0.10531570-0603-2 141 MAIN FRAME - FUSELAGE CENTER SECTION MEC DET T: 8200 FC SB SB 53-03371 2.00 B4-100142 I: 6800 FC1 2.00DETAILED INSPECTION OF THE FRAME BASE FITTINGSBETWEEN FRAME 41 AND FRAME 46.ACCESS: 147FZ 734* 0.14744* 0.10531570-0603-3 141 MAIN FRAME - FUSELAGE CENTER SECTION MEC DET T: 6400 FC SB SB 53-03371 2.00 B4-200142 I: 5300 FC1 2.00DETAILED INSPECTION OF THE FRAME BASE FITTINGSBETWEEN FRAME 41 AND FRAME 46.ACCESS: 147FZ 734* 0.14744* 0.10531571-0604-1 141 PUMP APERTURES MEC DET I: 19200 FC MRB S AMM SSI 5315711 5.00 B4-200142 AMM 281311/4011 5.00 C4DETAILED INSPECTION OF INTERNAL PUMP APERTURES AMM 282137/401F4IN CENTER WING BOX LOWER SKIN AND REINFORCINGS.PREP.: VAPOR SEAL, PUMP AND CANISTER REMOVED.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531571-0604-2 141 PUMP APERTURES MEC DET I: 22600 FC MRB S AMM SSI 5315711 5.00 B4-100142 AMM 281311/4011 5.00DETAILED INSPECTION OF INTERNAL PUMP APERTURES AMM 282137/401IN CENTER WING BOX LOWER SKIN AND REINFORCINGS.PREP.: VAPOR SEAL, PUMP AND CANISTER REMOVED.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 42APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531571-0604-2 * * * * * C O N T I N U E * * * * *ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25531572-0602-1 240 SKIN AROUND VHF 3 ANTENNA MEC DET T: 40000 FC ALI EASA AD1 0.30 IF VHF 3I: 9000 FC 2006-0071ANTENNADETAILED INSPECTION OF FUSELAGE SKIN AROUND FAA ADINSTALLEDVHF 3 ANTENNA FR47-FR48. 2007-04-11FROM 0 FC/FHTO LOVPREP : ANTENNA TO BE REMOVED ALI REFERENCE:531572-01-1531573-0602-1 240 SKIN AROUND ANTI-COLLISION LIGHT MEC DET T: 24000 FC ALI EASA AD1 0.20 ALLI: 5500 FC 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE SKIN AROUND ANTI- FAA ADTO LOVCOLLISION LIGHT BETWEEN FR 43 AND FR 44. 2007-04-11PREP : ANTI-COLLISION LIGHT TO BE REMOVED ALI REFERENCE:531573-01-4531603-0604-1 151 STRUCTURE - FRAMES 55 TO 58 MEC DET I: 27300 FC MRB S AMM SSI 5316031 1.00 B21521 1.00DETAILED INSPECTION OF INTERNAL STRUCTUREAROUND EMERGENCY EXIT BELOW CABIN FLOOR BETWEENFRAMES 55 AND 58 AND BETWEEN STRINGERS 26 AND 29.PREP.: LINING AND INSULATION REMOVED.531603-0604-2 151 STRUCTURE - FRAMES 55 TO 58 MEC DET I: 22600 FC MRB S AMM SSI 5316031 1.00 B4-1001521 1.00DETAILED INSPECTION OF INTERNAL STRUCTUREAROUND EMERGENCY EXIT BELOW CABIN FLOOR BETWEENFRAMES 55 AND 58 AND BETWEEN STRINGERS 26 AND 29.PREP.: LINING AND INSULATION REMOVED.531603-0604-3 151 STRUCTURE - FRAMES 55 TO 58 MEC DET I: 19200 FC MRB S AMM SSI 5316031 1.00 B4-2001521 1.00 C4DETAILED INSPECTION OF INTERNAL STRUCTUREF4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 43APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531603-0604-3 * * * * * C O N T I N U E * * * * *AROUND EMERGENCY EXIT BELOW CABIN FLOOR BETWEENFRAMES 55 AND 58 AND BETWEEN STRINGERS 26 AND 29.PREP.: LINING AND INSULATION REMOVED531605-0603-1 241 EMERG. EXIT DOOR CUTOUT NDT SDI T: ISB ISB NTM 5330521 0.75 ALL242 53-0204 PART 4,6,71 0.75DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053AREAS BEHIND SCUFF PLATES AT EMERGENCY EXITS CUTOUT. PART 6CNNOTE: SCUFF PLATES TO BE REMOVED. 1991-132-124(B)FAA AD 97-11-03ISB 53-0204ISB 53-0233531605-0604-1 240 STRUCTURE - FRAMES 55 TO 58 MEC DET T: 9 YE CPCP AMM SSI 5316051 6.00 ALL250 I: 5 YE MRB S1 6.00DETAILED INSPECTION OF INTERNAL STRUCTURE MRB REFERENCE:AROUND EMERGENCY EXITS ABOVE CABIN FLOOR UP TOSTRINGER 12 BETWEEN FRAME 55 AND 58. 531605-C604-A531605-C604-BAPPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2 OR G3AFTER INSPECTION.PREP.: LININGS AND FURNISHINGS IN DOOR AREAS ANDINSULATION REMOVED531605-0604-4 241 STRUCTURE AROUND EMERGENCY EXIT MEC DET T: 16000 FC ALI EASA AD1 1.00 B2242 OR 2006-00711 1.00 FROM 0 FC/FHDETAILED INSPECTION OF INTERNAL STRUCTURE AROUND 18000 FH FAA ADTO LOVEMERGENCY EXIT ABOVE CABIN FLOOR BETWEEN FR 55 AND I: 7500 FC 2007-04-11FR 59 AND BETWEEN STR 12 AND STR 26. OR8400 FH ALI REFERENCE:ACCESS: 844 531605-01-1* 0.10531605-0604-5 241 STRUCTURE AROUND EMERGENCY EXIT MEC DET T: 16000 FC ALI EASA AD1 1.00 B4-100242 OR 2006-00711 1.00 FROM 0 FC/FHDETAILED INSPECTION OF INTERNAL STRUCTURE AROUND 21700 FH FAA ADTO LOVEMERGENCY EXIT ABOVE CABIN FLOOR BETWEEN FR 55 AND I: 7500 FC 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 44APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531605-0604-5 * * * * * C O N T I N U E * * * * *FR 59 AND BETWEEN STR 12 AND STR 26. OR ALI REFERENCE:10200 FH 531605-01-2ACCESS: 844* 0.10531605-0604-6 241 STRUCTURE AROUND EMERGENCY EXIT MEC DET T: 16000 FC ALI EASA AD1 1.00 B4-200242 OR 2006-00711 1.00 C4DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND 35300 FH FAA ADF4EMERGENCY EXIT ABOVE CABIN FLOOR BETWEEN FR 55 AND I: 7500 FC 2007-04-11FROM 0 FC/FHFR 59 AND BETWEEN STR 12 AND STR 26. ORTO LOV16500 FH ALI REFERENCE:ACCESS: 844 531605-01-3* 0.10531700-0602-1 251 FRAME 57A AND FRAME 65 MEC GVI T: 20000 FH CN CN1 4.00 PRE 02643252 OR FAA AD 1983-102-053(B) 1 4.00 (53-0132)VISUAL INSPECTION OF STRINGER 5 CONNECTION AT FRAME 20000 FC ISB FAA AD 98-20-3665, LH AND RH, AND REINFORCING CROSS STRAP BETWEEN I: 3000 FH ISB 53-0143STRINGER 15 AND 16 AT FRAME 57A FOR CRACKS.531701-0603-1 154 AFT CARGO DOOR SILL BEAM MEC DET I: 5 YE CPCP AMM SSI 5317011 1.50 ALLMRB SDETAILED INSPECTION OF AFT CARGO COMPARTMENT MRB REFERENCE:DOOR SILL BEAM FROM FRAME 59 TO FRAME 64, INCLUDINGTORSION BOX AND ATTACHMENT AREAS OF FRAMES 60 TO 63 531701-C603-1(7 PLACES) BETWEEN STRINGERS 44 RH AND 46 RHNOTE: 01. DOOR SILL LATCHES AND GUIDES, BALLMATS,ROLLER TRACK AND INSULATION TO BE REMOVED.02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.ACCESS: 812* 0.01531703-0602-1 252 FRAME 59 MEC DET I: 7000 FC MRB S AMM SSI 5317031 0.20 ALLDETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS IN AREA OF FRAME 59 BETWEEN STRINGERS21R AND 22RSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 45APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531703-0604-1 252 FRAME 59 MEC DET I: 27300 FC MRB S AMM SSI 5317031 1.50 B2DETAILED INSPECTION OF FRAME 59 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 21R AND 22R.PREP.: LINING AND INSULATION REMOVED.531703-0604-2 252 FRAME 59 MEC DET I: 22600 FC MRB S AMM SSI 5317031 1.50 B4-100DETAILED INSPECTION OF FRAME 59 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 21R AND 22R.PREP.: LINING AND INSULATION REMOVED.531703-0604-3 252 FRAME 59 MEC DET I: 19200 FC MRB S AMM SSI 5317031 1.50 B4-200C4DETAILED INSPECTION OF FRAME 59 AT ATTACHMENTF4AREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 21R AND 22R.PREP.: LINING AND INSULATION REMOVED.531704-0602-1 154 FRAME 59 MEC DET I: 7000 FC MRB S AMM SSI 5317041 0.20 ALLDETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS IN AREA OF FRAME 59 BETWEEN STRINGERS46R AND 47R531704-0604-1 154 FRAME 59 MEC DET I: 27300 FC MRB S AMM SSI 5317041 0.50 B2DETAILED INSPECTION OF FRAME 59 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 46R AND 47R.PREP.: INSULATION REMOVED.ACCESS: 152FF* 11.43STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 46APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531704-0604-2 154 FRAME 59 MEC DET I: 22600 FC MRB S AMM SSI 5317041 0.50 B4-100DETAILED INSPECTION OF FRAME 59 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 46R AND 47R.PREP.: INSULATION REMOVED.ACCESS: 152FF* 11.43531704-0604-3 154 FRAME 59 MEC DET I: 19200 FC MRB S AMM SSI 5317041 0.50 B4-200C4DETAILED INSPECTION OF FRAME 59 AT ATTACHMENTF4AREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 46R AND 47R.PREP.: INSULATION REMOVED.ACCESS: 152FF* 11.43531705-0602-1 252 FRAME 64 MEC DET I: 7000 FC MRB S AMM SSI 5317051 0.20 ALLDETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS IN AREA OF FRAME 64 BETWEEN STRINGERS21R AND 22R531705-0604-1 252 FRAME 64 MEC DET I: 27300 FC MRB S AMM SSI 5317051 1.00 B2DETAILED INSPECTION OF FRAME 64 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 21R AND 22R.PREP.: LINING AND INSULATION REMOVED.531705-0604-2 252 FRAME 64 MEC DET I: 22600 FC MRB S AMM SSI 5317051 1.00 B4-100DETAILED INSPECTION OF FRAME 64 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 21R AND 22R.PREP.: LINING AND INSULATION REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 47APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531705-0604-3 252 FRAME 64 MEC DET I: 19200 FC MRB S AMM SSI 5317051 1.00 B4-200C4DETAILED INSPECTION OF FRAME 64 AT ATTACHMENTF4AREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 21R AND 22R.PREP.: LINING AND INSULATION REMOVED.531706-0602-1 154 FRAME 64 MEC DET I: 7000 FC MRB S AMM SSI 5317061 0.20 ALLDETAILED INSPECTION OF EXTERNAL SKIN ANDRIVETS IN AREA OF FRAME 64 BETWEEN STRINGERS46R AND 47R531706-0604-1 154 FRAME 64 MEC DET I: 27300 FC MRB S AMM SSI 5317061 0.50 B2DETAILED INSPECTION OF FRAME 64 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 46R AND 47R.PREP.: LINING AND FLOOR PANELS REMOVED.531706-0604-2 154 FRAME 64 MEC DET I: 22600 FC MRB S AMM SSI 5317061 0.50 B4-100DETAILED INSPECTION OF FRAME 64 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 46R AND 47R.PREP.: LINING AND FLOOR PANELS REMOVED.531706-0604-3 154 FRAME 64 MEC DET I: 19200 FC MRB S AMM SSI 5317061 0.50 B4-200C4DETAILED INSPECTION OF FRAME 64 AT ATTACHMENTF4AREA OF MACHINED FRAME TO FORMED FRAME BETWEENSTRINGERS 46R AND 47R.PREP.: LINING AND FLOOR PANELS REMOVED.531711-0602-1 252 FRAMES 60 TO 63 MEC DET I: 3000 FC ALI CN 2006-0071(B) 1 0.20 ALLFAA AD 96-13-11 FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 48APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531711-0602-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF AFT COMPARTMENT DOOR AT ALI REFERENCE: TO LOVATTACHMENT AREA OF FORMED FRAMES 60 TO 63 (4 PLACES) 531711-01-1BETWEEN STRINGERS 21RH AND 22RH.531711-0604-1 252 FRAMES 60 TO 63 MEC DET I: 27300 FC MRB S AMM SSI 5317111 3.00 B2DETAILED INSPECTION OF HINGE FITTINGS OF AFTCARGO COMPARTMENT DOOR AT ATTACHMENT AREAS OF FORMEDFRAMES 60 TO 63 (4 PLACES) TO HINGE FITTINGS BETWEENSTRINGERS 21R AND 22R.PREP.: CABIN LINING AND INSULATION REMOVED.531711-0604-2 252 FRAMES 60 TO 63 MEC DET I: 22600 FC MRB S AMM SSI 5317111 3.00 B4-100DETAILED INSPECTION OF HINGE FITTINGS OF AFTCARGO COMPARTMENT DOOR AT ATTACHMENT AREAS OF FORMEDFRAMES 60 TO 63 (4 PLACES) TO HINGE FITTINGS BETWEENSTRINGERS 21R AND 22R.PREP.: CABIN LINING AND INSULATION REMOVED.531711-0604-3 252 FRAMES 60 TO 63 MEC DET I: 19200 FC MRB S AMM SSI 5317111 3.00 B4-200C4DETAILED INSPECTION OF HINGE FITTINGS OF AFTF4CARGO COMPARTMENT DOOR AT ATTACHMENT AREAS OF FORMEDFRAMES 60 TO 63 (4 PLACES) TO HINGE FITTINGS BETWEENSTRINGERS 21R AND 22R.PREP.: CABIN LINING AND INSULATION REMOVED.531715-0603-1 162 FRAME 67 MEC DET I: 27300 FC MRB S AMM SSI 5317151 0.50 B21641 0.50DETAILED INSPECTION OF FRAME 67 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME AND MACHINEDFRAME BETWEEN STRINGERS 32RH AND 47RH.PREP.: LINING AND INSULATION REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 49APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531715-0603-2 162 FRAME 67 MEC DET I: 22600 FC MRB S AMM SSI 5317151 0.50 B4-1001641 0.50DETAILED INSPECTION OF FRAME 67 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME AND MACHINEDFRAME BETWEEN STRINGERS 32RH AND 47RH.PREP.: LINING AND INSULATION REMOVED.531715-0603-3 162 FRAME 67 MEC DET I: 19200 FC MRB S AMM SSI 5317151 0.50 B4-2001641 0.50 C4DETAILED INSPECTION OF FRAME 67 AT ATTACHMENTF4AREA OF MACHINED FRAME TO FORMED FRAME AND MACHINEDFRAME BETWEEN STRINGERS 32RH AND 47RH.PREP.: LINING AND INSULATION REMOVED.531716-0602-1 162 REAR CARGO COMPT.DOOR FRAME NDT SDI T: 10000 FH ISB ISB 53-01871 2.00 PRE 02380I: 2000 FH(53-0119)SPECIAL DETAILED INSPECTION ON THE EXTERNAL FLANGESOF REAR CARGO COMPARTMENT DOOR FRAME UPPER AND LOWERBEAMS FOR CRACKS531717-0603-1 162 FRAME 69 MEC DET I: 11200 FC MRB S AMM SSI 5317171 0.50 ALL1641 0.50DETAILED INSPECTION OF FRAME 69 AT ATTACHMENTAREA OF MACHINED FRAME TO FORMED FRAME AND MACHINEDFRAME BETWEEN STRINGERS 32RH AND 47RH.PREP.: LINING AND INSULATION REMOVED.531719-0603-2 162 BULK CARGO DOOR CUTOUT MEC SDI T: ISB ISB NTM 5330521 1.00 ALL53-0204 PART 4,6,7DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053AREAS BEHIND SCUFF PLATES AT BULK CARGO DOOR CUTOUT. PART 6CNNOTE: SCUFF PLATES TO BE REMOVED 1991-132-124(B)FAA AD 97-11-03ISB 53-0204ISB 53-0233STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 50APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531720-0603-1 172 STRUCTURE AROUND WASTE WATER CONNECTION MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 1.00 ALLBOX I: 30 MO 531720-C603-1GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE AROUND WASTE WATER CONNECTION BOXBETWEEN FRAME 78 AND FRAME 79 FROM STRINGER 45 LHTO STRINGER 51 LH.NOTE: APPLY TEMPORARY PROTECTION SYSTEM TYPE 1 ANDTYPE 2 AFTER INSPECTION.ACCESS : INSULATION REMOVEDACCESS: 162AZ 813* 0.02531813-0603-1 171 REAR PRESSURE BULKHEAD MEC DET I: 7000 FC MRB S AMM SSI 5318131 1.25 ALL1721 1.25DETAILED INSPECTION OF INTERNAL REAR PRESSUREBULKHEAD FORWARD FACE LOWER PORTION BELOW CABIN FLOORLINE.PREP.: INSULATION TO BE REMOVED.ACCESS: 162AZ* 0.01531814-0604-1 261 TORSION BOX FRAMES 72 TO 73 MEC DET I: 27300 FC MRB S AMM SSI 5318141 1.00 B22621 1.00DETAILED INSPECTION OF INTERNAL TORSION BOXRUN-OUT BETWEEN FRAMES 72 AND 73 STRINGERS 9 AND 11.PREP.: LINING AND INSULATION REMOVED.531814-0604-2 261 TORSION BOX FRAMES 72 TO 73 MEC DET I: 22600 FC MRB S AMM SSI 5318141 1.00 B4-1002621 1.00DETAILED INSPECTION OF INTERNAL TORSION BOXRUN-OUT BETWEEN FRAMES 72 AND 73 STRINGERS 9 AND 11.PREP.: LINING AND INSULATION REMOVED.531814-0604-3 261 TORSION BOX FRAMES 72 TO 73 MEC DET I: 19200 FC MRB S AMM SSI 5318141 1.00 B4-2002621 1.00 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 51APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531814-0604-3 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF INTERNAL TORSION BOXF4RUN-OUT BETWEEN FRAMES 72 AND 73 STRINGERS 9 AND 11.PREP.: LINING AND INSULATION REMOVED.531815-0602-2 250 SKIN AROUND AFT PAX DOOR MEC DET T: 5 YE CPCP MRB REFERENCE: 1 0.25 ALL260 I: 30 MO MRB S1 0.25DETAILED INSPECTION OF EXTERNAL SKIN 531815-C602-2AND RIVETS AROUND AFT PASSENGER/CREW DOOR ABOVE CABINFLOOR BETWEEN FRAMES 72 AND 76 AND STRINGERS 9 AND 26AND SURROUNDING OF DOOR CUT OUTS (25 CM/10 INCHES)AROUND DOOR CUT-OUT EDGES), INCLUDING FAIL SAFE RING,AND CUT OUT EDGES.NOTE: WHERE AREAS ARE COVERED BY SB 53-0204 AND SB53-0233, CPCP TASK IS NOT TO BE APPLIED.PREPARATION: PAX DOORS OPENED531815-0603-1 250 STRUCTURE AROUND AFT PAX DOOR MEC DET T: 9 YE CPCP AMM SSI 5318151 6.00 ALL260 I: 5 YE MRB S1 6.00DETAILED INSPECTION OF INTERNAL STRUCTURE MRB REFERENCE:AROUND AFT PASSENGER/CREW DOORS ABOVE CABIN FLOORBETWEEN FRAMES 72 AND 76 BETWEEN STRINGER 9 531815-C603-AAND STRINGER 26 LH/RH. 531815-C603-BNOTE: 01. LININGS AND FURNISHINGS IN DOOR AREAS ANDINSULATION IN FLOOR AREA REMOVED.02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.531815-0604-4 251 INTERNAL STRUCTURE AROUND AFT PAX/CREW MEC DET T: 20000 FC ALI EASA AD1 2.00 ALL252 DOOR I: 10000 FC 2006-00711 2.00 FROM 0 FC/FHFAA ADTO LOVDETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT 2007-04-11PASSENGER/CREW DOORS ABOVE CABIN FLOOR BETWEEN FR 72AND FR 76 BETWEEN STR 9 AND STR 26, TORSION BOX RUN- ALI REFERENCE:OUT BETWEEN FR 72/73 AND 76/77, STR 9 AND 11. 531815-01-1PREP : LINING AND INSULATION TO BE REMOVED* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 52APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531815-0604-4 * * * * * C O N T I N U E * * * * *ACCESS: 843* 0.10531816-0603-1 261 FRAME 73A MEC DET T: 20000 FC ALI EASA AD1 0.50 ALL262 I: 9000 FC 2006-00711 0.50 FROM 0 FC/FHDETAILED INSPECTION OF INTERNAL FRAME 73A FAA ADTO LOVBETWEEN STRINGER 11 AND 13 IN THE RADII BETWEEN FRAME 2007-04-11OUTER STRAP AND WEB.ALI REFERENCE:PREP.: PANELS AND INSULATION TO BE REMOVED. 531816-01-1531817-0604-1 171 FRAME 73 TO 76 NDT SDI I: 17700 FC MRB S AMM SSI 5318171 2.00 B2172 NTM 5318001 2.00 B4-100DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 6 AND 7STRUCTURE BELOW CABIN FLOOR AT AFT PASSENGER/CREWDOORS BETWEEN FRAME NO.73 AND 76 AND BETWEENSTRINGERS 24 AND 28.PREP.: INSULATION REMOVED.ACCESS: 162AZ* 0.01531817-0604-3 171 FRAME 73 TO 76 NDT SDI I: 15100 FC MRB S AMM SSI 5318171 2.00 B4-200172 NTM 5318001 2.00 C4DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 6 AND 7F4STRUCTURE BELOW CABIN FLOOR AT AFT PASSENGER/CREWDOORS BETWEEN FRAME NO.73 AND 76 AND BETWEENSTRINGERS 24 AND 28.PREP.: INSULATION REMOVED.531818-0604-1 261 TORSION BOX, FRAME 76 TO 77 MEC DET I: 27300 FC MRB S AMM SSI 5318181 1.00 B22621 1.00DETAILED INSPECTION OF INTERNAL TORSION BOXRUN OUT BETWEEN FRAMES 76 AND 77 STRINGERS 9 AND 11.PREP.: LINING AND INSULATION REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 53APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531818-0604-2 261 TORSION BOX, FRAME 76 TO 77 MEC DET I: 22600 FC MRB S AMM SSI 5318181 1.00 B4-1002621 1.00DETAILED INSPECTION OF INTERNAL TORSION BOXRUN OUT BETWEEN FRAMES 76 AND 77 STRINGERS 9 AND 11PREP.: LINING AND INSULATION REMOVED.531818-0604-3 261 TORSION BOX, FRAME 76 TO 77 MEC DET I: 19200 FC MRB S AMM SSI 5318181 1.00 B4-2002621 1.00 C4DETAILED INSPECTION OF INTERNAL TORSION BOXF4RUN OUT BETWEEN FRAMES 76 AND 77 STRINGERS 9 AND 11.PREP.: LINING AND INSULATION REMOVED.531819-0604-1 260 REAR PRESSURE BULKHEAD MEC DET I: 27300 FC MRB S AMM SSI 5318191 40.00 B2DETAILED INSPECTION OF REAR PRESSURE BULKHEADFORWARD FACE ABOVE CABIN FLOOR.PREP.: TOILETS, LINING AND INSULATION REMOVED.531819-0604-2 260 REAR PRESSURE BULKHEAD MEC DET I: 22600 FC MRB S AMM SSI 5318191 40.00 B4-100DETAILED INSPECTION OF REAR PRESSURE BULKHEADFORWARD FACE ABOVE CABIN FLOOR.PREP.: TOILETS, LINING AND INSULATION REMOVED.531819-0604-3 260 REAR PRESSURE BULKHEAD MEC DET I: 19200 FC MRB S AMM SSI 5318191 40.00 B4-200C4DETAILED INSPECTION OF REAR PRESSURE BULKHEADF4FORWARD FACE ABOVE CABIN FLOOR.PREP.: TOILETS, LINING AND INSULATION REMOVED.531820-0603-1 261 FUSELAGE-AFT PAX/CREW DOOR NDT SDI T: 8000 FC CN NTM 5318001 2.00 PRE 06925262 I: 4000 FC FAA AD PART 61 2.00 (53-0221)SPECIAL DETAILED INSPECTION OF THE INNER FLANGE OF ISB CNFRAME 73A RH AND LH BETWEEN BEAMS 5 AND 7 1988-061-083(B)FAA AD 89-03-09* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 54APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531820-0603-1 * * * * * C O N T I N U E * * * * *PREP.: OPEN AFT PASSENGER/CREW DOORS. REMOVE DOOR ISB 53-0220FRAME LININGS AND INSULATION531820-0603-2 171 FUSELAGE NDT SDI T: 24100 FC CN NTM 5318021 5.00 MSN 003-156172 I: 3400 FC FAA AD PART 41 5.00 PRE 06653SPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW ISB CN F-2002-639(53-0209)STRINGER 28 BETWEEN FRAME 72 AND FRAME 76 LH AND RH. FAA AD2004-08-05ISB 53-0357531820-0603-3 171 FUSELAGE NDT SDI T: 29500 FC CN NTM 5318021 5.00 MSN 157-305172 I: 5400 FC FAA AD PART 41 5.00 ORSPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW ISB CN F-2002-639MSN 003-156STRINGER 28 BETWEEN FRAME 72 AND FRAME 76 LH AND RH. FAA ADPOST 066532004-08-05(53-0209)ISB 53-0357531912-0603-1 310 PRESSURE BULKHEAD NDT SDI T: 12000 FC CN NTM 5319111 14.00 PRE 02476I: 6000 FC FAA AD PART 2, 4 AND6 (53-0121)SPECIAL DETAILED INSPECTION OF REAR PRESSURE BULKHEAD ISB CNAT INNER RIVET ROW OF CIRCUMFERENTIAL SPLICE IN AREAS 1980-218-028(B)1 AND 2 FAA AD 94-09-15ISB 53-0152ACCESS: 312AR* 0.01531912-0603-2 310 PRESSURE BULKHEAD NDT SDI T: 32000 FC CN NTM 5319111 7.00 PRE 02476I: 9000 FC FAA AD PART 2, 4 AND6 (53-0121)SPECIAL DETAILED INSPECTION OF PRESSURE BULKHEAD AT ISB CNINNER RIVET ROW OF RADIAL STIFFENER ATTACHMENT 1980-218-028(B)FITTINGS IN AREAS 3 AND 4. FAA AD 94-09-15ISB 53-0152ACCESS: 312AR* 0.01531921-0603-1 311 PRESSURE BULKHEAD NDT SDI T: 20000 FC ALI NTM 5319111 4.70 POST 02476I: 7200 FC PART 4 AND 6(53-0121)SPECIAL DETAILED INSPECTION OF PRESSURE BULKHEAD AT CN 2006-0071(B) FROM 0 FC/FHINNER RIVET ROW OF CIRCUMFERENTIAL SPLICE IN AREAS 1 FAA AD 96-13-11 TO LOVAND 2.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 55APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531921-0603-1 * * * * * C O N T I N U E * * * * *ACCESS: 312AR ALI REFERENCE: * 0.01531921-01-1531921-0603-2 311 PRESSURE BULKHEAD NDT SDI T: 32000 FC ALI NTM 5319111 2.40 POST 02476I: 7200 FC PART 4 AND 6(53-0121)SPECIAL DETAILED INSPECTION OF PRESSURE BULKHEAD AT CN 2006-0071(B) FROM 0 FC/FHINNER RIVET ROW OF RADIAL STIFFENER ATTACHMENT FAA AD 96-13-11 TO LOVFITTINGS 1, 5LH, 5RH, 9RH, 9LH AND 13 (AREAS 3 AND 4AS DEFINED BY NTM 531911) ALI REFERENCE:531921-02-1ACCESS: 312AR* 0.01531925-0603-1 313 FRAME NO. 91 COMPLETE MEC DET T: 11200 FC ALI CN 2006-0071(B) 1 0.50 B2314 OR CN FAA AD 96-13-11 1 0.50 FROM 0 FC/FHDETAILED INSPECTION OF FRAME NO.91 COMPLETE, 12800 FH FAA ADTO LOVINCLUDING CENTER FITTINGS DIAGONAL SUPPORTS, HINGE I: 8400 FC ALI REFERENCE:SUPPORT MEMBERS AND LUGS OF HINGE SUPPORT MEMBERS AND OR 531925-01-1FRAME. 9600 FHACCESS: 313AL* 0.14531925-0603-2 313 FRAME NO. 91 COMPLETE MEC DET T: 11000 FC ALI CN 2006-0071(B) 1 0.40 B4-100314 OR CN FAA AD 96-13-11 1 0.40 FROM 0 FC/FHDETAILED INSPECTION OF FRAME NO.91 COMPLETE, 15300 FH FAA ADTO LOVINCLUDING CENTER FITTINGS DIAGONAL SUPPORTS, HINGE I: 8300 FC ALI REFERENCE:SUPPORT MEMBERS AND LUGS OF HINGE SUPPORT MEMBERS AND OR 531925-01-2FRAME. 11500 FHACCESS: 313AL* 0.14531925-0603-3 313 FRAME NO.91 COMPLETE MEC DET T: 10000 FC ALI CN 2006-0071(B) 1 0.40 B4-200314 OR CN FAA AD 96-13-11 1 0.40 C4DETAILED INSPECTION OF FRAME NO.91 COMPLETE, 23000 FH FAA ADF4INCLUDING CENTER FITTINGS DIAGONAL SUPPORTS, HINGE I: 7500 FC ALI REFERENCE: FROM 0 FC/FHSUPPORT MEMBERS AND LUGS OF HINGE SUPPORT MEMBERS AND OR 531925-01-3TO LOVFRAME. 17000 FHACCESS: 313AL* 0.14STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 56APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531926-0603-1 313 FRAME 91 NDT SDI T: 24000 FC ISB AMM SSI 5319261 20.00 ALL314 I: 12000 FC MRB S NTM 5319001 20.00SPECIAL DETAILED INSPECTION OF FRAME 91, UPPER AND PART 4LOWER LUGS AND HINGE SUPPORT MEMBERS. ISB 53-258PREP: REMOVE HORIZONTAL STABILIZER ATTACH.FITTINGS531929-0603-1 311 REAR PRESSURE BULKHEAD MEC DET I: 8400 FC MRB S AMM SSI 5319291 0.25 ALL3121 0.25DETAILED INSPECTION OF REAR PRESSURE BULKHEADAFT FACE RIVETING OF ALL JOINTS.ACCESS: 312AR* 0.01531931-0603-1 311 REAR PRESSURE BULKHEAD MEC DET I: 30 MO CPCP AMM SSI 5319311 0.60 ALL312 MRB S1 0.60DETAILED INSPECTION OF REAR PRESSURE BULKHEAD MRB REFERENCE:LOWER AREA (BELOW STRINGER 26 LEVEL) AND STRUCTUREAROUND DRAINAGE HOLE BETWEEN FRAME 80 AND FRAME 81. 531931-C603-1NOTE:01.APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.NOTE:02.ENSURE DRAIN HOLES FREE OF ANY OBSTRUCTIONS.ACCESS: 312AR* 0.01R 531933-0603-1 170 REAR PRESSURE BULKHEAD NDT SDI T: 90 MO AD NTM 5130101 6.00 PRE 06788310 I: 8000 FC ISB PART 11 6.00 (53-0226)SPECIAL DETAILED INSPECTION OF LOWER ATTACHMENT NTM 531911ANGLES OF REAR PRESSURE BULKHEAD, FWD AND REAR FACES, CONFIG-1BELOW STRINGER 27 LEVEL. PART 2, 6AD F-2004-193NOTE: INSULATION TO BE REMOVED ISB 53-0363ACCESS: 162AZ 312AR* 0.01R 531933-0603-2 170 REAR PRESSURE BULKHEAD MEC DET T: 90 MO AD AD F-2004-1931 3.00 PRE 06788310 I: 3 YE ISB ISB 53-03631 3.00 (53-0226)DETAILED INSPECTION OF LOWER ATTACHMENT ANGLESOF REAR PRESSURE BULKHEAD, FWD AND REAR FACES, BELOW* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 57APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)531933-0603-2 * * * * * C O N T I N U E * * * * *STRINGER 27 LEVEL.NOTE: INSULATION TO BE REMOVEDACCESS: 162AZ 312AR* 0.01531933-0603-3 170 REAR PRESSURE BULKHEAD NDT SDI T: 90 MO AD NTM 5130101 6.00 POST 06788310 I: 8000 FC EUAD PART 11 6.00 (53-0226)SPECIAL DETAILED INSPECTION OF LOWER ATTACHMENT ISB NTM 531911ANGLES OF REAR PRESSURE BULKHEAD, FWD AND REAR FACES, CONFIG-1BELOW STRINGER 27 LEVEL. PART 2, 6AD 2005-26-16NOTE: INSULATION TO BE REMOVED CNF-1989-068-093ACCESS: 162AZ 312AR EUAD F-2004-193 * 0.01FAA AD 90-03-08ISB 53-0363531933-0603-4 170 REAR PRESSURE BULKHEAD MEC DET T: 90 MO AD AD 2005-26-161 3.00 POST 06788310 I: 5 YE EUAD CN1 3.00 (53-0226)DETAILED INSPECTION OF LOWER ATTACHMENT ANGLES ISB F-1989-068-093OF REAR PRESSURE BULKHEAD, FWD AND REAR FACES, BELOW EUAD F-2004-193STRINGER 27 LEVEL. FAA AD 90-03-08ISB 53-0363NOTE: INSULATION TO BE REMOVEDACCESS: 162AZ 312AR* 0.01532100-0603-1 130 SEAT TRACKS MEC DET I: 1500 FH ISB CN1 12.00 PRE 02109240 1990-222-116(B) 4 24.00DETAILED INSPECTION OF ALL DUMMY FAA ADSWIVELLING SEAT TRACKS BETWEEN FR. 38.2 AND FR. 40 2000-10-01AND BETWEEN FR. 54 AND FR. 54.2 FOR CRACKS, RUPTURE ISB 53-0103AND DISTORTION.ACCESS: 131BZ* 0.13532100-0603-3 130 SEAT TRACKS MEC DET I: 3000 FH ISB ISB 53-01794 20.00 POST 021092401 9.50 (53-0107)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 58APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)532100-0603-3 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF ALL DUMMY SWIVELLINGPRE 03135SEAT TRACKS BETWEEN FR.38.2 AND FR.40 AND BETWEEN(53-0188)FR.54 AND FR.54.2 FOR WEAR IN SIDE FITTINGSRECTANGULAR HOLES.ACCESS: 131BZ 131CZ 132EZ* 0.39533101-0602-1 211 UPPER SKIN PANEL, FRAME 10 MEC DET I: 8500 FC MRB S AMM SSI 5331011 0.10 ALL2121 0.10DETAILED INSPECTION OF EXTERNAL UPPER SKINSPLICE AT FRAME 10.533103-0602-1 211 SKIN PANEL SPLICES MEC DET I: 8500 FC MRB S AMM SSI 5331031 0.15 ALL2121 0.15DETAILED INSPECTION OF EXTERNAL SKINSPLICES AT WINDSHIELD LOWER SECTION BETWEEN FRAMES 0AND 10.533105-0602-1 211 SKIN PANEL AT FRAME 7 MEC DET I: 8500 FC MRB S AMM SSI 5331051 0.10 ALL2121 0.10DETAILED INSPECTION OF EXTERNAL UPPER SIDESKIN PANEL AT ATTACHMENT TO FRAME NO.7 BETWEEN WIND-SHIELD AND LONGITUDINAL SKIN SPLICE.533106-0602-1 121 UPPER SIDE SKIN PANEL MEC DET I: 11400 FC MRB S AMM SSI 5331061 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL UPPER SIDESKIN PANEL AT LOWER LONGITUDINAL SKIN SPLICE BETWEENFRAMES 0 AND 10.533107-0602-1 121 SIDE SKIN PANEL MEC DET I: 11400 FC MRB S AMM SSI 5331071 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL SIDE SKIN PANELATTACHMENT TO LOWER SKIN PANEL BETWEEN FRAMES 0 AND10.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 59APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533109-0602-1 121 LOWER SKIN PANEL MEC DET I: 11400 FC MRB S AMM SSI 5331091 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL LOWER SKINPANEL AT TRANSVERSE SPLICE TO ACCESS DOOR SURROUNDPANEL.533201-0602-1 210 SKIN PANEL, FRAMES 10 TO 18 MEC DET I: 8500 FC MRB S AMM SSI 5332011 0.20 ALL2201 0.20DETAILED INSPECTION OF EXTERNAL SKIN PANELSPLICES AT STRINGERS 9 L/H AND 9 R/H BETWEEN FRAMES10 AND 18.533209-0602-1 121 SKIN PANEL, FRAME 12 TO FRAME 13 MEC DET T: 19000 FC ALI EASA AD1 0.20 ALL122 I: 11400 FC 2006-00711 0.20 FROM 0 FC/FHDETAILED INSPECTION OF EXTERNAL SKIN FAA ADTO LOVPANELS BETWEEN FRAMES 12 AND 13 AND BETWEEN 2007-04-11STRINGERS 30 AND 40.ALI REFERENCE:533209-01-1533211-0602-1 121 SKIN PANEL SPLICES MEC DET I: 8500 FC MRB S AMM SSI 5332111 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL SKIN PANELSPLICES BETWEEN FRAMES 16A AND 18 AND STRINGERS 29 TO45 L/H AND R/H SIDES.533214-0602-1 121 NLG BAY SURROUND PANEL MEC DET I: 5700 FC MRB S AMM SSI 5332141 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL NOSE LANDINGGEAR BAY SURROUND PANEL AND DOUBLER AT REAR LH AND RHCORNER.ACCESS: 713* 0.06714* 0.06533214-0604-1 123 NLG BAY SURROUND PANEL NDT SDI I: 27300 FC MRB S AMM SSI 5332141 1.00 ALL124 NTM 5332001 1.00SPECIAL DETAILED INSPECTION OF NOSE GEAR SURROUND PART 2PANEL AND DOUBLER AT REAR LH AND RH CORNERS.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 60APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533214-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 713* 0.06714* 0.06533215-0602-1 121 NOSE GEAR BAY FRONT SECTION MEC DET I: 11400 FC MRB S AMM SSI 5332151 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL NOSEGEAR BAY FRONT SECTION SURROUND PANEL DIAGONAL SPLI-CING.533216-0602-1 121 NOSE GEAR BAY REAR SECTION MEC DET I: 11400 FC MRB S AMM SSI 5332161 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL NOSEGEAR BAY REAR SECTION SURROUND PANEL DIAGONAL SPLI-CING.533217-0602-1 121 NLG BAY, SURROUND PANEL MEC DET I: 7000 FC MRB S AMM SSI 5332171 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL NOSE LANDINGGEAR BAY SURROUND PANEL LONGITUDINAL SPLICING ATSTRINGER 43 BETWEEN FRAMES 17 AND 19.533218-0602-1 221 SKIN AROUND FWD PAX DOOR MEC DET I: 30 MO CPCP MRB REFERENCE: 1 0.10 ALL222 OR MRB S1 0.10DETAILED INSPECTION OF EXTERNAL SKIN 2800 FC 533218-C602-1AROUND FORWARD PASSENGER/CREW DOOR CUT-OUTS (25 CM/10 INCHES AROUND CUT-OUT EDGES), INCLUDING FAIL SAFERING, AND CUT-OUT EDGES BETWEEN FRAMES 13A AND 17 ANDFROM STRINGER 9 DOWN TO FLOOR.NOTE: 01. PAX DOORS TO BE OPENED02. WHERE AREAS ARE COVERED BY SB 53-0204 ANDSB 53-0233 CPCP TASK IS NOT TO BE APPLIED.533218-0602-2 221 SKIN AROUND FWD PAX DOOR MEC DET I: 3000 FH ISB ISB 53-00751 1.00 PRE 010552221 1.00DETAILED INSPECTION OF EXTERNAL DOUBLERSAROUND FWD PASS/CREW DOOR CUT-OUT BETWEEN FR.14 AND16A AND STRG.9 TO 28 FOR CRACKSSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 61APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533219-0602-1 121 NLG BAY, SURROUND PANEL MEC DET I: 11400 FC MRB S AMM SSI 5332191 0.10 ALL1221 0.10DETAILED INSPECTION OF EXTERNAL FUSELAGE SKINPANEL BETWEEN FRAMES 17 AND 19 AND STRINGER 43 L/HAND 43 R/H.533220-0603-1 220 FWD PAX/CREW DOOR CUTOUT MEC DET I: 6000 FH ISB ISB 53-00761 18.00 PRE 01115DETAILED INSPECTION OF FWD. PAX/CREW DOORCUT-OUT AT FR. 14 AND 16A FOR CRACKSPREP: REMOVE LINING AND INSULATION533220-0603-2 121 FWD PAX/CREW DOOR CUTOUT NDT SDI T: ISB ISB NTM 5330521 0.75 ALL122 53-0204 PART 4, 6, 71 0.75DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053AREAS BEHIND SCUFF PLATES AT FORWARD PASSENGER/CREW PART 6DOOR CUTOUT. CN1991-132-124(B)PREP.: SCUFF PLATES TO BE REMOVED FAA AD 97-11-03ISB 53-0204ISB 53-0233533220-0603-3 121 FWD PAX/CREW DOOR CUTOUT NDT SDI T: 20000 FC ISB NTM 5330531 1.25 PRE122 I: ISB PART 61 1.25 (53-0192)DETAILED AND SPECIAL DETAILED INSPECTION OF FWD 53-0227 CNPAX/CREW DOOR CUTOUT AT HOLES OF CORNER DOUBLERS, 1991-132-124(B)FAIL SAFE RING AND DOOR FRAMES. FAA AD 97-11-03ISB 53-0227533302-0602-1 121 FUS.SKIN, FRAMES 18 TO 19 MEC DET I: 7000 FC MRB S AMM SSI 5333021 0.20 ALLDETAILED INSPECTION OF EXTERNAL FUSELAGE SKINAROUND CUT-OUTS BETWEEN FRAMES 18 AND 19 AND BETWEENSTRINGERS 28L AND 34L.533304-0602-1 122 FUS.SKIN, FRAMES 18 TO 19 MEC DET I: 7000 FC MRB S AMM SSI 5333041 0.20 ALLDETAILED INSPECTION OF EXTERNAL FUSELAGE SKINAROUND CUT-OUTS BETWEEN FRAMES 18 AND 19 AND BETWEEN* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 62APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533304-0602-1 * * * * * C O N T I N U E * * * * *STRINGERS 28R AND 38R.533311-0602-1 230 FUS.SKIN, FRAMES 18 TO 40 MEC DET I: 7200 FC MRB S AMM SSI 5333111 0.20 B22401 0.20DETAILED INSPECTION OF EXTERNAL FUSELAGE SKINAND VISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAMES18 AND 40 AND BETWEEN STRINGERS 18 AND 22.533311-0602-2 230 FUS.SKIN, FRAMES 18 TO 40 MEC DET I: 6500 FC MRB S AMM SSI 5333111 0.20 B4-1002401 0.20DETAILED INSPECTION OF EXTERNAL FUSELAGE SKINAND VISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAMES18 AND 40 AND BETWEEN STRINGERS 18 AND 22.533311-0602-3 230 FUS.SKIN, FRAMES 18 TO 40 MEC DET I: 6400 FC MRB S AMM SSI 5333111 0.20 B4-2002401 0.20 C4DETAILED INSPECTION OF EXTERNAL FUSELAGE SKINF4AND VISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAMES18 AND 40 AND BETWEEN STRINGERS 18 AND 22.533313-0602-1 233 FUS.SKIN AROUND ANTENNA MEC DET I: 7000 FC MRB S AMM SSI 5333131 0.10 ALL2341 0.10DETAILED INSPECTION OF EXTERNAL FUSELAGE SKINAROUND ANTENNA CUT-OUT BETWEEN FRAMES 19 AND 21 FROMSTRINGER 1 TO CROWN CENTERLINE.533315-0602-1 133 FUS.SKIN, FRAMES 25 TO 26 MEC DET I: 9000 FC MRB S AMM SSI 5333151 0.10 ALL1341 0.10DETAILED INSPECTION OF EXTERNAL FUSELAGE SKINAROUND CUT-OUTS BETWEEN FRAMES 25 AND 26 FROM STRIN-GER 54 TO BOTTOM CENTERLINE.533329-0602-1 231 FUSELAGE BUTT JOINT MEC DET I: 3000 FC MRB S AMM SSI 5333291 0.20 C4F4DETAILED INSPECTION OF EXTERNAL FUSELAGE BUTTORJOINT BETWEEN UDC-DOOR AND MID PASSENGER/CREW DOOR,POST 06208BETWEEN FRAMES 27 AND 28 AT STRINGER 25L, EXTERNALMSN 256* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 63APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533329-0602-1 * * * * * C O N T I N U E * * * * *SURFACE.533331-0602-1 131 SKIN, UDC-DOOR CUT-OUT MEC DET T: 31600 FC ALI CN 2006-0071(B) 1 0.10 C4231 I: 7900 FC FAA AD 96-13-11 1 0.10 F4233 DETAILED INSPECTION OF (EXTERNAL) SKIN IN1 0.10 POST 06208CORNERS OF UDC-DOOR CUT-OUT. ALI REFERENCE: B4-2C533331-01-1FROM 0 FC/FHACCESS: 835* 0.05 TO LOV533331-0603-1 131 SKIN, UDC-DOOR CUT-OUT MEC DET T: 31600 FC ALI CN 2006-0071(B) 1 1.00 POST 06208231 I: 7900 FC FAA AD 96-13-11 1 1.00 MSN 256233 DETAILED INSPECTION OF FUSELAGE SKIN IN1 1.00 FROM 0 FC/FHCORNERS OF UPPER (MAIN) DECK CARGO DOOR CUT-OUT. ALI REFERENCE: TO LOV533331-01-1ACCESS: 835* 0.05533335-0603-1 233 STRUCTURE, FRAMES 20 TO 27 MEC DET I: 6000 FC MRB S AMM SSI 5333351 5.00 C4F4DETAILED INSPECTION OF INTERNAL SUPPORTSTRUCTURE OF HINGE FITTINGS OF UDC DOOR INCLUDINGLONGERON BETWEEN FRAMES 20 AND 27 AND BETWEENSTRINGERS 4 AND 5 PLUS DOOR ACTUATOR ATTACH FITTINGS.PREP.: LINING AND INSULATION REMOVED.533335-0603-2 233 STRUCTURE, FRAMES 20 TO 27 MEC DET I: 6000 FC MRB S AMM SSI 5333351 5.00 POST 06208MSN 256DETAILED INSPECTION OF INTERNAL SUPPORTSTRUCTURE OF HINGE FITTINGS OF UDC-DOOR INCLUDINGLONGERON BETWEEN FRAMES 20 AND 27 AND BETWEENSTRINGER 4 AND 5.PREP: HATRACKS, FUSELAGE LINING AND INSULATIONREMOVED.ACCESS: 835* 0.05STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 64APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533339-0603-1 131 UDC-DOOR LONGERON MEC DET T: 8400 FC ALI CN 2006-0071(B) 1 3.00 C4I: 4200 FC FAA AD 96-13-11 F4DETAILED INSPECTION OF (INTERNAL) ATTACHMENTPOST 06208AREAS OF LOCK FITTING AND LOWER UDC-DOOR LONGERON ALI REFERENCE: MSN 256BETWEEN FRAMES 20 AND 27 AND BETWEEN STRINGER 26 AND 533339-01-1B4-2C34.FROM 0 FC/FTO LOVPREP.: LINING AND INSULATION TO BE REMOVED.ACCESS: 811* 0.15533341-0603-1 130 FUSELAGE, FRAMES 20 AND 27 MEC DET I: 6000 FC MRB S AMM SSI 5333411 1.50 C42301 1.50 F4DETAILED INSPECTION OF INTERNAL FUSELAGEMSN 256FRAMES 20 AND 27 BETWEEN CROWN AND BOTTOM CENTER LINELH AND RH.PREP.: LINING AND INSULATION TO BE REMOVEDACCESS: 132BF 132CF 811* 0.43533343-0603-1 232 FUSELAGE, FRAMES 21 TO 26 MEC DET T: 8400 FC ALI CN 2006-0071(B) 1 1.00 C4234 I: 4200 FC FAA AD 96-13-11 1 1.00 F4DETAILED INSPECTION OF (INTERNAL) ATTACHMENTPOST 06208AREA OF TRUSS FRAMES WITH NORMAL FRAMES FROM FRAMES ALI REFERENCE: MSN 25621 TO 26 BETWEEN STRINGERS 5 AND 10 (6 PLACES). 533343-01-1B4-2CFROM 0 FC/FPREP.: LINING AND INSULATION TO BE REMOVED.TO LOV533345-0602-1 231 SKIN IN CUT-OUT CORNERS MEC DET T: 12000 FC MRB S AMM SSI 5333451 0.12 C4241 I: 3000 FC1 0.12 F4DETAILED INSPECTION OF EXTERNAL SKIN IN CUT-OROUT CORNERS OF MID PASSENGER/CREW DOOR, L/H.POST 06208MSN 256533401-0602-1 131 FUS.SKIN AROUND SPOTLIGHT MEC DET I: 7000 FC MRB S AMM SSI 5334011 0.10 ALL1321 0.10DETAILED INSPECTION OF EXTERNAL SKIN AROUNDSPOTLIGHT CUT-OUTS BETWEEN FRAMES 26 AND 27 ANDBETWEEN STRINGER 32 AND 34.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 65APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533403-0602-1 131 FUS. SKIN, FRAMES 27 TO 29 MEC DET I: 7000 FC MRB S AMM SSI 5334031 0.10 ALL1321 0.10DETAILED INSPECTION OF EXTERNAL SKIN AROUNDSTATIC PRESSURE PORT CUT-OUTS BETWEEN FRAMES 27 AND29 AND BETWEEN STRINGERS 40 TO 42.533407-0602-1 133 FUS. SKIN, FRAMES 36 TO 38 MEC DET T: 20000 FC ALI CN 2006-0071(B) 1 0.20 ALLI: 9000 FC FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE (EXTERNAL)TO LOVSKIN AROUND AIR CONDITIONING GROUND CONNECTION ALI REFERENCE:PANEL CUT-OUT BETWEEN FRAMES 36 AND 38 AND BETWEEN 533407-01-1STRINGERS 47LH AND 50LH533409-0604-1 130 FUS. SKIN, SLOT FLAP CUT-OUT NDT SDI I: 17700 FC MRB S AMM SSI 5334091 4.00 B2NTM 533400WITH SLOTSPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AROUND PART 6CUT-OUTSLOT FLAP CUT-OUT, BETWEEN FRAMES 37 AND 38.1B4-100STRINGERS 28 TO 34, ESPECIALLY IN CUT-OUT CORNERS INZONES 137/138.PREP.: FORWARD WING ROOT AND SLOT FAIRING OR BLANKINGPANEL REMOVED.533409-0604-2 130 FUS. SKIN, SLOT FLAP CUT-OUT NDT SDI I: 15100 FC MRB S AMM SSI 5334091 4.00 B4-200NTM 533400C4SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AROUND PART 6F4SLOT FLAP CUT-OUT, BETWEEN FRAMES 37 AND 38.1STRINGERS 28 TO 34, ESPECIALLY IN CUT-OUT CORNERS INZONES 137/138.PREP.: FORWARD WING ROOT AND SLOT FAIRING OR BLANKINGPANEL REMOVED.533415-0602-1 231 FUS. SKIN, FRAMES 26 TO 27 MEC DET T: 14200 FC ALI CN 2006-0071(B) 1 0.20 B2232 OR CN FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE (EXTERNAL) 26300 FC FAA ADTO LOVSKIN AROUND SPOTLIGHT CUT-OUTS BETWEEN FRAMES I: 7100 FC ALI REFERENCE:26 AND 27 AND BETWEEN STRINGERS 24 AND 26. 533415-01-1STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 66APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533415-0602-2 231 FUS.SKIN FRAMES 26 TO 27 MEC DET T: 14000 FC ALI CN 2006-0071(B) 1 0.20 B4-100232 OR CN FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE (EXTERNAL) 23300 FC FAA ADTO LOVSKIN AROUND POTLIGHT CUT-OUTS BETWEEN FRAMES I: 7000 FC ALI REFERENCE:26 AND 27 AND BETWEEN STRINGERS 24 AND 26. 533415-01-2533415-0602-3 231 FUS.SKIN FRAMES 26 TO 27 MEC DET T: 13800 FC ALI CN 2006-0071(B) 1 0.20 B4-200232 OR CN FAA AD 96-13-11 1 0.20 C4DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 23000 FC FAA ADF4SKIN AROUND SPOTLIGHT CUT-OUTS BETWEEN FRAMES 26 I: 6900 FC ALI REFERENCE: FROM 0 FC/FHAND 27 AND BETWEEN STRINGERS 24 AND 26, RH SIDE ONLY. 533415-01-3TO LOVNOTE: FOR C4, F4 AND B4-2C POST 6208, INSPECTION ISAPPLICABLE ONLY ON RH SIDE533417-0602-1 230 FUS. SKIN, FRAMES 32 TO 33 MEC DET I: 7200 FC MRB S AMM SSI 5334171 0.20 B2MSN 003-015DETAILED INSPECTION OF EXTERNAL SKINAROUND CUT-OUT FOR ESCAPE SLIDE SPOTLIGHT BETWEENFRAMES 32 AND 33 AND BETWEEN STRINGERS 22 TO 25.533417-0602-2 230 FUS. SKIN, FRAMES 32 TO 33 MEC DET I: 6500 FC MRB S AMM SSI 5334171 0.20 B4-100MSN 003-015DETAILED INSPECTION OF EXTERNAL SKINAROUND CUT-OUT FOR ESCAPE SLIDE SPOTLIGHT BETWEENFRAMES 32 AND 33 AND BETWEEN STRINGERS 22 TO 25.533423-0602-1 130 FUS. SKIN, FRAMES 27 TO 28 MEC DET I: 9000 FC MRB S AMM SSI 5334231 0.20 ALLDETAILED INSPECTION OF EXTERNAL SKINAROUND DRAIN VALVE BETWEEN FRAMES 27 AND 28 FROMSTRINGER 54 TO CENTERLINE.533425-0602-1 230 FUS. SKIN SPLICE, FRAME 26 MEC DET I: 7200 FC MRB S AMM SSI 5334251 0.20 B2DETAILED INSPECTION OF EXTERNAL SKIN SPLICEAT FRAME 26 FROM STRINGER 5 TO CROWN CENTER-LINE.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 67APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533425-0602-2 230 FUS. SKIN SPLICE, FRAME 26 MEC DET I: 6900 FC MRB S AMM SSI 5334251 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKIN SPLICEAT FRAME 26 FROM STRINGER 5 TO CROWN CENTER-LINE.533425-0602-3 230 FUS. SKIN SPLICE, FRAME 26 MEC DET I: 6800 FC MRB S AMM SSI 5334251 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN SPLICEF4AT FRAME 26 FROM STRINGER 5 TO CROWN CENTER-LINE.533427-0602-1 240 FUS.SKIN,FRAMES 38.2 TO 40 MEC DET I: 7200 FC MRB S AMM SSI 5334271 0.20 B2DETAILED INSPECTION OF EXTERNAL SKINFROM FRAME 38.2 TO 40 FROM STRINGER 5 TO CROWNCENTERLINE.533427-0602-2 240 FUS.SKIN,FRAMES 38.2 TO 40 MEC DET I: 6500 FC MRB S AMM SSI 5334271 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKINFROM FRAME 38.2 TO 40 FROM STRINGER 5 TO CROWNCENTERLINE.533427-0602-3 240 FUS.SKIN,FRAMES 38.2 TO 40 MEC DET I: 6400 FC MRB S AMM SSI 5334271 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKINF4FROM FRAME 38.2 TO 40 FROM STRINGER 5 TO CROWNCENTERLINE.533429-0604-1 137 FUS. SKIN, FRAMES 37 TO 39 MEC DET I: 9300 FC MRB S AMM SSI 5334291 0.50 B21381 0.50DETAILED INSPECTION OF INTERNAL FUSELAGE SKINAROUND CUT-OUTS FOR WIRE BUNDLES BETWEEN FRAMES 37AND 39 AND BETWEEN STRINGERS 27 AND 30.PREP.: INSULATION REMOVED.ACCESS: 131CZ* 0.13132EZ* 0.13STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 68APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533429-0604-2 137 FUS. SKIN, FRAMES 37 TO 39 MEC DET I: 8300 FC MRB S AMM SSI 5334291 0.50 B41381 0.50 C4DETAILED INSPECTION OF INTERNAL FUSELAGE SKINF4AROUND CUT-OUTS FOR WIRE BUNDLES BETWEEN FRAMES 37AND 39 AND BETWEEN STRINGERS 27 AND 30.PREP.: INSULATION REMOVED.ACCESS: 131CZ* 0.13132EZ* 0.13533430-0602-1 130 FUSELAGE SKIN AT FR.28A & 30A NDT SDI T: 18000 FC ISB NTM 5314031 0.50 ALLOR PART 6SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME 24000 FH CN F-2004-18528A AND FRAME 30A ABOVE STRINGER 30 LH/RH. I: 3000 FC FAA AD 96-17-14ISB 53-0283533435-0602-1 243 FUS.SKIN AT FRAME 34 MEC DET T: 17600 FC ALI EASA AD1 0.20 B2244 I: 8800 FC 2006-00711 0.20 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE (EXTERNAL)SKIN FAA ADTO LOVAT FRAME 34 FROM STRINGER 5 TO CROWN CENTERLINE. 2007-04-11ALI REFERENCE:533435-01-1533435-0602-2 243 FUS.SKIN AT FRAME 34 MEC DET T: 17800 FC ALI EASA AD1 0.20 B4-100244 I: 8900 FC 2006-00711 0.20 FROM 0 FC/FHDETAILED INSPECTION OF FUESELAGE (EXTERNAL) FAA ADTO LOVSKIN AT FRAME 34 FROM STRINGER 5 TO CROWN CENTERLINE. 2007-04-11ALI REFERENCE:533435-01-2533435-0602-3 243 FUS.SKIN AT FRAME 34 MEC DET T: 16000 FC ALI EASA AD1 0.20 B4-200244 I: 8000 FC 2006-00711 0.20 C4DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA ADF4SKIN AT FRAME 34 FROM STRINGER 5 TO CROWN CENTERLINE. 2007-04-11FROM 0 FC/FHTO LOVALI REFERENCE:533435-01-3STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 69APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533437-0602-1 130 SKIN AROUND MID PAX DOOR MEC DET T: 14000 FC CPCP MRB REFERENCE: 1 0.50 ALL230 I: 3500 FC 533437-C602-11 0.50 FROM 0 FC/FH240 DETAILED INSPECTION OF SURROUNDING OF MID1 0.50 TO LOVPASSENGER/CREW DOOR CUT-OUTS (25 CM/10 INCHES AROUNDSCUT-OUT EDGES), INCLUDING FAIL SAFE RING, AND CUT-OUTEDGES.NOTE : WHERE AREAS ARE COVERED BY SB 53-0204 ANDSB 53-0233, CPCP TASK IS NOT TO BE APPLIED.PREP : PAX DOORS OPENED,533437-0602-3 131 FUSELAGE SKIN, FR 28 TO 31 MEC DET T: 24000 FC ISB CN1 0.30 PRE 01358132 I: NOTE 1983-102-053(B) 1 0.30 (53-0027)DETAILED INSPECTION OF FUSELAGE AREA FAA AD 98-20-36FROM FR.28 TO FR.31 BETWEEN STRINGER 29 AND 31 FOR ISB 53-0112EVIDENCE OF CRACKING AT RIVET HOLES.NOTE: REPET INSPECTION AT 30000 FC, 36000 FC ANDSUBSEQUENTLY EVERY 3000 FC.533437-0602-4 130 SKIN AROUND MID PAX DOOR MEC DET T: 14000 FC ALI EASA AD1 0.50 ALL230 OR EASA AD 2006-00711 0.50 FROM 0 FC/FH240 DETAILED INSPECTION OF FUSELAGE SKIN AROUND 23300 FC FAA AD FAA AD1 0.50 TO LOVMID PASSENGER/CREW DOOR CUT-OUT BETWEEN FRAME 27 AND I: 3500 FC 2007-04-11FRAME 32 AND BETWEEN STRINGER 9 AND STRINGER 30INCLUDING SCUFF PLATE. ALI REFERENCE:533437-01-1533439-0603-1 130 MID PAX/CREW DOOR CUTOUT NDT SDI T: ISB ISB AMM SSI 5334391 2.00 ALL53-0204 MRB S NTM 533052DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE PART 4, 6, 7AREAS BEHIND SCUFF PLATES AT MID PASSENGER/CREW DOOR NTM 533053CUTOUT PART 6CNPREP.: SCUFF PLATE TO BE REMOVED. 1991-132-124(B)FAA AD 97-11-03ISB 53-0204ISB 53-0233STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 70APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533439-0603-2 130 MID PAX/CREW DOOR CUTOUT NDT SDI T: 20000 FC ISB NTM 5314001 2.50 PREI: ISB PART 2(53-0192)DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE 53-0227 NTM 533053MID DOOR CUTOUT AT HOLES, OF CORNER DOUBLERS, FAIL PART 6SAFE RING AND DOOR FRAMES. NTM 533400PART 2CN1991-132-124(B)FAA AD 97-11-03ISB 53-0227533439-0603-3 131 FUSELAGE NDT SDI T: 30300 FC CN NTM 5314061 8.00 PRE 02611132 I: 4100 FC ISB PART 41 8.00SPECIAL DETAILED INSPECTION OF LAP JOINT BELOW CN F-2002-639STRINGER 27 BETWEEN FRAME 28A AND FRAME 30A LH AND FAA ADRH. 2004-08-05ISB 53-0356PREP.: INSULATION TO BE REMOVED533507-0602-1 140 SKIN SPLICE, FR. 47 TO 48 MEC DET I: 8200 FC MRB S AMM SSI 5335071 0.20 B2DETAILED INSPECTION OF SKIN SPLICE BETWEENFRAMES 47 AND 48 AT STRINGER 36 FROM INSIDE OF MLGBAY.533507-0602-2 140 SKIN SPLICE, FR. 47 TO 48 MEC DET I: 7000 FC MRB S AMM SSI 5335071 0.20 B4-100DETAILED INSPECTION OF SKIN SPLICE BETWEENFRAMES 47 AND 48 AT STRINGER 36 FROM INSIDE OF MLGBAY.533507-0602-3 140 SKIN SPLICE, FR. 47 TO 48 MEC DET I: 5800 FC MRB S AMM SSI 5335071 0.20 B4-200C4DETAILED INSPECTION OF SKIN SPLICE BETWEENF4FRAMES 47 AND 48 AT STRINGER 36 FROM INSIDE OF MLGBAY.533511-0604-1 147 SKIN PANEL ATTACHMENT MEC DET I: 27300 FC MRB S AMM SSI 5335111 0.25 B21481 0.25DETAILED INSPECTION OF ATTACHMENT OF SKIN* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 71APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533511-0604-1 * * * * * C O N T I N U E * * * * *PANEL TO FRAME 47 BETWEEN STRINGERS 30 AND 36.ACCESS: 147KZ* 0.01148KZ* 0.01533511-0604-2 147 SKIN PANEL ATTACHMENT MEC DET I: 22600 FC MRB S AMM SSI 5335111 0.25 B4-1001481 0.25DETAILED INSPECTION OF ATTACHMENT OF SKINPANEL TO FRAME 47 BETWEEN STRINGERS 30 AND 36.ACCESS: 147KZ* 0.01148KZ* 0.01533511-0604-3 147 SKIN PANEL ATTACHMENT MEC DET I: 19200 FC MRB S AMM SSI 5335111 0.25 B4-2001481 0.25 C4DETAILED INSPECTION OF ATTACHMENT OF SKINF4PANEL TO FRAME 47 BETWEEN STRINGERS 30 AND 36.ACCESS: 147KZ* 0.01148KZ* 0.01533513-0602-1 240 SKIN SPLICES, FR.46 TO 48 MEC DET I: 8300 FC MRB S AMM SSI 5335131 0.20 B2DETAILED INSPECTION OF EXTERNAL SKIN SPLICESAT STRINGER 5 AND STRINGER 13 BETWEEN FRAME 46 ANDFRAME 48.533513-0602-2 240 SKIN SPLICES, FR.46 TO 48 MEC DET I: 6800 FC MRB S AMM SSI 5335131 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKIN SPLICESAT STRINGER 5 AND STRINGER 13 BETWEEN FRAME 46 ANDFRAME 48.533513-0602-3 240 SKIN SPLICES, FR.46 TO 48 MEC DET I: 6500 FC MRB S AMM SSI 5335131 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN SPLICESF4AT STRINGER 5 AND STRINGER 13 BETWEEN FRAME 46 ANDFRAME 48.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 72APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533515-0602-1 240 SKIN SPLICES, FR.53 TO 54A MEC DET I: 8200 FC MRB S AMM SSI 5335151 0.20 B2DETAILED INSPECTION OF EXTERNAL SKIN SPLICESAT STRINGER 5 BETWEEN FRAME 53 AND FRAME 54A.533515-0602-2 240 SKIN SPLICES, FR.53 TO 54A MEC DET I: 6800 FC MRB S AMM SSI 5335151 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKIN SPLICESAT STRINGER 5 BETWEEN FRAME 53 AND FRAME 54A.533515-0602-3 240 SKIN SPLICES, FR.53 TO 54A MEC DET I: 5700 FC MRB S AMM SSI 5335151 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN SPLICESF4AT STRINGER 5 BETWEEN FRAME 53 AND FRAME 54A.533517-0602-1 241 CABIN WINDOW FRAMES MEC DET T: 11000 FC ALI EASA AD1 0.25 B2242 OR 2006-00711 0.25 POST 01288DETAILED INSPECTION OF FUSELAGE (EXTERNAL)SKIN 12400 FH FAA ADFROM 0 FC/FHAND VISIBLE SECTIONS OF WINDOW FRAME FORGED COMPO- I: 5500 FC 2007-04-11TO LOVNENTS BETWEEN FRAMES 40 AND 54 AND STRINGERS 18 TO 28 OR6200 FH ALI REFERENCE:NOTE THRESHOLD: 11000 FC 18300 FC 533517-01-112400 FH 20700 FH533517-0602-2 240 CABIN WINDOW FRAMES MEC DET T: 2 YE MRB S AMM SSI 5335171 0.50 PRE 01288I: 1 YEDETAILED INSPECTION OF EXTERNAL SKINAND VISIBLE SECTIONS OF WINDOW FRAME FORGED COMPO-NENTS BETWEEN FRAMES 40 AND 54 AND STRINGERS 18 TO 22NOTE: IN CASE OF FINDINGS INSPECT REMAINING CABINWINDOW FRAMES I.A.W. TASK 533311-0602-1 ANDTASK 533725-0602-1533517-0602-4 241 CABIN WINDOW FRAMES MEC DET T: 9200 FC ALI EASA AD1 0.25 B4-100242 OR 2006-00711 0.25 POST 01288DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 12500 FH FAA ADFROM 0 FC/FHSKIN AND VISIBLE SECTIONS OF WINDOW FRAME FORGED I: 4600 FC 2007-04-11TO LOVCOMPONENTS BETWEEN FRAMES 40 AND 54 AND ORSTRINGERS 18 TO 28. 6200 FH ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 73APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533517-0602-4 * * * * * C O N T I N U E * * * * *533517-01-2NOTE THRESHOLD: 9200 FC 15300 FC12500 FH 20800 FH533517-0602-5 241 CABIN WINDOW FRAMES MEC DET T: 8600 FC ALI EASA AD1 0.25 B4-200242 OR 2006-00711 0.25 C4DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 19000 FH FAA ADF4SKIN AND VISIBLE SECTIONS OF WINDOW FRAME I: 4300 FC 2007-04-11POST 01288FORGED COMPONENTS AND BETWEEN FRAMES 40 AND 54 AND ORFROM 0 FC/FHSTRINGERS 18 TO 28. 9500 FH ALI REFERENCE: TO LOV533517-01-3NOTE THRESHOLD: 8600 FC 14300 FC19000 FH 31600 FH533521-0602-1 145 CUT-OUT IN SKIN AT FRAME 40 MEC DET I: 11000 FC MRB S AMM SSI 5335211 0.10 B21461 0.10DETAILED INSPECTION OF UPPER CUT-OUT FOR WINGCENTER BOX IN SKIN AT FRAME 40.533521-0602-2 145 CUT-OUT IN SKIN AT FRAME 40 MEC DET I: 9300 FC MRB S AMM SSI 5335211 0.10 B4-1001461 0.10DETAILED INSPECTION OF UPPER CUT-OUT FOR WINGCENTER BOX IN SKIN AT FRAME 40.533521-0602-3 145 CUT-OUT IN SKIN AT FRAME 40 MEC DET I: 7800 FC MRB S AMM SSI 5335211 0.10 B4-2001461 0.10 C4DETAILED INSPECTION OF UPPER CUT-OUT FOR WINGF4CENTER BOX IN SKIN AT FRAME 40.533601-0602-1 151 FUSELAGE SKIN,FRAMES 54 TO 58 MEC DET I: 8200 FC MRB S AMM SSI 5336011 0.15 B21521 0.15DETAILED INSPECTION OF EXTERNAL SKIN AT SHEARTIE ATTACHMENTS AND LONGITUDINAL SKIN SPLICES BETWEENFRAMES 54 AND 58 AND BETWEEN STRINGERS 31 AND 44.533601-0602-2 151 FUSELAGE SKIN, FRAMES 54 TO 58 MEC DET I: 7800 FC MRB S AMM SSI 5336011 0.15 B4-1001521 0.15* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 74APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533601-0602-2 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF EXTERNAL SKIN AT SHEARTIE ATTACHMENTS AND LONGITUDINAL SKIN SPLICES BETWEENFRAMES 54 AND 58 AND BETWEEN STRINGERS 31 AND 44.533601-0602-3 151 FUSELAGE SKIN, FRAMES 54 TO 58 MEC DET I: 7000 FC MRB S AMM SSI 5336011 0.15 B4-2001521 0.15 C4DETAILED INSPECTION OF EXTERNAL SKIN AT SHEARF4TIE ATTACHMENTS AND LONGITUDINAL SKIN SPLICES BETWEENFRAMES 54 AND 58 AND BETWEEN STRINGERS 31 AND 44.533605-0602-1 243 FUS. SKIN, FRAMES 56 TO 61 MEC DET T: 18600 FC ALI EASA AD1 0.10 B2244 OR 2006-00711 0.10 FROM 0 FC/FH253 DETAILED INSPECTION OF EXTERNAL SURFACE (SKIN) 21000 FH FAA AD1 0.10 TO LOV254 AROUND ANTENNA CUT-OUTS AT CROWN CENTERLINE BETWEEN I: 8000 FC 2007-04-111 0.10FRAME 56 AND 57 AND BETWEEN FRAME 60 AND 61 AND ORWIRE HOLES AT FR 57/58. 9000 FH ALI REFERENCE:533605-01-1PREP.: ADF SENSE AND LOOP ANTENNAE TO BE REMOVED.533605-0602-2 243 FUS.SKIN FRAMES 56 TO 61 MEC DET T: 13300 FC ALI EASA AD1 0.10 B4-100244 OR 2006-00711 0.10 FROM 0 FC/FH253 DETAILED INSPECTION OF EXTERNAL SURFACE (SKIN) 18000 FH FAA AD1 0.10 TO LOV254 AROUND ANTENNA CUT-OUTS AT CROWN CENTERLINE BETWEEN I: 8000 FC 2007-04-111 0.10FRAME 56 AND 57 AND BETWEEN FRAME 60 AND 61 AND WIRE ORHOLES AT FR 57/58. 10800 FH ALI REFERENCE:533605-01-2PREP.: ADF SENSE AND LOOP ANTENNA TO BE REMOVED.533605-0602-3 243 FUS.SKIN FRAMES 56 TO 61 MEC DET T: 11500 FC ALI EASA AD1 0.10 B4-200244 OR 2006-00711 0.10 C4253 DETAILED INSPECTION OF EXTERNAL SKIN AROUND 25400 FH FAA AD1 0.10 F4254 ANTENNA CUT-OUTS AT CROWN CENTERLINE BETWEEN FRAME 56 I: 6200 FC 2007-04-111 0.10 FROM 0 FC/FHAND 57 AND BETWEEN FRAME 60 AND 61 AND WIRE ORTO LOVHOLES AT FR 57/58. 13700 FH ALI REFERENCE:533605-01-3PREP.: ADF SENSE AND LOOP ANTENNAE TO BE REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 75APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533607-0602-1 240 JOINT AT FRAME 54 MEC DET I: 6800 FC MRB S AMM SSI 5336071 0.20 B2DETAILED INSPECTION OF EXTERNAL FUSELAGE JOINTSTRAP AT FRAME 54 FROM STRINGER 12 TO CROWN CENTER-LINE533607-0602-2 240 JOINT AT FRAME 54 MEC DET I: 6300 FC MRB S AMM SSI 5336071 0.20 B4-100DETAILED INSPECTION OF EXTERNAL FUSELAGE JOINTSTRAP AT FRAME 54 FROM STRINGER 12 TO CROWN CENTER-LINE533607-0602-3 240 JOINT AT FRAME 54 MEC DET I: 5400 FC MRB S AMM SSI 5336071 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL FUSELAGE JOINTF4STRAP AT FRAME 54 FROM STRINGER 12 TO CROWN CENTER-LINE533607-0604-1 243 JOINT AT FRAME 54 NDT SDI I: 27300 FC MRB S AMM SSI 5336071 2.00 B2244 NTM 5336001 2.00DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 2 AND 7JOINT STRAP AT FRAME 54 FROM STRINGER 12 TO CROWNCENTER LINE.PREP.: LINING AND INSULATION REMOVED.533607-0604-2 240 JOINT AT FRAME 54 NDT SDI I: 22600 FC MRB S AMM SSI 5336071 2.00 B4-100NTM 533600DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 2 AND 7JOINT STRAP AT FRAME 54 FROM STRINGER 12 TO CROWNCENTER LINE.PREP.: LINING AND INSULATION REMOVED.533607-0604-3 240 JOINT AT FRAME 54 NDT SDI I: 19200 FC MRB S AMM SSI 5336071 2.00 B4-200NTM 533600C4DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 2 AND 7F4JOINT STRAP AT FRAME 54 FROM STRINGER 12 TO CROWNCENTER LINE.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 76APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533607-0604-3 * * * * * C O N T I N U E * * * * *PREP.: LINING AND INSULATION REMOVED.533614-0602-1 250 SKIN AROUND EMERGENCY EXIT MEC DET T: 23300 FC ALI CN 2006-0071(B) 1 0.50 B2OR FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 26300 FHTO LOVSURFACE (SKIN) AROUND EMERGENCY EXITS BETWEEN I: 7000 FC ALI REFERENCE:FRAMES 54.1 - FR 58 AND BETWEEN CROWN CENTER LINE OR 533614-01-1AND STR 30. 7900 FH533614-0602-2 250 SKIN AROUND EMERGENCY EXIT MEC DET I: 30 MO CPCP MRB REFERENCE: 1 0.50 ALL533614-C602-2DETAILED INSPECTION OF SURROUNDING OFEMERGENCY EXIT CUT-OUTS (25 CM/10 INCHES AROUND CUT-OEDGES), INCLUDING FAIL SAFE RING, AND CUT-OUT EDGES.NOTE : WHERE AREAS ARE COVERED BY SB 53-0204 ANDSB 53-0233 CPCP TASK IS NOT TO BE APPLIED.PREP.: PAX DOORS OPENED533614-0602-3 250 SKIN AROUND EMERG. EXIT MEC DET T: 16600 FC ALI CN 2006-0071(B) 1 0.50 B4-100OR FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 22500 FHTO LOVSURFACE (SKIN) AROUND EMERGENCY EXITS BETWEEN I: 5000 FC ALI REFERENCE:FRAMES 54.1 - FR 58 AND BETWEEN CROWN CENTER LINE OR 533614-01-2AND STR 30. 6800 FH533614-0602-4 250 SKIN AROUND EMERG. EXIT MEC DET T: 14300 FC ALI CN 2006-0071(B) 1 0.50 B4-200OR FAA AD 96-13-11 C4DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 31600 FHF4SURFACE (SKIN) AROUND EMERGENCY EXITS BETWEEN I: 4300 FC ALI REFERENCE: FROM 0 FC/FHFRAMES 54.1 - FR 58 AND BETWEEN CROWN CENTER LINE OR 533614-01-3TO LOVAND BETWEEN STRINGER 1 AND STRINGER 30. 9500 FH533615-0603-1 251 EMERGENCY DOOR CUTOUT NDT SDI T: 18600 FC ALI NTM 5336001 4.00 B2261 OR PART 41 4.00 FROM 0 FC/FHVISUAL AND SPECIAL DETAILED INSPECTION OF FUSELAGE 21000 FH CN 2006-0071(B) TO LOVSKIN UNDER UPPER DOUBLER BETWEEN FRAME 57A AND AFT I: 8400 FC FAA AD 96-13-11END OF DOUBLER FROM STRINGER 14 TO 17. OR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 77APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533615-0603-1 * * * * * C O N T I N U E * * * * *9500 FH ALI REFERENCE:PREP.: LINING AND INSULATION REMOVED. 533615-01-1533615-0603-2 251 EMERGENCY DOOR CUTOUT NDT SDI T: 13300 FC ALI NTM 5336001 4.00 B4-100261 OR PART 41 4.00 FROM 0 FC/FHVISUAL AND SPECIAL DETAILED INSPECTION FUSELAGE SKIN 18100 FH CN 2006-0071(B) TO LOVUNDER UPPER DOUBLER BETWEEN FRAME 57A AND AFT END OF I: 6000 FC FAA AD 96-13-11DOUBLER FROM STRINGER 14 TO 17. OR8100 FH ALI REFERENCE:PREP.: LINING AND INSULATION REMOVED. 533615-01-2533615-0603-3 251 EMERGENCY DOOR CUTOUT NDT SDI T: 11500 FC ALI NTM 5336001 4.00 B4-200261 OR PART 41 4.00 C4VISUAL AND SPECIAL DETAILED INSPECTION OF FUSELAGE 25400 FH CN 2006-0071(B) F4SKIN UNDER UPPER DOUBLER BETWEEN FRAME 57A AND AFT I: 5200 FC FAA AD 96-13-11 FROM 0 FC/FHEND OF DOUBLER FROM STRINGER 14 TO 17. ORTO LOV11500 FH ALI REFERENCE:PREP.: LINING AND INSULATION REMOVED. 533615-01-3533616-0603-1 151 EMERGENCY DOOR CUTOUT NDT SDI T: 18600 FC ALI NTM 5336001 2.00 B2152 OR PART 41 2.00 FROM 0 FC/FH251 01. DETAILED INSPECTION OF FUSELAGE SKIN UNDER 21000 FH CN 2006-0071(B) 1 2.00 TO LOV261 LOWER DOUBLER BETWEEN FRAME 56A AND FRONT END I: 8400 FC FAA AD 96-13-11 1 2.00OF DOUBLER FROM STRINGER 25 TO 27. OR02. SPECIAL DETAILED INSPECTION OF PARTIAL AREAS. 9500 FH ALI REFERENCE:533616-01-1PREP.: CABIN AND CARGO COMPARTMENT LININGS TO BEREMOVED.533616-0603-2 151 EMERGENCY DOOR CUTOUT NDT SDI T: 13300 FC ALI NTM 5336001 2.00 B4-100152 OR PART 41 2.00 FROM 0 FC/FH251 01. DETAILED INSPECTION OF FUSELAGE SKIN 18100 FH CN 2006-0071(B) 1 2.00 TO LOV261 UNDER LOWER DOUBLER BETWEEN FRAME 56A AND I: 6000 FC FAA AD 96-13-11 1 2.00FRONT END OF DOUBLER FROM STRINGER 25 TO 27. OR02. SPECIAL DETAILED INSPECTION OF PARTIAL AREAS. 8100 FH ALI REFERENCE:533616-01-2PREP.: CABIN AND CARGO COMPARTMENT LININGS TO BEREMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 78APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533616-0603-3 151 EMERGENCY DOOR CUTOUT NDT SDI T: 11500 FC ALI NTM 5336001 2.00 B4-200152 OR PART 41 2.00 C4251 01. DETAILED INSPECTION OF FUSELAGE SKIN 25400 FH CN 2006-0071(B) 1 2.00 F4261 UNDER LOWER DOUBLER BETWEEN FRAME 56A AND I: 5200 FC FAA AD 96-13-11 1 2.00 FROM 0 FC/FHFRONT END OF DOUBLER FROM STRINGER 25 TO 27. ORTO LOV02. SPECIAL DETAILED INSPECTION OF PARTIAL AREAS. 11500 FH ALI REFERENCE:533616-01-3PREP.: CABIN AND CARGO COMPARTMENT LININGS TO BEREMOVED.533616-0603-4 153 FUSELAGE NDT SDI T: 30300 FC CN NTM 5316011 1.50 PRE 02611154 I: 4100 FC ISB PART 41 1.50SPECIAL DETAILED INSPECTION OF LAP JOINT AT STRINGER CN F-2002-63952 BETWEEN FRAME 56 AND FRAME 58 LH AND RH. FAA AD2004-08-05ISB 53-0356533617-0603-1 241 FUSELAGE SKIN FR. 55 TO 58 NDT SDI I: 6500 FC MRB S AMM SSI 5336171 4.00 B4-200242 NTM 5336001 4.00 C4251 VISUAL AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 41 4.00 F4252 SKIN UNDER OUTER DOUBLER BETWEEN FRAME 55 AND 58 FROM1 4.00 POST 02147STRINGER 10 TO 13, ESPECIALLY THE FIRST RIVET ROW.(53-0110)PRE 03072NOTE: 01. CABIN LININGS AND INSULATION REMOVEDNOTE 202. TASK APPLICABLE ONLY TO MSN 010, 070,073-074, 078-079, 083, 093-096, 098-101,106-107, 109-110, 114-117, 121-123,125-131, 133-141, 156, 170-171, 179533711-0602-1 250 FUSELAGE SKIN FR. 58 TO 65 MEC DET I: 6800 FC MRB S AMM SSI 5337111 0.33 B2DETAILED INSPECTION OF EXTERNAL SKIN AT SHEARTIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEENFRAME 58 AND 65 FROM STRINGER 5 TO 13FATIGUE RATE = 0.18533711-0602-2 250 FUSELAGE SKIN FR. 58 TO 65 MEC DET I: 6500 FC MRB S AMM SSI 5337111 0.33 B4-100DETAILED INSPECTION OF EXTERNAL SKIN AT SHEARTIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEEN* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 79APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533711-0602-2 * * * * * C O N T I N U E * * * * *FRAME 58 AND 65 FROM STRINGER 5 TO 13FATIGUE RATE = 0.18533711-0602-3 250 FUSELAGE SKIN FR. 58 TO 65 MEC DET I: 5800 FC MRB S AMM SSI 5337111 0.33 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN AT SHEARF4TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEENFRAME 58 AND 65 FROM STRINGER 5 TO 13FATIGUE RATE = 0.18533715-0602-1 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 6900 FC MRB S AMM SSI 5337151 0.33 B2DETAILED INSPECTION OF EXTERNAL SKIN ATSHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICESBETWEEN FRAMES 65 AND 72 FROM STRINGER 5 TO 13533715-0602-2 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 5900 FC MRB S AMM SSI 5337151 0.33 B4-100DETAILED INSPECTION OF EXTERNAL SKIN ATSHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICESBETWEEN FRAMES 65 AND 72 FROM STRINGER 5 TO 13533715-0602-3 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 5700 FC MRB S AMM SSI 5337151 0.33 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN ATF4SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICESBETWEEN FRAMES 65 AND 72 FROM STRINGER 5 TO 13533717-0602-1 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 6900 FC MRB S AMM SSI 5337171 0.33 B2DETAILED INSPECTION OF EXTERNAL SKIN ATSHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICESBETWEEN FRAME 65 AND 72 FROM STRINGER 13 TO 31.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 80APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533717-0602-2 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 5900 FC MRB S AMM SSI 5337171 0.33 B4-100DETAILED INSPECTION OF EXTERNAL SKIN ATSHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICESBETWEEN FRAME 65 AND 72 FROM STRINGER 13 TO 31.533717-0602-3 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 5700 FC MRB S AMM SSI 5337171 0.33 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN ATF4SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICESBETWEEN FRAME 65 AND 72 FROM STRINGER 13 TO 31.533725-0602-1 250 FUSELAGE SKIN FR. 54 TO 77 MEC DET I: 7000 FC MRB S AMM SSI 5337251 0.50 ALLDETAILED INSPECTION OF EXTERNAL SKIN ANDVISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAME54 AND 77 FROM STRINGER 18 TO 22.533727-0602-1 152 SKIN AROUND AFT CARGO DOOR MEC DET T: 18600 FC ALI CN1 0.16 B2154 I: 8400 FC 1989-019-097(B) 1 0.16 FROM 0 FC/FH162 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA AD 96-13-11 1 0.16 TO LOV164 SKIN AROUND AFT CARGO COMPARTMENT DOOR CUTOUT BETWEEN1 0.16252 FRAME 58 AND 65 FROM STRINGER 22RH TO 47RH ALI REFERENCE: 1 0.16533727-01-1533727-0602-3 152 SKIN AROUND AFT CARGO DOOR MEC DET T: 16600 FC ALI CN1 0.15 B4-100154 I: 7500 FC 1989-019-097(B) 1 0.15 FROM 0 FC/FH162 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA AD 96-13-11 1 0.15 TO LOV164 SKIN AROUND AFT CARGO COMPARTMENT DOOR CUTOUT BETWEEN1 0.15252 FRAME 58 AND 65 FROM STRINGER 22RH TO 47RH ALI REFERENCE: 1 0.15533727-01-2533727-0602-4 152 SKIN AROUND AFT CARGO DOOR MEC DET T: 18600 FC ALI CN1 0.15 B4-200154 I: 8400 FC 1989-019-097(B) 1 0.15 C4162 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA AD 96-13-11 1 0.15 F4164 SKIN AROUND AFT CARGO COMPARTMENT DOOR CUTOUT BETWEEN1 0.15 FROM 0 FC/FH252 FRAME 58 AND 65 FROM STRINGER 22RH TO 47RH ALI REFERENCE: 1 0.15 TO LOV533727-01-1STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 81APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533727-0603-2 171 AFT PASSENGER DOOR CUTOUT NDT SDI T: 20000 FC ISB NTM 5330531 2.50 PRE172 I: ISB PART 61 2.50 (53-0192)DETAILED AND SPECIAL DETAILED INSPECTION OF AFT 53-0227 NTM 533800PAX/CREW DOOR CUTOUT AT HOLES OF CORNER DOUBLERS, PART 2, 7FAIL SAFE RING AND DOOR FRAMES. NTM 533810PART 2CN1991-132-124(B)FAA AD 97-11-03ISB 53-0227533727-0603-3 162 AFT PASSENGER DOOR CUTOUT NDT SDI T: ISB ISB NTM 5330521 1.50 ALL53-0204 PART 4, 6, 7DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053AREAS BEHIND SCUFF PLATES AT AFT PASSENGER/CREW DOOR PART 6CUTOUT CN1991-132-124(B)PREP.: SCUFF PLATES TO BE REMOVED. FAA AD 97-11-03ISB 53-0204ISB 53-0233533729-0602-1 162 SKIN AROUND BULK CARGO DOOR MEC DET T: 23300 FC ALI EASA AD1 0.10 B2164 OR 2006-00711 0.10 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE SKIN AROUND 26500 FH FAA ADTO LOVBULK CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR.66 AND I: 7000 FC 2007-04-1170 FROM STRINGER 31RH TO 48RH ESPECIALLY CUTOUT ORCORNERS 8000 FH ALI REFERENCE:533729-01-1533729-0602-3 162 SKIN AROUND BULK CARGO DOOR MEC DET T: 22300 FC ALI EASA AD1 0.10 B4-100164 OR 2006-00711 0.10 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE (EXTERNAL) 31000 FH FAA ADTO LOVSKIN AROUND BULK CARGO DOOR CUTOUT BETWEEN FRAMES 66 I: 6700 FC 2007-04-11AND 70 AND STRINGER 31RH TO 48RH ESPECIALLY CUTOUT ORCORNERS. 9300 FH ALI REFERENCE:533729-01-2533729-0602-4 162 SKIN AROUND BULK CARGO DOOR MEC DET T: 21600 FC ALI EASA AD1 0.10 B4-200164 OR 2006-00711 0.10 C4DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 50100 FH FAA ADF4SKIN AROUND BULK CARGO DOOR CUTOUT BETWEEN FRAMES 66 I: 6500 FC 2007-04-11FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 82APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533729-0602-4 * * * * * C O N T I N U E * * * * *AND 70 AND STRINGER 31RH TO 48RH ESPECIALLY CUTOUT OR ALI REFERENCE: TO LOVCORNERS. 15100 FH 533729-01-3533730-0603-1 160 LONGITUDINAL LAP JOINT NDT SDI I: 7.5 MO ISB NTM 5131052 6.00 PRE 02611OR PART 1PRE 10715SPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP JOINT 1250 FC NTM 533005(53-0306)BETWEEN FRAMES 65 AND 72 AT STRINGER 57. PART 6CNNOTE: TASK TO BE PERFORMED ALTERNATING EXTERNAL 1998-150-246(B)FUSELAGE INSPECTION (NO ACCESS) AND INTERNAL FAA AD 99-26-15FUSELAGE INSPECTION (FLOOR PANELS AND ISB 53-0305INSULATION REMOVED)533731-0602-1 250 FUSELAGE SKIN SPLICE FR.58 MEC DET I: 6800 FC MRB S AMM SSI 5337311 0.20 B2DETAILED INSPECTION OF EXTERNAL SKIN SPLICEINCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGSAT FRAME 58 FROM STRINGER 12 TO CROWN CENTER LINENOTE: FOR PRE MOD 02526 AND 02147 THIS TASK CANBE COMBINED WITH TASK REF:533731-0602-2PREP.: ANTENNA COVER TO BE REMOVED.533731-0602-2 250 FUSELAGE SKIN SPLICE FR.58 MEC DET T: 18000 FH CN CN1 0.20 PRE 02147OR FAA AD 1983-102-053(B) (53-0110)DETAILED INSPECTION OF EXTERNAL SKIN OF 18000 FC ISB FAA AD 98-20-36 PRE 02348FUSELAGE AT FRAME 58 IN AREA BETWEEN STRINGER 5 LH I: 3000 FH ISB 53-0127PRE 02526AND STRINGER 5 RH FOR CRACKS(53-0128)PREP.: ANTENNA COVER TO BE REMOVED533731-0602-3 250 FUSELAGE SKIN SPLICE FR. 58 MEC DET I: 5400 FC MRB S AMM SSI 5337311 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN SPLICEF4INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGSAT FRAME 58 FROM STRINGER 12 TO CROWN CENTER LINENOTE: FOR PRE MOD 02526 AND 02147 THIS TASK CAN* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 83APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533731-0602-3 * * * * * C O N T I N U E * * * * *BE COMBINED WITH TASK REF:533731-0602-2PREP.: ANTENNA COVER TO BE REMOVED.533731-0602-4 250 FUSELAGE SKIN SPLICE FR. 58 MEC DET I: 6300 FC MRB S AMM SSI 5337311 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKIN SPLICEINCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGSAT FRAME 58 FROM STRINGER 12 TO CROWN CENTER LINENOTE: FOR PRE MOD 02526 AND 02147 THIS TASK CANBE COMBINED WITH TASK REF:533731-0602-2PREP.: ANTENNA COVER TO BE REMOVED533733-0602-1 250 FUSELAGE SKIN SPLICE FR.65 NDT DET I: 6900 FC MRB S AMM SSI 5337331 0.20 B2DETAILED INSPECTION OF EXTERNAL SKIN SPLICEINCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGSAT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE533733-0602-2 250 FUSELAGE SKIN SPLICE FR.65 NDT DET I: 6800 FC MRB S AMM SSI 5337331 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKIN SPLICEINCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGSAT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE533733-0602-3 250 FUSELAGE SKIN SPLICE FR.65 NDT DET I: 6400 FC MRB S AMM SSI 5337331 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN SPLICEF4INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGSAT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE533803-0602-1 172 SKIN, WASTE DRAIN MAST AREA MEC DET I: 8400 FC MRB S AMM SSI 5338031 0.20 ALLDETAILED INSPECTION OF SKIN AROUND AFT WASTEWATER DRAIN MASTSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 84APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533807-0602-1 260 FUSELAGE SKIN FR. 72 TO 80 MEC DET I: 8400 FC MRB S AMM SSI 5338071 0.20 ALLDETAILED INSPECTION OF EXTERNAL SKIN AT SHEARTIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEENFRAME 72 AND 80 FROM STRINGER 6 TO CROWN CENTERLINE533815-0602-1 250 FUSELAGE SKIN SPLICE.FR.72 NDT DET I: 7000 FC MRB S AMM SSI 5338151 0.20 MSN 003-052POST 03760DETAILED INSPECTION OF EXTERNAL SKIN SPLICE(53-0170)AT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE533815-0602-3 253 FUSELAGE SKIN SPLICE FR.72 NDT SDI I: 3000 FC ISB NTM 5121041 26.00 MSN 003-052254 PART 11 26.00 PRE 03760SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL SPLICE NTM 513106(53-0170)AT FR.72 FROM STRINGER 12 TO CROWN CENTER LINE. PART 1NTM 533809PART 4CN1983-102-053(B)FAA AD 98-20-36ISB 53-0101533821-0602-1 251 FUSELAGE SKIN FR. 73 TO 76 MEC DET T: 24600 FC ALI EASA AD1 0.20 B2252 OR 2006-00711 0.20 FROM 0 FC/FH261 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 28000 FH FAA AD1 0.20 TO LOV262 SKIN IN UPPER CORNERS ON AFT PASSENGER/CREW DOOR, I: 3700 FC 2007-04-111 0.20BETWEEN FRAMES 73/74 AND 75/76 FROM STRINGER 10 TO 12 OR4200 FH ALI REFERENCE:PREP.: DOORS TO BE OPENED 533821-01-1533821-0602-2 251 FUSELAGE SKIN FR 73 TO 76 MEC DET T: 23300 FC ALI EASA AD1 0.20 B4-100252 OR 2006-00711 0.20 FROM 0 FC/FH261 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 32400 FH FAA AD1 0.20 TO LOV262 SKIN IN UPPER CORNERS ON AFT PASSENGER/CREW DOOR, I: 3500 FC 2007-04-111 0.20BETWEEN FRAMES 73/74 AND 75/76 FROM STRINGER 10 TO 12 OR4800 FH ALI REFERENCE:PREP.: DOORS TO BE OPENED 533821-01-2STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 85APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533821-0602-3 251 FUSELAGE SKIN FR 73 TO 76 MEC DET T: 23300 FC ALI EASA AD1 0.20 B4-200252 OR 2006-00711 0.20 C4261 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 54000 FH FAA AD1 0.20 F4262 SKIN IN UPPER CORNERS ON AFT PASSENGER/CREW DOOR, I: 3500 FC 2007-04-111 0.20 FROM 0 FC/FHBETWEEN FRAMES 73/74 AND 75/76 FROM STRINGER 10 TO 12 ORTO LOV8100 FH ALI REFERENCE:PREP.: DOORS TO BE OPENED 533821-01-3533822-0602-1 250 FUSELAGE SKIN FR. 73 TO 76 MEC DET I: 2700 FC MRB S AMM SSI 5338221 0.20 B2DETAILED INSPECTION OF EXTERNAL SKIN AND SCUFFPLATE AT LOWER CORNERS OF AFT PAX/CREW DOORS, BETWEENFRAMES 73/74 AND 75/76 AND BETWEEN STRINGERS 24AND 27533822-0602-2 250 FUSELAGE SKIN FR. 73 TO 76 MEC DET I: 2600 FC MRB S AMM SSI 5338221 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKIN AND SCUFFPLATE AT LOWER CORNERS OF AFT PAX/CREW DOORS, BETWEENFRAMES 73/74 AND 75/76 AND BETWEEN STRINGERS 24AND 27533822-0602-3 250 FUSELAGE SKIN FR. 73 TO 76 MEC DET I: 2400 FC MRB S AMM SSI 5338221 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN AND SCUFFF4PLATE AT LOWER CORNERS OF AFT PAX/CREW DOORS, BETWEENFRAMES 73/74 AND 75/76 AND BETWEEN STRINGERS 24AND 27533822-0604-1 251 AFT PAX/CREW DOOR CUTOUT - LOWER CORNERS MEC DET I: 17700 FC MRB S AMM SSI 5338221 0.50 B22521 0.50 B4-100261 DETAILED INSPECTION OF INTERNAL STRUCTURE AT1 0.50262 LOWER CORNERS OF AFT PASSENGER/CREW DOOR CUTOUT1 0.50BETWEEN FRAME 73 AND 74 AND BETWEEN FRAME 75 AND 76FROM STRINGER 24 TO 27.PREP.: LINING AND INSULATION TO BE REMOVED.533822-0604-3 251 AFT PAX/CREW DOOR CUTOUT - LOWER CORNERS MEC DET I: 15100 FC MRB S AMM SSI 5338221 0.50 B4-2002521 0.50 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 86APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533822-0604-3 * * * * * C O N T I N U E * * * * *261 DETAILED INSPECTION OF INTERNAL STRUCTURE AT1 0.50 F4262 LOWER CORNERS OF AFT PASSENGER/CREW DOOR CUTOUT1 0.50BETWEEN FRAME 73 AND 74 AND BETWEEN FRAME 75 AND 76FROM STRINGER 24 TO 27.PREP.: LINING AND INSULATION TO BE REMOVED.533824-0602-2 170 LONGITUDINAL FUSELAGE JOINT NDT SDI I: 8000 FC ISB AMM SSI 5338241 3.00 MSN 003-036MRB S NTM 533800PRE 01421SPECIAL DETAILED INSPECTION OF LAP JOINTS AT STRINGER PART 4,6 AND 7(53-0033)51 LH AND RH BETWEEN FRAME 72 AND FRAME 80. ISB 53-0225PRE 07085(53-0223)533909-0602-1 312 SKIN CUT OUT FR. 82 TO 84 MEC DET I: 11200 FC MRB S AMM SSI 5339091 0.20 B2DETAILED INSPECTION OF INTERNAL SKIN CUT OUTBETWEEN FRAME 82 AND 84, FROM STRINGER 28R TO 33RACCESS: 312AR* 0.01533909-0602-2 312 SKIN CUT OUT FR. 82 TO 84 MEC DET I: 7300 FC MRB S AMM SSI 5339091 0.20 B4-100DETAILED INSPECTION OF INTERNAL SKIN CUT OUTBETWEEN FRAME 82 AND 84, FROM STRINGER 28R TO 33RACCESS: 312AR* 0.01533909-0602-3 312 SKIN CUT OUT FR. 82 TO 84 MEC DET I: 6200 FC MRB S AMM SSI 5339091 0.20 B4-200C4DETAILED INSPECTION OF INTERNAL SKIN CUT OUTF4BETWEEN FRAME 82 AND 84, FROM STRINGER 28R TO 33RACCESS: 312AR* 0.01533911-0602-1 310 FUSELAGE SKIN AT FRAME 80 MEC DET I: 8400 FC MRB S AMM SSI 5339111 0.20 B2* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 87APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533911-0602-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF EXTERNAL SKINAT FRAME 80 FROM CROWN TO BOTTOM CENTER LINE533911-0602-2 310 FUSELAGE SKIN AT FRAME 80 MEC DET I: 7500 FC MRB S AMM SSI 5339111 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKINAT FRAME 80 FROM CROWN TO BOTTOM CENTER LINE533911-0602-3 310 FUSELAGE SKIN AT FRAME 80 MEC DET I: 7900 FC MRB S AMM SSI 5339111 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKINF4AT FRAME 80 FROM CROWN TO BOTTOM CENTER LINE533915-0603-1 310 FUSELAGE SKIN AT FRAME 80 NDT SDI I: 8400 FC MRB S AMM SSI 5339151 2.00 MSN 005-008NTM 533900SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AND PART 4 AND 7EXTERNAL DOUBLER AT FRAME 80 FROM STRINGER 24 TOBOTTOM CENTER LINE, LH/RH.533935-0603-1 260 REAR PRESSURE BULKHEAD NDT SDI T: 24000 FC EASA AD NTM 5319111 2.00 ALL310 I: 8000 FC FAA AD PART 21 2.0001.DETAILED INSPECTION OF UPPER AREA (STRINGER ISB NTM 53191126LH/RH TO CROWN CENTER LINE ) OF REAR PRESSURE PART 6BULKHEAD FROM AFT FACE, EASA AD02.SPECIAL DETAILED INSPECTION FROM OUTBOARD. F-2005-093FAA ADNOTE: INSULATION TO BE REMOVED 2006-25-04ISB 53-0218ACCESS: 162AZ* 0.01312AR* 0.01533935-0603-2 260 REAR PRESSURE BULKHEAD NDT SDI T: 24000 FC EASA AD NTM 5319111 2.00 ALL310 I: 6000 FC FAA AD PART 61 2.0001.DETAILED INSPECTION OF ALL SERVICE ISB EASA ADAPERTURES IN REAR PRESSURE BULKHEAD. F-2005-09302.SPECIAL DETAILED INSPECTION OF APU FUEL APERTURES. FAA AD2006-25-04* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 88APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)533935-0603-2 * * * * * C O N T I N U E * * * * *NOTE: INSULATION TO BE REMOVED ISB 53-0218ACCESS: 162AZ* 0.01312AR* 0.01533935-0603-3 260 REAR PRESSURE BULKHEAD NDT SDI T: 24000 FC EASA AD NTM 5319111 0.50 ALL310 I: 6000 FC FAA AD PART 61 0.50SPECIAL DETAILED INSPECTION OF APU BLEED AIR ISB EASA ADAPERTURE. F-2005-093FAA ADNOTE: INSULATION TO BE REMOVED 2006-25-04ISB 53-0218ACCESS: 162AZ* 0.01312AR* 0.01534100-0603-1 131 SEAT AND DUMMY TRACK ATTACHMENTS MEC DET I: 6000 FC CN CN3 0.50 POST 03135132 FAA AD 1999-511-297(B) 3 0.50 (53-0188)151 DETAILED INSPECTION OF SEAT AND DUMMY TRACK ISB FAA AD 98-21-30 3 0.50 PRE 12167152 ATTACHMENTS LOCATED BETWEEN FRAME 38.2 AND FRAME 40 SB ISB 53-03293 0.50 (53-0358)AND BETWEEN FRAME 54 AND FRAME 54.2.PREP.: AFT CARGO COMPARTMENT: REMOVE CEILING PANELSBETWEEN FRAME 54 AND FRAME 54.2ACCESS: 131BZ 131CZ* 0.26132EZ* 0.13241AXF 241AYF 241UF 241VF 241WF* 1.22242ANF 242APF 242AQF 242ASF* 0.60534100-0603-2 131 SEAT AND DUMMY TRACK ATTACHMENTS NDT SDI T: 9000 FC MPD AMM 531544/6011 2.00 POST 12167132 I: 9000 FC1 2.00 (53-0358)151 SPECIAL DETAILED INSPECTION OF SEAT AND DUMMY TRACK1 2.00152 ATTACHMENTS LOCATED BETWEEN FRAME 38.2 AND FRAME 401 2.00AND BETWEEN FRAME 54 AND FRAME 54.2.PREP.: FWD AND AFT CARGO COMPARTMENT PARTITION ANDCEILING PANELS BETWEEN FRAME 38/38.2 ANDFRAME 54/54.2 REMOVALACCESS: 131BZ 131CZ* 0.26* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 89APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534100-0603-2 * * * * * C O N T I N U E * * * * *132EZ* 0.13534205-0602-1 120 NOSE GEAR ATTACH FITTING MEC DET I: 8500 FC MRB S AMM SSI 5342051 0.20 ALLDETAILED INSPECTION OF NOSE GEAR ACTUATINGCYLINDER ATTACH FITTING534205-0604-1 120 NOSE GEAR ATTACH FITTING MEC SDI I: 27300 FC MRB S AMM SSI 5342051 4.00 ALLNTM 531200SPECIAL DETAILED INSPECTION OF NOSE GEAR ACTUATING PART 4CYLINDER ATTACH FITTING NTM 531200PART 6534206-0602-1 120 NOSE GEAR ATTACH FITTING MEC DET I: 8500 FC MRB S AMM SSI 5342061 0.20 ALLDETAILED INSPECTION OF NOSE GEAR TELESCOPICDRAG STRUT ATTACH FITTING534213-0602-1 120 NLG DOOR HINGE FITTINGS MEC SDI I: 8500 FC MRB S AMM SSI 5342131 2.00 ALLNTM 531200DETAILED OR SPECIAL DETAILED INSPECTION OF NOSE GEAR PART 6DOOR HINGE FITTINGS ON FUSELAGE534213-0603-1 120 AFT HINGE BOLT-AFT NLG DOOR NDT SDI I: 2000 LG ISB NTM 5150001 6.00 PRE 04868ISB 53-0190(53-0191)SPECIAL DETAILED INSPECTION OF AFT NLG DOOR AFT HINGEBOLT FOR CRACKSACCESS: 121QF* 0.20534215-0602-1 120 NOSE GEAR HINGE FITTING MEC DET I: 7000 FC MRB S AMM SSI 5342151 0.20 ALL* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 90APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534215-0602-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF NOSE GEAR HINGE FITTING534215-0604-1 123 NOSE GEAR HINGE FITTING NDT SDI I: 27300 FC MRB S AMM SSI 5342151 2.00 ALL124 NTM 5343001 2.00SPECIAL DETAILED INSPECTION OF NOSE GEAR HINGE PART 6FITTING.534217-0604-1 121 NOSE GEAR HINGE FITTING NDT SDI I: 27300 FC MRB S AMM SSI 5342171 2.00 ALL122 NTM 5343001 2.00SPECIAL DETAILED INSPECTION OF NOSE GEAR HINGE PART 6FITTING.ACCESS: 121QF* 0.20122KF* 0.25534301-0604-1 132 CARGO DOOR JACK ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5343011 0.70 B2DETAILED INSPECTION OF FWD CARGO COMPARTMENTDOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOORBEAMS AT FRAMES 22 AND 23.PREP.: CEILING PANEL REMOVED.534301-0604-2 132 CARGO DOOR JACK ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5343011 0.70 B4-100DETAILED INSPECTION OF FWD CARGO COMPARTMENTDOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOORBEAMS AT FRAMES 22 AND 23.PREP.: CEILING PANEL REMOVED.534301-0604-3 132 CARGO DOOR JACK ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5343011 0.70 B4-200C4DETAILED INSPECTION OF FWD CARGO COMPARTMENTF4DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOOR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 91APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534301-0604-3 * * * * * C O N T I N U E * * * * *BEAMS AT FRAMES 22 AND 23.PREP.: CEILING PANEL REMOVED.534303-0604-1 132 HINGE FITTINGS. CARGO DOOR MEC DET I: 27300 FC MRB S AMM SSI 5343031 0.50 B2PRE 02295DETAILED INSPECTION OF HINGE FITTINGS OF FWDCARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO24A BETWEEN STRINGER 26R TO 27RACCESS: 132AR* 0.38534303-0604-2 132 HINGE FITTINGS CARGO DOOR MEC DET I: 27300 FC MRB S AMM SSI 5343031 0.50 B2POST 02295DETAILED INSPECTION OF HINGE FITTINGS OF FWDCARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO25 BETWEEN STRINGER 26R TO 27R.ACCESS: 132AR* 0.38534303-0604-3 132 HINGE FITTINGS CARGO DOOR MEC DET I: 22600 FC MRB S AMM SSI 5343031 0.50 B4-100PRE 02295DETAILED INSPECTION OF HINGE FITTINGS OF FWDCARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO25 BETWEEN STRINGER 26R TO 27R.ACCESS: 132AR* 0.38534303-0604-4 132 HINGE FITTINGS CARGO DOOR MEC DET I: 22600 FC MRB S AMM SSI 5343031 0.50 B4-100POST 02295DETAILED INSPECTION OF HINGE FITTINGS OF FWDCARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO25 BETWEEN STRINGER 26R TO 27R.ACCESS: 132AR* 0.38534303-0604-5 132 HINGE FITTINGS. CARGO DOOR MEC DET I: 19200 FC MRB S AMM SSI 5343031 0.50 B4-200C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 92APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534303-0604-5 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF HINGE FITTINGS OF FWDF4CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TOPRE 0229524A BETWEEN STRINGER 26R TO 27R534303-0604-6 132 HINGE FITTINGS CARGO DOOR MEC DET I: 19200 FC MRB S AMM SSI 5343031 0.50 B4-200C4DETAILED INSPECTION OF HINGE FITTINGS OF FWDF4CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TOPOST 0229525 BETWEEN STRINGER 26R TO 27R.534407-0602-1 231 HOOK ATTACHMENT FITTING MEC DET I: 8500 FC MRB S AMM SSI 5344071 0.40 ALL2321 0.40 EXCL. F4DETAILED INSPECTION OF HOOK ATTACHMENT FIT-TINGS OF MID PASSENGER DOOR CUTOUT UPPER FRAME.534507-0604-1 141 BRACE STRUTS , FR. 41 TO 46 MEC DET I: 27300 FC MRB S AMM SSI 5345071 0.25 B21421 0.25DETAILED INSPECTION OF BRACE STRUTS AT FRAMES41 TO 43, 45 AND 46 LOWER AND UPPER END FITTINGS ANDATTACH LUGS.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25534507-0604-2 141 BRACE STRUTS , FR. 41 TO 46 MEC DET I: 22600 FC MRB S AMM SSI 5345071 0.25 B4-1001421 0.25DETAILED INSPECTION OF BRACE STRUTS AT FRAMES41 TO 43, 45 AND 46 LOWER AND UPPER END FITTINGS ANDATTACH LUGS.ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25534507-0604-3 141 BRACE STRUTS , FR. 41 TO 46 MEC DET I: 19200 FC MRB S AMM SSI 5345071 0.25 B4-2001421 0.25 C4DETAILED INSPECTION OF BRACE STRUTS AT FRAMESF441 TO 43, 45 AND 46 LOWER AND UPPER END FITTINGS ANDATTACH LUGS.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 93APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534507-0604-3 * * * * * C O N T I N U E * * * * *ACCESS: 147AZ 147DZ* 0.25148AZ 148DZ* 0.25534509-0604-1 147 BRACE STRUTS, FR. 47 TO 54 MEC SDI I: 27300 FC MRB S AMM SSI 5345091 1.75 ALL148 NTM 5315001 1.75DETAILED OR SPECIAL DETAILED INSPECTION OF BRACE PART 6STRUTS BETWEEN FRAMES 47 AND 54 AT LOWER AND UPPEREND, INCLUDING FITTING AND ATTACHMENT LUGS.PREP.: REMOVE BOLTS AND BRACE STRUTS.ACCESS: 147KZ* 0.01148KZ* 0.01534511-0604-1 147 BRACE STRUT FORK-END FITTING MEC DET I: 27300 FC MRB S AMM SSI 5345111 0.15 B21481 0.15DETAILED INSPECTION OF STRUCTURAL BRACE STRUTFORK-END FITTING AND KEEL PICK-UP FITTING.ACCESS: 147CF* 0.01534511-0604-2 147 BRACE STRUT FORK-END FITTING MEC DET I: 22600 FC MRB S AMM SSI 5345111 0.15 B4-1001481 0.15DETAILED INSPECTION OF STRUCTURAL BRACE STRUTFORK-END FITTING AND KEEL PICK-UP FITTING.ACCESS: 147CF* 0.01534511-0604-3 147 BRACE STRUT FORK-END FITTING MEC DET I: 19200 FC MRB S AMM SSI 5345111 0.15 B4-2001481 0.15 C4DETAILED INSPECTION OF STRUCTURAL BRACE STRUTF4FORK-END FITTING AND KEEL PICK-UP FITTING.ACCESS: 147CF* 0.01534513-0604-1 140 BRACE STRUT FITTINGS MEC SDI I: 27300 FC MRB S AMM SSI 5345131 1.50 B2NTM 531500DETAILED OR SPECIAL DETAILED INSPECTION OF STRUCTURAL PART 6* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 94APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534513-0604-1 * * * * * C O N T I N U E * * * * *BRACE STRUT FORK-END FITTINGS AND ATTACH FITTINGS ATREAR SPAR AND PRESSURE WEB BEAMS.PREP.: REMOVE BOLTS AND BRACE STRUTS.ACCESS: 147BZ 147DZ 147KZ 148DZ 148KZ* 0.09534513-0604-2 140 BRACE STRUT FITTINGS MEC SDI I: 22600 FC MRB S AMM SSI 5345131 1.50 B4-100NTM 531500DETAILED OR SPECIAL DETAILED INSPECTION OF STRUCTURAL PART 6BRACE STRUT FORK-END FITTINGS AND ATTACH FITTINGS ATREAR SPAR AND PRESSURE WEB BEAMS.PREP.: REMOVE BOLTS AND BRACE STRUTS.ACCESS: 147BZ 147DZ 147KZ 148DZ 148KZ* 0.09534513-0604-3 140 BRACE STRUT FITTINGS MEC SDI I: 19200 FC MRB S AMM SSI 5345131 1.50 B4-200NTM 531500C4DETAILED OR SPECIAL DETAILED INSPECTION OF STRUCTURAL PART 6F4BRACE STRUT FORK-END FITTINGS AND ATTACH FITTINGS ATREAR SPAR AND PRESSURE WEB BEAMS.PREP.: REMOVE BOLTS AND BRACE STRUTS.ACCESS: 147BZ 147DZ 147KZ 148DZ 148KZ* 0.09534515-0602-1 147 MLG DOOR HINGE FITTINGS MEC DET I: 11400 FC MRB S AMM SSI 5345151 0.15 ALL1481 0.15DETAILED INSPECTION OF MAIN GEAR DOOR FWD ANDAFT HINGE FITTINGS.534517-0602-1 147 MLG DOOR SUPPORT FITTING MEC DET I: 11400 FC MRB S AMM SSI 5345171 0.15 ALL1481 0.15DETAILED INSPECTION OF MAIN GEAR DOOR ACTU-ATING CYLINDER SUPPORT FITTING AND CENTER HINGE.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 95APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534603-0602-1 251 HOOK ATTACHMENT FITTINGS MEC DET I: 8400 FC MRB S AMM SSI 5346031 0.15 ALL2521 0.15 EXCL. F4DETAILED INSPECTION OF HOOK ATTACHMENT FIT-TINGS AT UPPER FRAME OF EMERGENCY EXIT CUT-OUT.534701-0602-1 162 DOOR STOPS, BULK CARGO DOOR MEC DET I: 8400 FC MRB S AMM SSI 5347011 0.20 ALLDETAILED INSPECTION OF DOOR STOPS ON FRAMES OFBULK CARGO COMPARTMENT CUT-OUT534703-0604-1 152 CARGO DOOR JACK ATTACH. MEC DET I: 11200 FC MRB S AMM SSI 5347031 0.70 B2DETAILED INSPECTION OF AFT CARGO COMPARTMENTDOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOORBEAMS AT FRAMES 61 AND 62.PREP.: CEILING PANELS REMOVED.534703-0604-2 152 CARGO DOOR JACK ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5347031 0.70 B4-100DETAILED INSPECTION OF AFT CARGO COMPARTMENTDOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOORBEAMS AT FRAMES 61 AND 62.PREP.: CEILING PANELS REMOVED.534703-0604-3 152 CARGO DOOR JACK ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5347031 0.70 B4-200C4DETAILED INSPECTION OF AFT CARGO COMPARTMENTF4DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOORBEAMS AT FRAMES 61 AND 62.PREP.: CEILING PANELS REMOVED.534705-0604-4 152 HINGE FITTINGS, CARGO DOOR MEC DET T: 20000 FC ALI ALI REFERENCE: 1 0.30 ALLI: 8000 FC 534705-01-1FROM 0 FC/FHDETAILED INSPECTION OF HINGE FITTINGS OF AFTTO LOVCARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 60 TOFRAME 63 AND STRINGER 26R TO STRINGER 27R.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 96APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)534705-0604-4 * * * * * C O N T I N U E * * * * *ACCESS: 152BR* 0.27534803-0602-1 261 HOOK ATTACHMENT FITTINGS MEC DET I: 8400 FC MRB S AMM SSI 5348031 0.15 ALL2621 0.15 EXCL. F4DETAILED INSPECTION OF HOOK ATTACHMENT FITTINGS ON AFT PASSENGER DOOR CUTOUT UPPER FRAMES.534805-0603-1 260 FUSELAGE - DOOR AREA NDT SDI T: 10 YE ISB NTM 5318011 12.00 ALLI: 5 YE PART 6SPECIAL DETAILED INSPECTION OF FRAME 73A AND FRAME CN75A, AT DOOR FRAME AREA. 1996-135-199(B)FAA AD 98-06-31ACCESS: 162AZ ISB 53-0303* 0.01534901-0603-1 310 ATT.FITTINGS AT FR.86 - 87 MEC DET I: 11200 FC ALI CN 2006-0071(B) 1 3.00 B2OR FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF ATTACH FITTINGS 12700 FHTO LOVFOR HORIZONTAL STABILIZER TRIM ACTUATOR AND RIVETING ALI REFERENCE:AREA BETWEEN FRAMES 86 AND 87. 534901-01-1ACCESS: 312AR* 0.01534901-0603-2 310 ATT. FITTING AT FR 86 FR 87 MEC DET I: 10700 FC ALI CN 2006-0071(B) 1 3.00 B4-100OR FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF ATTACH FITTINGS FOR 14800 FHTO LOVHORIZONTAL STABILIZER TRIM ACTUATOR AND RIVETING AREA ALI REFERENCE:BETWEEN FRAME 86 AND 87. 534901-01-2ACCESS: 312AR* 0.01534901-0603-3 310 ATT. FITTING AT FR 86 FR 87 MEC DET I: 10100 FC ALI CN 2006-0071(B) 1 3.00 B4-200OR FAA AD 96-13-11 C4DETAILED INSPECTION OF ATTACH FITTINGS FOR 23400 FHF4HORIZONTAL STABILIZER TRIM ACTUATOR AND RIVETING AREA ALI REFERENCE: FROM 0 FC/FHBETWEEN FRAMES 86 AND 87. 534901-01-3TO LOVACCESS: 312AR* 0.01STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 97APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536101-0606-1 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI ST: 33000 FC ALI NTM 5311021 0.10 B2212 SI: 8600 FC PART 61 0.10 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071(B) TO 48000 FCBETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13-11AND CLOSING PANEL.ALI REFERENCE:NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-2 536101-02-1PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0606-2 211 WINDSHIELD FRAME MEC DET ST: 33000 FC ALI CN 2006-0071(B) 1 0.10 B2212 SI: 4700 FC FAA AD 96-13-11 1 0.10 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE INTERNALTO 48000 FCSTRUCTURE BETWEEN FRAME 2 AND 4, WINDSHIELD ALI REFERENCE:FRAME LOWER SECTION AND CLOSING PANEL. 536101-01-1NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-1PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0606-3 211 WINDSHIELD FRAME MEC DET I: 2400 FC ALI CN 2006-0071(B) 1 0.10 B2212 FAA AD 96-13-11 1 0.10 FROM 48000 FCDETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURETO LOVBETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENCE:AND CLOSING PANEL. 536101-01-2NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-1PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0606-4 211 WINDSHIELD FRAME MEC DET ST: 33000 FC ALI CN 2006-0071(B) 1 0.10 B4-100212 SI: 4700 FC FAA AD 96-13-11 1 0.10 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURETO 40000 FCBETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENCE:AND CLOSING PANEL. 536101-01-3NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-2PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 98APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536101-0606-4 * * * * * C O N T I N U E * * * * *(8.0 M/H)536101-0606-5 211 WINDSHIELD FRAME MEC DET ST: 33000 FC ALI CN 2006-0071(B) 1 0.10 B4-200212 SI: 4700 FC FAA AD 96-13-11 1 0.10 C4DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREF4BETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENCE: FROM 0 FC/FHAND CLOSING PANEL. 536101-01-4TO 34000 FCNOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-3PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0606-6 211 WINDSHIELD FRAME MEC DET I: 2400 FC ALI CN 2006-0071(B) 1 0.10 B4-100212 FAA AD 96-13-11 1 0.10 FROM 40000 FCDETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURETO LOVBETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENCE:AND CLOSING PANEL. 536101-01-5NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-4PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0606-7 211 WINDSHIELD FRAME MEC DET I: 2400 FC ALI CN 2006-0071(B) 1 0.10 B4-200212 FAA AD 96-13-11 1 0.10 C4DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREF4BETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENCE: FROM 34000 FCAND CLOSING PANEL. 536101-01-6TO LOVNOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-5PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0607-1 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI I: 7000 FC ALI NTM 5311021 0.10 B2212 PART 61 0.10 FROM 48000 FCSPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071(B) TO LOVBETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 99APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536101-0607-1 * * * * * C O N T I N U E * * * * *AND CLOSING PANEL. ALI REFERENCE:536101-02-2NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-3PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0607-2 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI ST: 33000 FC ALI NTM 5311021 0.10 B4-100212 SI: 8600 FC PART 61 0.10 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071(B) TO 40000 FCBETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13-11AND CLOSING PANEL.ALI REFERENCE:NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-4 536101-02-3PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0607-3 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI ST: 33000 FC ALI NTM 5311021 0.10 B4-200212 SI: 8600 FC PART 61 0.10 C4SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071(B) F4BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13-11 FROM 0 FC/FHAND CLOSING PANEL.TO 34000 FCALI REFERENCE:NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-5 536101-02-4PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536101-0607-4 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI I: 7000 FC ALI NTM 5311021 0.10 B4-100212 PART 61 0.10 FROM 40000 FCSPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071(B) TO LOVBETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13-11AND CLOSING PANEL.ALI REFERENCE:NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-6 536101-02-5PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 100APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536101-0607-5 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI I: 7000 FC ALI NTM 5311021 0.10 B4-200212 PART 61 0.10 C4SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071(B) F4BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13-11 FROM 34000 FCAND CLOSING PANEL.TO LOVALI REFERENCE:NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-7 536101-02-6PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.(8.0 M/H)536110-0606-1 211 COCKPIT INTERNAL STRUCTURE MEC DET ST: 25000 FC ALI CN 2006-0071(B) 1 0.15 B2212 SI: 9400 FC FAA AD 96-13-11 1 0.15 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE INTERNALTO 48000 FCSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENCE:AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-1JUNCTION, LH/RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-2PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0606-2 211 COCKPIT INTERNAL STRUCTURE NDT SDI ST: 25000 FC ALI CN 2006-0071(B) 1 0.15 B2212 SI: 11900 FC FAA AD 96-13-11 1 0.15 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALTO 48000 FCSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT ALI REFERENCE:FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-02-1JUNCTION, LH/RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-1PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0606-3 211 COCKPIT INTERNAL STRUCTURE MEC DET I: 9400 FC ALI CN 2006-0071(B) 1 0.15 B2212 FAA AD 96-13-11 1 0.15 FROM 48000 FCDETAILED INSPECTION OF FUSELAGE INTERNALTO LOVSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENCE:AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-2JUNCTION, LH/RH.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 101APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536110-0606-3 * * * * * C O N T I N U E * * * * *NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-1PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0606-4 211 COCKPIT INTERNAL STRUCTURE MEC DET ST: 25000 FC ALI CN 2006-0071(B) 1 0.15 B4-100212 SI: 9400 FC FAA AD 96-13-11 1 0.15 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE INTERNALTO 40000 FCSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENCE:AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-3JUNCTION, LH/RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-2PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0606-5 211 COCKPIT INTERNAL STRUCTURE MEC DET ST: 25000 FC ALI CN 2006-0071(B) 1 0.15 B4-200212 SI: 9400 FC FAA AD 96-13-11 1 0.15 C4DETAILED INSPECTION OF FUSELAGE INTERNALF4STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENCE: FROM 0 FC/FHAT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-4TO 34000 FCJUNCTION, LH/RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-3PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0606-6 211 COCKPIT INTERNAL STRUCTURE MEC DET I: 9400 FC ALI CN 2006-0071(B) 1 0.15 B4-100212 FAA AD 96-13-11 1 0.15 FROM 40000 FCDETAILED INSPECTION OF FUSELAGE INTERNALTO LOVSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENCE:AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-5JUNCTION, LH/RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-4PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 102APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536110-0606-7 211 COCKPIT INTERNAL STRUCTURE MEC DET I: 9400 FC ALI CN 2006-0071(B) 1 0.15 B4-200212 FAA AD 96-13-11 1 0.15 C4DETAILED INSPECTION OF FUSELAGE INTERNALF4STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENCE: FROM 34000 FCAT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-6TO LOVJUNCTION, LH/RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-5PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0607-1 211 COCKPIT INTERNAL STRUCTURE NDT SDI I: 11900 FC ALI NTM 5311041 0.15 B2212 PART 61 0.15 FROM 48000 FCSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071(B) TO LOVSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13-11FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9JUNCTION, LH/RH. ALI REFERENCE:536110-02-2NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-3PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0607-2 211 COCKPIT INTERNAL STRUCTURE NDT SDI ST: 25000 FC ALI NTM 5311041 0.15 B4-100212 SI: 11900 FC PART 61 0.15 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071(B) TO 40000 FCSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13-11FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9JUNCTION, LH/RH. ALI REFERENCE:536110-02-3NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-4PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0607-3 211 COCKPIT INTERNAL STRUCTURE NDT SDI ST: 25000 FC ALI NTM 5311041 0.15 B4-200212 SI: 11900 FC PART 61 0.15 C4SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071(B) F4STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13-11 FROM 0 FC/FHFRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9TO 34000 FCJUNCTION, LH/RH. ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 103APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536110-0607-3 * * * * * C O N T I N U E * * * * *536110-02-4NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-5PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0607-4 211 COCKPIT INTERNAL STRUCTURE NDT SDI I: 11900 FC ALI NTM 5311041 0.15 B4-100212 PART 61 0.15 FROM 40000 FCSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071(B) TO LOVSTRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13-11FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9JUNCTION, LH/RH. ALI REFERENCE:536110-02-5NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-6PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536110-0607-5 211 COCKPIT INTERNAL STRUCTURE NDT SDI I: 11900 FC ALI NTM 5311041 0.15 B4-200212 PART 61 0.15 C4SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071(B) F4STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13-11 FROM 34000 FCFRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9TO LOVJUNCTION, LH/RH. ALI REFERENCE:536110-02-6NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-7PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536111-0606-1 211 STRUCTURE LATERAL WINDOWS MEC DET T: SEE ISB ALI EASA AD1 0.25 PRE 03632212 I: SEE ISB FAA AD 2006-00711 0.25 FROM 0 FC/FHDETAILED INSPECTION OF UPPER FRAME SECTION OF ISB FAA ADTO LOVLATERAL WINDOW FWD TO FR7 SPLICE JUNCTION. 2007-04-11ISB 53-0348PREP.: REMOVE/INSTALL LININGS AND INSULATION.ALI REFERENCE:536111-01-1STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 104APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536112-0606-1 231 FUSELAGE FRAME 17 AND 19 MEC DET T: SEE ISB ALI EASA AD1 0.25 MSN 003 TO 156232 I: SEE ISB CN 2006-00711 0.25DETAILED INSPECTION OF STRINGER 12, BETWEEN ISB FAA ADFRAME 17 AND FRAME 19, LH AND RH SIDE. 2007-04-11ISB 53-0359PREP.: LININGS AND INSULATION REMOVED.ALI REFERENCE:536112-01-1536112-0606-2 231 FUSELAGE FRAME 17 AND 19 MEC DET T: 29000 FC ALI EASA AD1 0.25 MSN 157 TO 305232 I: 24900 FC CN 2006-00711 0.25DETAILED INSPECTION OF STRINGER 12, BETWEEN ISB FAA ADFRAME 17 AND FRAME 19, LH AND RH SIDE. 2007-04-11ISB 53-0359PREP.: LININGS AND INSULATION REMOVED.ALI REFERENCE:536112-01-1536113-0606-1 210 AFT FACE OF FORWARD PRESSURE BULKHEAD MEC DET T: 45000 FC ALI EASA AD1 0.25 ALLI: 9200 FC 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE FAA ADTO LOVBULKHEAD, ABOVE FLOOR LEVEL INCLUDING FR1, STRINGERS, 2007-04-11CONNECTION, SKIN AND VERTICAL BEAM.ALI REFERENCE:ACCESS: 121BL 536112-01-1* 0.01536114-0606-1 211 FIXATION BOLT AT FRAME 2, LOWER SURFACE MEC DET T: 40000 FC ALI EASA AD1 0.25 ALL212 I: 40000 FC 2006-00711 0.25 FROM 0 FC/FHDETAILED INSPECTION OF FIXATION BOLT AT FRAME 2, FAA ADTO LOVLOWER SURFACE OF CLOSING PANEL AND LOWER POST OF 2007-04-11FRONT WINDSHIELD.ALI REFERENCE:PREP.: 3 VU,4 VU, 5 VU TO BE DISPLACED , FRONT 536114-01-1WINDSHIELD TO BE REMOVEDR 536114-0606-2 211 FIXATION BOLT AT FRAME 2, LOWER SURFACE MEC DET T: 40000 FC ALI EASA AD1 0.25 ALL212 I: 40000 FC 2006-00711 0.25 FROM 0 FC/FHDETAILED INSPECTION OF FIXATION BOLT AT FRAME 2, FAA ADTO LOVLOWER SURFACE OF CLOSING PANEL AND LOWER POST OF 2007-04-11FRONT WINDSHIELD.ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 105APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536114-0606-2 * * * * * C O N T I N U E * * * * *PREP.: 3 VU,4 VU, 5 VU TO BE DISPLACED , FRONT 536114-01-2WINDSHIELD TO BE REMOVED536202-0606-1 221 FUSELAGE FRAME 14 AND 16A MEC DET T: 21000 FC ALI EASA AD1 0.20 B2222 I: 1200 FC 2006-00711 0.20 PRE 01115DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 0 FC/FHAND 16A, FORWARD AND REAR FACES, IN AREAS OF 2007-04-11T0 48000 FCCROSS BEAMS 1 AND 8, LH/RH.ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-8 536202-01-1PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0606-2 221 FUSELAGE FRAME 14 AND 16A MEC DET ST: 29000 FC ALI EASA AD1 0.20 B2222 SI: 1600 FC 2006-00711 0.20 POST 01115DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADPRE 01282AND 16A, FORWARD AND REAR FACES, IN AREAS OF 2007-04-11FROM 0 FC/FHCROSS BEAMS 1 AND 8, LH/RH.TO 48000 FCALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-9 536202-01-5PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0606-3 221 FUSELAGE FRAME 14 AND 16A MEC DET ST: 36000 FC ALI EASA AD1 0.20 B2222 SI: 9300 FC 2006-00711 0.20 POST 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 0 FC/FHAND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11TO 48000 FCBEAMS 1 AND 8, LH/RH.ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536203-0606-1 536202-01-9PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0606-4 221 FUSELAGE FRAME 14 AND 16A MEC DET ST: 21000 FC ALI EASA AD1 0.20 B4-100222 SI: 1300 FC 2006-00711 0.20 PRE 01115DETAILED INSPECTION OF FUSELAGE FRAME 14FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 106APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0606-4 * * * * * C O N T I N U E * * * * *AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS FAA ADTO 40000 FCBEAMS 1 AND 8, LH/RH. 2007-04-11NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-2 ALI REFERENCE:536202-01-2PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0606-5 221 FUSELAGE FRAME 14 AND 16A MEC DET ST: 29000 FC ALI EASA AD1 0.20 B4-100222 SI: 2000 FC 2006-00711 0.20 POST 01115DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADPRE 01282AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11FROM 0 FC/FHBEAMS 1 AND 8, LH/RH.TO 40000 FCALI REFERENCE:NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-3 536202-01-6PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0606-6 221 FUSELAGE FRAME 14 AND 16A MEC DET ST: 36000 FC ALI EASA AD1 0.20 B4-100222 SI: 4000 FC 2006-00711 0.20 POST 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 0 FC/FHAND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11TO 40000 FCBEAMS 1 AND 8, LH/RH.ALI REFERENCE:NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-4 536202-01-11PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0606-7 221 FUSELAGE FRAME 14 AND 16A MEC DET ST: 21000 FC ALI EASA AD1 0.20 B4-200222 SI: 1700 FC 2006-00711 0.20 C4DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADF4AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11PRE 01115BEAMS 1 AND 8, LH/RH.FROM 0 FC/FHALI REFERENCE: TO 34000 FCNOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-5 536202-01-3PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 107APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0606-8 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 21000 FC ALI NTM 5312011 0.20 B2222 SI: 6000 FC PART 61 0.20 PRE 01115SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADFROM 0 FC/FH14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071T0 48000 FCBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-1ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-1(2.0 M/H).536202-0606-9 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 29000 FC ALI NTM 5312011 0.20 B2222 SI: 9100 FC PART 61 0.20 POST 01115SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME T: 29000 FC EASA ADPRE 0128214 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS I: 9100 FC 2006-0071FROM 0 FC/FHBEAMS 1 AND 8, LH/RH. FAA ADTO 48000 FC2007-04-11NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-2ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-5(2.0 M/H).536202-0607-1 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 1200 FC ALI EASA AD1 0.20 B2222 2006-00711 0.20 PRE 01115DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 48000 FCAND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11TO LOVBEAMS 1 AND 8, LH/RH.ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-2 536202-01-4PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-2 221 FUSELAGE FRAME 14 AND 16A MEC DET ST: 29000 FC ALI EASA AD1 0.20 B4-200222 SI: 5000 FC 2006-00711 0.20 C4DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADF4AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11POST 01115BEAMS 1 AND 8, LH/RH.PRE 01282ALI REFERENCE: FROM 0 FC/FHNOTE 1: THIS TASK IS AN ALTERNATIVE TO 536202-0608-3 536202-01-7TO 34000 FCNOTE 2: GENERAL ALLOWANCE NOT APPLICABLE* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 108APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0607-2 * * * * * C O N T I N U E * * * * *PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-3 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 1600 FC ALI EASA AD1 0.20 B2222 2006-00711 0.20 POST 01115DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADPRE 01282AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11FROM 48000 FCBEAMS 1 AND 8, LH/RH.TO LOVALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-4 536202-01-8PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-4 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 9300 FC ALI EASA AD1 0.20 B2222 2006-00711 0.20 POST 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 48000 FCAND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11TO LOVBEAMS 1 AND 8, LH/RH.ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-5 536202-01-10PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-5 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 4000 FC ALI EASA AD1 0.20 B4-100222 2006-00711 0.20 POST 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 40000 FCAND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11TO LOVBEAMS 1 AND 8, LH/RH.ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-6 536202-01-12PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-6 221 FUSELAGE FRAME 14 AND 16A MEC DET T: 36000 FC ALI EASA AD1 0.20 B4-200222 I: 4000 FC 2006-00711 0.20 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 109APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0607-6 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADF4AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11POST 01282BEAMS 1 AND 8, LH/RH.FROM 0 FC/FHALI REFERENCE: TO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-7 536202-01-13PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-7 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 1200 FC ALI EASA AD1 0.20 B4-100222 2006-00711 0.20 PRE 01115DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 40000 FCAND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11TO LOVBEAMS 1 AND 8, LH/RH.ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-8 536202-01-14PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-8 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 1200 FC ALI EASA AD1 0.20 B4-200222 2006-00711 0.20 C4DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADF4AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11PRE 01115BEAMS 1 AND 8, LH/RH.FROM 34000 FCALI REFERENCE: TO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-9 536202-01-15PREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0607-9 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 1600 FC ALI EASA AD1 0.20 B4-100222 2006-00711 0.20 POST 01115DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADPRE 01282AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11FROM 40000 FCBEAMS 1 AND 8, LH/RH.TO LOVALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0609-1 536202-01-16PREP.: REMOVE/INSTALL LININGS AND INSULATION,* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 110APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0607-9 * * * * * C O N T I N U E * * * * *(2.0 M/H).536202-0608-1 221 FUSELAGE FRAME 14 AND 16A MEC DET I: 1600 FC ALI EASA AD1 0.20 B4-200222 2006-00711 0.20 C4DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADF4AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11POST 01115BEAMS 1 AND 8, LH/RH.PRE 01282ALI REFERENCE: FROM 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0609-2 536202-01-17TO LOVPREP.: REMOVE/INSTALL LININGS AND INSULATION,(2.0 M/H).536202-0608-2 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 6000 FC ALI NTM 5312011 0.20 B2222 PART 61 0.20 PRE 01115SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADFROM 48000 FC14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071TO LOVBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-1ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-4(2.0 M/H).536202-0608-3 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 29000 FC ALI NTM 5312011 0.20 B4-200222 SI: 8300 FC PART 61 0.20 C4SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADF414 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071POST 01115BEAMS 1 AND 8, LH/RH. FAA ADPRE 012822007-04-11FROM 0 FC/FHNOTE 1: THIS TASK IS AN ALTERNATIVE TO 536202-0607-2TO 34000 FCALI REFERENCE:NOTE 2: GENERAL ALLOWANCE NOT APPLICABLE 536202-02-7PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS(2.0 M/H).536202-0608-4 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 8300 FC ALI NTM 5312011 0.20 B2222 PART 61 0.20 POST 01115* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 111APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0608-4 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION (ROT)OF FUSELAGE FRAME 14 EASA ADPRE 01282AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071FROM 48000 FCBEAMS 1 AND 8, LH/RH. FAA ADTO LOV2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-3ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-8(2.0 M/H).536202-0608-5 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 13800 FC ALI NTM 5312011 0.20 B2222 PART 61 0.20 POST 01282SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADFROM 48000 FC14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071TO LOVBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-4ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-10(2.0 M/H).536202-0608-6 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 13800 FC ALI NTM 5312011 0.20 B4-100222 PART 61 0.20 POST 01282SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADFROM 40000 FC14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071TO LOVBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-5ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-12(2.0 M/H).536202-0608-7 221 FUSELAGE FRAME 14 AND 16A NDT SDI T: 36000 FC ALI NTM 5312011 0.20 B4-200222 I: 13800 FC PART 61 0.20 C4SPECIAL DETAILED INSPECTION (ROT)OF FUSELAGE FRAME 14 EASA ADF4AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071POST 01282BEAMS 1 AND 8, LH/RH. FAA ADFROM 0 FC/FH2007-04-11TO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-6ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-13* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 112APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0608-7 * * * * * C O N T I N U E * * * * *(2.0 M/H).536202-0608-8 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 6000 FC ALI NTM 5312011 0.20 B4-100222 PART 61 0.20 PRE 01115SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADFROM 40000 FC14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071TO LOVBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-7ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-14(2.0 M/H).536202-0608-9 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 6000 FC ALI NTM 5312011 0.20 B4-200222 PART 61 0.20 C4SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADF414 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071PRE 01115BEAMS 1 AND 8, LH/RH. FAA ADFROM 34000 FC2007-04-11TO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-8ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-15(2.0 M/H).536202-0609-1 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 8300 FC ALI NTM 5312011 0.20 B4-100222 PART 61 0.20 POST 01115SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADPRE 0128214 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071FROM 40000 FCBEAMS 1 AND 8, LH/RH. FAA ADTO LOV2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-9ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-16(2.0 M/H).536202-0609-2 221 FUSELAGE FRAME 14 AND 16A NDT SDI I: 8300 FC ALI NTM 5312011 0.20 B4-200222 PART 61 0.20 C4SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADF414 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071POST 01115* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 113APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536202-0609-2 * * * * * C O N T I N U E * * * * *BEAMS 1 AND 8, LH/RH. FAA ADPRE 012822007-04-11FROM 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-1TO LOVALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-17(2.0 M/H).536203-0606-1 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 36000 FC ALI NTM 5312011 0.40 B2222 SI: 13800 FC PART 61 0.40 POST 01282SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME T: 36000 FC EASA ADFROM 0 FC/FH14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS I: 13800 FC 2006-0071TO 48000 FCBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-3ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-9(2.0 M/H).536203-0606-2 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 21000 FC ALI NTM 5312011 0.40 B4-100222 SI: 6200 FC PART 61 0.40 PRE 01115SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADFROM 0 FC/FH14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071TO 40000 FCBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-4ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-2(2.0 M/H).536203-0606-3 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 29000 FC ALI NTM 5312011 0.40 B4-100222 SI: 10200 FC PART 61 0.40 POST 01115SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADPRE 0128214 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071FROM 0 FC/FHBEAMS 1 AND 8, LH/RH. FAA ADTO 40000 FC2007-04-11NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-5ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-6(2.0 M/H).STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 114APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536203-0606-4 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 36000 FC ALI NTM 5312011 0.40 B4-100222 SI: 13800 FC PART 61 0.40 POST 01282SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADFROM 0 FC/FH14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071TO 40000 FCBEAMS 1 AND 8, LH/RH. FAA AD2007-04-11NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-6ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-11(2.0 M/H).536203-0606-5 221 FUSELAGE FRAME 14 AND 16A NDT SDI ST: 21000 FC ALI NTM 5312021 0.40 B4-200222 SI: 6700 FC PART 61 0.40 C4SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA ADF414 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071PRE 01115BEAMS 1 AND 8, LH/RH. FAA ADFROM 0 FC/FH2007-04-11TO 34000 FCNOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-7ALI REFERENCE:PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-3(2.0 M/H).536204-0606-1 221 FUSELAGE FRAME 14 MEC DET T: 30000 FC ALI EASA AD1 0.15 B2222 I: 2600 FC 2006-00711 0.15 PRE 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 0 FC/FHAT FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11TO LOVPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE:(1.6 M/H). 536204-01-1536204-0606-2 221 FUSELAGE FRAME 14 MEC DET T: 38000 FC ALI EASA AD1 0.15 B2222 I: 10000 FC 2006-00711 0.15 POST 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA ADFROM 0 FC/FHAT FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11TO 48000 FCPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE:(1.6 M/H). 536204-01-5536204-0606-3 221 FUSELAGE FRAME 14 MEC DET T: 30000 FC ALI CN 2006-0071(B) 1 0.15 B4-100222 I: 3200 FC FAA AD 96-13-11 1 0.15 PRE 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 ATFROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 115APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536204-0606-3 * * * * * C O N T I N U E * * * * *FLOOR BEAM ATTACHMENT, LH/RH. ALI REFERENCE: TO 40000 FC536204-01-2PREP.: REMOVE/INSTALL LININGS AND INSULATION,(1.6 M/H).536204-0606-4 221 FUSELAGE FRAME 14 MEC DET T: 38000 FC ALI EASA AD1 0.15 B4-100222 I: 8500 FC 2006-00711 0.15 POST 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA ADFROM 0 FC/FHFLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11TO LOVPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE:(1.6 M/H). 536204-01-6536204-0606-5 221 FUSELAGE FRAME 14 MEC DET T: 30000 FC ALI EASA AD1 0.15 B4-200222 I: 4000 FC 2006-00711 0.15 C4DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA ADF4FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11PRE 01282FROM 0 FC/FHNOTE: THIS TASK IS AN ALTERNATIVE TO 536214-0606-1 ALI REFERENCE: TO 34000 FC536204-01-3PREP.: REMOVE/INSTALL LININGS AND INSULATION,(1.6 M/H).536204-0606-6 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 5312051 0.15 B2222 I: 4700 FC PART 41 0.15 PRE 01282SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADFROM 0 FC/FHFLOOR BEAM ATTACHMENT, LH/RH. 2006-0071TO 48000 FCFAA ADPREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11(1.6 M/H).ALI REFERENCE:536204-02-1536204-0606-7 221 FUSELAGE FRAME 14 NDT SDI T: 38000 FC ALI NTM 5312051 0.15 B2222 I: 10600 FC PART 41 0.15 POST 01282SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADFROM 0 FC/FHFLOOR BEAM ATTACHMENT, LH/RH. 2006-0071TO LOVFAA ADPREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 116APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536204-0606-7 * * * * * C O N T I N U E * * * * *(1.6 M/H). ALI REFERENCE:536204-02-5536204-0606-8 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 5312051 0.15 B4-100222 I: 5900 FC PART 41 0.15 PRE 01282SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADFROM 0 FC/FHFLOOR BEAM ATTACHMENT, LH/RH. 2006-0071TO 40000 FCFAA ADPREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11(1.6 M/H).ALI REFERENCE:536204-02-2536204-0606-9 221 FUSELAGE FRAME 14 NDT SDI T: 38000 FC ALI NTM 5312051 0.15 B4-100222 I: 10000 FC PART 41 0.15 POST 01282SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADFROM 0 FC/FHFLOOR BEAM ATTACHMENT, LH/RH. 2006-0071TO 40000 FCFAA ADPREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11(1.6 M/H).ALI REFERENCE:536204-02-6536204-0607-2 221 FUSELAGE FRAME 14 MEC DET T: 38000 FC ALI EASA AD1 0.15 B4-200222 I: 8500 FC 2006-00711 0.15 C4DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA ADF4FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11POST 01282FROM 0 FC/FHPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE: TO LOV(1.6 M/H). 536204-01-7536204-0607-4 221 FUSELAGE FRAME 14 MEC DET I: 8500 FC ALI EASA AD1 0.15 B2222 2006-00711 0.15 POST 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA ADFROM 48000 FCFLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11TO LOVPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE:(1.6 M/H). 536204-01-9STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 117APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536204-0607-5 221 FUSELAGE FRAME 14 MEC DET I: 2600 FC ALI EASA AD1 0.15 B4-100222 2006-00711 0.15 PRE 01282DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA ADFROM 40000 FCFLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11TO LOVPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE:(1.6 M/H). 536204-01-10536204-0607-6 221 FUSELAGE FRAME 14 MEC DET I: 2600 FC ALI EASA AD1 0.15 B4-200222 2006-00711 0.15 C4DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA ADF4FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11PRE 01282FROM 34000 FCPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE: TO LOV(1.6 M/H). 536204-01-11536204-0607-7 221 FUSELAGE FRAME 14 NDT SDI I: 4000 FC ALI NTM 5312051 0.15 B2222 PART 41 0.15 PRE 01282SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADFROM 48000 FCFLOOR BEAM ATTACHMENT, LH/RH. 2006-0071TO LOVFAA ADPREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11(1.6 M/H).ALI REFERENCE:536204-02-4536204-0607-8 221 FUSELAGE FRAME 14 NDT SDI T: 38000 FC ALI NTM 5312051 0.15 B4-200222 I: 10600 FC PART 41 0.15 C4SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADF4FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071POST 01282FAA ADFROM 0 FC/FHNOTE 01: THIS TASK IS AN ALTERNATIVE TO 536204-0607-2 2007-04-11TO LOVPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE:(1.6 M/H). 536204-02-7536204-0607-9 221 FUSELAGE FRAME 14 NDT SDI I: 10600 FC ALI NTM 5312051 0.15 B4-100222 PART 41 0.15 POST 01282SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADFROM 40000 FCFLOOR BEAM ATTACHMENT, LH/RH. 2006-0071TO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 118APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536204-0607-9 * * * * * C O N T I N U E * * * * *PREP.: REMOVE/INSTALL LININGS AND INSULATION, FAA AD(1.6 M/H). 2007-04-11ALI REFERENCE:536204-02-8536204-0608-2 221 FUSELAGE FRAME 14 MEC DET I: 4000 FC ALI NTM 5312051 0.15 B4-100222 PART 41 0.15 PRE 01282NDT INSPECTION OF FUSELAGE FRAME 14 AT FLOOR BEAM EASA ADFROM 40000 FCATTACHMENT, LH/RH. 2006-0071TO LOVFAA ADPREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11(1.6 M/H).ALI REFERENCE:536204-02-10536204-0608-4 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 5312051 0.15 B4-200222 I: 4000 FC PART 41 0.15 C4SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADF4FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071PRE 01282FAA ADFROM 0 FC/FHPREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11TO LOV(1.6 M/H).ALI REFERENCE:536204-02-3536205-0606-1 211 FUSELAGE FRAME 10 MEC DET ST: 24000 FC ALI CN 2006-0071(B) 1 0.20 POST 00726212 SI: 3100 FC FAA AD 96-13-11 1 0.20 (53-0902)DETAILED INSPECTION OF FUSELAGE FRAME 10 INNERSERIALFLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENCE: PRE 00600LEVEL, LH/RH. 536205-01-1FROM 0 FC/FHTO 48000 FCNOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TOLOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-6PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 119APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536205-0606-1 * * * * * C O N T I N U E * * * * *ACCESS: 221DF* 0.39222DF* 0.36536205-0606-2 211 FUSELAGE FRAME 10 MEC DET ST: 20000 FC ALI CN 2006-0071(B) 1 0.20 POST 00726212 SI: 2800 FC FAA AD 96-13-11 1 0.20 (53-0902)DETAILED INSPECTION OF FUSELAGE FRAME 10 INNERRETROFITFLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENCE: PRE 00600LEVEL, LH/RH. 536205-01-2FROM 0 FC/FHTO 48000 FCNOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TOLOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-7PREP.: 15 VU TO BE OPENED (REMOVAL NOT NECESSARY)LINING AND INSULATION.(EXTENDED AREA FOR AIRPLANE POST 726).ACCESS: 221DF* 0.39222DF* 0.36536205-0606-3 211 FUSELAGE FRAME 10 MEC DET I: 2800 FC ALI CN 2006-0071(B) 1 0.20 POST 00726212 FAA AD 96-13-11 1 0.20 (53-0902)DETAILED INSPECTION OF FUSELAGE FRAME 10 INNERPRE 00600FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENCE: FROM 48000 FCLEVEL, LH/RH. 536205-01-3TO LOVNOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TOLOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-8PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).ACCESS: 221DF* 0.39222DF* 0.36536205-0606-4 211 FUSELAGE FRAME 10 MEC DET ST: 20000 FC ALI CN 2006-0071(B) 1 0.20 POST 00600212 SI: 3100 FC FAA AD 96-13-11 1 0.20 FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 120APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536205-0606-4 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF FUSELAGE FRAME 10 INNER ALI REFERENCE: TO 48000 FCFLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR 536205-01-4LEVEL, LH/RH.NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TOLOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-9PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).ACCESS: 221DF* 0.39222DF* 0.36536205-0606-5 211 FUSELAGE FRAME 10 MEC DET I: 3400 FC ALI CN 2006-0071(B) 1 0.20 POST 00600212 FAA AD 96-13-11 1 0.20 FROM 48000 FCDETAILED INSPECTION OF FUSELAGE FRAME 10 INNERTO LOVFLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENCE:LEVEL, LH/RH. 536205-01-5NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TOLOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0607-1PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).ACCESS: 221DF* 0.39222DF* 0.36536205-0606-6 211 FUSELAGE FRAME 10 NDT SDI ST: 24000 FC ALI NTM 5311011 0.20 POST 00726212 SI: 10000 FC PART 6 PROC A1 0.20 (53-0902)SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071(B) SERIALINNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13-11 PRE 00600FLOOR LEVEL, LH/RH.FROM 0 FC/FHALI REFERENCE: TO 48000 FCNOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-1LOWER END OF REINFORCEMENT* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 121APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536205-0606-6 * * * * * C O N T I N U E * * * * *NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-1PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).ACCESS: 221DF 222DF* 0.75536205-0606-7 211 FUSELAGE FRAME 10 NDT SDI ST: 20000 FC ALI NTM 5311011 0.20 POST 00726212 SI: 8700 FC PART 6 PROC A1 0.20 (53-0902)SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071(B) RETROFITINNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13-11 PRE 00600FLOOR LEVEL, LH/RH.FROM 0 FC/FHALI REFERENCE: TO 48000 FCNOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-2LOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-2PREP.: 15 VU TO BE OPENED (REMOVAL NOT NECESSARY)LINING AND INSULATION.(EXTENDED AREA FOR AIRPLANE POST 726).ACCESS: 221DF* 0.39222DF* 0.36536205-0606-8 211 FUSELAGE FRAME 10 NDT SDI I: 8700 FC ALI NTM 5311011 0.20 POST 00726212 PART 6 PROC A1 0.20 (53-0902)SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071(B) PRE 00600INNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13-11 FROM 48000 FCFLOOR LEVEL, LH/RH.TO LOVALI REFERENCE:NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-3LOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-3PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).ACCESS: 221DF 222DF* 0.75STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 122APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536205-0606-9 211 FUSELAGE FRAME 10 NDT SDI ST: 20000 FC ALI NTM 5311011 0.20 POST 00600212 SI: 6800 FC PART 6 PROC B1 0.20 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071(B) TO 48000 FCINNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13-11FLOOR LEVEL, LH/RH.ALI REFERENCE:NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-4LOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-4PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).ACCESS: 221DF* 0.39222DF* 0.36536205-0607-1 211 FUSELAGE FRAME 10 NDT SDI I: 9000 FC ALI NTM 5311011 0.20 POST 00600212 PART 6 PROC B1 0.20 FROM 48000 FCSPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071(B) TO LOVINNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13-11FLOOR LEVEL, LH/RH.ALI REFERENCE:NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-5LOWER END OF REINFORCEMENTNOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-5PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGSAND INSULATION, (10.0 M/H).ACCESS: 221DF* 0.39222DF* 0.36536207-0606-1 123 FUSELAGE FRAME 17 NDT SDI ST: 30000 FC ALI NTM 5312031 1.50 B2124 SI: 4200 FC CN 2006-0071(B) 1 1.50 POST 00797SPECIAL DETAILED INSPECTION (X-RAY) OF NLG BAY, T: 30000 FC FAA AD 96-13-11 (53-0905)FUSELAGE INTERNAL SKIN, DOUBLERS AND CORNER FLANGE AT I: 4200 FCRETROFITFR17, LH/RH. ALI REFERENCE: FROM 0 FC/FH536207-01-1TO 48000 FCNOTE: GRACE PERIOD = 2400 FCPREP.: NOSE LANDING GEAR DOORS TO BE OPENED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 123APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536207-0606-2 123 FUSELAGE FRAME 17 NDT SDI ST: 31000 FC ALI NTM 5312031 1.50 B2124 SI: 4800 FC CN 2006-0071(B) 1 1.50 POST 00797SPECIAL DETAILED INSPECTION (X-RAY) OF NLG BAY, T: 31000 FC FAA AD 96-13-11 (53-0905)FUSELAGE INTERNAL SKIN, DOUBLERS AND CORNER FLANGE AT I: 4800 FCSERIALFR17, LH/RH. ALI REFERENCE: FROM 0 FC/FH536207-01-2TO 48000 FCNOTE: GRACE PERIOD = 2400 FCPREP.: NOSE LANDING GEAR DOORS TO BE OPENED.536207-0606-3 123 FUSELAGE FRAME 17 NDT SDI ST: 31000 FC ALI NTM 5312031 1.50 B4-100124 SI: 6700 FC PART 21 1.50 POST 00797SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 31000 FC CN 2006-0071(B) (53-0905)DOUBLER AND LOWER FLANGE OF FRAME 17, FORWARD PART I: 6700 FC FAA AD 96-13-11 FROM 0 FC/FHFROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOMTO 40000 FCCENTER LINE LH/RH. ALI REFERENCE:536207-01-3PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.536207-0606-4 123 FUSELAGE FRAME 17 NDT SDI ST: 31000 FC ALI NTM 5312031 1.50 B4-200124 SI: 3000 FC PART 21 1.50 C4SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 31000 FC CN 2006-0071(B) F4DOUBLER AND LOWER FLANGE OF FRAME 17, FORWARD PART I: 3000 FC FAA AD 96-13-11 POST 00797FROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOM(53-0905)CENTER LINE LH/RH. ALI REFERENCE: FROM 0 FC/FH536207-01-4TO 34000 FCPREP.: NOSE LANDING GEAR DOORS TO BE OPENED.536207-0606-5 123 FUSELAGE FRAME 17 NDT SDI I: 3000 FC ALI NTM 5312031 1.50 B2124 PART 21 1.50 POST 00797SPECIAL DETAILED INSPECTION (X-RAY) OF NLG BAY, CN 2006-0071(B) FROM 48000 FCFUSELAGE INTERNAL SKIN, DOUBLERS AND CORNER FLANGE AT FAA AD 96-13-11 TO LOVFR17, LH/RH.ALI REFERENCE:NOTE: GRACE PERIOD = 2400 FC (FOR B2 ONLY) 536207-01-5PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.536207-0606-6 123 FUSELAGE FRAME 17 NDT SDI I: 3000 FC ALI NTM 5312031 1.50 B4-100124 PART 21 1.50 POST 00797SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071(B) (53-0905)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 124APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536207-0606-6 * * * * * C O N T I N U E * * * * *DOUBLER AND LOWER FLANGE OF FRAME 17, FORWARD PART FAA AD 96-13-11 FROM 40000 FCFROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOMTO LOVCENTER LINE LH/RH. ALI REFERENCE:536207-01-6PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.536207-0606-7 123 FUSELAGE FRAME 17 NDT SDI I: 3000 FC ALI NTM 5312031 1.50 B4-200124 PART 21 1.50 C4SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071(B) F4DOUBLER AND LOWER FLANGE OF FRAME 17, FORWARD PART FAA AD 96-13-11 POST 00797FROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOM(53-0905)CENTER LINE LH/RH. ALI REFERENCE: FROM 34000 FC536207-01-7TO LOVPREP.: NOSE LANDING GEAR DOORS TO BE OPENED.536208-0605-1 211 FUSELAGE SKIN FRAME 10 MEC DET T: 18300 FC ISB NTM 5130101 0.50 POST 00793212 I: 3600 FC PART 11 0.50 (53-0906)DETAILED INSPECTION OF REAR LOWER CORNER OF NTM 531202NOTETHE FLIGHT COMPARTMENT AFT WINDOW AND ADJACENT PART 2PRE 01446FUSELAGE SKIN. AD 2000-10-01CNNOTE: EFFECTIVITY IS POST PARTIAL MOD 00793 90-222-116(B)EMBOBIMENT, AS DEFINED PER ISB 53-278. ISB 53-0278536208-0605-2 211 FUSELAGE SKIN FRAME 10 MEC DET T: 22000 FC ISB NTM 5130101 0.50 POST 00793212 I: 3600 FC PART 11 0.50 (53-0906)DETAILED INSPECTION OF REAR LOWER CORNER OF NTM 531202PRE 01446THE FLIGHT COMPARTMENT AFT WINDOW AND ADJACENT PART 2FUSELAGE SKIN. AD 2000-10-01CN90-222-116(B)ISB 53-0278536208-0605-3 211 FUSELAGE SKIN FRAME 10 MEC DET T: 26000 FC ISB NTM 5130101 0.50 POST 00793212 I: 5000 FC PART 11 0.50 (53-0906)DETAILED INSPECTION OF REAR LOWER CORNER OF NTM 531202POST 01446THE FLIGHT COMPARTMENT AFT WINDOW AND ADJACENT PART 2FUSELAGE SKIN. AD 2000-10-01* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 125APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536208-0605-3 * * * * * C O N T I N U E * * * * *CN90-222-116(B)ISB 53-0278536210-0606-1 223 FR 13 BETWEEN STR 1 AND 2, LH/RH MEC DET ST: 32000 FC ALI CN 2006-0071(B) 1 TBD B2224 SI: 10000 FC FAA AD 96-13-11 1 TBD FROM 0 FC/FHDETAILED INSPECTION OF FRAME 13 BETWEEN T: 32000 FCTO 48000 FCSTRINGER 1 AND 2, LH/RH I: 10000 FC ALI REFERENCE:536210-01-1PREP.: CEILING PANELS AND INSULATION TO BE REMOVED.536210-0606-2 223 FR 13 BETWEEN STR 1 AND 2, LH/RH MEC DET I: 10000 FC ALI CN 2006-0071(B) 1 TBD B2224 FAA AD 96-13-11 1 TBD FROM 48000 FCDETAILED INSPECTION OF FRAME 13 BETWEENTO LOVSTRINGER 1 AND 2, LH/RH ALI REFERENCE:536210-01-2PREP.: CEILING PANELS AND INSULATION TO BE REMOVED.536210-0606-3 223 FR 13 BETWEEN STR 1 AND 2, LH/RH MEC DET ST: 32000 FC ALI CN 2006-0071(B) 1 TBD B4-100224 SI: 10000 FC FAA AD 96-13-11 1 TBD FROM 0 FC/FHDETAILED INSPECTION OF FRAME 13 BETWEEN T: 32000 FCTO 40000 FCSTRINGER 1 AND 2, LH/RH I: 10000 FC ALI REFERENCE:536210-01-3PREP.: CEILING PANELS AND INSULATION TO BE REMOVED.536210-0606-4 223 FR 13 BETWEEN STR 1 AND 2, LH/RH MEC DET ST: 32000 FC ALI CN 2006-0071(B) 1 TBD B4-200224 SI: 10000 FC FAA AD 96-13-11 1 TBD C4DETAILED INSPECTION OF FRAME 13 BETWEEN T: 32000 FCF4STRINGER 1 AND 2, LH/RH I: 10000 FC ALI REFERENCE: FROM 0 FC/FH536210-01-4TO 34000 FCPREP.: CEILING PANELS AND INSULATION TO BE REMOVED.536210-0606-5 223 FR 13 BETWEEN STR 1 AND 2, LH/RH MEC DET I: 10000 FC ALI CN 2006-0071(B) 1 TBD B4-100224 FAA AD 96-13-11 1 TBD FROM 40000 FCDETAILED INSPECTION OF FRAME 13 BETWEENTO LOVSTRINGER 1 AND 2, LH/RH ALI REFERENCE:536210-01-5PREP.: CEILING PANELS AND INSULATION TO BE REMOVED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 126APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536210-0606-6 223 FR 13 BETWEEN STR 1 AND 2, LH/RH MEC DET I: 10000 FC ALI CN 2006-0071(B) 1 TBD B4-200224 FAA AD 96-13-11 1 TBD C4DETAILED INSPECTION OF FRAME 13 BETWEENF4STRINGER 1 AND 2, LH/RH ALI REFERENCE: FROM 34000 FC536210-01-6TO LOVPREP.: CEILING PANELS AND INSULATION TO BE REMOVED.536214-0606-1 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 5312051 0.30 B4-200222 I: 4000 FC PART 41 0.30 C4SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA ADF4FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071PRE 01282FAA ADFROM 0 FC/FHNOTE : THIS TASK IS AN ALTERNATIVE TO 536204-0606-5 2007-04-11TO 34000 FCPREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENCE:(1.6 M/H). 536204-02-3536215-0603-1 121 FUSELAGE NOSE SECTION MEC DET T: 6600 FC ISB ISB 53-03881 0.30 ALL122 I: SEE ISB1 0.30DETAILED INSPECTION OF THE CROSSBEAM ON NLG FR 15AWEB FACE AT ATTACHMENT FITTING OF RACK 107VU FITTING.ACCESS: 121BL* 0.01536225-0606-1 223 FUSELAGE SKIN AT FRAME 13 NDT SDI ST: 32000 FC ALI NTM 5312041 1.00 ALL224 SI: 14000 FC PART 61 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.B.)TO 40000 FC13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD25 LH/RH. 2006-0071FAA ADNOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-XALI REFERENCE:PREP.:INSULATION AND BOLTS. 536225-01-1536225-0606-2 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 5312041 1.00 PRE 01282224 I: 8300 FC PART 61 1.00 FROM 40000 FCSPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.B.)TO LOV13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD25 LH/RH. 2006-0071* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 127APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536225-0606-2 * * * * * C O N T I N U E * * * * *NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS FAA ADTASK 536225-0606-X 2007-04-11PREP.:INSULATION AND BOLTS. ALI REFERENCE:536225-01-2536225-0606-3 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 5312041 1.00 POST 01282224 I: 14000 FC PART 61 1.00 FROM 40000 FCSPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.B.)TO LOV13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD25 LH/RH. 2006-0071FAA ADNOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-XALI REFERENCE:PREP.:INSULATION AND BOLTS. 536225-01-3536225-0606-4 223 FUSELAGE SKIN AT FRAME 13 NDT SDI ST: 32000 FC ALI NTM 5312041 1.00 B2224 SI: 7100 FC PART 61 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)TO 40000 FC13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD25 LH/RH. 2006-0071FAA ADNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-1ALI REFERENCE:PREP.:INSULATION 536225-02-1536225-0606-5 223 FUSELAGE SKIN AT FRAME 13 NDT SDI ST: 32000 FC ALI NTM 5312041 1.00 B4-100224 SI: 8000 FC PART 61 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)TO 40000 FC13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD25 LH/RH. 2006-0071FAA ADNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-1ALI REFERENCE:PREP.:INSULATION. 536225-02-2STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 128APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536225-0606-6 223 FUSELAGE SKIN AT FRAME 13 MEC SDI ST: 32000 FC ALI NTM 5312041 1.00 B4-200224 SI: 5600 FC PART 61 1.00 C4SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)F413 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA ADFROM 0 FC/FH25 LH/RH. 2006-0071TO 40000 FCFAA ADNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-1ALI REFERENCE:PREP.:INSULATION. 536225-02-3536225-0606-7 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 5312041 1.00 PRE 01282224 I: 3300 FC PART 61 1.00 FROM 40000 FCSPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)TO LOV13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD25 LH/RH. 2006-0071FAA ADNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-2ALI REFERENCE:PREP.:INSULATION. 536225-02-4536225-0606-8 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 5312041 1.00 B2224 I: 6200 FC PART 61 1.00 B4-100SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)POST 0128213 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA ADFROM 40000 FC25 LH/RH. 2006-0071TO LOVFAA ADNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-3ALI REFERENCE:PREP.:INSULATION. 536225-02-5536225-0606-9 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 5312041 1.00 B4-200224 I: 5600 FC PART 61 1.00 C4SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)F413 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA ADPOST 0128225 LH/RH. 2006-0071FROM 40000 FCFAA ADTO LOVNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 536225-0606-3ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 129APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536225-0606-9 * * * * * C O N T I N U E * * * * *PREP.:INSULATION. 536225-02-8536230-0606-1 221 INTERNAL STRUCTURE AT CABIN FLOOR NDT SDI T: 22000 FC ALI NTM 5362301 TBD ALL222 I: 3300 FC PART 41 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE AT FRAME 16A EASA ADTO LOVINTERNAL STRUCTURE AT CABIN FLOOR LEVEL, IN AREA OF 2006-0071PASSENGER/CREW DOOR LOWER KEEL JUNCTION, LH/RH FAA AD2007-04-11ALI REFERENCE:536230-01-1536231-0606-1 221 INTERNAL STRUCTURE NDT SDI T: 18500 FC ALI NTM 5362311 TBD ALL222 I: 13000 FC PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FUSELAGE AT FRAME 16A EASA ADTO LOVJOINT BETWEEN STRINGER 28 AND STRINGER 30, LH/RH 2006-0071FAA ADPREP: REMOVE LINING AND INSULATION 2007-04-11ALI REFERENCE:536231-01-1536231-02-1536232-0606-1 121 INTERNAL STRUCTURE MEC DET T: 45000 FC ALI EASA AD1 0.30 ALL122 I: 40000 FC 2006-00711 0.30 FROM 0 FC/FHDETAILED INSPECTION OF FRAME 19 WEB AT LEVEL OF FAA ADTO LOVSTR 43LH AND RH. 2007-04-11ACCESS: 121BL ALI REFERENCE: * 0.01536232-01-1536233-0606-1 211 INTERNAL STRUCTURE MEC SDI T: 48000 FC ALI NTM 5362331 0.30 ALL212 I: 24000 FC EASA AD PART 61 0.30 FROM 0 FC/FH221 SPECIAL DETAILED INSPECTION OF ROD UNDER PASSENGERS FAA AD EASA AD1 0.30 TO LOV222 FLOOR AT FR 10LH AND RH. 2006-00711 0.30FAA ADPREP.: LINING AND INSULATION, 15VU, 50VU LH TOILET 2007-04-11TO BE REMOVED.ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 130APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536233-0606-1 * * * * * C O N T I N U E * * * * *536233-01-1536234-0606-1 123 INTERNAL STRUCTURE MEC DET T: 45000 FC ALI EASA AD1 0.30 PRE 03632124 I: 3800 FC 2006-00711 0.30 FROM 0 FC/FHDETAILED INSPECTION OF NLG BAY ROOF PANEL BETWEEN FAA ADTO LOVFR 15 AND FR 17. 2007-04-11ACCESS: 713 ALI REFERENCE: * 0.06714 536234-01-1* 0.06536234-0606-2 123 INTERNAL STRUCTURE MEC DET T: 45000 FC ALI EASA AD1 0.30 POST 03632124 I: 6000 FC 2006-00711 0.30 FROM 0 FC/FHDETAILED INSPECTION OF NLG BAY ROOF PANEL BETWEEN FAA ADTO LOVFR 15 AND FR 17. 2007-04-11ACCESS: 713 ALI REFERENCE: * 0.06714 536234-01-2* 0.06536235-0606-1 121 NOSE GEAR BAY ARCHES UPPER AND LOWER MEC DET T: 48000 FC ALI EASA AD1 0.30 B2122 CORNERS I: 8500 FC 2006-00711 0.30 FROM 0 FC/FHFAA ADTO LOVDETAILED INSPECTION OF NOSE GEAR BAY ARCHES UPPER AND 2007-04-11LOWER CORNERS,BETWEEN FR 11A AND FR 16A INCLUDED,INCLUDING STRUTS ATTACHMENT LUGS, FRAMES ATTACHMENTS ALI REFERENCE:AT STG 44LH AND RH. 536235-01-1ACCESS: 121KF 121MF 121NF 121PF 121QF* 0.94122EF 122GF 122HF 122JF 122KF* 1.04536235-0606-2 121 NOSE GEAR BAY ARCHES UPPER AND LOWER MEC DET T: 40000 FC ALI EASA AD1 0.30 B4-100122 CORNERS I: 8500 FC 2006-00711 0.30 FROM 0 FC/FHFAA ADTO LOVDETAILED INSPECTION OF NOSE GEAR BAY ARCHES UPPER AND 2007-04-11LOWER CORNERS,BETWEEN FR 11A AND FR 16A INCLUDED,INCLUDING STRUTS ATTACHMENT LUGS, FRAMES ATTACHMENTS ALI REFERENCE:AT STG 44LH AND RH. 536235-01-2ACCESS: 121KF 121MF 121NF 121PF 121QF* 0.94122EF 122GF 122HF 122JF 122KF* 1.04STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 131APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536235-0606-3 121 NOSE GEAR BAY ARCHES UPPER AND LOWER MEC DET T: 34000 FC ALI EASA AD1 0.30 B4-200122 CORNERS I: 8500 FC 2006-00711 0.30 C4FAA ADF4DETAILED INSPECTION OF NOSE GEAR BAY ARCHES UPPER AND 2007-04-11FROM 0 FC/FHLOWER CORNERS,BETWEEN FR 11A AND FR 16A INCLUDED,TO LOVINCLUDING STRUTS ATTACHMENT LUGS, FRAMES ATTACHMENTS ALI REFERENCE:AT STG 44LH AND RH. 536235-01-3ACCESS: 121KF 121MF 121NF 121PF 121QF* 0.94122EF 122GF 122HF 122JF 122KF* 1.04536301-0606-1 100 LONGITUDINAL LAP JOINTS MEC GVI T: 33000 FC ALI EASA AD1 0.60 B2200 I: 3900 FC CN 2006-00711 0.60 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA ADFROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11TO 48000 FCNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0607-1 AND 536301-0608-1 536301-02-1NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0606-2 100 LONGITUDINAL LAP JOINTS MEC GVI T: 33000 FC ALI EASA AD1 0.60 B4-100200 I: 6400 FC CN 2006-00711 0.60 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA ADFROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11TO 40000 FCNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0607-2 AND 536301-0608-2 536301-01-2NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0606-3 100 LONGITUDINAL LAP JOINTS MEC GVI T: 33000 FC ALI EASA AD1 0.60 B4-200200 I: 2000 FC CN 2006-00711 0.60 C4GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA ADF4LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11POST 02611FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 132APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536301-0606-3 * * * * * C O N T I N U E * * * * *NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE: TO 34000 FC536301-0607-3 AND 536301-0608-3 536301-01-3NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0606-4 100 LONGITUDINAL LAP JOINTS MEC GVI I: 2000 FC ALI EASA AD1 0.60 B2200 CN 2006-00711 0.60 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA ADFROM 48000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11TO LOVNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0607-4 AND 536301-0608-4 536301-01-4NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0606-5 100 LONGITUDINAL LAP JOINTS MEC GVI I: 2000 FC ALI EASA AD1 0.60 B4-100200 CN 2006-00711 0.60 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA ADFROM 40000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11TO LOVNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0607-5 AND 536301-0608-5 536301-01-5NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0606-6 100 LONGITUDINAL LAP JOINTS MEC GVI I: 2000 FC ALI EASA AD1 0.60 B4-200200 CN 2006-00711 0.60 C4GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA ADF4LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11POST 02611FROM 34000 FCNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE: TO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 133APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536301-0606-6 * * * * * C O N T I N U E * * * * *536301-0607-6 AND 536301-0608-6 536301-01-6NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39ACCESS: 513AB 613AB* 0.58536301-0607-1 100 LONGITUDINAL LAP JOINTS MEC DET T: 33000 FC ALI CN 2006-0071(B) 1 0.30 B2200 I: 4700 FC CN FAA AD 96-13-11 1 0.30 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENCE: TO 48000 FC536301-02-1NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS536301-0606-1 AND 536301-0608-1NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0607-2 100 LONGITUDINAL LAP JOINTS MEC DET T: 33000 FC ALI CN 2006-0071(B) 1 0.30 B4-100200 I: 7000 FC CN FAA AD 96-13-11 1 0.30 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENCE: TO 40000 FC536301-02-2NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS536301-0606-2 AND 536301-0608-2NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0607-3 100 LONGITUDINAL LAP JOINTS MEC DET T: 33000 FC ALI CN 2006-0071(B) 1 0.30 B4-200200 I: 2900 FC CN FAA AD 96-13-11 1 0.30 C4DETAILED INSPECTION OF LOWER SKIN OF ALL FAA ADF4LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENCE: POST 02611536301-02-3FROM 0 FC/FHNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKSTO 34000 FC536301-0606-3 AND 536301-0608-3* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 134APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536301-0607-3 * * * * * C O N T I N U E * * * * *NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39ACCESS: 513AB 613AB* 0.58536301-0607-4 100 LONGITUDINAL LAP JOINTS MEC DET I: 2900 FC ALI CN 2006-0071(B) 1 0.30 B2200 CN FAA AD 96-13-11 1 0.30 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 48000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENCE: TO LOV536301-02-4NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS536301-0606-4 AND 536301-0608-4NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0607-5 100 LONGITUDINAL LAP JOINTS MEC DET I: 2900 FC ALI CN 2006-0071(B) 1 0.30 B4-100200 CN FAA AD 96-13-11 1 0.30 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 40000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENCE: TO LOV536301-02-5NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS536301-0606-5 AND 536301-0608-5NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0607-6 100 LONGITUDINAL LAP JOINTS MEC DET I: 2900 FC ALI CN 2006-0071(B) 1 0.30 B4-200200 CN FAA AD 96-13-11 1 0.30 C4DETAILED INSPECTION OF LOWER SKIN OF ALL FAA ADF4LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENCE: POST 02611536301-02-6FROM 34000 FCNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKSTO LOV536301-0606-6 AND 536301-0608-6* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 135APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536301-0607-6 * * * * * C O N T I N U E * * * * *NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39ACCESS: 513AB 613AB* 0.58536301-0608-1 100 LONGITUDINAL LAP JOINTS MEC SDI T: 33000 FC ALI NTM 5330021 3.30 B2200 I: 12900 FC CN PART 61 3.30 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13-11 TO 48000 FCNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0606-1 AND 536301-0607-1 536301-03-1NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0608-2 100 LONGITUDINAL LAP JOINTS MEC SDI T: 33000 FC ALI NTM 5330021 3.30 B4-100200 I: 8900 FC CN PART 61 3.30 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13-11 TO 40000 FCNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0606-2 AND 536301-0607-2 536301-03-2NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0608-3 100 LONGITUDINAL LAP JOINTS MEC SDI T: 33000 FC ALI NTM 5330021 3.30 B4-200200 I: 8900 FC CN PART 61 3.30 C4SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) F4LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13-11 POST 02611FROM 0 FC/FHNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE: TO 34000 FC536301-0606-3 AND 536301-0607-3 536301-03-3NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 136APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536301-0608-3 * * * * * C O N T I N U E * * * * *31; LH/RH BETWEEN FRAMES 38.1 AND 39ACCESS: 513AB 613AB* 0.58536301-0608-4 100 LONGITUDINAL LAP JOINTS MEC SDI I: 8900 FC ALI NTM 5330021 3.30 B2200 CN PART 61 3.30 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 48000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13-11 TO LOVNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0606-4 AND 536301-0607-4 536301-03-4NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0608-5 100 LONGITUDINAL LAP JOINTS MEC SDI I: 8900 FC ALI NTM 5330021 3.30 B4-100200 CN PART 61 3.30 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 40000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13-11 TO LOVNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE:536301-0606-5 AND 536301-0607-5 536301-03-5NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39:ACCESS: 513AB 613AB* 0.58536301-0608-6 100 LONGITUDINAL LAP JOINTS MEC SDI I: 8900 FC ALI NTM 5330021 3.30 B4-200200 CN PART 61 3.30 C4SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) F4LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13-11 POST 02611FROM 34000 FCNOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENCE: TO LOV536301-0606-6 AND 536301-0607-6 536301-03-6NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31; LH/RH BETWEEN FRAMES 38.1 AND 39* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 137APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536301-0608-6 * * * * * C O N T I N U E * * * * *ACCESS: 513AB 613AB* 0.58536311-0606-1 134 FWD CARGO DOOR LOCK FITTING MEC DET T: 32000 FC ALI CN 2006-0071(B) 1 1.00 B2I: 4200 FC FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF ATTACHMENT AREA OF LOCKTO 48000 FCFITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR POST ALI REFERENCE:02295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL AND 536311-01-1STRINGER 45 RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-4PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-2 134 FWD CARGO DOOR LOCK FITTING MEC DET T: 32000 FC ALI CN 2006-0071(B) 1 1.00 B4-100I: 5600 FC FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF ATTACHMENT AREA OF LOCKTO 40000 FCFITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR POST ALI REFERENCE:2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL AND 536311-01-2STRINGER 45 RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-5PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-3 134 FWD CARGO DOOR LOCK FITTING MEC DET T: 32000 FC ALI CN 2006-0071(B) 1 1.00 B4-200I: 3500 FC FAA AD 96-13-11 C4DETAILED INSPECTION OF ATTACHMENT AREA OF LOCKF4FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR POST ALI REFERENCE: FROM 0 FC/FH02295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL AND 536311-01-3TO 34000 FCSTRINGER 45 RH.NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-6PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 138APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536311-0606-3 * * * * * C O N T I N U E * * * * *(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-4 134 FWD CARGO DOOR LOCK FITTING NDT SDI T: 32000 FC ALI NTM 5313001 1.00 B2I: 8400 FC PART 6FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) TO 48000 FCLOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13-11POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILLAND STRINGER 45 RH. ALI REFERENCE:536311-02-1NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-1PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-5 134 FWD CARGO DOOR LOCK FITTING NDT SDI T: 32000 FC ALI NTM 5313001 1.00 B4-100I: 8000 FC PART 6FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) TO 40000 FCLOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13-11POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILLAND STRINGER 45 RH. ALI REFERENCE:536311-02-2NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-2PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-6 134 FWD CARGO DOOR LOCK FITTING NDT SDI T: 32000 FC ALI NTM 5313001 1.00 B4-200I: 7500 FC PART 6C4SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) F4LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13-11 FROM 0 FC/FHPOST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILLTO 34000 FCAND STRINGER 45 RH. ALI REFERENCE:536311-02-3NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-3* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 139APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536311-0606-6 * * * * * C O N T I N U E * * * * *PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-7 134 FWD CARGO DOOR LOCK FITTING NDT SDI I: 4800 FC ALI NTM 5313001 1.00 B2PART 6FROM 48000 FCSPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) TO LOVLOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13-11POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILLAND STRINGER 45 RH. ALI REFERENCE:536311-02-4PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-8 134 FWD CARGO DOOR LOCK FITTING NDT SDI I: 4800 FC ALI NTM 5313001 1.00 B4-100PART 6FROM 40000 FCSPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) TO LOVLOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13-11POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILLAND STRINGER 45 RH. ALI REFERENCE:536311-02-5PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)ACCESS: 132BF 132CF 811* 0.43536311-0606-9 134 FWD CARGO DOOR LOCK FITTING NDT SDI I: 4800 FC ALI NTM 5313001 1.00 B4-200PART 6C4SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) F4LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13-11 FROM 34000 FCPOST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILLTO LOVAND STRINGER 45 RH. ALI REFERENCE:536311-02-6PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(0,6 M/H)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 140APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536311-0606-9 * * * * * C O N T I N U E * * * * *ACCESS: 132BF 132CF 811* 0.43536355-0606-1 233 UDC CARGO DOOR HINGE FTG NDT SDI T: 12000 FC ALI NTM 5333001 2.00 F4NOTE 01 PART 6OR01. DETAILED (INTERNAL AND EXTERNAL) I: 11200 FC CN 2006-0071(B) C4INSPECTION OF HINGE FITTINGS FOR UPPER (MAIN) FAA AD 96-13-11 ORDECK CARGO DOOR, FROM FUSELAGE FRAME 20 TO 27,B4-2CINCLUDING SURROUNDING SKIN BETWEEN STR 4 AND 5 LH ALI REFERENCE: POST 06208536355-01-1IN CARGO CONFIG02. SPECIAL DETAILED INSPECTION OF UPPER BOLT ROW OF 536355-02-1FROM 0 FC/FHHINGE FITTINGS FOR UDC DOORTO LOVNOTE: ON A/C RETROFITTED TO C4 SERIES THE VALUEFOR INSPECTION THRESHOLD APPLIES FROM THETIME OF THE RETROFIT.PREP.: REMOVE/INSTALL LININGS AND INSULATION.REMOVE FASTENER (UPPER ROW) FROM UPPER HINGEFITTING.(6.0 M/H)ACCESS: 835* 0.05536355-0606-2 233 UDC CARGO DOOR HINGE FTG NDT SDI T: 12000 FC ALI NTM 5333001 2.00 C4NOTE 02. PART 6OR01. DETAILED INTERNAL AND EXTERNAL I: 11200 FC CN 2006-0071(B) B4-2CINSPECTION OF HINGE FITTINGS FOR UPPER (MAIN) FAA AD 96-13-11 POST 06208DECK CARGO DOOR, FROM FUSELAGE FRAME 20 TO 27,IN PAX CONFIGINCLUDING SURROUNDING SKIN BETWEEN STR 4 AND 5 LH ALI REFERENCE: FROM 0 FC/FH536355-01-1TO LOV02. SPECIAL DETAILED INSPECTION OF UPPER BOLT ROW OF 536355-02-1HINGE FITTINGS FOR UDC DOORNOTE: ON A/C RETROFITTED TO C4 SERIES THE QUOTEDVALUE FOR INSPECTION THRESHOLD APPLIESFROM THE TIME OF THE RETROFIT.PREP.: REMOVE/INSTALL FUSELAGE CEILING,LININGS, HATRACK AND INSULATION.REMOVE/INSTALL FASTENER (UPPER ROW) FROMUPPER HINGE FITTING.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 141APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536355-0606-2 * * * * * C O N T I N U E * * * * *(15.0 M/H)536359-0606-1 231 UDC DOOR LOCK FITTING MEC DET T: 13200 FC ALI CN 2006-0071(B) 1 1.00 F4I: 11200 FC FAA AD 96-13-11 POST 06208DETAILED INSPECTION OF UPPER (MAIN) DECK CARGOFROM 0 FC/FHDOOR LOCK FITTING LUGS AND ECCENTRIC BOLTS AT ALI REFERENCE: TO LOVFUSELAGE FRAMES 20B TO 26A (8 PLACES), LH. 536359-01-1PREP.: LINING REMOVED, ECCENTRIC BOLTS TO BE REMOVED.(4.0 M/H)ACCESS: 835* 0.05536359-0606-2 231 UDC DOOR LOCK FITTING MEC DET T: 13200 FC ALI CN 2006-0071(B) 1 1.00 C4I: 11200 FC FAA AD 96-13-11 ORDETAILED INSPECTION OF UPPER (MAIN) DECK CARGOB4-2CDOOR LOCK FITTING LUGS AND ECCENTRIC BOLTS AT ALI REFERENCE: POST 06208FUSELAGE FRAME 20B TO 26A,(8 PLACES), LH. 536359-01-1FROM 0 FC/FHTO LOVPREP.: 01. PASSENGER CONFIGURATION:REMOVE/INSTALL HATRACKS, FUSELAGELINING, CEILING AND INSULATION.02. ECCENTRIC BOLTS TO BE REMOVED.(4.0 M/H)ACCESS: 835* 0.05536365-0606-1 121 LONGITUDINAL BUTT JOINTS NDT SDI T: 22000 FC ALI NTM 5330011 7.00 C4131 I: 6100 FC PART 61 7.00 POST 02611230 SPECIAL DETAILED INSPECTION OF LONGITUDINAL BUTT CN 2006-0071(B) 1 7.00 FROM 0 FC/FH232 JOINTS BETWEEN FRAMES 18 AND 33 (IN THE FOLLOWING FAA AD 96-13-11 1 7.00 TO 34000 FC233 AREAS:) 01. BUTT JOINT BETWEEN STR 3 AND 4 FROM FRAME1 7.0029 TO 33, LH ALI REFERENCE:02. BUTT JOINT BETWEEN STR 8 AND 10 FROM FRAME 536365-01-118 TO 29, RH03. BUTT JOINT BETWEEN STR 34 AND 35 FROM FRAME18 TO 30, LHNOTE: REMOVE/INSTALL UPPER DECK CARGO COMPARTMENTSEALING PANELS, FORWARD COMPARTMENT SIDEWALL* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 142APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536365-0606-1 * * * * * C O N T I N U E * * * * *PANELS, INSULATION.536365-0606-2 121 LONGITUDINAL BUTT JOINTS NDT SDI I: 5800 FC ALI NTM 5330011 7.00 C4131 PART 61 7.00 POST 02611230 SPECIAL DETAILED INSPECTION OF LONGITUDINAL BUTT CN 2006-0071(B) 1 7.00 FROM 34000 FC232 JOINTS BETWEEN FRAMES 18 AND 33 (IN THE FOLLOWING FAA AD 96-13-11 1 7.00 TO LOV233 AREAS:) 01. BUTT JOINT BETWEEN STR 3 AND 4 FROM FRAME1 7.0029 TO 33, LH ALI REFERENCE:02. BUTT JOINT BETWEEN STR 8 AND 10 FROM FRAME 536365-01-218 TO 29, RH03. BUTT JOINT BETWEEN STR 34 AND 35 FROM FRAME18 TO 30, LHNOTE: REMOVE/INSTALL UPPER DECK CARGO COMPARTMENTSEALING PANELS, FORWARD COMPARTMENT SIDEWALLPANELS, INSULATION.536367-0606-1 121 LONGITUDINAL BUTT JOINT MEC GVI T: 33000 FC ALI CN 2006-0071(B) 1 0.80 C4131 I: 2400 FC FAA AD 96-13-11 1 0.80 F4GENERAL VISUAL INSPECTION OF SKIN AT LONGITUDINALB4-2CBUTT JOINT AREA AT STR 35 FROM FRAME 18 TO 30, LH ALI REFERENCE: POST 6208536367-01-1FROM 0 FC/FHNOTE : THIS TASK HAS TO BE DONE AS THE SAME TIME ASTO LOWTASK 536367-0606-2536367-0606-2 121 LONGITUDINAL BUTT JOINT MEC DET T: 33000 FC ALI CN 2006-0071(B) 1 0.50 C4131 I: 11000 FC FAA AD 96-13-11 1 0.50 F4DETAILED INSPECTION OF LONGITUDINAL BUTTB4-2CJOINT (AREA) AT STR 35 BETWEEN (FROM) FRAME 18 TO ALI REFERENCE: POST 620830 LH 536367-02-1FROM 0 FC/FHTO LOWNOTE : THIS TASK HAS TO BE DONE AS THE SAME TIME ASTASK 536367-0606-1536369-0606-1 200 UPPER HALF OF FUSELAGE MEC GVI T: 20000 FC ALI CN 2006-0071(B) 1 TBD ALLI: 5000 FC FAA AD 96-13-11 FROM 0 FC/FHGENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALTO LOVSURFACE - UPPER HALF OF FUSELAGE - SECTION 13 TO 18 ALI REFERENCE:(FR 18 TO 80), FROM STR 26 (LH,RH) TO CROWN CENTER 536369-01-1* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 143APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536369-0606-1 * * * * * C O N T I N U E * * * * *LINE536403-0606-1 231 FUSELAGE FRAME 28A AND 30A MEC DET T: 28000 FC ALI CN 2006-0071(B) 1 1.50 B2232 I: 9300 FC FAA AD 96-13-11 1 1.50 FROM 0 FC/FH233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A1 1.50 TO 48000 FC234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENCE: 1 1.50241 SUPPORT 536403-01-11 1.50242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE1 1.50EACH FRAME), LH/RH.PREP.: REMOVE/INSTALL HATRACK, LINING AND INSULATION.(12.0 M/H)536403-0606-2 231 FUSELAGE FRAME 28A AND 30A MEC DET T: 28000 FC ALI CN 2006-0071(B) 1 1.50 B4-100232 I: 10100 FC FAA AD 96-13-11 1 1.50 FROM 0 FC/FH233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A1 1.50 TO 40000 FC234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENCE: 1 1.50241 SUPPORT 536403-01-21 1.50242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE1 1.50EACH FRAME), LH/RH.PREP.: REMOVE/INSTALL HATRACK, LINING AND INSULATION.(12.0 M/H)536403-0606-3 231 FUSELAGE FRAME 28A AND 30A MEC DET T: 28000 FC ALI CN 2006-0071(B) 1 1.50 B4-200232 I: 9200 FC FAA AD 96-13-11 1 1.50 C4233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A1 1.50 F4234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENCE: 1 1.50 FROM 0 FC/FH241 SUPPORT 536403-01-31 1.50 TO 34000 FC242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE1 1.50EACH FRAME), LH/RH.PREP.: REMOVE/INSTALL HATRACK, LINING AND INSULATION.(12.0 M/H)536403-0606-4 231 FUSELAGE FRAME 28A AND 30A MEC DET I: 6000 FC ALI CN 2006-0071(B) 1 1.50 B2232 FAA AD 96-13-11 1 1.50 FROM 48000 FC233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A1 1.50 TO LOV234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENCE: 1 1.50* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 144APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536403-0606-4 * * * * * C O N T I N U E * * * * *241 SUPPORT 536403-01-41 1.50242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE1 1.50EACH FRAME), LH/RH.PREP.: REMOVE/INSTALL HATRACK, LINING AND INSULATION.(12.0 M/H)536403-0606-5 231 FUSELAGE FRAME 28A AND 30A MEC DET I: 6000 FC ALI CN 2006-0071(B) 1 1.50 B4-100232 FAA AD 96-13-11 1 1.50 FROM 40000 FC233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A1 1.50 TO LOV234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENCE: 1 1.50241 SUPPORT 536403-01-51 1.50242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE1 1.50EACH FRAME), LH/RH.PREP.: REMOVE/INSTALL HATRACK, LINING AND INSULATION.(12.0 M/H)536403-0606-6 231 FUSELAGE FRAME 28A AND 30A MEC DET I: 6000 FC ALI CN 2006-0071(B) 1 1.50 B4-200232 FAA AD 96-13-11 1 1.50 C4233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A1 1.50 F4234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENCE: 1 1.50 FROM 34000 FC241 SUPPORT 536403-01-61 1.50 TO LOV242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE1 1.50EACH FRAME), LH/RH.PREP.: REMOVE/INSTALL HATRACK, LINING AND INSULATION.(12.0 M/H)536405-0606-1 233 PASSENGER DOOR FRAME MEC DET T: 28000 FC ALI EASA AD1 1.50 B2234 I: 9300 FC FAA AD 2006-00711 1.50 FROM 0 FC/FH243 DETAILED INSPECTION OF PASSENGER DOOR FRAME FAA AD1 1.50 TO 48000 FC244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2007-04-111 1.50NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-4 ALI REFERENCE:536405-01-1PREP.: REMOVE/INSTALL CABIN SIDE LINING ANDINSULATION. (2.5 M/H)STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 145APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536405-0606-2 233 PASSENGER DOOR FRAME MEC DET T: 28000 FC ALI EASA AD1 1.50 B4-100234 I: 10100 FC FAA AD 2006-00711 1.50 FROM 0 FC/FH243 DETAILED INSPECTION OF PASSENGER DOOR FRAME FAA AD1 1.50 TO 40000 FC244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2007-04-111 1.50NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-5 ALI REFERENCE:536405-01-2PREP.: REMOVE/INSTALL CABIN SIDE LINING ANDINSULATION. (2.5 M/H)536405-0606-3 233 PASSENGER DOOR FRAME MEC DET I: 10100 FC ALI EASA AD1 1.50 B4-200234 EASA AD 2006-00711 1.50 C4243 DETAILED INSPECTION OF PASSENGER DOOR FRAME FAA AD FAA AD1 1.50 F4244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2007-04-111 1.50 FROM 0 FC/FHTO 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-6 ALI REFERENCE:536405-01-2PREP.: REMOVE/INSTALL CABIN SIDE LINING ANDINSULATION.536405-0606-4 233 PASSENGER DOOR FRAME NDT SDI T: 28000 FC ALI NTM 5314131 1.50 B2234 I: 10200 FC FAA AD PART 61 1.50 FROM 0 FC/FH243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD1 1.50 TO 48000 FC244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-00711 1.50FAA ADNOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-1 2007-04-11PREP.: REMOVE/INSTALL CABIN SIDE LINING AND ALI REFERENCE:INSULATION. (2.5 M/H) 536405-02-1536405-0606-5 233 PASSENGER DOOR FRAME NDT SDI T: 28000 FC ALI NTM 5314131 1.50 B4-100234 I: 11100 FC FAA AD PART 61 1.50 FROM 0 FC/FH243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD1 1.50 TO 40000 FC244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-00711 1.50FAA ADNOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-2 2007-04-11PREP.: REMOVE/INSTALL CABIN SIDE LINING AND ALI REFERENCE:INSULATION. (2.5 M/H) 536405-02-6STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 146APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536405-0606-6 233 PASSENGER DOOR FRAME NDT SDI T: 28000 FC ALI NTM 5314131 1.50 B4-200234 I: 11100 FC FAA AD PART 61 1.50 C4243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD1 1.50 F4244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-00711 1.50 FROM 0 FC/FHFAA ADTO 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-3 2007-04-11PREP.: REMOVE/INSTALL CABIN SIDE LINING AND ALI REFERENCE:INSULATION. (2.5 M/H) 536405-02-2536405-0606-7 233 PASSENGER DOOR FRAME NDT SDI I: 7000 FC ALI NTM 5314131 1.50 B2234 FAA AD PART 61 1.50 POST 00751243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD1 1.50 (53-0247)244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-00711 1.50 FROM 48000 FCFAA ADTO LOVPREP.: REMOVE/INSTALL CABIN SIDE LINING AND 2007-04-11INSULATION. (2.5 M/H)ALI REFERENCE:536405-02-3536405-0606-8 233 PASSENGER DOOR FRAME NDT SDI I: 7000 FC ALI NTM 5314131 1.50 B4-100234 FAA AD PART 61 1.50 POST 00751243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD1 1.50 (53-0247)244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-00711 1.50 FROM 40000 FCFAA ADTO LOVPREP.: REMOVE/INSTALL CABIN SIDE LINING AND 2007-04-11INSULATION. (2.5 M/H)ALI REFERENCE:536405-02-4536405-0606-9 233 PASSENGER DOOR FRAME NDT SDI I: 7000 FC ALI NTM 5314131 1.50 B4-200234 FAA AD PART 61 1.50 C4243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD1 1.50 F4244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-00711 1.50 POST 00751FAA AD(53-0247)PREP.: REMOVE/INSTALL CABIN SIDE LINING AND 2007-04-11FROM 34000 FCINSULATION. (2.5 M/H)TO LOVALI REFERENCE:536405-02-5STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 147APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536407-0606-1 131 PASSENGER DOOR CUT-OUT MEC DET T: 31000 FC ALI CN 2006-0071(B) 1 0.50 B2132 I: 2000 FC FAA AD 96-13-11 1 0.50 FROM 0 FC/FH233 DETAILED (INTERNAL AND EXTERNAL) INSPECTION1 0.50 TO 48000 FC234 OF PASSENGER DOOR CUT OUT REINFORCEMENT BETWEEN ALI REFERENCE: 1 0.50243 FRAMES 30 AND 30A AND BETWEEN STRINGERS 27 AND 536407-01-11 0.50244 28, LH/RH.1 0.50NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-3PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION.(1.3 M/H)536407-0606-2 131 PASSENGER DOOR CUT-OUT MEC DET T: 31000 FC ALI CN 2006-0071(B) 1 0.50 B4-100132 I: 2400 FC FAA AD 96-13-11 1 0.50 FROM 0 FC/FH233 DETAILED (INTERNAL AND EXTERNAL) INSPECTION1 0.50 TO 40000 FC234 OF PASSENGER DOOR CUT OUT REINFORCEMENT BETWEEN ALI REFERENCE: 1 0.50243 FRAMES 30 AND 30A AND BETWEEN STRINGERS 27 AND 536407-01-21 0.50244 28, LH/RH.1 0.50NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536407-0606-4PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION.(1.3 M/H)536407-0606-3 131 PASSENGER DOOR CUT-OUT NDT SDI T: 31000 FC ALI NTM 5314011 0.50 B2132 I: 4100 FC PART 61 0.50 FROM 0 FC/FH233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071(B) 1 0.50 TO 48000 FC234 REINFORCEMENT BETWEEN FRAMES 30 AND 30A AND BETWEEN FAA AD 96-13-11 1 0.50243 STRINGERS 27 AND 28, LH/RH.1 0.50244 ALI REFERENCE: 1 0.50NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-1 536407-02-1PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION.(1.3 M/H)536407-0606-4 131 PASSENGER DOOR CUT-OUT NDT SDI T: 31000 FC ALI NTM 5314011 0.50 B4-100132 I: 4800 FC PART 61 0.50 FROM 0 FC/FH233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071(B) 1 0.50 TO 40000 FC234 REINFORCEMENT BETWEEN FRAMES 30 AND 30A AND BETWEEN FAA AD 96-13-11 1 0.50243 STRINGERS 27 AND 28, LH/RH.1 0.50244 ALI REFERENCE: 1 0.50NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-2 536407-02-2* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 148APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536407-0606-4 * * * * * C O N T I N U E * * * * *PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION.(1.3 M/H)536407-0606-5 131 PASSENGER DOOR CUT-OUT MEC DET T: 31000 FC ALI CN 2006-0071(B) 1 0.50 B4-200132 I: 3000 FC FAA AD 96-13-11 1 0.50 C4233 DETAILED INTERNAL AND EXTERNAL INSPECTION OF1 0.50 F4234 PASSENGER DOOR CUT OUT REINFORCEMENT BETWEEN FRAME ALI REFERENCE: 1 0.50 FROM 0 FC/FH243 30 AND FRAME 30A AND BETWEEN STRINGER 27 AND 536407-01-31 0.50 TO 34000 FC244 STRINGER 28, LH/RH.1 0.50NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-6PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION.(1.3 M/H)536407-0606-6 131 PASSENGER DOOR CUT-OUT NDT SDI T: 31000 FC ALI NTM 5314011 0.50 B4-200132 I: 3100 FC PART 61 0.50 C4233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071(B) 1 0.50 F4234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13-11 1 0.50 FROM 0 FC/FH243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.1 0.50 TO 34000 FC244 ALI REFERENCE: 1 0.50536407-02-3NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-5PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION.(1.3 M/H)536407-0606-7 131 PASSENGER DOOR CUT-OUT NDT SDI I: 3000 FC ALI NTM 5314011 0.50 B2132 PART 61 0.50 FROM 48000 FC233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071(B) 1 0.50 TO LOV234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13-11 1 0.50243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.1 0.50244 ALI REFERENCE: 1 0.50PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION. 536407-02-4(1.3 M/H)536407-0606-8 131 PASSENGER DOOR CUT-OUT NDT SDI I: 3000 FC ALI NTM 5314011 0.50 B4-100132 PART 61 0.50 FROM 40000 FC* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 149APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536407-0606-8 * * * * * C O N T I N U E * * * * *233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071(B) 1 0.50 TO LOV234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13-11 1 0.50243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.1 0.50244 ALI REFERENCE: 1 0.50PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION. 536407-02-5(1.3 M/H)536407-0606-9 131 PASSENGER DOOR CUT-OUT NDT SDI I: 3000 FC ALI NTM 5314011 0.50 B4-200132 PART 61 0.50 C4233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071(B) 1 0.50 F4234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13-11 1 0.50 FROM 34000 FC243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.1 0.50 TO LOV244 ALI REFERENCE: 1 0.50PREP.: REMOVE/INSTALL SIDE LINING AND INSULATION. 536407-02-6(1.3 M/H)536415-0606-1 131 FUSELAGE INTERNAL STRUCTURE MEC DET T: 28000 FC ALI CN 2006-0071(B) 1 1.00 B2132 I: 9300 FC FAA AD 96-13-11 1 1.00 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE INTERNALTO 48000 FCSTRUCTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENCE:FRAMES 27 AND 32 AND BETWEEN STRINGERS 26 AND 31, 536415-01-1LH/RH.PREP.: REMOVE/INSTALL CARGO COMPARTMENT LINING ANDINSULATION. (1.3 M/H)536415-0606-2 131 FUSELAGE INTERNAL STRUCTURE MEC DET T: 28000 FC ALI CN 2006-0071(B) 1 1.00 B4-100132 I: 10100 FC FAA AD 96-13-11 1 1.00 FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE INTERNALTO 40000 FCSTRUCTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENCE:FRAMES 27 AND 32 AND BETWEEN STRINGERS 26 AND 31, 536415-01-2LH/RH.PREP.: REMOVE/INSTALL CARGO COMPARTMENT LINING ANDINSULATION. (1.3 M/H)536415-0606-3 131 FUSELAGE INTERNAL STRUCTURE MEC DET T: 28000 FC ALI CN 2006-0071(B) 1 1.00 B4-200132 I: 9500 FC FAA AD 96-13-11 1 1.00 C4DETAILED INSPECTION OF FUSELAGE INTERNALF4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 150APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536415-0606-3 * * * * * C O N T I N U E * * * * *STRUKTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENCE: FROM 0 FC/FHFRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-3TO 34000 FCSTRINGER 31, LH/RH.PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING ANDINSULATION. (1.3 M/H)536415-0606-4 131 FUSELAGE INTERNAL STRUCTURE MEC DET I: 6000 FC ALI CN 2006-0071(B) 1 1.00 B2132 FAA AD 96-13-11 1 1.00 FROM 48000 FCDETAILED INSPECTION OF FUSELAGE INTERNALTO LOVSTRUKTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENCE:FRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-4STRINGER 31, LH/RH.PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING ANDINSULATION. (1.3 M/H)536415-0606-5 131 FUSELAGE INTERNAL STRUCTURE MEC DET I: 6000 FC ALI CN 2006-0071(B) 1 1.00 B4-100132 FAA AD 96-13-11 1 1.00 FROM 40000 FCDETAILED INSPECTION OF FUSELAGE INTERNALTO LOVSTRUKTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENCE:FRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-5STRINGER 31, LH/RH.PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING ANDINSULATION. (1.3 M/H)536415-0606-6 131 FUSELAGE INTERNAL STRUCTURE MEC DET I: 6000 FC ALI CN 2006-0071(B) 1 1.00 B4-200132 FAA AD 96-13-11 1 1.00 C4DETAILED INSPECTION OF FUSELAGE INTERNALF4STRUKTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENCE: FROM 34000 FCFRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-6TO LOVSTRINGER 31, LH/RH.PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING ANDINSULATION. (1.3 M/H)536421-0606-1 230 MID PASSENGER DOOR PANEL MEC DET T: 40000 FC ALI CN 2006-0071(B) 1 1.00 B4-100I: 12000 FC CN FAA AD 96-13-11 FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 151APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536421-0606-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF SECTION 14, MID FAA AD ALI REFERENCE: TO LOVPASSENGER DOOR PANEL AT RUN-OUT OF FRAME PROFILE AT 536421-01-1STRINGER 12, FRAME 29 AND FRAME 30, LH/RH.PREP.: REMOVE LININGS, CEILING, HATRACKS ANDINSULATION.536421-0606-2 230 MID PASSENGER DOOR PANEL MEC DET T: 34000 FC ALI CN 2006-0071(B) 1 1.00 B4-200I: 12000 FC CN FAA AD 96-13-11 C4DETAILED INSPECTION OF SECTION 14, MID FAA ADF4PASSENGER DOOR PANEL AT RUN-OUT OF FRAME PROFILE AT ALI REFERENCE: FROM 0 FC/FHSTRINGER 12, FRAME 29 AND FRAME 30, LH/RH. 536421-01-2TO LOVPREP.: FOR CARGO CONFIGURATION REMOVE LINING ANDINSULATION.FOR PASSENGER COFIGURATION REMOVE LINING,CEILING, HATRACKS AND INSULATION.536502-0603-1 100 LONGITUDINAL LAP JOINTS MEC GVI T: 32000 FC ALI CN 2006-0071(B) 1 3.00 B2200 I: 2500 FC CN FAA AD 96-13-11 1 3.00 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENCE: TO 48000 FCEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-1NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0604-1 AND 536502-0605-1N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0603-2 100 LONGITUDINAL LAP JOINTS MEC GVI T: 32000 FC ALI CN 2006-0071(B) 1 3.00 B4-100200 I: 4300 FC CN FAA AD 96-13-11 1 3.00 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENCE: TO 40000 FCEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-2* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 152APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0603-2 * * * * * C O N T I N U E * * * * *NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0604-2 AND 536502-0605-2N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0603-3 100 LONGITUDINAL LAP JOINTS MEC GVI T: 32000 FC ALI CN 2006-0071(B) 1 3.00 B4-200200 I: 2000 FC CN FAA AD 96-13-11 1 3.00 C4GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA ADF4LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENCE: POST 02611EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-3FROM 0 FC/FHTO 34000FCNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0604-3 AND 536502-0605-3N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0603-4 100 LONGITUDINAL LAP JOINTS MEC GVI I: 1900 FC ALI CN 2006-0071(B) 1 3.00 B2200 CN FAA AD 96-13-11 1 3.00 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 48000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENCE: TO LOVEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-4NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0604-4 AND 536502-0605-4N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 153APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0603-4 * * * * * C O N T I N U E * * * * *ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0603-5 100 LONGITUDINAL LAP JOINTS MEC GVI I: 1900 FC ALI CN 2006-0071(B) 1 3.00 B4-100200 CN FAA AD 96-13-11 1 3.00 POST 02611GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA ADFROM 40000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENCE: TO LOVEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-5NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0604-5 AND 536502-0605-5N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0603-6 100 LONGITUDINAL LAP JOINTS MEC GVI I: 1900 FC ALI CN 2006-0071(B) 1 3.00 B4-200200 CN FAA AD 96-13-11 1 3.00 C4GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA ADF4LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENCE: POST 02611EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-6FROM 34000 FCTO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0604-6 AND 536502-0605-6N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0604-1 100 LONGITUDINAL LAP JOINTS MEC DET T: 32000 FC ALI CN 2006-0071(B) 1 3.00 B2200 I: 3400 FC CN FAA AD 96-13-11 1 3.00 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA ADFROM 0 FC/FHLAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENCE: TO 48000 FCLAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-1* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 154APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0604-1 * * * * * C O N T I N U E * * * * *NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0603-1 AND 536502-0605-1N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0604-2 100 LONGITUDINAL LAP JOINTS MEC DET T: 32000 FC ALI CN 2006-0071(B) 1 3.00 B4-100200 I: 5400 FC CN FAA AD 96-13-11 1 3.00 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA ADFROM 0 FC/FHLAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENCE: TO 40000 FCLAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-2NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0603-2 AND 536502-0605-2N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0604-3 100 LONGITUDINAL LAP JOINTS MEC DET T: 32000 FC ALI CN 2006-0071(B) 1 3.00 B4-200200 I: 2300 FC CN FAA AD 96-13-11 1 3.00 C4DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA ADF4LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENCE: POST 02611LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-3FROM 0 FC/FHTO 34000FCNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0603-3 AND 536502-0605-3N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 155APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0604-4 100 LONGITUDINAL LAP JOINTS MEC DET I: 2300 FC ALI CN 2006-0071(B) 1 3.00 B2200 CN FAA AD 96-13-11 1 3.00 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA ADFROM 48000 FCLAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENCE: TO LOVLAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-4NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0603-4 AND 536502-0605-4N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0604-5 100 LONGITUDINAL LAP JOINTS MEC DET I: 2300 FC ALI CN 2006-0071(B) 1 3.00 B4-100200 CN FAA AD 96-13-11 1 3.00 POST 02611DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA ADFROM 40000 FCLAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENCE: TO LOVLAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-5NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0603-5 AND 536502-0605-5N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0604-6 100 LONGITUDINAL LAP JOINTS MEC DET I: 2300 FC ALI CN 2006-0071(B) 1 3.00 B4-200200 CN FAA AD 96-13-11 1 3.00 C4DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA ADF4LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENCE: POST 02611LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-6FROM 34000 FCTO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS536502-0603-6 AND 536502-0605-6N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 156APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0604-6 * * * * * C O N T I N U E * * * * *PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0605-1 100 LONGITUDINAL LAP JOINTS NDT SDI T: 32000 FC ALI NTM 5330041 3.00 B2200 I: 12800 FC CN PART 61 3.00 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13-11 TO 48000 FCEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.ALI REFERENCE:NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-1536502-0603-1 AND 536502-0604-1N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0605-2 100 LONGITUDINAL LAP JOINTS NDT SDI T: 32000 FC ALI NTM 5330041 3.00 B4-100200 I: 8900 FC CN PART 61 3.00 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 0 FC/FHLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13-11 TO 40000 FCEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.ALI REFERENCE:NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-2536502-0603-2 AND 536502-0604-2N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0605-3 100 LONGITUDINAL LAP JOINTS NDT SDI T: 32000 FC ALI NTM 5330041 3.00 B4-200200 I: 8900 FC CN PART 61 3.00 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 157APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0605-3 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) F4LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13-11 POST 02611EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.FROM 0 FC/FHALI REFERENCE: TO 34000FCNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-3536502-0603-3 AND 536502-0604-3N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0605-4 100 LONGITUDINAL LAP JOINTS NDT SDI I: 8900 FC ALI NTM 5330041 3.00 B2200 CN PART 61 3.00 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 48000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13-11 TO LOVEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.ALI REFERENCE:NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-4536502-0603-4 AND 536502-0604-4N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0605-5 100 LONGITUDINAL LAP JOINTS NDT SDI I: 8900 FC ALI NTM 5330041 3.00 B4-100200 CN PART 61 3.00 POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) FROM 40000 FCLONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13-11 TO LOVEXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.ALI REFERENCE:NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-5536502-0603-5 AND 536502-0604-5N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 158APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0605-5 * * * * * C O N T I N U E * * * * *PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0605-6 100 LONGITUDINAL LAP JOINTS NDT SDI I: 8900 FC ALI NTM 5330041 3.00 B4-200200 CN PART 61 3.00 C4SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071(B) F4LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13-11 POST 02611EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.FROM 34000 FCALI REFERENCE: TO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-6536502-0603-6 AND 536502-0604-6N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31LH/RH BETWEEN FRAME 54 AND FRAME 55.ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0606-1 100 LONGITUDINAL LAP JOINTS NDT SDI T: 28000 FC ALI NTM 5330041 3.00 B2I: 9000 FC CN PART 6POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071(B) FROM 0 FC/FHLONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13-11 TO 48000 FCLH/RH.ALI REFERENCE:PREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-1NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0606-2 100 LAP JOINT AT STRINGER 52 NDT SDI T: 28000 FC ALI NTM 5330041 2.50 B4-100I: 10200 FC CN PART 6POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071(B) FROM 0 FC/FHLONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13-11 TO 40000 FC* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 159APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0606-2 * * * * * C O N T I N U E * * * * *LH/RH. ALI REFERENCE:536502-04-2PREP.: REMOVE FLOOR PANELS AND INSULATION.NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55536502-0606-3 100 LONGITUDINAL LAP JOINTS NDT SDI T: 28000 FC ALI NTM 5330041 3.00 B4-200I: 6500 FC CN PART 6C4SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071(B) F4LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13-11 POST 02611LH/RH.FROM 0 FC/FHALI REFERENCE: TO 34000FCPREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-3NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0606-4 100 LONGITUDINAL LAP JOINTS NDT SDI I: 6500 FC ALI NTM 5330041 3.00 B2CN PART 6POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071(B) FROM 48000 FCLONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13-11 TO LOVLH/RH.ALI REFERENCE:PREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-4NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0606-5 100 LONGITUDINAL LAP JOINTS NDT SDI I: 6500 FC ALI NTM 5330041 3.00 B4-100CN PART 6POST 02611SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071(B) FROM 40000 FCLONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13-11 TO LOVLH/RH.ALI REFERENCE:PREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-5* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 160APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536502-0606-5 * * * * * C O N T I N U E * * * * *NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55ACCESS: 577ET 577GT 677ET 677GT* 2.60536502-0606-6 100 LONGITUDINAL LAP JOINTS NDT SDI I: 6500 FC ALI NTM 5330041 3.00 B4-200CN PART 6C4SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071(B) F4LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13-11 POST 02611LH/RH.FROM 34000 FCALI REFERENCE: TO LOVPREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-6NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER31, LH/RH BETWEEN FRAMES 54 AND 55ACCESS: 577ET 577GT 677ET 677GT* 2.60536503-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI ST: 25000 FC ALI NTM 5315131 1.00 B2142 OR CN PART 41 1.00 POST 01669SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 27700 FH FAA AD CN 2006-0071(B) RETROFITREAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 3300 FC FAA AD 96-13-11 (53-0061)STIFFENERS NO. 1, 2 AND 4, LH/RH. ORFROM 0 FC/FH3700 FH ALI REFERENCE: TO 48000 FCNOTE:THRESHOLD SARTS COUNTING FROM ENTRY INTO SERVICE 536503-01-1ACCESS: 147AZ* 0.23148AZ* 0.23536503-0606-2 141 CENTER WING BOX REAR SPAR NDT SDI ST: 25000 FC ALI NTM 5315131 1.00 B2142 OR CN PART 41 1.00 POST 01669SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 27700 FH FAA AD CN 2006-0071(B) SERIALREAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 3300 FC FAA AD 96-13-11 FROM 0 FC/FHSTIFFENERS NO. 1, 2 AND 4, LH/RH. ORTO 48000 FC3900 FH ALI REFERENCE:ACCESS: 147AZ 536503-01-2* 0.23148AZ* 0.23STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 161APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536503-0606-3 141 CENTER WING BOX REAR SPAR NDT SDI ST: 29000 FC ALI NTM 5315131 1.00 B4-100142 OR CN PART 41 1.00 POST 01669SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 39100 FH FAA AD CN 2006-0071(B) RETROFITREAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 6400 FC FAA AD 96-13-11 (53-0061)STIFFENERS NO. 1, 2 AND 4, LH/RH. ORFROM 0 FC/FH8600 FH ALI REFERENCE: TO 40000 FCNOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-4SERVICEACCESS: 147AZ* 0.23148AZ* 0.23536503-0606-4 141 CENTER WING BOX REAR SPAR NDT SDI ST: 30000 FC ALI NTM 5315131 1.00 B4-100142 OR CN PART 41 1.00 POST 01669SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 40500 FH FAA AD CN 2006-0071(B) SERIALSPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS SI: 6800 FC FAA AD 96-13-11 PRE 02626NO. 1, 2 AND 4, LH/RH. ORFROM 0 FC/FH9200 FH ALI REFERENCE: TO 40000 FCACCESS: 147AZ 536503-01-5* 0.23148AZ* 0.23536503-0606-5 141 CENTER WING BOX REAR SPAR NDT SDI ST: 24000 FC ALI NTM 5315131 1.00 B4-200142 OR CN PART 41 1.00 C4SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 49200 FH FAA AD CN 2006-0071(B) F4REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 4200 FC FAA AD 96-13-11 POST 01669STIFFENERS NO. 1, 2 AND 4, LH/RH. ORRETROFIT8600 FH ALI REFERENCE: (53-0061)NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-9FROM 0 FC/FHSEVICETO 34000 FCACCESS: 147AZ* 0.23148AZ* 0.23536503-0606-6 141 CENTER WING BOX REAR SPAR NDT SDI ST: 25000 FC ALI NTM 5315131 1.00 B4-200142 OR CN PART 41 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 51200 FH FAA AD CN 2006-0071(B) F4SPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS SI: 4800 FC FAA AD 96-13-11 POST 01669NO. 1, 2 AND 4, LH/RH. ORSERIAL9800 FH ALI REFERENCE: PRE 02626ACCESS: 147AZ 536503-01-10* 0.23 FROM 0 FC/FH148AZ* 0.23 TO 34000 FCSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 162APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536503-0606-7 141 CENTER WING BOX REAR SPAR NDT SDI I: 2700 FC ALI NTM 5315131 1.00 B2142 OR CN PART 41 1.00 FROM 48000 FCSPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 3000 FH FAA AD CN 2006-0071(B) TO LOVREAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13-11STIFFENERS NO. 1, 2 AND 4, LH/RH.ALI REFERENCE:ACCESS: 147AZ 536503-01-3* 0.23148AZ* 0.23536503-0606-8 141 CENTER WING BOX REAR SPAR NDT SDI I: 2900 FC ALI NTM 5315131 1.00 B4-100142 OR CN PART 41 1.00 POST 02626SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 3900 FH FAA AD CN 2006-0071(B) FROM 40000 FCSPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS FAA AD 96-13-11 TO LOVNO. 1, 2 AND 4, LH/RH.ALI REFERENCE:ACCESS: 147AZ 536503-01-6* 0.23148AZ* 0.23536503-0606-9 141 CENTER WING BOX REAR SPAR NDT SDI I: 3300 FC ALI NTM 5315131 1.00 B4-100142 OR CN PART 41 1.00 POST 01669SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 4450 FH FAA AD CN 2006-0071(B) SERIALSPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS FAA AD 96-13-11 PRE 02626NO. 1, 2 AND 4, LH/RH.FROM 40000 FCALI REFERENCE: TO LOVACCESS: 147AZ 536503-01-7* 0.23148AZ* 0.23536503-0607-1 141 CENTER WING BOX REAR SPAR NDT SDI I: 3300 FC ALI NTM 5315131 1.00 B4-100142 OR CN PART 41 1.00 POST 01669SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 4450 FH FAA AD CN 2006-0071(B) RETROFITREAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13-11 (53-0061)STIFFENERS NO. 1, 2 AND 4, LH/RH.FROM 40000 FCALI REFERENCE: TO LOVNOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-8SERVICEACCESS: 147AZ* 0.23148AZ* 0.23536503-0607-2 141 CENTER WING BOX REAR SPAR NDT SDI I: 2400 FC ALI NTM 5315131 1.00 B4-200142 OR CN PART 41 1.00 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 163APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536503-0607-2 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 4900 FH FAA AD CN 2006-0071(B) F4REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13-11 POST 01669STIFFENERS NO. 1, 2 AND 4, LH/RH.RETROFITALI REFERENCE: (53-0061)NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-11FROM 34000 FCSERVICETO LOVACCESS: 147AZ* 0.23148AZ* 0.23536503-0607-3 141 CENTER WING BOX REAR SPAR NDT SDI I: 2400 FC ALI NTM 5315131 1.00 B4-200142 OR CN PART 41 1.00 C4SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 4900 FH FAA AD CN 2006-0071(B) F4REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13-11 POST 01669STIFFENERS NO. 1, 2 AND 4, LH/RH.SERIALALI REFERENCE: PRE 02626NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-12FROM 34000 FCSERVICETO LOVACCESS: 147AZ* 0.23148AZ* 0.23536503-0607-4 141 CENTER WING BOX REAR SPAR NDT SDI I: 2100 FC ALI NTM 5315131 1.00 B4-200142 OR CN PART 41 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 4300 FH FAA AD CN 2006-0071(B) F4SPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS FAA AD 96-13-11 POST 02626NO. 1, 2 AND 4, LH/RH.FROM 0 FC/FHALI REFERENCE: TO LOVACCESS: 147AZ 536503-01-13* 0.23148AZ* 0.23536505-0606-1 141 CENTER WING BOX STRINGERS NDT SDI T: SEE SB ALI NTM 5315011 16.00 ALL142 I: SEE SB CN PART 41 16.00 SB 53-0243SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD CN 2006-0071(B) FROM 0 FC/FHCENTER WING BOX FORWARD AND REAR LOWER PANEL MAIN FAA ADTO LOVSTRINGERS AT CROSSING AREA. 96-13-11-01-1SB 53-0243ACCESS: 147AZ 147DZ 147FZ 734* 0.40148AZ 148DZ 744 ALI REFERENCE: * 0.36536505-01-1STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 164APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536506-0606-2 141 CENTER WING BOX NDT SDI ST: 26000 FC ALI NTM 5315181 1.00 B2142 OR CN PART 21 1.00 PRE 03476SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 28900 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 6200 FC FAA AD 96-13-11 TO 48000 FCTO REAR SPARS LH/RH. OR6900 FH ALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-01-1* 3.23148AZ 641AB 642CB* 3.23536506-0606-3 141 CENTER WING BOX NDT SDI ST: 35000 FC ALI NTM 5315181 1.00 B2142 OR CN PART 21 1.00 POST 03476SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 38800 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 9600 FC FAA AD 96-13-11 TO 40000 FCTO REAR SPARS LH/RH. OR44400 FH10600 FH ALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-01-4* 3.23148AZ 641AB 642CB* 3.23536506-0606-4 141 CENTER WING BOX NDT SDI ST: 32000 FC ALI NTM 5315181 1.00 B4-100142 OR CN PART 21 1.00 PRE 02626SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 43200 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 8000 FC FAA AD 96-13-11 TO 40000 FCTO REAR SPARS LH/RH. OR10800 FH ALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-01-6* 3.23148AZ 641AB 642CB* 3.23536506-0606-5 141 CENTER WING BOX NDT SDI ST: 24000 FC ALI NTM 5315181 1.00 B4-200142 OR CN PART 21 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 49200 FH FAA AD CN 2006-0071(B) F4WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 6300 FC FAA AD 96-13-11 PRE 02626TO REAR SPARS LH/RH. ORFROM 0 FC/FH12900 FH ALI REFERENCE: TO 34000 FCACCESS: 147AZ 541AB 542CB 536506-01-8* 3.23148AZ 641AB 642CB* 3.23536506-0606-6 141 CENTER WING BOX NDT SDI ST: 31000 FC ALI NTM 5315181 1.00 B4-200142 OR CN PART 21 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 63500 FH FAA AD CN 2006-0071(B) F4WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 6500 FC FAA AD 96-13-11 POST 02626TO REAR SPARS LH/RH. ORFROM 0 FCFH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 165APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536506-0606-6 * * * * * C O N T I N U E * * * * *ACCESS: 147AZ 541AB 542CB 13300 FH ALI REFERENCE: * 3.23 TO 40000 FC148AZ 641AB 642CB 536506-01-11* 3.23 82000 FH536506-0606-7 141 CENTER WING BOX NDT SDI I: 6000 FC ALI NTM 5315181 1.00 B2142 OR CN PART 21 1.00 PRE 03476SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 6700 FH FAA AD CN 2006-0071(B) FROM 48000 FCWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13-11 TO 53600 FCTO REAR SPARS LH/RH.57900 FHALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-01-2* 3.23148AZ 641AB 642CB* 3.23536506-0606-8 141 CENTER WING BOX NDT SDI I: 1200 FC ALI NTM 5315181 1.00 B2142 OR CN PART 21 1.00 PRE 03476SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 1300 FH FAA AD CN 2006-0071(B) FROM 53600 FCWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13-11 57900 FHTO REAR SPARS LH/RH.TO LOVALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-01-3* 3.23148AZ 641AB 642CB* 3.23536506-0606-9 141 CENTER WING BOX NDT SDI ST: 31000 FC ALI NTM 5315181 1.00 B2142 SI: 6500 FC CN PART 21 1.00 POST 03476SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO T: 31000 FC FAA AD CN 2006-0071(B) TO 40000 FCWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 6500 FC FAA AD 96-13-11 44400 FHTO REAR SPARS LH/RH.TO LOVALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-01-5* 3.23148AZ 641AB 642CB* 3.23536506-0607-1 141 CENTER WING BOX NDT SDI I: 6300 FC ALI NTM 5315181 1.00 B4-100142 OR CN PART 21 1.00 PRE 02626SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 8300 FH FAA AD CN 2006-0071(B) FROM 40000 FCWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13-11 TO LOVTO REAR SPARS LH/RH.ALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-01-7* 3.23148AZ 641AB 642CB* 3.23STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 166APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536506-0607-2 141 CENTER WING BOX NDT SDI I: 5300 FC ALI NTM 5315181 1.00 B4-200142 OR CN PART 21 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 10900 FH FAA AD CN 2006-0071(B) F4WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13-11 PRE 02626TO REAR SPARS LH/RH.FROM 34000 FCALI REFERENCE: TO 40000 FCACCESS: 147AZ 541AB 542CB 536506-01-9* 3.23 82000-FH148AZ 641AB 642CB* 3.23536506-0607-3 141 CENTER WING BOX NDT SDI I: 5600 FC ALI NTM 5315181 1.00 B4-200142 OR CN PART 21 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 11600 FH FAA AD CN 2006-0071(B) F4WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13-11 PRE 02626TO REAR SPARS LH/RH.FROM 40000 FCALI REFERENCE: 82000 FHACCESS: 147AZ 541AB 542CB 536506-01-10* 3.23 TO LOV148AZ 641AB 642CB* 3.23536506-0607-4 141 CENTER WING BOX NDT SDI I: 5600 FC ALI NTM 5315181 1.00 B4-200142 OR CN PART 21 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 11600 FH FAA AD CN 2006-0071(B) F4WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13-11 POST 02626TO REAR SPARS LH/RH.FROM 40000 FCALI REFERENCE: 82000 FHACCESS: 147AZ 541AB 542CB 536506-01-12* 3.23 TO LOV148AZ 641AB 642CB* 3.23536506-0607-5 141 CENTER WING BOX NDT SDI T: 29200 FC ALI NTM 5315181 1.00 B2142 OR CN PART 41 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 31500 FH FAA AD CN 2006-0071(B) TO LOVWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 3100 FC FAA AD 96-13-11TO REAR SPARS LH/RH. OR3300 FH ALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-02-1* 3.23148AZ 641AB 642CB* 3.23536506-0607-6 141 CENTER WING BOX NDT SDI T: 33900 FC ALI NTM 5315181 1.00 B4-100142 OR CN PART 41 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 45100 FH FAA AD CN 2006-0071(B) TO LOVWING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 4200 FC FAA AD 96-13-11TO REAR SPARS LH/RH. OR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 167APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536506-0607-6 * * * * * C O N T I N U E * * * * *ACCESS: 147AZ 541AB 542CB 5600 FH ALI REFERENCE: * 3.23148AZ 641AB 642CB 536506-02-2* 3.23536506-0607-7 141 CENTER WING BOX NDT SDI T: 29700 FC ALI NTM 5315181 1.00 B4-200142 OR CN PART 41 1.00 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 61800 FH FAA AD CN 2006-0071(B) F4WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 4000 FC FAA AD 96-13-11 FROM 0 FC/FHTO REAR SPARS LH/RH. ORTO LOV8300 FH ALI REFERENCE:ACCESS: 147AZ 541AB 542CB 536506-02-3* 3.23148AZ 641AB 642CB* 3.23536509-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI T: SEE ISB ALI CN 2006-0071(B) 1 0.15 PRE 02626142 I: SEE ISB CN FAA AD 96-13-11 1 0.15 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD ISB 53-0275TO LOVCENTER WING BOX REAR SPAR AROUND ACCESS DOOR CUT-OUTS ISBLH/RH. ALI REFERENCE:536509-01-1ACCESS: 147AZ* 0.23148AZ* 0.23536510-0606-1 141 CENTER WING BOX REAR SPAR MEC DET T: 34000 FC ALI EASA AD1 0.50 B4-100142 OR CN 2006-00711 0.50 FROM 0 FC/FHDETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 45900 FH FAA AD FAA ADTO 40000 FCREINFORCING PLATES AT CROSSING AREA WITH STRINGERS I: 6000 FC 2007-04-11FROM RIB 1 LH TO RIB 1 RH. OR8100 FH ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-01-1536510-0606-5PREP.: REMOVE/INSTALL INSULATION AND SEALANT.ACCESS: 147AZ* 0.23148AZ* 0.23536510-0606-2 141 CENTER WING BOX REAR SPAR MEC DET I: 3200 FC ALI EASA AD1 0.50 B4-100142 OR CN 2006-00711 0.50 FROM 40000 FCDETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 4300 FH FAA AD FAA ADTO LOVREINFORCING PLATES AT CROSSING AREA WITH STRINGERS 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 168APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536510-0606-2 * * * * * C O N T I N U E * * * * *FROM RIB 1 LH TO RIB 1 RH. ALI REFERENCE:536510-01-2NOTE : THIS TASK IS AN ALTERNATIVE TO TASK536510-0606-5PREP.: REMOVE/INSTALL INSULATION AND SEALANT.ACCESS: 147AZ* 0.23148AZ* 0.23536510-0606-3 141 CENTER WING BOX REAR SPAR MEC DET T: 27000 FC ALI EASA AD1 0.50 B4-200142 OR CN 2006-00711 0.50 C4DETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 55300 FH FAA AD FAA ADF4REINFORCING PLATES AT CROSSING AREA WITH STRINGERS I: 3500 FC 2007-04-11FROM 0 FC/FHFROM RIB 1 LH TO RIB 1 RH. ORTO 34000 FC7200 FH ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-01-3536510-0606-6PREP.: REMOVE/INSTALL INSULATION AND SEALANT.ACCESS: 147AZ* 0.23148AZ* 0.23536510-0606-4 141 CENTER WING BOX REAR SPAR MEC DET I: 2400 FC ALI EASA AD1 0.50 B4-200142 OR CN 2006-00711 0.50 C4DETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 4900 FH FAA AD FAA ADF4REINFORCING PLATES AT CROSSING AREA WITH STRINGERS 2007-04-11FROM 34000 FCFROM RIB 1 LH TO RIB 1 RH.TO LOVALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-01-4536510-0606-6PREP.: REMOVE/INSTALL INSULATION AND SEALANT.ACCESS: 147AZ* 0.23148AZ* 0.23536510-0606-5 141 CENTER WING BOX REAR SPAR NDT SDI T: 34000 FC ALI NTM 5315201 0.50 B4-100142 OR CN PART 41 0.50 FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 169APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536510-0606-5 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION OF CENTER WING BOX, PUMP 45900 FH FAA AD CN 2006-0071(B) TO LOVHOLES REINFORCING PLATES AT CROSSING AREA WITH I: 9500 FC FAA AD 96-13-11STRINGERS FROM RIB 1 LH TO RIB 1 RH. OR12800 FH ALI REFERENCE:NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-02-1536510-0606-1 AND TASK 536510-0606-2PREP.: REMOVE/INSTALL INSULATION AND SEALANT.ACCESS: 147AZ* 0.23148AZ* 0.23536510-0606-6 141 CENTER WING BOX REAR SPAR NDT SDI T: 27000 FC ALI NTM 5315201 0.50 B4-200142 OR CN PART 41 0.50 C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX, PUMP 55300 FH FAA AD CN 2006-0071(B) F4HOLES REINFORCING PLATES AT CROSSING AREA WITH I: 7300 FC FAA AD 96-13-11 FROM 0 FC/FHSTRINGERS FROM RIB 1 LH TO RIB 1 RH. ORTO LOV14900 FH ALI REFERENCE:PREP.: REMOVE/INSTALL INSULATION AND SEALANT. 536510-02-2ACCESS: 147AZ* 0.23148AZ* 0.23536511-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI T: SEE ISB ALI NTM 5315021 1.00 PRE SB142 I: SEE ISB CN PART 41 1.00 (53-0282)SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD EASA ADFROM 0 FC/FHCENTER WING BOX REAR SPAR AT RIB 1 INTERNAL ANGLE ISB 2006-0071TO LOVRUNOUT LH/RH. FAA AD2007-04-11ACCESS: 147AZ* 0.23148AZ ALI REFERENCE: * 0.23536511-01-1536512-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI T: SEE SB ALI NTM 5315041 2.00 ALL142 I: SEE SB CN PART 61 2.00 SB 53-0265SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR FAA AD CN 2006-0071(B) FROM 0 FC/FHSPAR AND BOTTOM PANEL UNDERNEATH INTERNAL ANGLE AT FAA AD 96-13-11 TO LOVRIB 1 AREA, LH/RH. SB 53-0265ACCESS: 147AZ ALI REFERENCE: * 0.23* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 170APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536512-0606-1 * * * * * C O N T I N U E * * * * *148AZ 536512-01-1* 0.23536513-0606-1 141 FRAME 47 - LOWER JUNCTION NDT SDI T: SEE SB ALI NTM 5315041 2.00 ALL142 I: SEE SB CN PART 61 2.00 SB 53-0299SPECIAL DETAILED INSPECTION OF FRAME 47 AT AREA OF FAA AD CN 2006-0071(B) FROM 0 FC/FHLOWER JUNCTION WITH OUTER WING. ISB FAA AD 96-13-11 TO LOV(HOLES H,I,K,L,M AND N ) ISB 53-0299ACCESS: 147AZ ALI REFERENCE: * 0.23148AZ 536513-01-1* 0.23536515-0606-1 141 FRAME 47 LOWER RADIUS NDT SDI T: SEE SB ALI NTM 5315031 2.00 ALL142 I: SEE SB CN PART 61 2.00 SB 53-0259SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD CN 2006-0071(B) FROM 0 FC/FHFRAME 47 LOWER RADIUS LH/RH. ISB FAA AD 96-13-11 TO LOVISB 53-0259ACCESS: 571AB* 0.10671AB ALI REFERENCE: * 0.10536515-01-1536516-0606-1 140 FRAME 47 UPPER RADIUS NDT SDI T: SEE SB AD NTM 531529 PART 1 0.50 B2I: SEE SB CN 4 AND 6SPECIAL DETAILED INSPECTION OF THE FRAME 47, UPPER ISB AD 2007-26-14RADIUS. SB CN F-2006-016FAA ADACCESS: 577BT 677BT 2003-06-04* 0.43ISB 53-0246536516536516-0606-4 140 FRAME 47 UPPER RADIUS NDT SDI T: SEE SB AD NTM 531529 PART 1 0.50 B4-100I: SEE SB CN 4 AND 6SPECIAL DETAILED INSPECTION OF THE FRAME 47, UPPER ISB AD 2007-26-14RADIUS. SB CN F-2006-016FAA ADACCESS: 577BT 677BT 2003-06-04* 0.43ISB 53-0246536516STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 171APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536516-0606-6 140 FRAME 47 UPPER RADIUS NDT SDI T: SEE SB AD NTM 5315291 0.50 B4-200I: SEE SB CN PART 4 AND 6C4SPECIAL DETAILED INSPECTION OF THE FRAME 47, UPPER ISB AD 2007-26-14F4RADIUS. CN F-2006-016FAA ADNOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS TASK 2003-06-04536523-0606-X ISB 53-0246ACCESS: 577BT 677BT* 0.43536521-0606-2 243 FUSELAGE AT FRAME 40 MEC DET ST: 21000 FC ALI CN 2006-0071(B) 1 0.50 B2244 OR CN FAA AD 96-13-11 1 0.50 PRE 02974DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 23700 FH FAA ADFROM 0 FC/FHAREAS AT FRAME 40, LH/RH. SI: 11900 FC ALI REFERENCE: TO 48000 FCOR 536521-01-1PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 13400 FHCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0606-3 243 FUSELAGE AT FRAME 40 MEC DET ST: 26000 FC ALI CN 2006-0071(B) 1 0.50 B2244 OR CN FAA AD 96-13-11 1 0.50 POST 02974DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 29400 FH FAA ADFROM 0 FC/FHAREAS AT FRAME 40, LH/RH. SI: 13200 FC ALI REFERENCE: TO 48000 FCOR 536521-01-3PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 14900 FHCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0606-4 243 FUSELAGE AT FRAME 40 MEC DET ST: 19000 FC ALI CN 2006-0071(B) 1 0.50 B4-100244 OR CN FAA AD 96-13-11 1 0.50 PRE 02974DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 25800 FH FAA ADFROM 0 FC/FHAREAS AT FRAME 40, LH/RH. SI: 11000 FC ALI REFERENCE: TO 40000 FCOR 536521-01-5PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 14900 FHCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0606-5 243 FUSELAGE AT FRAME 40 MEC DET ST: 25000 FC ALI CN 2006-0071(B) 1 0.50 B4-100244 OR CN FAA AD 96-13-11 1 0.50 POST 02974DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 34000 FH FAA ADFROM 0 FC/FHAREAS AT FRAME 40, LH/RH. SI: 12700 FC ALI REFERENCE: TO 40000 FC* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 172APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536521-0606-5 * * * * * C O N T I N U E * * * * *OR 536521-01-7PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 17300 FHCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0606-6 243 FUSELAGE AT FRAME 40 MEC DET ST: 19000 FC ALI CN 2006-0071(B) 1 0.50 B4-200244 OR CN FAA AD 96-13-11 1 0.50 C4DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 42000 FH FAA ADF4AREAS AT FRAME 40, LH/RH. SI: 9600 FC ALI REFERENCE: PRE 02974OR 536521-01-9FROM 0 FC/FHPREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 21200 FHTO 34000 FCCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0606-7 243 FUSELAGE AT FRAME 40 MEC DET ST: 24000 FC ALI CN 2006-0071(B) 1 0.50 B4-200244 OR CN FAA AD 96-13-11 1 0.50 C4DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 53000 FH FAA ADF4AREAS AT FRAME 40, LH/RH. SI: 10000 FC ALI REFERENCE: POST 02974OR 536521-01-11FROM 0 FC/FHPREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 22100 FHTO 34000 FCCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0607-1 243 FUSELAGE AT FRAME 40 MEC DET I: 8200 FC ALI CN 2006-0071(B) 1 0.50 B2244 OR CN FAA AD 96-13-11 1 0.50 PRE 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 9200 FH FAA ADFROM 48000 FCCOUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENCE: TO LOV536521-01-2PREP.: REMOVE/INSTALL LINING, INSULATION AND AIRCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0607-2 243 FUSELAGE AT FRAME 40 MEC DET I: 10000 FC ALI CN 2006-0071(B) 1 0.50 B2244 OR CN FAA AD 96-13-11 1 0.50 POST 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 11300 FH FAA ADFROM 48000 FCCOUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENCE: TO LOV536521-01-4PREP.: REMOVE/INSTALL LINING, INSULATION AND AIRCONDITIONING PIPE. REMOVE SEALANT IF* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 173APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536521-0607-2 * * * * * C O N T I N U E * * * * *INSTALLED.536521-0607-3 243 FUSELAGE AT FRAME 40 MEC DET I: 7600 FC ALI CN 2006-0071(B) 1 0.50 B4-100244 OR CN FAA AD 96-13-11 1 0.50 PRE 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 10300 FH FAA ADFROM 40000 FCCOUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENCE: TO LOV536521-01-6PREP.: REMOVE/INSTALL LINING, INSULATION AND AIRCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0607-4 243 FUSELAGE AT FRAME 40 MEC DET I: 10000 FC ALI CN 2006-0071(B) 1 0.50 B4-100244 OR CN FAA AD 96-13-11 1 0.50 POST 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 22100 FH FAA ADFROM 40000 FCCOUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENCE: TO LOV536521-01-8PREP.: REMOVE/INSTALL LINING, INSULATION AND AIRCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0607-5 243 FUSELAGE AT FRAME 40 MEC DET I: 7300 FC ALI CN 2006-0071(B) 1 0.50 B4-200244 OR CN FAA AD 96-13-11 1 0.50 C4DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 16100 FH FAA ADF4AREAS AT FRAME 40, LH/RH. ALI REFERENCE: PRE 02974536521-01-10FROM 34000 FCPREP.: REMOVE/INSTALL LINING, INSULATION AND AIRTO LOVCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.536521-0607-6 243 FUSELAGE AT FRAME 40 MEC DET I: 10000 FC ALI CN 2006-0071(B) 1 0.50 B4-200244 OR CN FAA AD 96-13-11 1 0.50 C4DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 22100 FH FAA ADF4COUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENCE: POST 02974536521-01-12FROM 34000 FCPREP.: REMOVE/INSTALL LINING, INSULATION AND AIRTO LOVCONDITIONING PIPE. REMOVE SEALANT IFINSTALLED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 174APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536523-0606-2 241 SPLICE PLATE AT FRAME 40 NDT SDI ST: 42000 FC ALI NTM 5315231 0.75 B2242 OR CN PART 61 0.75 FROM 0 FC/FH243 SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF SPLICE 47500 FH FAA AD EASA AD1 0.75 TO 48000 FC244 PLATE AT FRAME 40 CIRCUMFERENTIAL SKIN SPLICE FROM SI: 6000 FC 2006-00711 0.75STRINGER 13 LH/RH TO CROWN CENTER LINE. OR FAA AD6800 FH 2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-7 ALI REFERENCE:536523-01-1536523-0606-3 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 6000 FC ALI NTM 5315231 0.75 B2242 OR CN PART 61 0.75 FROM 48000 FC243 SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF SPLICE 6800 FH FAA AD EASA AD1 0.75 TO LOV244 PLATE AT THE CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 2006-00711 0.75FROM STRINGER 13 LH/RH TO CROWN CENTER LINE. FAA AD2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-8 ALI REFERENCE:536523-01-2536523-0606-4 241 SPLICE PLATE AT FRAME 40 NDT SDI ST: 39000 FC ALI NTM 5315231 0.75 B4-100242 OR CN PART 61 0.75 FROM 0 FC/FH243 SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 53000 FH FAA AD EASA AD1 0.75 TO 40000 FC244 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 FROM SI: 5800 FC 2006-00711 0.75STRINGER 13 LH/RH TO CROWN CENTER LINE. OR FAA AD7900 FH 2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-9 ALI REFERENCE:536523-01-3536523-0606-5 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 5800 FC ALI NTM 531523 PART 1 0.75 B4-100242 OR CN 61 0.75 FROM 40000 FC243 SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 7900 FH FAA AD EASA AD1 0.75 TO LOV244 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 FROM 2006-00711 0.75STRINGER 13 LH/RH TO CROWN CENTER LINE. FAA AD2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0607-1 ALI REFERENCE:536523-01-4STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 175APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536523-0606-6 241 SPLICE PLATE AT FRAME 40 NDT SDI T: 37800 FC ALI NTM 5315231 0.75 B4-200242 OR CN PART 61 0.75 C4243 SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 83500 FH FAA AD EASA AD1 0.75 F4244 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 FROM I: 5600 FC 2006-00711 0.75 FROM 0 FC/FHSTRINGER 13 LH/RH TO CROWN CENTER LINE. OR FAA ADTO LOV12400 FH 2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS TASK536523-0607-2 ALI REFERENCE:536523-01-5536523-0606-7 241 SPLICE PLATE AT FRAME 40 NDT SDI ST: 42000 FC ALI NTM 5315231 0.75 B2242 OR CN PART 61 0.75 FROM 0 FC/FH243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 47500 FH FAA AD EASA AD1 0.75 TO 48000 FC244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO SI: 15500 FC 2006-00711 0.75CROWN CENTER LINE LH/RH. OR FAA AD17500 FH 2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-2 ALI REFERENCE:536523-02-1PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BEREMOVED.536523-0606-8 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 15500 FC ALI NTM 5315231 0.75 B2242 OR CN PART 61 0.75 FROM 48000 FC243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 17500 FH FAA AD EASA AD1 0.75 TO LOV244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO 2006-00711 0.75CROWN CENTER LINE LH/RH. FAA AD2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-3 ALI REFERENCE:536523-02-2PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BEREMOVED.536523-0606-9 241 SPLICE PLATE AT FRAME 40 NDT SDI ST: 39000 FC ALI NTM 5315231 0.75 B4-100242 OR CN PART 61 0.75 FROM 0 FC/FH243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 53000 FH FAA AD EASA AD1 0.75 TO 40000 FC244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO SI: 14400 FC 2006-00711 0.75CROWN CENTER LINE LH/RH. OR FAA AD19600 FH 2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-4 ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 176APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536523-0606-9 * * * * * C O N T I N U E * * * * *536523-02-3PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BEREMOVED.536523-0607-1 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 14400 FC ALI NTM 5315231 0.75 B4-100242 OR CN PART 61 0.75 FROM 40000 FC243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 19600 FH FAA AD EASA AD1 0.75 TO LOV244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO 2006-00711 0.75CROWN CENTER LINE LH/RH. FAA AD2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-5 ALI REFERENCE:536523-02-4PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BEREMOVED.536523-0607-2 241 SPLICE PLATE AT FRAME 40 NDT SDI T: 37800 FC ALI NTM 5315231 0.75 B4-200242 OR CN PART 61 0.75 C4243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 83500 FH FAA AD EASA AD1 0.75 F4244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO I: 13900 FC 2006-00711 0.75 FROM 0 FC/FHCROWN CENTER LINE LH/RH. OR FAA ADTO LOV30700 FH 2007-04-11NOTE: THIS TASK CAN BE DONE AT THE SAME TIME ASTASK 536523-0606-6 ALI REFERENCE:536523-02-5PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BEREMOVED.536529-0606-1 141 CENTER WING BOX DOUBLER RUNOUT NDT SDI T: SEE ISB ALI NTM 5315051 0.50 ALL142 I: SEE ISB FAA AD PART 61 0.50 ISB 53-0242SPECIAL DETAILED OR GENERAL VISUAL INSPECTION OF ISB EASA ADFROM 0 FC/FHTHE CENTER WING BOX CENTER SPAR AT CUTOUT DOUBLER 2006-0071(B)TO LOVRUN OUT. FAA AD 96-13-11ISB 53-0242ACCESS: 147AZ 147DZ 734* 0.36148AZ 148DZ 744 ALI REFERENCE: * 0.36536529-01-1STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 177APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536535-0606-1 141 CENTER WING BOX LOW. PANELS NDT SDI T: SEE ISB ALI NTM 5315061 2.00 ALL142 I: SEE ISB CN PART 61 2.00 SB 53-0244SPECIAL DETAILED OR GENERAL VISUAL INSPECTION OF THE FAA AD CN 2006-0071(B) FROM 0 FC/FHCENTER WING BOX FORWARD AND REAR LOWER PANEL MAIN ISB FAA AD 96-13-11 TO LOVSTRINGERS AT DRAINAGE HOLES. ISB 53-0244ACCESS: 147AZ 147DZ 734 ALI REFERENCE: * 0.36148AZ 148DZ 744 536535-01-1* 0.36536541-0606-1 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 5315221 5.00 B2641 OR CN PART 41 5.00 PRE 00317SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 23300 FH FAA AD CN 2006-0071(B) PRE 08486CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 7100 FC FAA AD 96-13-11 (57-0179)FRONT TO REAR SPAR, EXTERNAL SIDE. ORFROM 0 FC/FH7900 FH ALI REFERENCE: TO LOVACCESS: 577AT 577BT 536541-01-1* 0.28677AT 677BT* 0.28536541-0606-2 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 5315221 5.00 B2641 OR CN PART 61 5.00 PRE 00317SPECIAL DETAILED INSPECTION OF OUTER WING TO CENTER 23300 FH FAA AD CN 2006-0071(B) POST 08486WING BOX UPPER SPLICE AND PANEL AT RIB 1 FROM I: 5500 FC FAA AD 96-13-11 (57-0179)FRONT TO REAR SPAR, EXTERNAL SIDE. ORFROM 0 FC/FH6100 FH ALI REFERENCE: TO LOVNOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE 536541-02-1ACCESS: 577AT 577BT* 0.28677AT 677BT* 0.28536541-0606-3 541 OUTER WING TO CENTER WING NDT SDI T: 25000 FC ALI NTM 5315221 5.00 B2641 OR CN PART 41 5.00 POST 00317SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 27700 FH FAA AD CN 2006-0071(B) PRE 08486CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 9300 FC FAA AD 96-13-11 (57-0179)FRONT TO REAR SPAR, EXTERNAL SIDE. ORFROM 0 FC/FH10300 FH ALI REFERENCE: TO LOVACCESS: 577AT 577BT 536541-01-2* 0.28677AT 677BT* 0.28536541-0606-4 541 OUTER WING TO CENTER WING NDT SDI T: 25000 FC ALI NTM 5315221 5.00 B2641 OR CN PART 41 5.00 POST 00317SPECIAL DETAILED INSPECTION (US AND EDDY CURRENT) OF 27700 FH FAA ADPOST 08486* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 178APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536541-0606-4 * * * * * C O N T I N U E * * * * *OUTER WING TO CENTER WING BOX UPPER SPLICE AND PANEL I: 7200 FC NTM 531522(57-0179)AT RIB 1, FROM FRONT TO REAR SPAR, EXTERNAL SIDE. OR PART 6FROM 0 FC/FH8000 FH CN 2006-0071(B) TO LOVNOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE FAA AD 96-13-11ACCESS: 577AT 577BT ALI REFERENCE: * 0.28677AT 677BT 536541-02-3* 0.28536541-0606-5 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 5315221 5.00 B4-100641 OR CN PART 41 5.00 PRE 10089SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 28300 FH FAA AD CN 2006-0071(B) (57-0191)CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 8300 FC FAA AD 96-13-11 FROM 0 FC/FHFRONT TO REAR SPAR, EXTERNAL SIDE. ORTO LOV11200 FH ALI REFERENCE:ACCESS: 577AT 577BT 536541-01-3* 0.28677AT 677BT* 0.28536541-0606-6 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 5315221 5.00 B4-100641 OR CN PART 41 5.00 POST 10752SPECIAL DETAILED INSPECTION (US AND EDDY CURRENT) OF 28300 FH FAA AD NTM 531522(57-0191)OUTER WING TO CENTER WING BOX UPPER SPLICE AND PANEL I: 6400 FC PART 6POST 11213AT RIB 1, FROM FRONT TO REAR SPAR, EXTERNAL SIDE. OR CN 2006-0071(B) (57-0191)8600 FH FAA AD 96-13-11 POST 10089NOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE(57-0191)ALI REFERENCE: FROM 0 FC/FHACCESS: 577AT 577BT 536541-02-5* 0.28 TO LOV677AT 677BT* 0.28536541-0606-7 541 OUTER WING TO CENTER WING NDT SDI T: 14000 FC ALI NTM 5315221 5.00 B4-200641 OR CN PART 41 5.00 C4SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 28700 FC FAA AD CN 2006-0071(B) F4CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 5700 FC FAA AD 96-13-11 PRE 10089FRONT TO REAR SPAR, EXTERNAL SIDE. OR(57-0191)11700 FH ALI REFERENCE: FROM 0 FC/FHACCESS: 577AT 577BT 536541-01-4* 0.28 TO LOV677AT 677BT* 0.28536541-0606-8 541 OUTER WING TO CENTER WING NDT SDI T: 14000 FC ALI NTM 5315221 5.00 B4-200641 OR FAA AD PART 41 5.00 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 179APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536541-0606-8 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION (US AND EDDY CURRENT) OF 28700 FH NTM 531522F4OUTER WING TO CENTER WING BOX UPPER SPLICE AND PANEL I: 4400 FC PART 6POST 10089AT RIB 1, FROM FRONT TO REAR SPAR, EXTERNAL SIDE. OR FAA AD 96-13-11 (57-0191)9000 FHPOST 11213NOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE ALI REFERENCE: (57-0191)536541-02-7FROM 0 FC/FACCESS: 577AT 577BT* 0.28 TO LOV677AT 677BT* 0.28536543-0606-1 541 FRAME 40 OUTBOARD LOWER RADIUS NDT SDI T: SEE SB ALI NTM 5315171 0.50 PRE 10453641 I: SEE SB FAA AD PART 61 0.50 (53-0297)SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF ISB EASA ADFROM 0 FC/FHFRAME 40 OUTBOARD LOWER RADIUS IN AREA OF CENTER WING 2006-0071TO LOVBOX TO FUSELAGE CONNECTION FORWARD FACE LH/RH. FAA AD2007-04-11ACCESS: 513AB ISB 53-0268* 0.40613AB* 0.18ALI REFERENCE:536543-01-1536544-0606-1 141 CENTER WING BOX LOWER PANEL NDT SDI T: SEE SB ALI NTM 5315071 12.50 ALL142 I: SEE SB FAA AD PART 41 12.50 SB 53-0252143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER ISB EASA AD1 12.50 FROM 0 FC/FH144 PANEL AT FUSELAGE TO CENTER WING BOX JUNCTION FITTING 2006-00711 12.50 TO LOVLH/RH. FAA AD2007-04-11ACCESS: 147AZ 734 ISB 53-0252* 0.33148AZ 744* 0.33ALI REFERENCE:536544-01-2536545-0606-1 141 CENTER WING BOX LOWER PANEL STRINGER NDT SDI T: SEE ISB ALI NTM 5315081 7.50 SB 53-0245142 I: SEE ISB FAA AD PART 41 7.50 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER ISB AND PART 6TO LOVPANEL STRINGERS REINFORCEMENT STRAP JUNCTIONS. CN 2006-0071(B)FAA AD 96-13-11PREP.: VAPOR SEAL PARTLY REMOVED ISB 53-0245ACCESS: 147AZ 147DZ 734 ALI REFERENCE: * 0.36148AZ 148DZ 744 536545-01-1* 0.36STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 180APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536546-0606-1 542 CENTER WING SPAR NDT SDI T: 26000 FC ALI NTM 5315191 2.00 B2642 OR FAA AD PART 41 2.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 28800 FH CN 2006-0071(B) TO 48000 FCRIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, I: 7200 FC FAA AD 96-13-11LH/RH. OR8000 FH ALI REFERENCE:NOTE: REMOVE SEALANT AND NUTS. 536546-01-1ACCESS: 541AB 542CB* 3.00641AB 642CB* 3.00536546-0606-2 542 CENTER WING SPAR NDT SDI I: 7100 FC ALI NTM 5315191 2.00 B2642 OR FAA AD PART 41 2.00 FROM 48000 FCSPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 7900 FH CN 2006-0071(B) TO LOVRIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, FAA AD 96-13-11LH/RH.ALI REFERENCE:NOTE: REMOVE SEALANT AND NUTS. 536546-01-2ACCESS: 541AB 542CB* 3.00641AB 642CB* 3.00536546-0606-3 542 CENTER WING SPAR NDT SDI T: 22000 FC ALI NTM 5315191 2.00 B4-100642 OR FAA AD PART 41 2.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 29700 FH CN 2006-0071(B) TO LOVRIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, I: 5800 FC FAA AD 96-13-11LH/RH. OR7800 FH ALI REFERENCE:NOTE: REMOVE SEALANT AND NUTS. 536546-01-3ACCESS: 541AB 542CB* 3.00641AB 642CB* 3.00536546-0606-4 542 CENTER WING SPAR NDT SDI T: 16000 FC ALI NTM 5315191 2.00 B4-200642 OR FAA AD PART 41 2.00 C4SPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 32800 FH CN 2006-0071(B) F4RIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, I: 3700 FC FAA AD 96-13-11 FROM 0 FC/FHLH/RH. ORTO LOV7600 FH ALI REFERENCE:NOTE: REMOVE SEALANT AND NUTS. 536546-01-4ACCESS: 541AB 542CB* 3.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 181APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536546-0606-4 * * * * * C O N T I N U E * * * * *641AB 642CB* 3.00536547-0606-1 141 CENTER WING BOX - RIB 1 NDT SDI T: 25000 FC ALI NTM 5315151 1.00 B2142 OR FAA AD PART 61 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF CENTER WING BOX, 27700 FH CN 2006-0071(B) TO LOVCENTER SPAR TO RIB 1 JUNCTION, INBOARD SIDE, LH/RH. I: 12000 FC FAA AD 96-13-11ORACCESS: 147AZ 13300 FH ALI REFERENCE: * 0.23148AZ 536547-01-1* 0.23536548-0606-1 141 FUSELAGE/CENTER WING BOX NDT SDI T: SEE ISB ALI NTM SEE SB1 8.00 SB 53-0310142 I: ISE ISB FAA AD CN 2006-0071(B) 1 8.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF FRAME 40 FORWARD ISB FAA AD 96-13-11 TO LOVFITTING RADIUS AT TENSION BOLT JUNCTION. ISB 53-0310ACCESS: 512AB 513AB 513BB ALI REFERENCE: * 0.79612AB 613AB 613BB 536548-01-1* 0.56536549-0606-1 141 TENSION BOLT HOLES - FRAME 40 TO CENTER NDT SDI T: SEE SB ALI NTM 5315281 TBD SB 53-0304142 WING BOX JUNCTION I: SEE SB FAA AD PART 61 TBD FROM 0 FC/FH241 ISB CN 2006-0071(B) 1 TBD TO LOV242 SPECIAL DETAILED INSPECTION OF FRAME 40 TO CENTER FAA AD 96-13-11 1 TBDWING CONNECTION AT UPPER SKIN LEVEL TENSION BOLTS ISB 53-0304JUNCTION.ALI REFERENCE:PREP.: REMOVE PASSENGER SEATS AND FLOOR COVERING IN 536549-01-1CABIN, BETWEEN FR 39 AND FR 40, LH AND RH.ACCESS: 811* 0.15241SF 241TF 241WF 241XF 513AB 841* 2.05242SF 242TF 242WF 242XF 613AB 841* 1.18536551-0604-1 145 UPPER FLANGE OF TRANSVERSAL FLOOR BEAM MEC DET T: 48000 FC ALI EASA AD1 TBD B2146 I: 13200 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF TRANSVERSAL FLOOR BEAM UPPER FAA ADTO LOVFLANGE FROM BEAM 5 TO FRAME 50, LH/RH. 2007-04-11PREP.: DUCTS TO BE REMOVED ALI REFERENCE:536551-01-1STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 182APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536551-0604-2 145 UPPER FLANGE OF TRANSVERSAL FLOOR BEAM MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100146 I: 13200 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF TRANSVERSAL FLOOR BEAM UPPER FAA ADTO LOVFLANGE FROM BEAM 5 TO FRAME 50, LH/RH. 2007-04-11PREP.: DUCTS TO BE REMOVED ALI REFERENCE:536551-01-1536551-0604-3 145 UPPER FLANGE OF TRANSVERSAL FLOOR BEAM MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200146 I: 13200 FC FAA AD 2006-00711 TBD C4DETAILED INSPECTION OF TRANSVERSAL FLOOR BEAM UPPER FAA ADF4FLANGE FROM BEAM 5 TO FRAME 50, LH/RH. 2007-04-11FROM 0 FC/FHTO LOVPREP.: DUCTS TO BE REMOVED ALI REFERENCE:536551-01-1536553-0604-1 143 CENTER WING BOX LOWER PANELS NDT SDI T: 48000 FC ALI NTM 5365531 TBD B2144 I: 8100 FC FAA AD PART 41 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF CENTER WING BOX BOTTOM EASA ADTO LOVSKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR FROM 2006-0071RIB 1 LH TO RIB 1 RH. FAA AD2007-04-11PREP.: VAPOUR SEAL TO BE DISPLACEDALI REFERENCE:ACCESS: 147FZ 734 536553-01-1* 0.14744* 0.10536553-0604-2 143 CENTER WING BOX LOWER PANELS NDT SDI T: 40000 FC ALI NTM 5365531 TBD B4-100144 I: 10100 FC FAA AD PART 41 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF CENTER WING BOX BOTTOM EASA ADTO LOVSKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR FROM 2006-0071RIB 1 LH TO RIB 1 RH. FAA AD2007-04-11PREP.: VAPOUR SEAL TO BE DISPLACEDALI REFERENCE:ACCESS: 147FZ 734 536553-01-2* 0.14744* 0.10536553-0604-3 143 CENTER WING BOX LOWER PANELS NDT SDI T: 34000 FC ALI NTM 5365531 TBD B4-200144 I: 10500 FC FAA AD PART 41 TBD C4SPECIAL DETAILED INSPECTION OF CENTER WING BOX BOTTOMF4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 183APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536553-0604-3 * * * * * C O N T I N U E * * * * *SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR FROM EASA ADFROM 0 FC/FHRIB 1 LH TO RIB 1 RH. 2006-0071TO LOVFAA ADPREP.: VAPOUR SEAL TO BE DISPLACED 2007-04-11ACCESS: 147FZ 734 ALI REFERENCE: * 0.14744 536553-01-3* 0.10536554-0606-1 145 FRAME FOOT RUNOUTS FRAME 48 TO FRAME 54 NDT SDI T: SEE SB ALI NTM 5315091 2.00 ALL146 I: SEE SB FAA AD PART 61 2.00 SB 53-0238SPECIAL DETAILED INSPECTION OF FRAME FOOT RUNOUTS ISB EASA ADFROM 0 FC/FHFROM FRAME 48 TO FRAME 54 BETWEEN STRINGER 24 AND 2006-0071TO LOVSTRINGER 28 AND FILLETS OF FRAME 48 TO FRAME 54 ON LH FAA ADAND RH SIDES. 2007-04-11ISB 53-0238PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION,MAIN DECK FLOOR PANELS TO BE REMOVED ALI REFERENCE:536554-01-1ACCESS: 832* 0.10842* 0.10536555-0606-1 145 FRAME FOOT RUNOUTS FRAME 41 TO FRAME 46 NDT SDI T: SEE SB ALI NTM 5315091 8.00 ALL146 I: SEE SB FAA AD PART 61 8.00 SB 53-0345SPECIAL DETAILED INSPECTION OF FRAME FOOT RUNOUTS ISB EASA ADFROM 0 FC/FHFROM FRAME 41 TO FRAME 46 BETWEEN STRINGER 24 AND 2006-0071TO LOVSTRINGER 28 LH/RH. FAA AD2007-04-11PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, ISB 53-0345MAIN DECK FLOOR PANELS TO BE REMOVEDALI REFERENCE:ACCESS: 832 536555-01-1* 0.10536556-0606-1 145 GANTRIES AND CENTER WING BOX AT FRAME 46 MEC DET T: 48000 FC ALI EASA AD0 N/A B2146 OR FAA AD 2006-00710 N/A FROM 0 FC/FHDETAILED INSPECTION OF JUNCTION BETWEEN GANTRIES 53300 FH FAA ADTO LOVAND CENTER WING BOX UPPER PANEL AT FRAME 46, FROM I: 22000 FC 2007-04-11GANTRY 1 TO GANTRY 5 LH/RH. OR25000 FH ALI REFERENCE:PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R 536556-01-1MAIN DECK FLOOR PANELS TO BE REMOVEDSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 184APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536556-0606-2 145 GANTRIES AND CENTER WING BOX AT FRAME 46 MEC DET T: 40000 FC ALI EASA AD0 N/A B4-100146 OR FAA AD 2006-00710 N/A FROM 0 FC/FHDETAILED INSPECTION OF JUNCTION BETWEEN GANTRIES 55600 FH FAA ADTO LOVAND CENTER WING BOX UPPER PANEL AT FRAME 46, FROM I: 22000 FC 2007-04-11GANTRY 1 TO GANTRY 5 LH/RH. OR30300 FH ALI REFERENCE:PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R 536556-01-2MAIN DECK FLOOR PANELS TO BE REMOVED536556-0606-3 145 GANTRIES AND CENTER WING BOX AT FRAME 46 MEC DET T: 34000 FC ALI EASA AD0 N/A B4-200146 OR FAA AD 2006-00710 N/A C4DETAILED INSPECTION OF JUNCTION BETWEEN GANTRIES 74800 FH FAA ADF4AND CENTER WING BOX UPPER PANEL AT FRAME 46, FROM I: 22000 FC 2007-04-11FROM 0 FC/FHGANTRY 1 TO GANTRY 5 LH/RH. ORTO LOV48400 FH ALI REFERENCE:PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R 536556-01-3MAIN DECK FLOOR PANELS TO BE REMOVED536557-0606-1 241 CENTER WING BOX FRONT SPAR MEC DET T: 48000 FC ALI EASA AD0 N/A B2242 I: 8100 FC FAA AD 2006-00710 N/A FROM 0 FC/FHDETAILED INSPECTION OF SEAT TRACK FITTINGS BETWEEN FAA ADTO LOVFRAME 48 AND FRAME 53 LH/RH 2007-04-11PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R ALI REFERENCE:MAIN DECK FLOOR PANELS TO BE REMOVED 536557-01-1536557-0606-2 241 CENTER WING BOX FRONT SPAR MEC DET T: 40000 FC ALI EASA AD0 N/A B4-100242 I: 8100 FC FAA AD 2006-00710 N/A FROM 0 FC/FHDETAILED INSPECTION OF SEAT TRACK FITTINGS BETWEEN FAA ADTO LOVFRAME 48 AND FRAME 53 LH/RH 2007-04-11PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R ALI REFERENCE:MAIN DECK FLOOR PANELS TO BE REMOVED 536557-01-2536557-0606-3 241 CENTER WING BOX FRONT SPAR MEC DET T: 34000 FC ALI EASA AD0 N/A B4-200242 I: 8100 FC FAA AD 2006-00710 N/A C4DETAILED INSPECTION OF SEAT TRACK FITTINGS BETWEEN FAA ADF4FRAME 48 AND FRAME 53 LH/RH 2007-04-11FROM 0 FC/FHTO LOVPREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R ALI REFERENCE:MAIN DECK FLOOR PANELS TO BE REMOVED 536557-01-3STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 185APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536560-0606-1 141 CENTER WING BOX MEC DET T: 24000 FC ALI EASA AD1 TBD ALL142 I: 10000 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF CENTER WING BOX FRONT SPAR FAA ADTO LOVVERTICAL STIFFENER. 2007-04-11ACCESS: 147FZ 147GZ 147MZ ALI REFERENCE: * 0.13148GZ 148HZ 536560-01-1* 0.05R 536561-0606-1 141 CENTER WING BOX NDT SDI T: NOTE AD NTM 5130101 4.00 B2142 I: NOTE FAA PART 11 4.00 POSTSPECIAL DETAILED INSPECTION OF THE LOWER CORNER ANGLE ISB NTM 531504(53-0282)FITTING AT FRAME 47. PART 2,4 AND 6AD EU 2007-150NOTE: FOR INTERVAL AND THRESHOLD SEE ISB. FAA AD2008-14-09ACCESS: 147AZ ISB 53-0381* 0.23148AZ* 0.23R 536561-0606-2 141 CENTER WING BOX NDT SDI T: NOTE AD NTM 5130101 4.00 B4, C4, F4142 I: NOTE FAA PART 11 4.00 POSTSPECIAL DETAILED INSPECTION OF THE LOWER CORNER ANGLE ISB NTM 531504(53-0291)FITTING AT FRAME 47. PART 2,4 AND 6AD EU 2007-150NOTE: FOR INTERVAL AND THRESHOLD SEE ISB. FAA AD2008-14-09ACCESS: 147AZ ISB 53-0383* 0.23148AZ* 0.23536578-0604-1 147 INSPECTION OF MAIN LANDING GEAR CUTOUT MEC DET T: 21000 FC ALI EASA AD1 TBD POST 07301148 LOWER SKIN I: 6150 FC FAA AD 2006-00711 TBD (53-0239)151 FAA AD1 TBD FROM 0 FC/FH152 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL 2007-04-111 TBD TO LOV153 LAP JOINT AT STRINGER 36 AND STRINGER 44 LH/RH FROM1 TBD154 FRAME 54 TO MAIN LANDING GEAR CUT OUT INTERNAL ALI REFERENCE: 1 TBDSURFACE AND FRAME 54 TEE FITTING. 536578-01-1NOTE: THRESHOLD AFTER EMBODIMENT OF 07301 (53-0239)ACCESS: 147RZ* 0.01148RZ* 0.01577AB 577BB* 0.98677AB 677BB* 0.98STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 186APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536590-0606-1 145 CENTER FUSELAGE LONGITUDINAL BEAM AT NDT SDI T: 24000 FC ALI NTM 5365900 N/A ALL146 FRAME 49 I: 7500 FC FAA AD PART 60 N/A FROM 0 FC/FHEASA ADTO LOVSPECIAL DETAILED INSPECTION OF CENTER FUSELAGE 2006-0071LONGITUDINAL BEAM (GANTRY) VERTICAL STIFFENER AT FAA ADFRAME 49. 2007-04-11PREP.: PASSENGER SEATS, INSULATION, MAIN DECK FLOOR ALI REFERENCE:PANELS TO BE REMOVED 536590-01-1536596-0603-1 147 FUSELAGE - FUSELAGE CENTER SECTION NDT SDI T: SEE SB FAA AD NTM 53-15-111 16.00 ALL148 I: SEE SB PART 4 AND 61 16.00SPECIAL DETAILED INSPECTION OF THE LEFT AND RIGHT EASA ADGANTRIES 1,2,3,4 AND 5 LOWER FLANGE BETWEEN 2006-177FRAME 47 AND FRAME 54. FAA AD2004-18-13PREP.: FLOOR PANEL TO BE REMOVED ISB 53-0379ACCESS: 734 831* 0.20744* 0.10536597-0602-1 241 FUSELAGE CENTER SECTION MEC DET T: 48000 FC ALI EASA AD1 2.00 B2242 I: 5100 FC FAA AD 2006-00711 2.00 PRE 02611DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA ADFROM 48000FCTO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11TO LOVEXTERNAL.ALI REFERENCE:536597-02-7536597-0602-2 241 FUSELAGE CENTER SECTION MEC DET T: 48000 FC ALI EASA AD1 2.00 B2242 I: 8000 FC FAA AD 2006-00711 2.00 POST 02611DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA ADFROM 48000 FCTO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11TO LOVEXTERNAL.ALI REFERENCE:536597-02-8536597-0602-3 241 FUSELAGE CENTER SECTION MEC DET T: 40000 FC ALI EASA AD1 2.00 B4-100242 I: 5100 FC FAA AD 2006-00711 2.00 PRE 02611DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA ADFROM 40000 FCTO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11TO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 187APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536597-0602-3 * * * * * C O N T I N U E * * * * *EXTERNAL. ALI REFERENCE:536597-02-9536597-0602-4 241 FUSELAGE CENTER SECTION MEC DET T: 40000 FC ALI EASA AD1 2.00 B4-100242 I: 8000 FC FAA AD 2006-00711 2.00 POST 02611DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA ADFROM 40000 FCTO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11TO LOVEXTERNAL.ALI REFERENCE:536597-02-10536597-0602-5 241 FUSELAGE CENTER SECTION MEC DET T: 34000 FC ALI EASA AD1 2.00 B4-200242 I: 5100 FC FAA AD 2006-00711 2.00 C4DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA ADF4TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11PRE 02611EXTERNAL.FROM 34000 FCALI REFERENCE: TO LOV536597-02-11536597-0602-6 241 FUSELAGE CENTER SECTION MEC DET T: 34000 FC ALI EASA AD1 2.00 B4-200242 I: 8000 FC FAA AD 2006-00711 2.00 C4DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA ADF4TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11POST 02611EXTERNAL.FROM 34000 FCALI REFERENCE: TO LOV536597-02-12536597-0606-1 241 FUSELAGE CENTER SECTION NDT SDI T: SEE ISB ALI NTM 5315101 2.00 B2242 I: SEE ISB FAA AD PART 61 2.00 FROM 0 FC/FHSPECIAL DETAILED OR DETAILED INSPECTION OF STRINGER ISB EASA ADTO 48000 FCRUN OUTS AT FRAME 47 FORWARD AND REAR INTERNAL SIDE 2006-0071FROM STRINGER 22 TO STRINGER 28. FAA AD2007-04-11PREP.: PASSENGER SEATS, INSULATION, MAIN DECK ISB 53-0237FLOOR PANELS TO BE REMOVEDALI REFERENCE:ACCESS: 831 536597-01-1* 0.10841* 0.10STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 188APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536597-0606-2 241 FUSELAGE CENTER SECTION NDT SDI T: SEE ISB ALI NTM 5315101 2.00 B4-100242 I: SEE ISB FAA AD PART 61 2.00 FROM 0 FC/FHSPECIAL DETAILED OR DETAILED INSPECTION OF STRINGER ISB EASA ADTO 40000 FCRUN OUTS AT FRAME 47 FORWARD AND REAR INTERNAL SIDE 2006-0071FROM STRINGER 22 TO STRINGER 28. FAA AD2007-04-11PREP.: PASSENGER SEATS, INSULATION, MAIN DECK ISB 53-0237FLOOR PANELS TO BE REMOVEDALI REFERENCE:ACCESS: 831 536597-01-1* 0.10841* 0.10536597-0606-3 241 FUSELAGE CENTER SECTION NDT SDI T: SEE ISB ALI NTM 5315101 2.00 B4-200242 I: SEE ISB CN PART 61 2.00 C4SPECIAL DETAILED OR DETAILED INSPECTION OF STRINGER FAA AD EASA ADF4RUN OUTS AT FRAME 47 FORWARD AND REAR INTERNAL SIDE ISB 2006-0071FROM 0 FC/FHFROM STRINGER 22 TO STRINGER 28. FAA ADTO 34000 FC2007-04-11PREP.: PASSENGER SEATS, INSULATION, MAIN DECK ISB 53-0237FLOOR PANELS TO BE REMOVEDALI REFERENCE:ACCESS: 831 536597-01-1* 0.10841* 0.10536598-0606-1 145 GANTRIES 1 TO 5 MEC DET T: 21000 FC ALI EASA AD1 0.25 B2146 OR FAA AD 2006-00711 0.25 PRE 07757DETAILED INSPECTION OF GANTRIES 1 TO 5, 23900 FH FAA AD(53-0272)LH/RH, AT FRAME 46. I: 1100 FC 2007-04-11FROM 0 FC/FHORTO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-1 1200 FH ALI REFERENCE:536598-01-1ACCESS: 241AEF 241AFF 241AGF 241AHF* 0.58242AAF 242ABF 242ZF* 0.43536598-0606-2 145 GANTRIES 1 TO 5 MEC DET T: 21000 FC ALI EASA AD1 0.25 B4-100146 OR FAA AD 2006-00711 0.25 PRE 07757DETAILED INSPECTION OF GANTRIES 1 TO 5, 29200 FH FAA AD(53-0272)LH/RH, AT FRAME 46. I: 1100 FC 2007-04-11PRE 03474ORFROM 0 FC/FHNOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-2 1500 FH ALI REFERENCE: TO LOVAND 536598-0607-3 536598-01-2* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 189APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536598-0606-2 * * * * * C O N T I N U E * * * * *ACCESS: 241AEF 241AFF 241AGF 241AHF* 0.58242AAF 242ABF 242ZF* 0.43536598-0606-3 145 GANTRIES 1 TO 5 MEC DET T: 21000 FC ALI EASA AD1 0.25 B4-200146 OR FAA AD 2006-00711 0.25 C4DETAILED INSPECTION OF GANTRIES 1 TO 5, 48700 FH FAA ADF4LH/RH, AT FRAME 46. I: 1200 FC 2007-04-11PRE 07757OR(53-0272)NOTE : THIS TASK IS AN ALTRNATIVE TO 536598-0607-4 2800 FH ALI REFERENCE: PRE 03474536598-01-3FROM 0 FC/FHACCESS: 241AEF 241AFF 241AGF 241AHF* 0.58 TO LOV242AAF 242ABF 242ZF* 0.43536598-0606-5 145 GANTRIES 1 TO 5 MEC DET T: 26000 FC ALI EASA AD1 0.25 B4-200146 OR FAA AD 2006-00711 0.25 C4DETAILED INSPECTION OF GANTRIES 1 TO 5, 60300 FH FAA ADF4LH/RH, AT FRAME 46. I: 2500 FC 2007-04-11PRE 07757OR(53-0272)NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-5 5800 FH ALI REFERENCE: POST 03474536598-01-4FROM 0 FC/FHACCESS: 241DF 241EF 241FF 241HF* 2.25 TO 34000 FC242AF 242BF 242ZF* 1.35536598-0606-6 145 GANTRIES 1 TO 5 MEC DET I: 2100 FC ALI EASA AD1 0.25 B4-200146 OR FAA AD 2006-00711 0.25 C4DETAILED INSPECTION OF GANTRIES 1 TO 5, 4800 FH FAA ADF4LH/RH, AT FRAME 46. 2007-04-11PRE 07757(53-0272)NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-5 ALI REFERENCE: POST 03474536598-01-5FROM 34000 FCACCESS: 241DF 241EF 241FF 241HF* 2.25 TO LOV242AF 242BF 242ZF* 1.35536598-0607-1 145 GANTRIES 1 TO 5 NDT SDI T: 21000 FC ALI NTM 5315211 0.25 B2146 OR FAA AD PART 61 0.25 PRE 07757SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 23900 FH EASA AD(53-0272)AT FRAME 46. I: 6600 FC 2006-0071FROM 0 FC/FHOR FAA ADTO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-1 7500 FH 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 190APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536598-0607-1 * * * * * C O N T I N U E * * * * *ACCESS: 241AEF 241AFF 241AGF 241AHF ALI REFERENCE: * 0.58242AAF 242ABF 242ZF 536598-02-1* 0.43536598-0607-2 145 GANTRIES 1 TO 5 NDT SDI T: 21000 FC ALI NTM 5315211 0.25 B4-100146 OR FAA AD PART 61 0.25 PRE 07757SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 29200 FH EASA AD(53-0272)AT FRAME 46. I: 7000 FC 2006-0071PRE 03474OR FAA ADFROM 0 FC/FHNOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-2 9700 FH 2007-04-11TO 40000 FCACCESS: 241AEF 241AFF 241AGF 241AHF ALI REFERENCE: * 0.58242AAF 242ABF 242ZF 536598-02-2* 0.43536598-0607-3 145 GANTRIES 1 TO 5 NDT SDI I: 6600 FC ALI NTM 5315211 0.25 B4-100146 OR FAA AD PART 61 0.25 PRE 07757SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 9200 FH EASA AD(53-0272)AT FRAME 46. 2006-0071PRE 03474FAA ADFROM 40000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-2 2007-04-11TO LOVACCESS: 241AEF 241AFF 241AGF 241AHF ALI REFERENCE: * 0.58242AAF 242ABF 242ZF 536598-02-3* 0.43536598-0607-4 145 GANTRIES 1 TO 5 NDT SDI T: 21000 FC ALI NTM 5315211 0.25 B4-200146 OR FAA AD PART 61 0.25 C4SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 48700 FH EASA ADF4LH/RH AT FRAME 46. I: 7000 FC 2006-0071PRE 07757OR FAA AD(53-0272)NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-3 16200 FH 2007-04-11PRE 03474FROM 0 FC/FHACCESS: 241AEF 241AFF 241AGF 241AHF ALI REFERENCE: * 0.58 TO LOV242AAF 242ABF 242ZF 536598-02-4* 0.43536598-0607-5 145 OANTRIES 1 TO 5 MEC SDI T: 26000 FC ALI NTM 5315211 0.25 B4-200146 OR FAA AD PART 61 0.25 C4SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 60300 FH EASA ADF4AT FRAME 46. I: 8000 FC 2006-0071PRE 07757OR FAA AD(53-0272)NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-5 18500 FH 2007-04-11POST 03474* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 191APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536598-0607-5 * * * * * C O N T I N U E * * * * *AND 536598-0606-6 ALI REFERENCE: FROM 0 FC/FH536598-02-5TO LOVACCESS: 241AEF 241AFF 241AGF 241AHF* 0.58242AAF 242ABF 242ZF* 0.43536599-0606-1 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET T: 32000 FC ALI EASA AD1 0.15 B2148 OR FAA AD 2006-00711 0.15 FROM 0 FC/FHDETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 36100 FH FAA ADTO 48000 FCCENTER WING BOX REAR SPAR ATTACHMENT FITTINGS AND I: 5600 FC 2007-04-11TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN ORFRAME 47 AND FRAME 48 LH/RH. 6300 FH ALI REFERENCE:536599-01-1NOTE: THIS TASK IS AN ALTERNATIVE TO 53699-0606-4PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0606-2 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET T: 30000 FC ALI EASA AD1 0.15 B4-100148 OR FAA AD 2006-00711 0.15 FROM 0 FC/FHDETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 41100 FH FAA ADTO 40000 FCCENTER WING BOX REAR SPAR ATTACHMENT FITTINGS AND I: 6500 FC 2007-04-11TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN ORFRAME 47 AND FRAME 48 LH/RH. 8900 FH ALI REFERENCE:536599-01-3NOTE: THIS TASK IS AN ALTERNATIVE TO 53699-0606-5PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0606-3 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET T: 28000 FC ALI EASA AD1 0.15 B4-200148 OR FAA AD 2006-00711 0.15 C4DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 63500 FH FAA ADF4CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS AND I: 6000 FC 2007-04-11FROM 0 FC/FHTO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN ORTO 34000 FCFRAME 47 AND FRAME 48 LH/RH. 13600 FH ALI REFERENCE:536599-01-5NOTE: THIS TASK IS AN ALTERNATIVE TO 53699-0606-6PREP.: MAIN LANDING GEAR DOORS OPENED.STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 192APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536599-0606-4 147 PRESSURIZED FLOOR AT FRAME 47 NDT SDI T: 32000 FC ALI NTM 5315271 0.15 B2148 OR FAA AD PART 61 0.15 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 36100 FH EASA ADTO 48000 FCPANELS TO CENTER WING BOX REAR SPAR ATTACHMENT I: 13200 FC 2006-0071FITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS OR FAA ADBETWEEN FRAME 47 AND FRAME 48 LH/RH. 14900 FH 2007-04-11NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0606-1 ALI REFERENCE:536599-02-1PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0606-5 147 PRESSURIZED FLOOR AT FRAME 47 NDT SDI T: 30000 FC ALI NTM 5315271 0.15 B4-100148 OR FAA AD PART 61 0.15 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 41100 FH EASA ADTO LOVPANELS TO CENTER WING BOX REAR SPAR ATTACHMENT I: 9900 FC 2006-0071FITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS OR FAA ADBETWEEN FRAME 47 AND FRAME 48 LH/RH. 13500 FH 2007-04-11NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0606-2 ALI REFERENCE:AND 536599-0607-2 536599-02-3PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0606-6 147 PRESSURIZED FLOOR AT FRAME 47 NDT SDI T: 28000 FC ALI NTM 5315271 0.15 B4-200148 OR FAA AD PART 61 0.15 C4SPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 63500 FH EASA ADF4PANELS TO CENTER WING BOX REAR SPAR ATTACHMENT I: 8300 FC 2006-0071FROM 0 FC/FHFITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS OR FAA ADTO LOVBETWEEN FRAME 47 AND FRAME 48 LH/RH. 18800 FH 2007-04-11NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0606-3 ALI REFERENCE:AND 536599-0607-3 536599-02-4PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0607-1 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET I: 3000 FC ALI EASA AD1 0.15 B2148 OR FAA AD 2006-00711 0.15 FROM 48000 FCDETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 3400 FH FAA ADTO LOVCENTER WING BOX REAR SPAR ATTACHMENT FITTINGS 2007-04-11AND TO HORIZONTAL BEAM ATTACHMENT FITTING BETWEENFRAME 47 AND FRAME 48 LH/RH. ALI REFERENCE:536599-01-2* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 193APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536599-0607-1 * * * * * C O N T I N U E * * * * *NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0607-4PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0607-2 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET I: 2700 FC ALI EASA AD1 0.15 B4-100148 OR FAA AD 2006-00711 0.15 FROM 40000 FCDETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 3700 FH FAA ADTO LOVCENTER WING BOX REAR SPAR ATTACHMENT FITTINGS 2007-04-11AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEENFRAME 47 AND FRAME 48 LH/RH. ALI REFERENCE:536599-01-4NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0607-5PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0607-3 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET I: 2300 FC ALI EASA AD1 0.15 B4-200148 OR FAA AD 2006-00711 0.15 C4DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 5200 FH FAA ADF4CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS 2007-04-11FROM 34000 FCAND TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEENTO LOVFRAME 47 AND FRAME 48 LH/RH. ALI REFERENCE:536599-01-6NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0607-6PREP.: MAIN LANDING GEAR DOORS OPENED.536599-0607-4 147 PRESSURIZED FLOOR AT FRAME 47 NDT SDI I: 10000 FC ALI NTM 5315271 0.15 B2148 OR FAA AD PART 61 0.15 FROM 48000 FCSPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 11300 FH EASA ADTO LOVPANELS TO CENTER WING BOX REAR SPAR ATTACHMENT 2006-0071FITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS FAA ADBETWEEN FRAME 47 AND FRAME 48 LH/RH. 2007-04-11NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0607-1 ALI REFERENCE:536599-02-2PREP.: MAIN LANDING GEAR DOORS OPENED.536601-0606-1 251 EMERGENCY EXIT TORSION BOX BEAM NDT NDT T: SEE SB ALI NTM 5316001 0.25 ALL252 I: SEE SB CN PART 61 0.25 SB 53-0254* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 194APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536601-0606-1 * * * * * C O N T I N U E * * * * *253 NDT INSPECTION OF EMERGENCY EXIT FAA AD CN 2006-0071(B) 1 0.25 FROM 0 FC/FH254 TORSION BOX BEAM BETWEEN FRAME 57 A AND FRAME 58 ISB FAA AD 96-13-11 1 0.25 TO LOVFROM STRINGER 14 TO STRINGER 15 LH/RH. ISB 53-0254PREP.: OVERHEAD STOWAGE COMPARTMENT, UPPER SIDEWALL ALI REFERENCE:PANELS BETWEEN FRAME 57 A AND FRAME 58 TO 536601-01-1BE REMOVED.BE REMOVED.ACCESS: 833* 0.10843* 0.10536602-0606-1 243 SPLICE PLATE AT FRAME 54.3 NDT SDI T: SEE SB ALI NTM 5330211 8.00 ALL244 I: SEE SB CN PART 41 8.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION (US AND EDDY CURRENT) OF FAA AD NTM 533021TO LOVSPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FRAME ISB PART 654.3 FROM STRINGER 12 TO CROWN CENTER LINE LH/RH. CN 2006-0071(B)FAA AD 96-13-11ISB 53-0257ALI REFERENCE:536602-01-1536603-0606-1 243 SPLICE PLATE AT FRAME 55 NDT SDI T: SEE SB ALI NTM 5330211 8.00 ALL244 I: SEE SB CN PART 41 8.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD AND PART 6TO 42500 FCCIRCUMFERENTIAL SKIN SPLICE AT FRAME 55 FROM STRINGER ISB CN 2006-0071(B)12 TO STRINGER 5 LH/RH. FAA AD 96-13-11ISB 53-0257PREP.: HATRACKS, LININGS, INSULATION TO BE REMOVED.ALI REFERENCE:536603-01-1536651-0606-2 243 FUSELAGE AT FRAME 54 MEC DET T: 19000 FC ALI CN 2006-0071(B) 1 0.50 B2244 OR CN FAA AD 96-13-11 1 0.50 PRE 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 21500 FH FAA ADFROM 0 FC/FHCOUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 7000 FC ALI REFERENCE: TO LOVLH/RH. OR 536651-01-1MSN 4 EXCLUDED7900 FHPREP.: LINING, INSULATION AND SEALANT REMOVED* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 195APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536651-0606-2 * * * * * C O N T I N U E * * * * *NOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0607-2536651-0606-3 243 FUSELAGE AT FRAME 54 MEC DET T: 25000 FC ALI CN 2006-0071(B) 1 0.50 B2244 OR CN FAA AD 96-13-11 1 0.50 POST 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 28200 FH FAA ADFROM 0 FC/FHCOUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 8500 FC ALI REFERENCE: TO LOVLH/RH. OR 536651-01-29600 FHPREP.: LINING, INSULATION AND SEALANT REMOVEDNOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0607-3536651-0606-4 243 FUSELAGE AT FRAME 54 MEC DET T: 18000 FC ALI CN 2006-0071(B) 1 0.50 B4-100244 OR CN FAA AD 96-13-11 1 0.50 PRE 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 24500 FH FAA ADFROM 0 FC/FHCOUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 6400 FC ALI REFERENCE: TO LOVLH/RH. OR 536651-01-38700 FHPREP.: LINING, INSULATION AND SEALANT REMOVEDNOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0607-4536651-0606-5 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI CN 2006-0071(B) 1 0.50 B4-100244 OR CN FAA AD 96-13-11 1 0.50 POST 02974DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 32600 FC FAA ADFROM 0 FC/FHCOUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 8300 FC ALI REFERENCE: TO LOVLH/RH. OR 536651-01-411300 FHPREP.: LINING, INSULATION AND SEALANT REMOVEDNOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0607-5536651-0606-6 243 FUSELAGE AT FRAME 54 MEC DET T: 18000 FC ALI CN 2006-0071(B) 1 0.50 B4-200244 OR CN FAA AD 96-13-11 1 0.50 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 196APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536651-0606-6 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 39800 FH FAA AD ALI REFERENCE: F4COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 6400 FC 536651-01-5PRE 02974LH/RH. ORFROM 0 FC/FH14100 FHTO LOVPREP.: LINING, INSULATION AND SEALANT REMOVEDNOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0607-6536651-0606-7 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI CN 2006-0071(B) 1 0.50 B4-200244 OR CN FAA AD 96-13-11 1 0.50 C4DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 53000 FH FAA ADF4COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 8300 FC ALI REFERENCE: POST 02974LH/RH. OR 536651-01-6FROM 0 FC/FH18300 FHTO LOVPREP.: LINING, INSULATION AND SEALANT REMOVEDNOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0607-7536651-0607-2 243 FUSELAGE AT FRAME 54 MEC DET T: 19000 FC ALI NTM 5315251 0.50 B2244 OR CN PART 61 0.50 PRE 02974SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 21500 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHSTRINGER 13 COUPLING AREAS AT FRAME 54 I: 9200 FC FAA AD 96-13-11 TO LOVCIRCUMFERENTIAL JOINT LH/RH. OR10400 FH ALI REFERENCE:PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-1NOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0606-2536651-0607-3 243 FUSELAGE AT FRAME 54 MEC DET T: 25000 FC ALI NTM 5315251 0.50 B2244 OR CN PART 61 0.50 POST 02974SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 28200 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHSTRINGER 13 COUPLING AREAS AT FRAME 54 I: 9700 FC FAA AD 96-13-11 TO LOVCIRCUMFERENTIAL JOINT LH/RH. OR10900 FH ALI REFERENCE:PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-2NOTE: THIS TASK IS AN ALTERNATIVE TO* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 197APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536651-0607-3 * * * * * C O N T I N U E * * * * *TASK 536651-0606-3536651-0607-4 243 FUSELAGE AT FRAME 54 MEC DET T: 18000 FC ALI NTM 5315251 0.50 B4-100244 OR CN PART 61 0.50 PRE 02974SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 24500 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHSTRINGER 13 COUPLING AREAS AT FRAME 54 I: 8200 FC FAA AD 96-13-11 TO LOVCIRCUMFERENTIAL JOINT LH/RH. OR11100 FH ALI REFERENCE:PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-3NOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0606-4536651-0607-5 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI NTM 5315251 0.50 B4-100244 OR CN PART 61 0.50 POST 02974SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 32600 FC FAA AD CN 2006-0071(B) FROM 0 FC/FHSTRINGER 13 COUPLING AREAS AT FRAME 54 I: 9400 FC FAA AD 96-13-11 TO LOVCIRCUMFERENTIAL JOINT LH/RH. OR12800 FH ALI REFERENCE:PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-4NOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0606-5536651-0607-6 243 FUSELAGE AT FRAME 54 MEC SDI T: 18000 FC ALI NTM 5315251 0.50 B4-200244 OR CN PART 61 0.50 C4SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 39800 FH FAA AD CN 2006-0071(B) F4STRINGER 13 COUPLING AREAS AT FRAME 54 I: 8200 FC FAA AD 96-13-11 PRE 02974CIRCUMFERENTIAL JOINT LH/RH. ORFROM 0 FC/FH18100 FH ALI REFERENCE: TO LOVPREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-5NOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0606-6536651-0607-7 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI NTM 5315251 0.50 B4-200244 OR CN PART 61 0.50 C4SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 53000 FH FAA AD CN 2006-0071(B) F4STRINGER 13 COUPLING AREAS AT FRAME 54 I: 9400 FC FAA AD 96-13-11 POST 02974* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 198APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536651-0607-7 * * * * * C O N T I N U E * * * * *CIRCUMFERENTIAL JOINT LH/RH. OR ALI REFERENCE: FROM 0 FC/FH20800 FH 536651-02-6TO LOVPREP.: LINING, INSULATION AND SEALANT REMOVEDNOTE: THIS TASK IS AN ALTERNATIVE TOTASK 536651-0606-7536652-0606-2 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 5330211 0.25 B2244 OR FAA AD PART 41 0.25 FROM 0 FC/FHSPECIAL DETAILED INSPECTION (LF-EC) OF SPLICE PLATE 59700 FH EASA ADTO 48000 FCAT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO I: 6100 FC 2006-0071CROWN CENTERLINE RH/LH. OR FAA AD6900 FH 2007-04-11ALI REFERENCE:536652-01-1536652-0606-3 243 SPLICE PLATE AT FRAME 54 NDT SDI I: 6100 FC ALI NTM 5315261 0.25 B2244 OR FAA AD PART 61 0.25 FROM 48000 FCSPECIAL DETAILED INSPECTION (LF-EC) OF SPLICE PLATE 6900 FH EASA ADTO LOVAT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO 2006-0071CROWN CENTERLINE RH/LH. FAA AD2007-04-11ALI REFERENCE:536652-01-2536652-0606-4 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 5315261 0.25 B4-100244 OR FAA AD PART 61 0.25 FROM 0 FC/FHSPECIAL DETAILED INSPECTION (LF-EC) OF SPLICE PLATE 59700 FH EASA ADTO LOVAT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO I: 5700 FC 2006-0071CROWN CENTERLINE RH/LH. OR FAA AD7700 FH 2007-04-11ALI REFERENCE:536652-01-3536652-0606-5 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 5315261 0.25 B4-200244 OR FAA AD PART 61 0.25 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 199APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536652-0606-5 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION (LF-EC) OF SPLICE PLATE 97000 FH EASA ADF4AT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO I: 5700 FC 2006-0071FROM 0 FC/FHCROWN CENTERLINE RH/LH. OR FAA ADTO LOV12600 FH 2007-04-11ALI REFERENCE:536652-01-4536652-0606-6 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 47000 FC ALI NTM 5315261 0.25 B2244 OR FAA AD PART 61 0.25 FROM 0 FC/FHSPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 53100 FH EASA ADTO 48000 FCFRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN I: 18400 FC 2006-0071CENTERLINE RH/LH. OR FAA AD20800 FH 2007-04-11ALI REFERENCE:536652-02-1536652-0606-7 243 SPLICE PLATE AT FRAME 54 NDT SDI I: 18400 FC ALI NTM 5315261 0.25 B2244 OR FAA AD PART 61 0.25 FROM 48000 FCSPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 20800 FH EASA ADTO LOVFRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN 2006-0071CENTERLINE RH/LH. FAA AD2007-04-11ALI REFERENCE:536652-02-2536652-0606-8 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 5315261 0.25 B4-100244 OR FAA AD PART 61 0.25 FROM 0 FC/FHSPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 59700 FH EASA ADTO LOVFRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN I: 10300 FC 2006-0071CENTERLINE RH/LH. OR FAA AD14000 FH 2007-04-11ALI REFERENCE:536652-02-3STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 200APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536652-0606-9 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 5315261 0.25 B4-200244 OR FAA AD PART 61 0.25 C4SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 97000 FH EASA ADF4FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN I: 10300 FC 2006-0071FROM 0 FC/FHCENTERLINE RH/LH. OR FAA ADTO LOV22800 FH 2007-04-11ALI REFERENCE:536652-02-4536653-0602-1 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENCE: 1 TBD B2242 FRAME 55 OR 536653-01-11 TBD FROM 0 FC/FH243 45600 FH1 TBD TO LOV244 DETAILED INSPECTION OF SECTION 16 IN AREA OF I: 12000 FC1 TBDSTRINGER COUPLING RUN OUT AT CIRCUMFERENTIAL JOINT ORFRAME 55 FROM STRINGER 5 TO STRINGER 12 LH/RH 13600 FHEXTERNAL SURFACE.536653-0602-2 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENCE: 1 TBD B4-100242 FRAME 55 OR 536653-01-21 TBD FROM 0 FC/FH243 55600 FH1 TBD TO LOV244 DETAILED INSPECTION OF SECTION 16 IN AREA OF I: 12000 FC1 TBDSTRINGER COUPLING RUN OUT AT CIRCUMFERENTIAL JOINT ORFRAME 55 FROM STRINGER 5 TO STRINGER 12 LH/RH 16600 FHEXTERNAL SURFACE.536653-0602-3 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200242 FRAME 55 OR 2006-00711 TBD C4243 78800 FH FAA AD1 TBD F4244 DETAILED INSPECTION OF SECTION 16 IN AREA OF I: 10500 FC 2007-04-111 TBD FROM 0 FC/FHSTRINGER COUPLING RUN OUT AT CIRCUMFERENTIAL JOINT ORTO LOVFRAME 55 FROM STRINGER 5 TO STRINGER 12 LH/RH 24300 FH ALI REFERENCE:EXTERNAL SURFACE. 536653-01-3536654-0604-1 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENCE: 1 TBD B2242 FRAME 55 OR 536654-01-11 TBD FROM 0 FC/FH243 45600 FH1 TBD TO LOV244 DETAILED INSPECTION OF STRINGER COUPLING AT I: 12000 FC1 TBDCIRCUMFERENTIAL JOINT FRAME 55 STRINGER 5 TO ORSTRINGER 12 LH/RH INTERNAL. 13600 FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 201APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536654-0604-1 * * * * * C O N T I N U E * * * * *PREP:. LININGS AND INSULATION TO BE REMOVED536654-0604-2 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENCE: 1 TBD B4-100242 FRAME 55 OR 536654-01-21 TBD FROM 0 FC/FH243 55600 FH1 TBD TO LOV244 DETAILED INSPECTION OF STRINGER COUPLING AT I: 12000 FC1 TBDCIRCUMFERENTIAL JOINT FRAME 55 STRINGER 5 TO ORSTRINGER 12 LH/RH INTERNAL. 16600 FHPREP:. LININGS AND INSULATION TO BE REMOVED536654-0604-3 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200242 FRAME 55 OR 2006-00711 TBD C4243 78800 FH FAA AD1 TBD F4244 DETAILED INSPECTION OF STRINGER COUPLING AT I: 10500 FC 2007-04-111 TBD FROM 0 FC/FHCIRCUMFERENTIAL JOINT FRAME 55 STRINGER 5 TO ORTO LOVSTRINGER 12 LH/RH INTERNAL. 24300 FH ALI REFERENCE:536654-01-3PREP:. LININGS AND INSULATION TO BE REMOVED536701-0606-1 162 FUSELAGE BETWEEN FRAME 66 AND FRAME 67 MEC DET T: SEE SB ALI CN 2006-0071(B) 1 1.50 ALL164 I: SEE SB CN FAA AD 96-13-11 1 1.50 SB 53-0255DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE FAA AD ISB 53-0255FROM 0 FC/FHBETWEEN AND INCLUDING FRAME 66 AND FRAME 67 FROM ISBTO LOVSTRINGER 42 TO STRINGER 46, RH. ALI REFERENCE:536701-01-1PREP.: FLOOR PANELS, LININGS AND INSULATIONTO BE REMOVED.ACCESS: 813* 0.01536702-0606-1 253 SPLICE PLATE AT FRAME 58 NDT SDI T: SEE SB ALI NTM 5330211 4.00 ALL254 I: SEE SB CN PART 4 AND 61 4.00 SB 53-0260SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071(B) FROM 0 FC/FHCIRCUMFERENTIAL SKIN SPLICE AT FRAME 58, FROM ISB FAA AD 96-13-11 TO LOVSTRINGER 13 TO CROWN CENTER LINE LH/RH. ISB 53-0260TO 42500 FCPREP.: HATRACKS LININGS INSULATION TO BE REMOVED. ALI REFERENCE:536702-01-1STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 202APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536703-0606-1 253 SPLICE PLATE AT FRAME 65 NDT SDI T: SEE SB ALI NTM 5330211 4.00 B2254 I: SEE SB CN PART 4 AND 61 4.00 SB 53-0261SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071(B) FROM 0 FC/FHCIRCUMFERENTIAL SKIN SPLICE AT FRAME 65 FROM STRINGER ISB FAA AD 96-13-11 TO 42500 FC13 TO CROWN CENTERLINE LH/RH ISB 53-0261PREP.: LININGS, HATRACKS, INSULATION ALI REFERENCE:TO BE REMOVED. 536703-01-1536703-0606-2 253 SPLICE PLATE AT FRAME 65 NDT SDI T: SEE SB ALI NTM 5330211 4.00 B4-100254 I: SEE SB CN PART 4 AND 61 4.00 SB 53-0261SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071(B) FROM 0 FC/FHCIRCUMFERENTIAL SKIN SPLICE AT FRAME 65 FROM STRINGER ISB FAA AD 96-13-11 TO 41700 FC13 TO CROWN CENTERLINE LH/RH ISB 53-0261PREP.: LININGS, HATRACKS, INSULATION ALI REFERENCE:TO BE REMOVED. 536703-01-2536703-0606-3 253 SPLICE PLATE AT FRAME 65 NDT SDI T: SEE SB ALI NTM 5330211 4.00 B4-200254 I: SEE SB CN PART 4 AND 61 4.00 C4SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071(B) F4CIRCUMFERENTIAL SKIN SPLICE AT FRAME 65 FROM STRINGER ISB FAA AD 96-13-11 SB 53-026113 TO CROWN CENTERLINE LH/RH ISB 53-0261FROM 0 FC/FHTO 48000 FCPREP.: LININGS, HATRACKS, INSULATION ALI REFERENCE:TO BE REMOVED. 536703-01-3536704-0606-1 154 FUSELAGE FRAME 60 TO 63 MEC DET ST: 30000 FC ALI CN 2006-0071(B) 1 1.00 B2SI: 7000 FC FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF ATTACHMENT AREA OFTO 48000 FCFRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN ALI REFERENCE:STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE. 536704-01-1NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-4PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0606-2 154 FUSELAGE FRAME 60 TO 63 MEC DET ST: 30000 FC ALI CN 2006-0071(B) 1 1.00 B4-200SI: 5600 FC FAA AD 96-13-11 C4DETAILED INSPECTION OF ATTACHMENT AREAF4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 203APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536704-0606-2 * * * * * C O N T I N U E * * * * *OF FRAMES 60 TO 63, TO LOCK FITTINGS BETWEEN ALI REFERENCE: FROM 0 FC/FHSTRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-3TO 34000 FCNOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-5PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0606-3 154 FUSELAGE FRAME 60 TO 63 MEC DET ST: 30000 FC ALI CN 2006-0071(B) 1 1.00 B4-100SI: 8400 FC FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF ATTACHMENT AREATO 40000 FCOF FRAMES 60 TO 63, TO LOCK FITTINGS BETWEEN ALI REFERENCE:STRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-2NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-6PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0606-4 154 FUSELAGE FRAME 60 TO 63 NDT SDI ST: 30000 FC ALI NTM 5317001 1.00 B2SI: 11600 FC PART 6FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) TO 48000 FCFRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13-11STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.ALI REFERENCE:NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-1 536704-02-1PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0606-5 154 FUSELAGE FRAME 60 TO 63 NDT SDI ST: 30000 FC ALI NTM 5317001 1.00 B4-200SI: 9100 FC PART 6C4SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) F4FRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13-11 FROM 0 FC/FHSTRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.TO 34000 FCALI REFERENCE:NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-2 536704-02-3PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 204APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536704-0606-6 154 FUSELAGE FRAME 60 TO 63 NDT SDI ST: 30000 FC ALI NTM 5317001 1.00 B4-100SI: 10000 FC PART 6FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) TO 40000 FCFRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13-11STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.ALI REFERENCE:NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-3 536704-02-2PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0607-1 154 FUSELAGE FRAME 60 TO 63 MEC DET I: 5600 FC ALI CN 2006-0071(B) 1 1.00 B2FAA AD 96-13-11 FROM 48000 FCDETAILED INSPECTION OF ATTACHMENT AREA OFTO LOVFRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN ALI REFERENCE:STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE. 536704-01-4NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0607-4PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0607-2 154 FUSELAGE FRAME 60 TO 63 MEC DET I: 5600 FC ALI CN 2006-0071(B) 1 1.00 B4-100FAA AD 96-13-11 FROM 40000 FCDETAILED INSPECTION OF ATTACHMENT AREATO LOVOF FRAMES 60 TO 63, TO LOCK FITTINGS BETWEEN ALI REFERENCE:STRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-5NOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-5PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0607-3 154 FUSELAGE FRAME 60 TO 63 MEC DET I: 5600 FC ALI CN 2006-0071(B) 1 1.00 B4-200FAA AD 96-13-11 C4DETAILED INSPECTION OF ATTACHMENT AREAF4OF FRAMES 60 TO 63, TO LOCK FITTINGS BETWEEN ALI REFERENCE: FROM 34000 FCSTRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-6TO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-6PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 205APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536704-0607-3 * * * * * C O N T I N U E * * * * *(12.0 M/H)536704-0607-4 154 FUSELAGE FRAME 60 TO 63 NDT SDI I: 9100 FC ALI NTM 5317001 1.00 B2PART 6FROM 48000 FCSPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071(B) TO LOVFRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13-11STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.ALI REFERENCE:NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0607-1 536704-02-4PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0607-5 154 FUSELAGE FRAME 60 TO 63 NDT SDI I: 9100 FC ALI NTM 5317001 1.00 B4-100PART 6FROM 40000 FCSPECIAL DETAILED INSPECTION (EDDY CURRENT) OF CN 2006-0071(B) TO LOVATTACHMENT AREA OF FRAME 60 TO FRAME 63, TO LOCK FAA AD 96-13-11FITTINGS BETWEEN STRINGER 44 AND STRINGER 48 RH,INTERNAL STRUCTURE. ALI REFERENCE:536704-02-5NOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-2PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536704-0607-6 154 FUSELAGE FRAME 60 TO 63 NDT SDI I: 9100 FC ALI NTM 5317001 1.00 B4-200PART 6C4SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF CN 2006-0071(B) F4ATTACHMENT AREA OF FRAME 60 TO FRAME 63, TO LOCK FAA AD 96-13-11 FROM 34000 FCFITTINGS BETWEEN STRINGER 44 AND STRINGER 48 RH,TO LOVINTERNAL STRUCTURE. ALI REFERENCE:536704-02-6NOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-3PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.(12.0 M/H)536705-0606-1 240 FUSELAGE INTERNAL STRUCTURE MEC DET T: 40000 FC ALI CN 2006-0071(B) 1 TBD B2I: 6000 FC FAA AD 96-13-11 B4-100* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 206APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536705-0606-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF FUSELAGE INTERNAL ALI REFERENCE: FROM 0 FC/FHSTRUCTURE FROM FRAME 59 TO FRAME 64, AND FROM 536705-01-1TO LOVSTRINGER 18 TO STRINGER 23, LH/RH, IN FRAMECOUPLING AREAS.ACCESS: REMOVE LINING AND INSULATION536705-0606-2 240 FUSELAGE INTERNAL STRUCTURE MEC DET T: 34000 FC ALI CN 2006-0071(B) 1 TBD B4-200I: 6000 FC FAA AD 96-13-11 C4DETAILED INSPECTION OF FUSELAGE INTERNALF4STRUCTURE FROM FRAME 59 TO FRAME 64, AND FROM ALI REFERENCE: FROM 0 FC/FHSTRINGER 18 TO STRINGER 23, LH/RH, IN FRAME 536705-01-2TO LOVCOUPLING AREAS.ACCESS: REMOVE LINING AND INSULATION536706-0606-1 253 STRINGER COUPLINGS NDT SDI T: 46000 FC ALI NTM 5131051 TBD B4-100254 I: 8200 FC PART 11 TBD PRE 02643SPECIAL DETAILED INSPECTION OF STRINGER COUPLINGS CN 2006-0071(B) (53-0132)FROM STRINGER 5LH TO STRINGER 5RH AT FR 65 FAA AD 96-13-11 FROM 0 FC/FHTO LOVPREP.: REMOVE LININGS, HATRACKS, CEILING PANELS AND ALI REFERENCE:INSULATION 536706-01-1536707-0604-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 58 MEC DET T: 40000 FC ALI EASA AD1 TBD B2254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF STRINGER COUPLINGS AT 45600 FH FAA ADTO LOVCIRCUMFERENTIAL JOINT FRAME 58 FROM STRINGER 12 LH I: 12000 FC 2007-04-11TO STRINGER 12 RH INTERNAL. OR13600 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536707-01-1ACCESS: 843* 0.10536707-0604-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 58 MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF STRINGER COUPLINGS AT 55600 FH FAA ADTO LOVCIRCUMFERENTIAL JOINT FRAME 58 FROM STRINGER 12 LH I: 12000 FC 2007-04-11TO STRINGER 12 RH INTERNAL. OR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 207APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536707-0604-2 * * * * * C O N T I N U E * * * * *16600 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536707-01-2ACCESS: 843* 0.10536707-0604-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 58 MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200254 OR 2006-00711 TBD C4DETAILED INSPECTION OF STRINGER COUPLINGS AT 78800 FH FAA ADF4CIRCUMFERENTIAL JOINT FRAME 58 FROM STRINGER 12 LH I: 10500 FC 2007-04-11FROM 0 FC/FHTO STRINGER 12 RH INTERNAL. ORTO LOV24300 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536707-01-3ACCESS: 843* 0.10536708-0604-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 65 MEC DET T: 40000 FC ALI EASA AD1 TBD B2254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF STRINGER COUPLINGS AT 45600 FH FAA ADTO LOVAT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11LH/RH INTERNAL OR13600 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536708-01-1ACCESS: 843* 0.10536708-0604-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 65 MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF STRINGER COUPLINGS AT 55600 FH FAA ADTO LOVAT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11LH/RH INTERNAL OR16600 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536708-01-2ACCESS: 843* 0.10536708-0604-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 65 MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200254 OR 2006-00711 TBD C4DETAILED INSPECTION OF STRINGER COUPLINGS AT 78800 FH FAA ADF4AT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE I: 10500 FC 2007-04-11FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 208APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536708-0604-3 * * * * * C O N T I N U E * * * * *LH/RH INTERNAL OR ALI REFERENCE: TO LOV24300 FH 536708-01-3ACCESS: REMOVE LINING AND INSULATIONACCESS: 843* 0.10536709-0604-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD1 TBD B2254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF STRINGER COUPLINGS AT 45600 FH FAA ADTO LOVAT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11LH/RH INTERNAL OR13600 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536709-01-1ACCESS: 834* 0.10536709-0604-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF STRINGER COUPLINGS AT 55600 FH FAA ADTO LOVAT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11LH/RH INTERNAL OR16600 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536709-01-2ACCESS: 834* 0.10536709-0604-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200254 OR 2006-00711 TBD C4DETAILED INSPECTION OF STRINGER COUPLINGS AT 78800 FH FAA ADF4AT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE I: 10500 FC 2007-04-11FROM 0 FC/FHLH/RH INTERNAL ORTO LOV24300 FH ALI REFERENCE:ACCESS: REMOVE LINING AND INSULATION 536709-01-3ACCESS: 834* 0.10536710-0602-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD1 TBD B2254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF SKIN IN AREA OF STRINGER 45600 FHTO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 209APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536710-0602-1 * * * * * C O N T I N U E * * * * *COUPLING RUN OUT AT FRAME 72 FROM STRINGER 12 TO I: 18000 FC FAA ADCROWN CENTER LINE LH/RH. OR 2007-04-1120500 FHALI REFERENCE:536710-01-1536710-0602-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100254 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF SKIN IN AREA OF STRINGER 55600 FH FAA ADTO LOVCOUPLING RUN OUT AT FRAME 72 FROM STRINGER 12 TO I: 18000 FC 2007-04-11CROWN CENTER LINE LH/RH. OR25000 FH ALI REFERENCE:536710-01-2536710-0602-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200254 OR 2006-00711 TBD C4DETAILED INSPECTION OF SKIN IN AREA OF STRINGER 78800 FH FAA ADF4COUPLING RUN OUT AT FRAME 72 FROM STRINGER 12 TO I: 15000 FC 2007-04-11FROM 0 FC/FHCROWN CENTER LINE LH/RH. ORTO LOV34800 FH ALI REFERENCE:536710-01-3536711-0606-1 152 AFT CARGO COMPARTMENT DOOR LOOK MEC DET T: 48000 FC ALI EASA AD1 TBD B2154 STRUCTURE I: 10000 FC 2006-00711 TBD FROM 0 FC/FHFAA ADTO LOVDETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR 2007-04-11LOCK FITTINGS, BUSHES, ECCENTRIC BOLTS ANDSURROUNDING STRUCTURE FROM FRAME 60 TO FRAME 63 AND ALI REFERENCE:FROM STRINGER 44 RH TO STRINGER 46 RH. 536711-01-1PREP.: ECCENTRIC BOLTS TO BE REMOVEDACCESS: 812* 0.01536711-0606-2 152 AFT CARGO COMPARTMENT DOOR LOOK MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100154 STRUCTURE I: 10000 FC 2006-00711 TBD FROM 0 FC/FHFAA ADTO LOVDETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR 2007-04-11LOCK FITTINGS, BUSHES, ECCENTRIC BOLTS AND* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 210APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536711-0606-2 * * * * * C O N T I N U E * * * * *SURROUNDING STRUCTURE FROM FRAME 60 TO FRAME 63 AND ALI REFERENCE:FROM STRINGER 44 RH TO STRINGER 46 RH. 536711-01-2PREP.: ECCENTRIC BOLTS TO BE REMOVEDACCESS: 812* 0.01536711-0606-3 152 AFT CARGO COMPARTMENT DOOR LOOK MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200154 STRUCTURE I: 10000 FC 2006-00711 TBD C4FAA ADF4DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR 2007-04-11FROM 0 FC/FHLOCK FITTINGS, BUSHES, ECCENTRIC BOLTS ANDTO LOVSURROUNDING STRUCTURE FROM FRAME 60 TO FRAME 63 AND ALI REFERENCE:FROM STRINGER 44 RH TO STRINGER 46 RH. 536711-01-3PREP.: ECCENTRIC BOLTS TO BE REMOVEDACCESS: 812* 0.01536801-0606-1 253 SPLICE PLATE AT FRAME 72 NDT SDI T: SEE SB ALI NTM 5330211 4.00 ALL254 I: SEE SB PART 41 4.00 SB 53-0262SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT NTM 533021FROM 0 FC/FHCIRCUMFERENTIAL SKIN SPLICE AT FRAME 72 FROM STRINGER PART 6TO 40750 FC4 TO STRINGER 12 LH/RH. CN 2006-0071(B)FAA AD 96-13-11PREP.: HATRACKS, LINING AND INSULATION AND BOLT SB 53-0262REMOVALALI REFERENCE:536801-01-1536901-0606-1 311 FUSELAGE TAIL SECTION NDT SDI T: 20200 FC ALI NTM 5319001 3.25 ALL312 I: 7700 FC CN PART 61 3.25 SB 53-0256SPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071(B) FROM 0 FC/FHSTABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13-11 TO LOVSTRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256BETWEEN STRINGER 24 AND STRINGER 27 LH/RH.ALI REFERENCE:NOTE: AREA 3 INSPECTION AND COLDWORKING 536901-01-1PREP.: FOR ACCESS SEE SBSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 211APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536901-0606-2 311 FUSELAGE TAIL SECTION NDT SDI T: 54000 FC ALI NTM 5319001 3.25 B2312 I: 3800 FC CN PART 61 3.25 FROM 48000 FCSPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071(B) TO LOVSTABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13-11STRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256BETWEEN STRINGER 24 AND STRINGER 27 LH/RH.ALI REFERENCE:NOTE: AREA 3 AFTER COLDWORKING PROCESS 536901-02-1PREP.: FOR ACCESS SEE SB536901-0606-3 311 FUSELAGE TAIL SECTION NDT SDI T: 52000 FC ALI NTM 5319001 3.25 B4-100312 I: 3800 FC CN PART 61 3.25 FROM 40000 FCSPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071(B) TO LOVSTABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13-11STRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256BETWEEN STRINGER 24 AND STRINGER 27 LH/RH.ALI REFERENCE:NOTE: AREA 3 INSPECTION AND COLDWORKING 536901-02-2PREP.: FOR ACCESS SEE SB536901-0606-5 311 FUSELAGE TAIL SECTION NDT SDI T: 43000 FC ALI NTM 5319001 3.25 B4-200312 I: 3800 FC CN PART 61 3.25 C4SPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071(B) F4STABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13-11 FROM 34000 FCSTRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256TO LOVBETWEEN STRINGER 24 AND STRINGER 27 LH/RH.ALI REFERENCE:NOTE: AREA 3 AFTER COLDWORKING PROCESS 536901-02-3PREP.: FOR ACCESS SEE SBACCESS: 312AR* 0.01536902-0606-1 311 FUSELAGE TAIL SECTION NDT SDI T: 24000 FC ALI NTM 5319001 TBD ALL312 I: 12000 FC PART 41 TBD SB 53-0258SPECIAL DETAILED INSPECTION (US) OF OF FUSELAGE EASA ADFROM 0 FC/FHHORIZONTAL STABILIZER ATTACH FITTINGS LH/RH AND THE 2006-0071TO LOVUPPER AND LOWER FRAME LUGS OF FRAME 91 LH/RH. FAA AD2007-04-11ACCESS: 313AL SB 53-0258* 0.14* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 212APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536902-0606-1 * * * * * C O N T I N U E * * * * *ALI REFERENCE:536902-01-1536903-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD1 TBD B2312 I: 6600 FC 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF LONGITUDINAL BRACE EXTERNAL FAA ADTO LOVSURFACE IN CORNER AREAS OF VERTICAL STABILIZER 2007-04-11ATTACHMENT FITTING CUT OUTS AT FRAME 81/82,FRAME 84/85 AND FRAME 86/87 LH/RH. ALI REFERENCE:536903-01-1ACCESS: 311AZ 311BZ 323AL 323BL* 1.30323AR 323BR* 0.82536903-0604-2 311 FUSELAGE TAIL SECTION MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100312 I: 6600 FC 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF LONGITUDINAL BRACE EXTERNAL FAA ADTO LOVSURFACE IN CORNER AREAS OF VERTICAL STABILIZER 2007-04-11ATTACHMENT FITTING CUT OUTS AT FRAME 81/82,FRAME 84/85 AND FRAME 86/87 LH/RH. ALI REFERENCE:536903-01-2ACCESS: 311AZ 311BZ 323AL 323BL* 1.30323AR 323BR* 0.82536903-0604-3 311 FUSELAGE TAIL SECTION MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200312 I: 6600 FC 2006-00711 TBD C4DETAILED INSPECTION OF LONGITUDINAL BRACE EXTERNAL FAA ADF4SURFACE IN CORNER AREAS OF VERTICAL STABILIZER 2007-04-11FROM 0 FC/FHATTACHMENT FITTING CUT OUTS AT FRAME 81/82,TO LOVFRAME 84/85 AND FRAME 86/87 LH/RH. ALI REFERENCE:536903-01-3ACCESS: 311AZ 311BZ 323AL 323BL* 1.30323AR 323BR* 0.82536905-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD1 TBD B2312 I: 6000 FC 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF INTERNAL STRUCTURE AT FIN TO FAA ADTO LOVFUSELAGE FORWARD, MID AND AFT ATTACH FITTINGS IN 2007-04-11RIVETING AREA OF SKIN TO LONGITUDINAL BRACE AND OFLONGITUDINAL BRACE OF VERTICAL STABILIZER ATTACH ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 213APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)536905-0604-1 * * * * * C O N T I N U E * * * * *FITTINGS FRAME 81/82, FRAME 84/85, FRAME 86/87 536905-01-1AND STRINGER 6 LH/RH TO CROWN CENTERLINE.ACCESS: 312AR* 0.01536905-0604-2 311 FUSELAGE TAIL SECTION MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100312 I: 6000 FC 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF INTERNAL STRUCTURE AT FIN TO FAA ADTO 57000 FCFUSELAGE FORWARD, MID AND AFT ATTACH FITTINGS IN 2007-04-11RIVETING AREA OF SKIN TO LONGITUDINAL BRACE AND OFLONGITUDINAL BRACE OF VERTICAL STABILIZER ATTACH ALI REFERENCE:FITTINGS FRAME 81/82, FRAME 84/85, FRAME 86/87 536905-01-2AND STRINGER 6 LH/RH TO CROWN CENTERLINE.ACCESS: 312AR* 0.01536905-0604-3 311 FUSELAGE TAIL SECTION MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200312 I: 6000 FC 2006-00711 TBD C4DETAILED INSPECTION OF INTERNAL STRUCTURE AT FIN TO FAA ADF4FUSELAGE FORWARD, MID AND AFT ATTACH FITTINGS IN 2007-04-11FROM 0 FC/FHRIVETING AREA OF SKIN TO LONGITUDINAL BRACE AND OFTO 57000 FCLONGITUDINAL BRACE OF VERTICAL STABILIZER ATTACH ALI REFERENCE:FITTINGS FRAME 81/82, FRAME 84/85, FRAME 86/87 536905-01-3AND STRINGER 6 LH/RH TO CROWN CENTERLINE.ACCESS: 312AR* 0.01538001-0603-1 145 FUSELAGE OVERWING PANELS MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 1.00 ALL146 I: 5 YE 538001-C603-11 1.00GENERAL VISUAL INSPECTION OF FUSELAGE OVERWING PANELSBETWEEN FR.39 AND FR.54 BELOW CABIN FLOOR LEVEL(STR 26) TO STR 33 LH/RH EXTERNAL SURFACE.NOTE: TEMPORARY PROTECTION SYSTEMS TYPE 1, G2 OR G3TO BE APPLIED UNDER FAIRING ONLY.PREP.: FAIRING TO BE REMOVEDACCESS: 577AB 577AT 577BB 577BT 577CT 577DT* 3.68577ET 577GT* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 214APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538001-0603-1 * * * * * C O N T I N U E * * * * *677AB 677AT 677BB 677BT 677CT 677DT* 3.68677ET 677GT538011-0602-1 100 LOWER FUSELAGE-LONGT.JOINTS MEC DET T: 5 YE CPCP MRB REFERENCE: 1 0.70 ALLI: 30 MO 538011-C602-1DETAILED INSPECTION OF EXTERNAL SURFACE OFLONGITUDINAL JOINTS, FROM FRAME 18 TO FRAME 72, BELOWPASSENGER FLOOR LEVEL (STRINGER 26) TO STRINGER33 LH/RH.NOTE: THIS TASK IS APPLICABLE IN THOSE AREASNOT COVERED BY SB 53-0178.538013-0602-1 137 KRUEGER SLOT FLAP CUT-OUT DOUBLER MEC DET I: 5 YE CPCP MRB REFERENCE: 1 0.10 B2K,138 538013-C602-11 0.10 B2 MSN 049 051513 DETAILED INSPECTION OF KRUEGER SLOT FLAP1 0.10 059 AND ON,613 CUTOUT DOUBLER EXTERNAL SURFACE, AS FAR AS VISIBLE.1 0.10 B4 C4 F4538014-0603-1 513 KRUEGER FLAP MEC DET I: 5 YE CPCP MRB REFERENCE: 1 0.10 B2K613 538014-C603-11 0.10 B4DETAILED INSPECTION OF KRUEGER FLAP INTERNALC4SUPPORT STRUCTURE.F4NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2OR G3 AFTER INSPECTIONPREP.: KRUEGER FLAP EXTENDED538015-0603-1 513 FUS.STRUCT. UNDER WING ROOT FAIRING MEC DET I: 5 YE CPCP ISB 53-03281 0.10 B2613 ISB1 0.10DETAILED INSPECTION OF FUSELAGE STRUCTURE MRB REFERENCE:BETWEEN FRAME 38 AND FRAME 40 UNDER WING ROOT FAIRING 538015-C603-1NOTE 1. FOR PRE MOD 04201 A/C (PRE MSN 255), ISB53-0238 IS ALSO APPLICABLE2. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 512BB 513BB* 0.43* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 215APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538015-0603-1 * * * * * C O N T I N U E * * * * *612BB 613BB* 0.43538015-0603-2 513 FUS.STRUCT. UNDER WING ROOT FAIRING MEC DET I: 5 YE CPCP ISB 53-03281 0.10 B2K613 ISB1 0.10 B4DETAILED INSPECTION OF FUSELAGE STRUCTURE MRB REFERENCE: C4BETWEEN FRAME 38 AND FRAME 40 UNDER WING ROOT FAIRING 538015-C603-2F4NOTE: 1. FOR PRE MOD 04201 A/C (PRE MSN 255), ISB53-0328 IS ALSO APPLICABLE2. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONPREP.: KRUEGER FLAP EXTENDED, VERTICAL SCREWEDPROTECTIVE PANEL (COVER PLATE) REMOVED.ACCESS: 513AB* 0.40613AB* 0.18538021-0602-1 100 LOWER FUSELAGE-CIRCUMFERENTIAL JOINTS MEC DET T: 5 YE CPCP MRB REFERENCE: 1 0.40 ALLI: 30 MO 538021-C602-1DETAILED INSPECTION OF CIRCUMFERENTIAL JOINTSFROM FRAME 18 TO FRAME 72, BETWEEN FLOOR LEVEL(STRINGER 26) AND STRINGER 33, L/H WITHOUT FAIRINGREMOVAL.NOTE: THIS TASK IS APPLICABLE IN THOSE AREASNOT COVERED BY SB 53-0178.538031-0603-1 171 TAIL BUMPER CAVITY MEC DET I: 5 YE CPCP SIL 53-0411 0.30 ALLDETAILED INSPECTION OF TAIL BUMPER CAVITY MRB REFERENCE:BETWEEN FRAME 74 AND FRAME 79. 538031-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 171BL* 0.01STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 216APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538050-0603-1 110 FWD PRESSURE BULKHEAD MEC DET I: 9 YE CPCP AMM SSI 5311071 2.50 ALLMRB SDETAILED INSPECTION OF FORWARD FACE OF FORWARD MRB REFERENCE:PRESSURE BULKHEAD (FRAME 1).538050-C602-1NOTE: SHIELD TO BE REMOVEDACCESS: 110AL* 0.01538051-0602-1 100 LWR.FUSELAGE DOOR CUT-OUTS MEC DET T: 5 YE CPCP AMM SSI 5313131 2.20 ALLI: 30 MO MRB S AMM SSI 531315DETAILED INSPECTION OF EXTERNAL SURROUNDINGS AMM SSI 531317OF CARGO, SERVICING AND ACCESS DOOR CUT-OUTS (25 AMM SSI 531407CM/10 INCHES AROUND CUT-OUT), INCLUDING CARGO DOOR AMM SSI 533113EDGES AND SKIN PANEL AROUND GLIDE ANTENNA CUT-OUT. AMM SSI 533115AMM SSI 533327NOTE: ACCESS PANEL 134BR AS APPLICABLE AMM SSI 533405AMM SSI 533801ACCESS: 121AL 121BL 121CL 121DL 122AR 122BR AMM SSI 533805* 0.36122CR 132BR 134AR 134BR 135AL 135BL136AR 136BR 152AR 171AL 172AR 172BR MRB REFERENCE:811 812 813538051-C602-1538052-0603-1 100 NLG BAY, SURROUND PANELS MEC DET T: 5 YE CPCP AMM SSI 5332131 0.30 ALL123 I: 30 MO MRB S1 0.30124 DETAILED INSPECTION OF EXTERNAL AND INTERNAL MRB REFERENCE: 1 0.30SKIN PANELS, SURROUNDING NOSE LANDING GEAR BAY CUTOUT(25 CM/10 INCHES AROUND CUT-OUT). 538052-C603-1ACCESS: 713* 0.06134AR 136AR 714* 0.07538053-0603-1 100 MLG BAY, SURROUND PANELS MEC DET T: 5 YE CPCP MRB REFERENCE: 1 0.60 ALL147 I: 30 MO 538053-C603-11 0.60148 DETAILED INSPECTION OF EXTERNAL SKIN PANELS,1 0.60SURROUNDING MAIN LANDING GEAR BAY CUTOUT(25 CM/10 INCHES AROUND CUT-OUT).ACCESS: 734* 0.10744* 0.10STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 217APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538071-0602-1 100 CUT-OUT OF AIR COND. SYSTEM DOOR MEC DET T: 5 YE CPCP MRB REFERENCE: 1 0.30 ALLI: 30 MO 538071-C602-1DETAILED INSPECTION OF EXTERNAL SURROUNDINGS(25CM/10 INCHES AROUND FAIRING EDGES) OF AIRCONDITIONING SYSTEM DOORACCESS: 134AR 136AR* 0.01538081-0602-1 100 LOWER FUSELAGE-LONGITUDINAL JOINTS MEC DET T: 5 YE CPCP MRB REFERENCE: 1 1.20 ALLI: 30 MO 538081-C602-1DETAILED INSPECTION OF LONGITUDINAL JOINTBELOW STRINGER 33 LH/RH, BETWEEN FRAME 18 AND FRAME72 WITHOUT FAIRING REMOVAL, EXTERNAL SURFACE.NOTE: THIS TASK IS APPLICABLE IN THOSE AREAS NOTCOVERED BY SB 53-0178.538091-0602-1 100 LOWER FUSELAGE-CIRCUMFERENTIAL JOINTS MEC DET T: 5 YE CPCP MRB REFERENCE: 1 1.00 ALLI: 30 MO 538091-C602-1DETAILED INSPECTION OF CIRCUMFERENTIAL JOINTSBELOW STRINGER 33 LH/RH, BETWEEN FRAME 18 AND FRAME72 WITHOUT FAIRING REMOVAL, EXTERNAL SURFACE.NOTE: THIS TASK IS ONLY APPLICABLE IN THOSEAREAS NOT COVERED BY SB 53-0178538102-0603-1 121 WASTE/WATER CONNECTION BOX MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 0.33 MSN 005 AND UPI: 30 MO 538102-C603-1VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTUREAROUND WASTE WATER CONNECTION BOX BETWEEN FRAME 12AND FRAME 12A FROM STRINGER 37 TO AVIONICSCOMPARTMENT FLOOR LEVEL, LH.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 131AZ* 0.01538111-0603-1 121 FUSELAGE INTERNAL STRUCTURE MEC DET I: 5 YE CPCP AMM SSI 5332202 2.50 ALL122 MRB S2 2.50DETAILED INSPECTION OF FUSELAGE INTERNAL* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 218APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538111-0603-1 * * * * * C O N T I N U E * * * * *STRUCTURE BELOW PASSENGER DOORS BETWEEN FRAME 11 ANDFRAME 20, AND BELOW GALLEY AND TOILET AREAS FROM 538111-C603-1CABIN FLOOR LEVEL TO AVIONIC COMPARTMENT FLOOR PANELSNOTE 01. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3. TO BE SPRAYED WITH PROPER NOZZLE,WITH INSULATION LIFTED.02. INSULATION TO BE LIFTED ENOUGH TO INSPECTTHE STRUCTURE WITHOUT REMOVAL OF ELECTRICALDEVICE.ACCESS: 131AZ* 0.01132AZ* 0.01538121-0603-1 121 BILGE AREAS MEC DET T: 5 YE CPCP SIL 53-0611 2.50 ALL122 I: 30 MO1 2.50DETAILED INSPECTION OF BILGE AREA UNDERNEATH MRB REFERENCE:AVIONIC COMPARTMENT FLOOR PANELS FROM FRAME 1 TO 538121-C603-1FRAME 20.NOTE: 01. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONNOTE: 02. IMPROVE DRAINAGE IN ACCORDANCE WITHSB 53-0234 IS RECOMMENDED.NOTE: 03. IMPROVE CORROSION RESISTANCE ON STRINGER 44AT FRAME 17 IS RECOMMENDED IN ACCORDANCEWITH SIL 53-061 IN BILGE AREA.NOTE: 04. INSULATION TO BE REMOVED.ACCESS: 121CF 121DF 121EF 121FF 121GF 121HF* 2.84121JF 121KF 121LF 121MF 121NF 121PF121QF 121TF 121UF 121VF 121WF 121YF121ZF122AF 122BF 122CF 122DF 122EF 122GF* 1.91122HF 122JF 122KF 122LF 122MF 122NF122PF 122QFSTRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 219APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538153-0602-1 131 UPPER FUSELAGE - UDC DOOR CUT OUT MEC DET I: 5 YE CPCP MRB REFERENCE: 1 0.20 C4231 538153-C602-11 0.20 F4233 DETAILED INSPECTION OF UPPER (MAIN) DECK CARGO1 0.20 MSN 256DOOR SURROUNDING PANELS (25 CM/10 IN. AROUND CUT OUT)AND CUT OUT EDGES.NOTE: WHEN DOOR MECHANISM NOT FITTED, CUT OUT EDGEINSPECTED AS FAR AS VISIBLE.ACCESS: 835* 0.05538161-0602-1 200 CABIN WINDOW FRAMES MEC DET I: 5 YE CPCP MRB REFERENCE: 1 2.00 ALL538161-C602-1DETAILED INSPECTION OF VISIBLE PART OFPASSENGER WINDOW FORGINGS BETWEEN FRAME 18 AND FRAME77, EXTERNAL SURFACE.538171-0602-1 210 COCKPIT WINDOW FRAMES MEC DET I: 5 YE CPCP AMM SSI 5311331 0.60 ALLMRB S AMM SSI 531135DETAILED INSPECTION OF EXTERNAL SURFACE OFCOCKPIT WINDOW SURROUNDINGS. MRB REFERENCE:538171-C602-1538173-0603-1 123 NLG BAY MEC GVI I: 5 YE CPCP AMM SSI 5312271 1.00 ALL124 MRB S AMM SSI 5312391 1.00GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY AMM SSI 531241INCLUDING NOSE LANDING GEAR DOOR HINGES. AMM SSI 531245AMM SSI 531247NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION MRB REFERENCE:ACCESS: 713 538173-C603-1* 0.06714* 0.06538233-0603-1 131 STRUCTURE BELOW MID PAX DOOR MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 1.50 ALL132 538233-C603-11 1.50GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE BELOW MID PASSENGER/CREW DOOR BETWEEN FRAME27 AND FRAME 32 FROM STRINGER 26 TO STRINGER 30 LH/RH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 220APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538233-0603-1 * * * * * C O N T I N U E * * * * *NOTE: 01. SIDE LINING INSULATION TO BE REMOVED.NOTE: 02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION BELOW DOORS.(0,5 M / 20 INCHES)ACCESS: 811* 0.15538235-0603-1 131 STRUCTURE BELOW UDC DOOR MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 2.00 C4538235-C603-1F4GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE BELOW UPPER DECK CARGO DOOR, BETWEEN FRAME19 AND FRAME 28 FROM STRINGER 26 TO STRINGER 30, LH.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION BELOW DOOR.(0,5 M / 20 INCHES)PREP.: SIDE LINING AND INSULATION TO BE REMOVED.ACCESS: 811* 0.15538245-0603-1 132 FWD CARGO COMP DOOR CUTOUT MEC GVI T: 9 YE CPCP MRB REFERENCE: 1 1.50 ALLI: 5 YE 538245-C603-1GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE AROUND FORWARD CARGO COMPARTMENT DOORCUT-OUT FROM FRAME 19 TO FRAME 26, AND BETWEENSTRINGER 26 AND STRINGER 41RH.NOTE: 01. SIDE LINING AND INSULATION TO BE REMOVED.NOTE: 02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 811* 0.15538265-0603-1 132 FWD CARGO COMP DOOR FRAMES MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 0.50 ALL134 I: 30 MO 538265-C603-11 0.50GENERAL VISUAL INSPECTION OF FUSELAGE FORWARD CARGOCOMPARTMENT DOOR CUT-OUT, VISUAL PART OF LATERAL* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 221APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538265-0603-1 * * * * * C O N T I N U E * * * * *FRAMES 20A AND 25A (24B FOR 96 INCHES CARGOCOMPARTMENT DOORS), FROM STRINGER 36RH TO ATTACHMENTTO SILL BEAM, SILL BEAM UPPER FLANGE AS FAR ASVISIBLE AND SILL BEAM STRUCTURE INCLUDING LOCKFITTINGS.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 811* 0.15538295-0603-1 135 FRAMES 39 AND 54 MEC DET I: 5 YE CPCP MRB REFERENCE: 1 0.50 POST 08057136 538295-C603-11 0.50 (21-0116)153 DETAILED INSPECTION OF FRAME 39 AND FRAME 541 0.50 POST 05946154 BELOW CARGO FLOOR LEVEL.1 0.50 (53-0201)NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 137ALF 137AMF* 0.65138PF 138QF 811* 0.78151AF 151BF 151CF* 0.45152AF 152BF 812* 0.39538295-0603-2 135 FRAMES 39 AND 54 MEC DET I: 4 YE ISB CN 2003-317(B)1 0.50 PRE 08057136 FAA AD1 0.50 (21-0116)153 DETAILED INSPECTION OF FRAME 39 AND FRAME 54 2005-15-091 0.50 OR154 BELOW CARGO FLOOR LEVEL. ISB 53-02861 0.50 PRE 05946(53-0201)NOTE 1: INSULATION TO BE REMOVED.ACCESS: 137ALF 137AMF* 0.65138PF 138QF 811* 0.78151AF 151BF 151CF* 0.45152AF 152BF 812* 0.39538325-0603-1 120 FUSELAGE - DRAIN VALVES MEC DET I: 5 YE CPCP MRB REFERENCE: 1 1.00 ALL130 538325-C603-11 1.00140 DETAILED INSPECTION OF FUSELAGE INTERNAL1 1.00150 STRUCTURE AROUND DRAIN VALVES AND DRAIN PLUGS AT1 1.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 222APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538325-0603-1 * * * * * C O N T I N U E * * * * *160 BOTTOM CENTER LINE BETWEEN FRAME 18 AND FRAME 80.1 1.001701 1.00PREP.: REMOVE/INSTALL INSULATIONS, CARGO FLOORPANELS AND BALLMATS.ACCESS: 811* 0.15812* 0.01538435-0603-1 143 AIR CONDITIONING COMPARTM. MEC DET I: 5 YE CPCP AMM SSI 5315022 1.00 ALL144 MRB S2 1.00DETAILED INSPECTION OF AFT FACE AT PRESSURE MRB REFERENCE:BULKHEAD INCLUDING FRAME 39 AND 25 CM OF SKIN.538435-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 147GZ 147HZ* 0.05148GZ 148HZ* 0.05538537-0603-1 143 KEEL BEAM INTERNAL STRUCTURE MEC DET I: 5 YE CPCP AMM SSI 5305031 0.75 ALL144 MRB S1 0.75147 DETAILED INSPECTION OF KEEL BEAM INTERNAL MRB REFERENCE: 1 0.75148 STRUCTURE.1 0.75538537-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 143AF 143BF 143CF 143DF* 0.33147AF 147BF 147CF 147FZ 147GZ 733* 0.22148AF 148GZ 734* 0.15538547-0603-1 147 MLG FUSELAGE CUTOUT MEC DET I: 5 YE CPCP AMM SSI 5335031 0.50 ALL148 MRB S AMM SSI 5335051 0.50DETAILED INSPECTION OF MAIN LANDING GEARFUSELAGE CUTOUT SURROUNDING, INTERNAL AND EXTERNAL MRB REFERENCE:SURFACE.(25 CM/10 INCHES AROUND CUT-OUT)538547-C603-1ACCESS: 734* 0.10744* 0.10STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 223APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538553-0603-1 152 AFT CARGO COMPT.DOOR CUTOUT MEC GVI T: 9 YE CPCP MRB REFERENCE: 1 1.70 ALLI: 5 YE 538553-C603-1GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENTDOOR CUT-OUT FROM FRAME 59 TO FRAME 64 BETWEENSTRINGER 26 AND STRINGER 41RH. INTERNAL STRUCTURE.NOTE 01: SIDE LINING AND INSULATION TO BE REMOVED.NOTE 02: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 812* 0.01538555-0603-1 151 CABIN FLOOR STRUCTURE MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 1.50 ALL152 I: 30 MO 538555-C603-11 1.50GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTUREBELOW TOILETS (IF FITTED), BETWEEN FRAME 54C ANDFRAME 60.NOTE 01: CEILING PANELS IN GALLEY/TOILET AREATO BE REMOVED.NOTE 02: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1AND TYPE 2 AFTER INSPECTIONNOTE 03: THIS TASK MAY BE COMBINED WITH CORROSIONINSPECTION 531610-C603-1 AND 531620-C603-1ACCESS: 812* 0.01538557-0603-1 152 AFT CARGO COMPT.DOOR FRAMES MEC GVI T: 5 YE CPCP AMM SSI 5317011 0.25 ALL154 I: 30 MO MRB S1 0.25GENERAL VISUAL INSPECTION OF FUSELAGE AFT CARGO MRB REFERENCE:COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERALFRAMES (FRAME 59A AND FRAME 63A) FROM STR 36RH TO 538557-C603-1ATTACHMENT TO SILL BEAM, SILL BEAM UPPER FLANGE ASFAR AS VISIBLE AND SILL BEAM STRUCTURE INCLUDINGLOCK FITTINGS.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 812* 0.01STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 224APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538587-0603-1 162 BULK CARGO COMP.DOOR CUTOUT MEC DET I: 5 YE CPCP MRB REFERENCE: 1 1.00 ALL538587-C603-1DETAILED INSPECTION OF INTERNAL STRUCTUREAROUND BULK CARGO COMPARTMENT DOOR CUTOUT FROM FRAME66 TO FRAME 70 BETWEEN STRINGER 32RH AND CARGO FLOORLEVEL.NOTE 01: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONNOTE 02: SIDE LINING, INSULATION TO BE REMOVED.ACCESS: 813* 0.01538589-0603-1 162 BULK CARGO COMP.DOOR FRAMES MEC GVI T: 5 YE CPCP SIL 53-0301 0.30 ALLI: 30 MOGENERAL VISUAL INSPECTION OF REAR (BULK) CARGO MRB REFERENCE:COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL 538589-C603-1FRAMES (FRAME 67 AND FRAME 69) FROM STRINGER 41RH TOATTACHMENT TO SILL BEAM AND SILL BEAM AS FAR ASVISIBLE.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 813* 0.01538592-0603-1 162 BULK CARGO COMPARTMENT DOOR FRAMES NDT SDI I: 10 YE EUAD NTM 5131081 1.50 B1ISB PART 1B2-1CSPECIAL DETAILED INSPECTION OF BULK CARGO COMPARTMENT EUADB2K-3CDOOR AREA AT FRAME 67 BETWEEN STRINGER 33 AND 200-262-313(B)B2-203STRINGER 48 AND AT FRAME 69 BETWEEN STRINGER 33 AND ISB 53-0339B4-2CSTRINGER 47.B4-103B4-203NOTE: SIDE LININGS, INSULATION TO BE REMOVED.POST 02140(53-0109)ACCESS: 813* 0.01538593-0603-1 162 BULK CARGO COMP. DOOR SILL BEAM MEC DET T: 5 YE CPCP MRB REFERENCE: 1 0.60 ALLI: 30 MO 538593-C603-1DETAILED INSPECTION OF REAR (BULK) CARGO DOORSILL BEAM, INCLUDING DOOR FRAMES 67 AND 69 FROM* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 225APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538593-0603-1 * * * * * C O N T I N U E * * * * *STRINGER 42RH TO STRINGER 47RH.NOTE 01: INNER SCUFF PLATE REMOVEDNOTE 02: FLOOR PANELS, INSULATION TO BE REMOVEDNOTE 03: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 813* 0.01538617-0603-1 171 AFT CABIN - FLOOR STRUCTURE MEC DET T: 5 YE CPCP MRB REFERENCE: 1 0.60 ALL172 I: 30 MO 538617-C603-11 0.60DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE BELOW GALLEY AND TOILETS AND DRAINAGE HOLESIN FRAME 80.NOTE 01: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1AND TYPE 2 AFTER INSPECTIONNOTE 02: ENSURE DRAIN HOLES ARE FREE FROM ANYOBSTRUCTIONS (TASK 513000-0502-3).ACCESS: 162AZ* 0.01538679-0603-1 231 STRUCTURE AROUND UDC DOOR MEC DET T: 9 YE CPCP MRB REFERENCE: 1 2.00 C4I: 5 YE 538679-C603-1F4DETAILED INSPECTION OF INTERNAL STRUCTUREMSN 256AROUND UPPER (MAIN) DECK CARGO DOOR ABOVE CABIN FLOORLEVEL UP TO STRINGER 15 LH, BETWEEN FRAME 19 ANDFRAME 28.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONPREP.: SIDE PANELS, DOOR FRAME PANELS AND INSULATIONTO BE REMOVED.538691-0603-1 233 STRUCTURE AROUND UDC DOOR MEC DET T: 9 YE CPCP MRB REFERENCE: 1 4.00 C4I: 5 YE 538691-C603-1F4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 226APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538691-0603-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF INTERNAL STRUCTUREMSN 256AROUND UPPER (MAIN) DECK CARGO DOOR ABOVE STRINGER 15UP TO STRINGER 3 LH, BETWEEN FRAME 19 AND FRAME 28.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTONPREP.: SIDE PANELS, DOOR FRAME PANELS AND INSULATIONTO BE REMOVED.538693-0603-1 230 UDC DOOR FRAMES MEC DET I: 5 YE CPCP MRB REFERENCE: 1 1.00 C4538693-C603-1F4DETAILED INSPECTION OF FUSELAGE DOOR FRAMESLOWER PORTION (50 CM/20 INCHES), APERTURE FACE OFUPPER (MAIN) DECK CARGO DOOR.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 835* 0.05538709-0603-1 221 FUSELAGE - DOOR FRAMES MEC DET T: 5 YE CPCP SIL 53-0301 1.00 ALL222 I: 30 MO1 1.00231 DETAILED INSPECTION OF FUSELAGE DOOR CUT-OUT, MRB REFERENCE: 1 1.00232 LOWER PORTION OF LATERAL FRAMES (50CM / 20 INCHES 538709-C603-11 1.00251 ABOVE FLOOR LEVEL) OF FORWARD, MID, AFT PAX/CREW1 1.00252 DOORS AND EMERGENCY EXITS.1 1.002611 1.00262 NOTE 01: LOWER DOOR FRAME PANELS TO BE REMOVED1 1.00NOTE 02: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 831* 0.10841* 0.10832* 0.10842* 0.10834* 0.10844* 0.10833* 0.10843* 0.10STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 227APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538769-0603-1 311 FRAME 91 MEC DET T: 9 YE CPCP MRB REFERENCE: 1 0.50 ALL312 I: 5 YE 538769-C603-11 0.50DETAILED INSPECTION OF THE ASSEMBLY CROWN TOBOTTOM CENTER LINE INCLUDING FRAME 91 TAIL CONEATTACHMENT FITTINGS.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 313AL* 0.14538779-0603-1 311 HORIZONTAL TAIL PLANE CUT-OUT MEC DET T: 9 YE CPCP AMM SSI 5319131 0.50 ALL312 I: 5 YE MRB S AMM SSI 5319141 0.50DETAILED INSPECTION OF HORIZONTAL TAIL PLANE NTM 531900CUTOUT BETWEEN FRAME 86 AND FRAME 91 INCLUDING CORNER PART 7FITTINGS AND LONGERONS.MRB REFERENCE:NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION 538779-C603-1ACCESS: 313AL* 0.14312AR* 0.01538789-0603-1 311 FUSELAGE TAIL-MACHINED FRAMES MEC DET T: 9 YE CPCP AMM SSI 5319011 1.50 ALL312 I: 5 YE MRB S AMM SSI 5319031 1.50DETAILED INSPECTION OF ALL MACHINED FRAMES AT AMM SSI 531905UPPER LOBE FROM STRINGER 14 LH/RH TO CROWN CENTER AMM SSI 531907LINE AND VERTICAL STABILIZER ATTACH FITTINGS AMM SSI 531909INCLUDING RIVETING OF FITTING TO FRAMES AND LATERAL AMM SSI 531911FRAMES.MRB REFERENCE:NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION 538789-C603-1ACCESS: 312AR* 0.01538789-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 20000 FC ALI EASA AD1 TBD ALL312 I: 11500 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF MACHINED FRAMES AND SHEARTIES FAA ADTO LOVAT UPPER LOBE FROM STRINGER 14 LH/RH TO CROWN CENTER 2007-04-11LINE AND VERTICAL STABILIZER ATTACH FITTINGSINCLUDING RIVETING OF FITTING TO FRAMES AND LATERAL ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 228APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538789-0604-1 * * * * * C O N T I N U E * * * * *FRAMES. 538789-01-1ACCESS: 312AR* 0.01538791-0603-1 311 FUSELAGE TAIL-FRAME BRACING MEC DET T: 9 YE CPCP AMM SSI 5319031 1.50 ALL312 I: 5 YE MRB S AMM SSI 5319071 1.50DETAILED INSPECTION OF FRAME BRACING, BETWEEN AMM SSI 531911FRAME 81 AND FRAME 82, FRAME 84 AND FRAME 85, FRAME86 AND FRAME 87. MRB REFERENCE:NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, 538791-C603-1G2 OR G3 AFTER INSPECTIONACCESS: 312AR* 0.01538829-0603-1 315 FUSELAGE - APU COMPARTMENT MEC GVI T: IMPL.AGE CPCP MRB REFERENCE: 1 0.50 ALL316 15 YE 538829-C603-11 0.50GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL I: 9 YESTRUCTURE BETWEEN FRAME 95 AND 100.ACCESS: 313AL 315AL* 0.17316AR* 0.02538839-0603-1 310 FUSELAGE TAIL-UNDERNEATH FIN FAIRING MEC DET I: 5 YE CPCP AMM SSI 5319151 0.50 ALLMRB SDETAILED INSPECTION OF FUSELAGE EXTERNAL MRB REFERENCE:SURFACE UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TOFUSELAGE ATTACHMENT FITTINGS INCLUDING TRANSVERSE 538839-C603-1LOAD FITTINGS.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONEXCLUDING THE CONICAL FIN TO FUSELAGEATTACHMENT BOLTS.ACCESS: 323AL 323AR 323BL 323BR* 1.62538839-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD1 TBD B2312 OR 2006-00711 TBD FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 229APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)538839-0604-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE 54200 FH FAA ADTO LOVUNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 5200 FC 2007-04-11FUSELAGE ATTACHMENT FITTINGS. OR5800 FH ALI REFERENCE:ACCESS: 323BL 538839-01-1* 0.41323BR* 0.44538839-0604-2 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD1 TBD B4-100312 OR 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE 54200 FH FAA ADTO LOVUNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 5200 FC 2007-04-11FUSELAGE ATTACHMENT FITTINGS. OR5800 FH ALI REFERENCE:ACCESS: 323BL 538839-01-2* 0.41323BR* 0.44538839-0604-3 311 FUSELAGE TAIL SECTION MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200312 OR 2006-00711 TBD C4DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE 75100 FH FAA ADF4UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 4000 FC 2007-04-11FROM 0 FC/FHFUSELAGE ATTACHMENT FITTINGS. ORTO LOV8800 FH ALI REFERENCE:ACCESS: 323BL 538839-01-3* 0.41323BR* 0.44539001-0603-1 241 FUSELAGE CENTER SECTION NDT SDI T: 10800 FC CN NTM 5131041 0.50 B2242 OR FAA AD PART 11 0.50SPECIAL DETAILED INSPECTION OF STIFFENERS ON THE FR 13900 FH ISB CN40 I: 2000 FC 1998-028-242(B)OR FAA ADACCESS: OPEN SIDEWALL PANELS AS REQUIRED 2600 FH 2000-20-15ISB 53-0332ACCESS: 131CZ* 0.13132EZ* 0.13539001-0603-2 241 FUSELAGE CENTER SECTION NDT SDI T: 7500 FC CN NTM 5131041 0.50 B4-100242 OR FAA AD PART 11 0.50SPECIAL DETAILED INSPECTION OF STIFFENERS ON THE FR 14600 FH ISB CN40 I: 1400 FC 1998-028-242(B)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 230APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)539001-0603-2 * * * * * C O N T I N U E * * * * *OR FAA ADACCESS: ACCESS: OPEN SIDEWALL PANELS AS REQUIRED 2800 FH 2000-20-15ISB 53-0332ACCESS: 131CZ* 0.13132EZ* 0.13539001-0603-3 241 FUSELAGE CENTER SECTION NDT SDI T: 7200 FC CN NTM 5131041 0.50 B4-200242 OR FAA AD PART 11 0.50SPECIAL DETAILED INSPECTION OF STIFFENERS ON THE FR 14000 FH CN40 I: 1400 FC 1998-028-242(B)OR FAA ADACCESS: ACCESS: OPEN SIDEWALL PANELS AS REQUIRED 2800 FH 2000-20-15SB 53-0332ACCESS: 131CZ* 0.13132EZ* 0.13539003-0603-1 148 CENTER SECTION FRAME 39 TO FRAME 54 MEC DET I: 9000 FC ISB ISB 53-01041 1.00 MSN 033DETAILED INSPECTION OF TWO SPOTFACES ONATTACHMENT BRACKETS539005-0603-1 713 NOSE GEAR AFT DOOR NDT SDI T: 4000 FC ISB NTM 5150001 0.25 PRE 08344714 I: 2000 FC ISB 53-02771 0.25 (53-0279)SPECIAL DETAILED INSPECTION OF AFT HINGE BOLTASSEMBLYACCESS: REMOVE THE NOSE GEAR AFT PANEL AND FLOORPANEL AND FLOOR PANELS 121PF, 122JF539006-0603-1 141 WING CENTER BOX NDT SDI I: ISB ISB NTM 5130001 6.00 B2142 53-0287 PART 11 6.00 POSTSPECIAL DETAILED INSPECTION OF AREA OF RIB 1 NTM 513010(53-0282)PART 1ACCESS: 542CB CN : TBD* 1.50642CB ISB 53-0287* 1.50539007-0603-2 141 CENTER SECTION NDT SDI I: ISB CN CN1 1.00 ALL142 53-0296 FAA AD F-1998-481-2701 1.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 231APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)539007-0603-2 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION OF THE AFT FITTING AT FR ISB FAA AD40. 2002-07-05ISB 53-0296ACCESS: 147FZ 147GZ* 0.07148GZ* 0.03539008-0603-1 121 ELECTRONIC RACK 101VU MEC DET T: 7000 FC CN CN1 0.50 PRE 10414122 I: 2300 FC FAA AD 1992-253-138(B) 1 0.50 (53-0294)DETAILED INSPECTION OF THE LOWER ATTACHMENT ISB FAA AD 96-12-15BEAM. ISB 53-0300ACCESS: 121BL* 0.01539009-0603-1 151 EMERGENCY EXIT NDT SDI T: 18 MO CN NTM 5120131 0.25 ALL152 I: 18 MO FAA AD PART 11 0.25241 SPECIAL DETAILED INSPECTION OF THE SKIN PANEL ISB NTM 5140001 0.25242 PART 11 0.25251 CN1 0.25252 1997-357-231(B) 1 0.25FAA AD 98-20-13ISB 53-0301539010-0603-1 831 DOORS MEC DET T: 10000 FC CN CN1 0.25 PRE 11286841 I: 600 FC FAA AD 1997-124-223(B) 1 0.25 (53-0334)DETAILED INSPECTION OF THE DOOR STOPS ISB FAA AD 98-20-22ISB 53-0309ACCESS: OPEN THE DOORS539010-0603-2 831 DOORS MEC DET T: 20000 FC CN CN1 0.25 POST 11286841 I: 4500 FC FAA AD 1997-124-223(B) 1 0.25 (53-0334)DETAILED INSPECTION OF THE DOOR STOPS ISB FAA AD 98-20-22ISB 53-0309ACCESS: OPEN THE DOORS539011-0603-1 251 EMERGENCY EXIT DOOR FRAMES NDT SDI T: 10 YE ISB NTM 5330541 5.00 ALL252 I: 5 YE PART 61 5.00SPECIAL DETAILED INSPECTION OF EMERGENCY EXIT ISB 53-0311DOORFRAMES STRUCTURE* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 232APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)539011-0603-1 * * * * * C O N T I N U E * * * * *ACCESS: REMOVE THE DOORFRAME LININGS, REMOVE THEINSULATION TO THE INSPECTED AREA539012-0603-1 147 CENTER SECTION NDT SDI T: 11000 FC ISB NTM 5130101 2.00 B2148 I: 2100 FC PART 11 2.00SPECIAL DETAILED INSPECTION OF THE FORWARD CANTED NTM 513105FRAME PART 6ISB 53-0314ACCESS: OPEN THE MAIN LANDING GEAR DOORSR 539013-0603-1 123 NLG BAY NDT SDI T: 10000 FC ISB NTM 5130101 1.00 ALL124 I: 3400 FC PART 11 1.00SPECIAL DETAILED INSPECTION OF LOWER HOLES OF THE NTM 513104KEEL BEAM OF NLG BAY CONNECTING FITTING IN NLG BAY PART 1BETWEEN FR 13 AND FR 14. ISB 53-0327ACCESS: REMOVE INSULATION AS REQUIREDACCESS: 121NF 122HF 713 811* 0.60132AZ 714 831* 0.16539014-0603-1 131 FUSELAGE MEC DET T: ISB ISB ISB 53-03411 4.00 B4-100132 53-03411 4.00 B4-200135 DETAILED INSPECTION OF THE SKIN PANELS AT I: 1400 FC1 4.00 PRE (53-0336)136 THE LAP JOINT BETWEEN STRINGERS 42 AND 43 AND1 4.00137 BETWEEN FRAMES 37 AND 39 LH AND RH CRACKS1 4.001381 4.00ACCESS: 131ABF 131AFF* 0.30132LF 132NF* 0.91137AM* 0.31138QF* 0.30539015-0603-1 145 CENTER SECTION NDT SDI I: ISB CN NTM 5130101 5.00 B4146 53-0350 FAA AD PART 11 5.00 C4241 SPECIAL DETAILED INSPECTION OF HOLES FR 47 SPLICE ISB CN 2002-184(B)1 5.00 F4242 FITTING BETWEEN STRG 24 AND STRG 25 LH AND RH SIDES. FAA AD1 5.002004-20-14* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 233APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)539015-0603-1 * * * * * C O N T I N U E * * * * *ACCESS: REMOVE THE PASSENGER SEATS, LOWER SIDEWALL ISB 53-0350PANELS, INSULATION AT FR 47539016-0603-1 231 FUSELAGE FORWARD SECTION NDT SDI I: 2500 FC ISB NTM 5314051 5.00 MSN 003 TO 156232 PART 41 5.00SPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW CN 2002-639(B)STRINGER 11 BETWEEN FRAME 28A AND FRAME 31 LH/RH. FAA AD2000-02-39ACCESS: REMOVE THE FWD UPPER, CENTER UPPER AND AFT ISB 53-0354UPPER DOOR-FRAME PANELS539016-0603-2 231 FUSELAGE FORWARD SECTION NDT SDI I: 6500 FC ISB NTM 5314051 5.00 MSN 157 TO 305232 PART 41 5.00SPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW CN 2002-639(B)STRINGER 11 BETWEEN FRAME 28A AND FRAME 31 LH/RH. FAA AD2000-02-39ACCESS: REMOVE THE FWD UPPER, CENTER UPPER AND AFT ISB 53-0354UPPER DOOR-FRAME PANELS539017-0603-1 131 FUSELAGE FORWARD AND AFT INTERMEDIATE NDT SDI T: 30300 FC CN NTM 5314060 N/A MSN 001 TO 156132 SECTION I: 4100 FC ISB PART 40 N/A B2153 NTM 5316010 N/A B4-100154 SPECIAL DETAILED INSPECTION OF SKIN LAP JOINTS BELOW PART 40 N/A B4-200STRINGER 27 BETWEEN FRAME 28A AND FRAME 30A LH AND CN 2002-639(B)F4RH, AND AT STRINGER 52 BETWEEN FRAME 56 AND FRAME 58 FAA ADLH AND RH. 2004-08-05ISB 53-0356ACCESS: REMOVE THE INSULATION IN THE AREA TO INSPECT.539017-0603-2 131 FUSELAGE FORWARD AND AFT INTERMEDIATE NDT SDI T: 30300 FC AD NTM 5314060 N/A MSN 001 TO 156132 SECTION I: 4100 FC CN PART 40 N/A C4153 ISB NTM 5316010 N/A154 SPECIAL DETAILED INSPECTION OF SKIN LAP JOINTS BELOW PART 40 N/ASTRINGER 27 BETWEEN FRAME 28A AND FRAME 30A RH, AND AD 2004-08-05AT STRINGER 52 BETWEEN FRAME 56 AND FRAME 58 LH AND CN 2002-639(B)RH. ISB 53-0356ACCESS: REMOVE THE INSULATION IN THE AREA TO INSPECT.* * * * * E N D * * * * *STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION:3-53 PAGE 234APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540001-0602-1 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 5600 FC MRB S AMM SSI 5400011 0.17 B24161 0.17425 DETAILED INSPECTION OF JUNCTION OF RIB NO. 81 0.17426 AND SIDE PANEL.1 0.17540001-0602-2 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 4600 FC MRB S AMM SSI 5400011 0.17 B4-1004161 0.17425 DETAILED INSPECTION OF JUNCTION OF RIB NO. 81 0.17426 AND SIDE PANEL.1 0.17540001-0602-3 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 4400 FC MRB S AMM SSI 5400011 0.17 B4-2004161 0.17 C4425 DETAILED INSPECTION OF JUNCTION OF RIB NO. 81 0.17 F4426 AND SIDE PANEL.1 0.17540002-0604-1 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 27300 FC MRB S AMM SSI 5400021 0.33 B24161 0.33425 DETAILED INSPECTION OF JUNCTION OF RIB NO.81 0.33426 AND SIDE PANEL.1 0.33ACCESS: 415AL* 0.08416AR* 0.05425AL* 0.08426AR* 0.05540002-0604-2 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 22600 FC MRB S AMM SSI 5400021 0.33 B4-1004161 0.33425 DETAILED INSPECTION OF JUNCTION OF RIB NO.81 0.33426 AND SIDE PANEL.1 0.33ACCESS: 415AL* 0.08416AR* 0.05425AL* 0.08426AR* 0.05540002-0604-3 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 19200 FC MRB S AMM SSI 5400021 0.33 B4-2004161 0.33 C4425 DETAILED INSPECTION OF JUNCTION OF RIB NO.81 0.33 F4426 AND SIDE PANEL.1 0.33* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540002-0604-3 * * * * * C O N T I N U E * * * * *ACCESS: 415AL* 0.08416AR* 0.05425AL* 0.08426AR* 0.05540003-0602-1 473 RIB 18 TO SIDE PANEL JUNCT. MEC DET I: 8400 FC MRB S AMM SSI 5400031 0.17 B24741 0.17 PRE 02434483 DETAILED INSPECTION OF RIB 18 TO SIDE1 0.17484 PANEL JUNCTION.1 0.17540003-0602-2 473 RIB 18 TO SIDE PANEL JUNCT. MEC DET I: 7000 FC MRB S AMM SSI 5400031 0.17 B4-1004741 0.17 PRE 02434483 DETAILED INSPECTION OF RIB 18 TO SIDE1 0.17484 PANEL JUNCTION.1 0.17540003-0602-3 473 RIB 18 TO SIDE PANEL JUNCT. MEC DET I: 6600 FC MRB S AMM SSI 5400031 0.17 B4-2004741 0.17 C4483 DETAILED INSPECTION OF RIB 18 TO SIDE1 0.17 F4484 PANEL JUNCTION.1 0.17 PRE 02434540004-0602-1 473 RIB 18 & SIDE PANEL JUNCT. MEC DET I: 5600 FC MRB S AMM SSI 5400041 0.17 B24741 0.17 POST 02434483 DETAILED INSPECTION OF JUNCTION OF RIB 181 0.17 OR484 WITH SIDE PANELS.1 0.17 POST 02738540004-0602-2 473 RIB 18 & SIDE PANEL JUNCT. MEC DET I: 4600 FC MRB S AMM SSI 5400041 0.17 B4-1004741 0.17 POST 02434483 DETAILED INSPECTION OF JUNCTION OF RIB 181 0.17 OR484 WITH SIDE PANELS.1 0.17 POST 02738540004-0602-3 473 RIB 18 & SIDE PANEL JUNCT. MEC DET I: 4400 FC MRB S AMM SSI 5400041 0.17 B4-2004741 0.17 C4483 DETAILED INSPECTION OF JUNCTION OF RIB 181 0.17 F4484 WITH SIDE PANELS, INCLUDING ZONES 474/484.1 0.17 POST 02434ORPOST 02738STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540004-0603-1 473 RIB 18 TO SIDE PANEL JUNCTION NDT SDI I: 8400 FC MRB S AMM SSI 5400041 1.00 B2474 NTM 5410001 1.00 POST 02434483 DETAILED AND SPECIAL DETAILED INSPECTION OF RIB 18 PART 21 1.00 OR484 INCLUDING JUNCTION WITH SIDE PANELS AND UPPER SPAR.1 1.00 POST 02738ACCESS: 473AL 473CL* 0.29474AR 474CR* 0.29483AL 483CL* 0.29484AR 484CR* 0.29540004-0603-2 473 RIB 18 TO SIDE PANEL JUNCTION NDT SDI I: 7000 FC MRB S AMM SSI 5400041 1.00 B4-100474 NTM 5410001 1.00 POST 02434483 DETAILED AND SPECIAL DETAILED INSPECTION OF RIB 18 PART 21 1.00 OR484 INCLUDING JUNCTION WITH SIDE PANELS AND UPPER SPAR.1 1.00 POST 02738ACCESS: 473AL 473CL* 0.29474AR 474CR* 0.29483AL 483CL* 0.29484AR 484CR* 0.29540004-0603-3 473 RIB 18 TO SIDE PANEL JUNCTION NDT SDI I: 6600 FC MRB S AMM SSI 5400041 1.00 B4-200474 NTM 5410001 1.00 C4483 DETAILED AND SPECIAL DETAILED INSPECTION OF RIB 18 PART 21 1.00 F4484 INCLUDING JUNCTION WITH SIDE PANELS AND UPPER SPAR.1 1.00 POST 02434ORACCESS: 473AL 473CL* 0.29 POST 02738474AR 474CR* 0.29483AL 483CL* 0.29484AR 484CR* 0.29540005-0604-1 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 27300 FC MRB S AMM SSI 5400051 1.00 B2416 NTM 5410001 1.00 PRE 02434425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 21 1.00426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.1 1.00ACCESS: 413EL 415AL* 0.25416AR* 0.05423EL 425AL* 0.25426AR* 0.05STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540005-0604-2 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 22600 FC MRB S AMM SSI 5400051 1.00 B4-100416 NTM 5410001 1.00 PRE 02434425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 21 1.00426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.1 1.00ACCESS: 413EL 415AL* 0.25416AR* 0.05425AL* 0.08426AR* 0.05540005-0604-3 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 19200 FC MRB S AMM SSI 5400051 1.00 B4-200416 NTM 5410001 1.00 C4425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 21 1.00 F4426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.1 1.00 PRE 02434ACCESS: 413EL 415AL* 0.25416AR* 0.05423EL 425AL* 0.25426AR* 0.05540006-0603-1 470 NACELLES/PYLON RIB 1 TO 18 MEC DET I: 4000 FH ISB CN1 1.00 POST 00733480 1990-222-116(B) 1 1.00 PRE 02434DETAILED EXTERNAL AND INTERNAL INSPECTION OF FAA AD 96-0808THE BOLT/NUT ASSEMBLIES DIAMETER 6.35 MM (0.21 IN) ISB 54-0045BETWEEN RIB 8 AND RIB 18 AND CHECK NUTS FOR TIGHTNESSNOTE: ENGINE FIRE EXTINGUISHER BOTTLES REMOVEDACCESS: 413CL 413DL 414CR 414DR 415AL 416AR* 5.56471AL 471BL 472AR 472BR 473AL 473BL473CL 473DL 474BR 474CR 474DR 475AL475BL 475CL 476AR 476BR423CL 423DL 424CR 424DR 425AL 426AR* 5.59481AL 481BL 482AR 482BR 483BL 483CL483DL 484AR 484BR 484CR 484DR 485AL485BL 485CL 486AR 486BR540006-0604-1 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 27300 FC MRB S AMM SSI 5400061 1.00 B2416 NTM 5410001 1.00 POST 02434425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 21 1.00426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.1 1.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540006-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 413GL 415AL* 0.24416AR* 0.05423GL 425AL* 0.24426AR* 0.05540006-0604-2 415 LOWER SPAR BETWEEN RIB 7/9 MEC SDI I: 22600 FC MRB S AMM SSI 5400061 2.00 B4-100416 NTM 5410001 2.00 POST 02434425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 21 2.00426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.1 2.00ACCESS: 413GL 415AL* 0.24416AR* 0.05423GL 425AL* 0.24426AR* 0.05540006-0604-3 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 19200 FC MRB S AMM SSI 5400061 1.00 B4-200416 NTM 5410001 1.00 C4425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 21 1.00 F4426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.1 1.00 POST 02434ACCESS: 413GL 415AL* 0.24416AR* 0.05423GL 425AL* 0.24426AR* 0.05540007-0602-1 473 JUNCTION OF SIDE PANEL MEC DET I: 8400 FC MRB S AMM SSI 5400071 0.17 B2474 AMM SSI 5400081 0.17483 DETAILED INSPECTION OF SIDE PANEL TO1 0.17484 UPPER SPAR JUNCTION BETWEEN RIB 12 AND 18.1 0.17540007-0602-2 473 JUNCTION OF SIDE PANEL MEC DET I: 7000 FC MRB S AMM SSI 5400071 0.17 B4-100474 AMM SSI 5400081 0.17483 DETAILED INSPECTION OF SIDE PANEL TO1 0.17484 UPPER SPAR JUNCTION BETWEEN RIB 12 AND 18.1 0.17STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540007-0602-3 473 JUNCTION OF SIDE PANEL MEC DET I: 6600 FC MRB S AMM SSI 5400071 0.17 B4-200474 AMM SSI 5400081 0.17 C4483 DETAILED INSPECTION OF SIDE PANEL TO1 0.17 F4484 UPPER SPAR JUNCTION BETWEEN RIB 12 AND 18.1 0.17540009-0604-1 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 27300 FC MRB S AMM SSI 5400091 1.00 B2474 NTM 5410001 1.00 PRE 02434483 DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 21 1.00484 SPAR CAPS AND WEB BETWEEN RIB 12 AND 18.1 1.00ACCESS: 471BL 473AL 473BL* 0.55472BR 474BR* 0.75481BL 483BL* 0.82482BR 484AR 484BR* 0.50540009-0604-2 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 22600 FC MRB S AMM SSI 5400091 1.00 B4-100474 NTM 5410001 1.00 PRE 02434483 DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 21 1.00484 SPAR CAPS AND WEB BETWEEN RIB 12 AND 18.1 1.00ACCESS: 471BL 473AL 473BL* 0.55472BR 474BR* 0.75481BL 483BL* 0.82482BR 484AR 484BR* 0.50540009-0604-3 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 19200 FC MRB S AMM SSI 5400091 1.00 B4-200474 NTM 5410001 1.00 C4483 DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 21 1.00 F4484 SPAR CAPS AND WEB BETWEEN RIB 12 AND 18.1 1.00 PRE 02434ACCESS: 471BL 473AL 473BL* 0.55472BR 474BR* 0.75481BL 483BL* 0.82482BR 484AR 484BR* 0.50540010-0604-1 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 27300 FC MRB S AMM SSI 5400101 1.00 B2474 NTM 5410001 1.00 POST 02434483 VISUAL AND SPECIAL DETAILED INSPECTION OF UPPER SPAR PART 21 1.00484 CAP AND WEB.BETWEEN RIB 12 AND 18.1 1.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540010-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 471BL 473AL 473BL* 0.55472BR 474AR 474BR* 0.76481BL 483AL 483BL* 0.84482BR 484AR 484BR* 0.50540010-0604-2 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 22600 FC MRB S AMM SSI 5400101 1.00 B4-100474 NTM 5410001 1.00 POST 02434483 VISUAL AND SPECIAL DETAILED INSPECTION OF UPPER SPAR PART 21 1.00484 CAP AND WEB.BETWEEN RIB 12 AND 18.1 1.00ACCESS: 471BL 473AL 473BL* 0.55472BR 474AR 474BR* 0.76481BL 483AL 483BL* 0.84482BR 484AR 484BR* 0.50540010-0604-3 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 19200 FC MRB S AMM SSI 5400101 1.00 B4-200474 NTM 5410001 1.00 C4483 VISUAL AND SPECIAL DETAILED INSPECTION OF UPPER SPAR PART 21 1.00 F4484 CAP AND WEB.BETWEEN RIB 12 AND 18.1 1.00 POST 02434ACCESS: 471BL 473AL 473BL* 0.55472BR 474AR 474BR* 0.76481BL 483AL 483BL* 0.84482BR 484AR 484BR* 0.50540011-0603-2 471 SPIGOT RECEPTACLE FITTING MEC DET T: 7,5 YE ISB AMM SSI 5400111 0.50 POST 02434472 I: 5 YE MRB S ISB 54-00761 0.50 PRE 10459473 DETAILED INSPECTION OF SPIGOT RECEPTACLE1 0.50 (54-0077)474 FITTING INCLUDING SPHERICAL BEARING AND BUSH.1 0.50 PRE 102614811 0.50 (54-0076)482 PREP.: SPHERICAL BEARING AND BUSH TO BE REMOVED1 0.504831 0.504841 0.50ACCESS: 471AL 471BL* 0.35472AR 472BR* 0.53473AL* 0.01474AR* 0.01481AL 481BL* 0.55482AR 482BR* 0.36* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540011-0603-2 * * * * * C O N T I N U E * * * * *483AL* 0.01484AR* 0.01540011-0603-3 471 SPIGOT RECEPT. FITTING MEC DET I: 10 YE MRB S AMM SSI 5400111 0.50 POST 024344721 0.50 POST 10459473 DETAILED INSPECTION OF SPIGOT RECEPTACLE1 0.50 (54-0077)474 FITTING INCLUDING SPHERICAL BEARING AND BUSH.1 0.504811 0.50482 NOTE: SPHERICAL BEARING AND BUSH TO BE REMOVED1 0.504831 0.504841 0.50ACCESS: 471AL 471BL* 0.35472AR 472BR* 0.53473AL* 0.01481AL 481BL* 0.55482AR 482BR* 0.36484AR* 0.01540011-0603-4 471 SPIGOT RECEPTACLE FITTING MEC DET T: 7,5 YE ISB ISB 54-00761 0.50 POST 02434472 I: 7,5 YE1 0.50 PRE 10459473 DETAILED INSPECTION OF SPIGOT RECEPTACLE1 0.50 (54-0077)474 FITTING INCLUDING SPHERICAL BEARING AND BUSH.1 0.50 POST 102614811 0.50 (54-0076)482 PREP.: SPHERICAL BEARING AND BUSH TO BE REMOVED1 0.504831 0.504841 0.50ACCESS: 471AL 471BL* 0.35472AR 472BR* 0.53473AL* 0.01474AR* 0.01481AL 481BL* 0.55482AR 482BR* 0.36483AL* 0.01484AR* 0.01540012-0603-1 413 NACELLES/PYLONS - RIB 8 MEC DET T: 10700 FH ISB ISB 54-00891 0.50 PRE 02434414 I: 10700 FH1 0.50 PRE 10822423 DETAILED INSPECTION OF THE TRUSS BARS AT THE1 0.50 (54-0090)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)540012-0603-1 * * * * * C O N T I N U E * * * * *424 HYDRAULIC BRACKET ATTACHMENTS AT RIB 8.1 0.50PREP: -BLEED AIR PRECOOLER AND COLD AIR INLET DUCTTO BE REMOVED-HYDRAULIC BRACKETS AT RIB 8 TO BR REMOVEDACCESS: 413EL* 0.17423EL* 0.17541001-0604-1 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 27300 FC MRB S AMM SSI 5410011 1.00 B2416 NTM 5410001 1.00 PRE 02434425 SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 21 1.00426 AND SIDE PANELS FROM RIB 1 TO 2.1 1.00ACCESS: 413EL 451AL* 0.19452AR* 0.01423EL* 0.17461AL 462AR* 0.02541001-0604-2 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 22600 FC MRB S AMM SSI 5410011 1.00 B4-100416 NTM 5410001 1.00 PRE 02434425 SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 21 1.00426 AND SIDE PANELS FROM RIB 1 TO 2.1 1.00ACCESS: 413EL 451AL* 0.19452AR* 0.01423EL* 0.17461AL 462AR* 0.02541001-0604-3 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 19200 FC MRB S AMM SSI 5410011 1.00 B4-200416 NTM 5410001 1.00 C4425 SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 21 1.00 F4426 AND SIDE PANELS FROM RIB 1 TO 2.1 1.00 PRE 02434ACCESS: 413EL 451AL* 0.19452AR* 0.01423EL* 0.17461AL 462AR* 0.02STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541002-0604-1 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 27300 FC MRB S AMM SSI 5410021 2.00 B2425 NTM 5410001 2.00 POST 02434SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2AND SIDE PANELS FROM RIB 1 TO 2 INCLUDING ZONES416/426ACCESS: 413GL 451AL 452AR* 0.19423GL 461AL 462AR* 0.19541002-0604-2 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 22600 FC MRB S AMM SSI 5410021 2.00 B4-100425 NTM 5410001 2.00 POST 02434SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2AND SIDE PANELS FROM RIB 1 TO 2 INCLUDING ZONES416/426ACCESS: 413GL 451AL 452AR* 0.19423GL 461AL 462AR* 0.19541002-0604-3 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 19200 FC MRB S AMM SSI 5410021 2.00 B4-200425 NTM 5410001 2.00 C4SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2F4AND SIDE PANELS FROM RIB 1 TO 2 INCLUDING ZONESPOST 02434416/426ACCESS: 413GL 451AL 452AR* 0.19423GL 461AL 462AR* 0.19541003-0604-1 415 LUGS PYLON-WING ATTACH MEC SDI I: 27300 FC MRB S AMM SSI 5410031 40.00 B2425 NTM 5440001 40.00DETAILED AND SPECIAL DETAILED INSPECTION OF PYLON TO PART 4WING ATTACH FITTING LUGS AT RIB 12, WITH LINKS NTM 544000REMOVED, INCLUDING ZONES 416 426 473 474 483 484 PART 6ACCESS: 471AL 472AR* 0.61481AL 482AR* 0.62541003-0604-2 415 LUGS PYLON-WING ATTACH MEC SDI I: 22600 FC MRB S AMM SSI 5410031 40.00 B4-100425 NTM 5440001 40.00DETAILED AND SPECIAL DETAILED INSPECTION OF PYLON TO PART 4WING ATTACH FITTING LUGS AT RIB 12, WITH LINKS NTM 544000REMOVED, INCLUDING ZONES 416 426 473 474 483 484 PART 6* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541003-0604-2 * * * * * C O N T I N U E * * * * *ACCESS: 471AL 472AR* 0.61481AL 482AR* 0.62541003-0604-3 471 LUGS PYLON-WING ATTACH MEC SDI I: 19200 FC MRB S AMM SSI 5410031 40.00 B4-200481 NTM 5440001 40.00 C4DETAILED AND SPECIAL DETAILED INSPECTION OF PYLON TO PART 4F4WING ATTACH FITTING LUGS AT RIB 12, WITH LINKS NTM 544000REMOVED, INCLUDING ZONES 415 416 425 426 473 474 483 PART 6484PREP: ENGINE TO BE REMOVEDACCESS: 471AL 472AR* 0.61481AL 482AR* 0.62541005-0604-1 415 RIB 12 & ATTACH FITTING MEC DET I: 27300 FC MRB S AMM SSI 5410051 0.33 B24251 0.33DETAILED INSPECTION OF RIB 12 AND PORTION OFTHE WING ATTACHMENT FITTING INSIDE THE PYLONINCLUDING ZONES 416, 426, 473, 474, 483 AND 484ACCESS: 415AL 416AR 473AL* 0.14425AL 426AR 484AR* 0.14541005-0604-2 415 RIB 12 & ATTACH FITTING MEC DET I: 22600 FC MRB S AMM SSI 5410051 0.33 B4-1004251 0.33DETAILED INSPECTION OF RIB 12 AND PORTION OFTHE WING ATTACHMENT FITTING INSIDE THE PYLONINCLUDING ZONES 416, 426, 473, 474, 483 AND 484ACCESS: 415AL 416AR 473AL* 0.14425AL 426AR 484AR* 0.14541005-0604-3 415 RIB 12 & ATTACH FITTING MEC DET I: 19200 FC MRB S AMM SSI 5410051 0.33 B4-2004251 0.33 C4DETAILED INSPECTION OF RIB 12 AND PORTION OFF4THE WING ATTACHMENT FITTING INSIDE THE PYLONINCLUDING ZONES 416, 426, 473, 474, 483 AND 484* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541005-0604-3 * * * * * C O N T I N U E * * * * *ACCESS: 415AL 416AR 473AL* 0.14425AL 426AR 484AR* 0.14541007-0604-1 473 LUGS PYLON-WING ATTACH NDT SDI I: 27300 FC MRB S AMM SSI 5410071 5.00 B2483 NTM 5440001 5.00 PRE 02434SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4FITTING LUG AT RIB 18 INCLUDING ZONES 474 AND 484 NTM 544000PART 6ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03541007-0604-2 473 LUGS PYLON-WING ATTACH NDT SDI I: 22600 FC MRB S AMM SSI 5410071 5.00 B4-100483 NTM 5440001 5.00 PRE 02434SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4FITTING LUG AT RIB 18 INCLUDING ZONES 474 AND 484 NTM 544000PART 6ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03541007-0604-3 473 LUGS PYLON-WING ATTACH NDT SDI I: 19200 FC MRB S AMM SSI 5410071 5.00 B4-200483 NTM 5440001 5.00 C4SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4F4FITTING LUG AT RIB 18 INCLUDING ZONES 474 AND 484 NTM 544000PRE 02434PART 6ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03541008-0603-1 473 LUG PYLON-WING ATTACH NDT SDI I: 8400 FC MRB S AMM SSI 5410081 5.00 B2483 NTM 5440001 5.00 POST 02434SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4FITTING LUG AT RIB 18 NTM 544000PART 6ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541008-0603-2 473 LUG PYLON-WING ATTACH NDT SDI I: 7000 FC MRB S AMM SSI 5410081 5.00 B4-100483 NTM 5440001 5.00 POST 02434SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4FITTING LUG AT RIB 18 NTM 544000PART 6ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03541008-0603-3 473 LUG PYLON-WING ATTACH NDT SDI I: 6600 FC MRB S AMM SSI 5410081 5.00 B4-200483 NTM 5440001 5.00 C4SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4F4FITTING LUG AT RIB 18 NTM 544000POST 02434PART 6ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03541009-0604-1 473 PYLON-WING ATTACH RIB 18 MEC SDI I: 27300 FC MRB S AMM SSI 5410091 0.33 B2483 NTM 541000 PART 1 0.33 PRE 02434SPECIAL DETAILED INSPECTION OF JUNCTION OF PYLON TO 2WING ATTACHMENT FITTING TO RIB 18 AND SIDE WALLSINCLUDING ZONES 474/484.ACCESS: 473AL 473CL 474CR* 0.56483CL 484AR 484CR* 0.56541009-0604-2 473 PYLON-WING ATTACH RIB 18 MEC SDI I: 22600 FC MRB S AMM SSI 5410091 0.33 B4-100483 NTM 541000 PART 1 0.33 PRE 02434SPECIAL DETAILED INSPECTION OF JUNCTION OF PYLON TO 2WING ATTACHMENT FITTING TO RIB 18 AND SIDE WALLSINCLUDING ZONES 474/484.541009-0604-3 473 PYLON-WING ATTACH RIB 18 MEC SDI I: 19200 FC MRB S AMM SSI 5410091 0.33 B4-200483 NTM 541000 PART 1 0.33 C4SPECIAL DETAILED INSPECTION OF JUNCTION OF PYLON TO 2F4WING ATTACHMENT FITTING TO RIB 18 AND SIDE WALLSPRE 02434INCLUDING ZONES 474/484.STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541010-0603-1 470 PYLON OUTER LATERAL PANELS NDT SDI T: 30000 FH ISB NTM 5440041 2.50 GE480 OR PART 41 2.50 PRE 10598SPECIAL DETAILED INSPECTION OF PYLON OUTER LATERAL 15000 FC EASA AD(54-0085)PANEL BETWEEN RIB 12 AND RIB 18. I: 3000 FH 1990-116(B)PRE 02434OR FAA AD 96-08-08ACCESS: 473AL 15 MO ISB 54-0084* 0.01484AR* 0.01541011-0604-1 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 27300 FC MRB S AMM SSI 5410111 2.00 B2425 NTM 5410001 2.00 PRE 02434DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2SPAR CAPS AND WEB BETWEEN RIB 8 AND 12, INCLUDINGZONES 416/426ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13541011-0604-2 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 22600 FC MRB S AMM SSI 5410111 2.00 B4-100425 NTM 5410001 2.00 PRE 02434DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2SPAR CAPS AND WEB BETWEEN RIB 8 AND 12, INCLUDINGZONES 416/426ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13541011-0604-3 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 19200 FC MRB S AMM SSI 5410111 2.00 B4-200425 NTM 5410001 2.00 C4DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2F4SPAR CAPS AND WEB BETWEEN RIB 8 AND 12, INCLUDINGPRE 02434ZONES 416/426ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13541012-0604-1 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 27300 FC MRB S AMM SSI 5410121 2.00 B2425 NTM 5410001 2.00 POST 02434DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2SPAR CAPS AND WEB BETWEEN RIB 8 AND 12 INCLUDINGZONES 416/426* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541012-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13541012-0604-2 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 22600 FC MRB S AMM SSI 5410121 2.00 B4-100425 NTM 5410001 2.00 POST 02434DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2SPAR CAPS AND WEB BETWEEN RIB 8 AND 12 , INCLUDINGZONES 416/426ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13541012-0604-3 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 19200 FC MRB S AMM SSI 5410121 2.00 B4-200425 NTM 5410001 2.00 C4DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2F4SPAR CAPS AND WEB BETWEEN RIB 8 AND 12 INCLUDINGPOST 02434ZONES 416/426.ACCESS: 415AL 416AR* 0.13425AL 426AR* 0.13541101-0603-1 415 NACELLES/PYLONS ENG DET T: 8000 FH CN CN EU1 3.00 GE416 I: 750 FH FAA AD 1990-222-116(B) 1 3.00 PRE 07175425 DETAILED INSPECTION OF RIB 6 SKIN PANEL LH AND RH ISB FAA AD1 3.00 (54-0067)426 AROUND FIRST CORE COWL FITTING. 2000-10-011 3.00 PRE 02434ISB 54-0066NOTE: CORECOWL DOORS TO BE OPENED.541102-0603-1 415 NACELLES/PYLONS NDT SDI T: 7000 FH ISB ISB 54-0681 2.00 GE416 I: 1200 FH1 2.00 MSN 003 TO 161425 SPECIAL DETAILED INSPECTION OF INNER TEE BRACKETS1 2.00 PW426 ON AFFECTED RIBS ON LH AND RH ENGINE PYLONS.1 2.00NOTE : PRECOOLER, RODS AND AIR DUCTS TO BE REMOVED.541105-0603-1 415 NACELLE/PYLON-LOWER SPAR NDT SDI T: 9000 FC CN NTM 5440101 2.00 GE416 I: 2500 FC FAA AD PART 6 OR 91 2.00 POST 02434425 SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB1 2.00 PRE 10328* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541105-0603-1 * * * * * C O N T I N U E * * * * *426 UPPER SURFACE BETWEEN RIB 9 AND RIB 10. EASA AD1 2.00 (54-0079)1992-049-130(B)ACCESS: 415AL FAA AD 95-10-03 * 0.08416AR ISB 54-0071* 0.05425AL* 0.08426AR* 0.05541105-0603-2 415 NACELLE/PYLON-LOWER SPAR NDT SDI T: 6000 FC CN NTM 5440101 1.00 PW416 I: 2500 FC FAA AD PART 6 OR 91 1.00 PRE 10328425 SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD1 1.00 (54-0079)426 UPPER SURFACE BETWEEN RIB 9 AND RIB 10. 1992-049-130(B) 1 1.00FAA AD 95-10-03ACCESS: 415AL ISB 54-0071* 0.08416AR* 0.05425AL* 0.08426AR* 0.05541107-0603-1 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 10900 FC CN NTM 5440111 1.00 GE423 I: 6700 FC FAA AD PART 6 OR 91 1.00 PRE 10335SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD(54-0080)BETWEEN RIB 6 AND RIB 7. 1993-228-154(B) POST 02434FAA ADPREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE 2000-10-18REMOVED ISB 54-0073ACCESS: 413GL* 0.17423GL* 0.17541107-0603-2 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 8600 FC CN NTM 5440111 1.00 PW423 I: 5700 FC FAA AD PART 6 OR 91 1.00 PRE 10335SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD(54-0080)BETWEEN RIB 6 AND RIB 7. 1993-228-154(B) POST 02434FAA ADPREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE 2000-10-18REMOVED ISB 54-0073ACCESS: 413GL* 0.17423GL* 0.17STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541107-0603-3 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 10900 FC CN NTM 5440111 1.00 GE423 I: 6700 FC FAA AD PART 6 OR 91 1.00 PRE 10335SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD(54-0080)BETWEEN RIB 6 AND RIB 7. 1993-228-154(B) PRE 02434FAA ADPREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE 2000-10-18REMOVED ISB 54-0073ACCESS: 413GL* 0.17423GL* 0.17541107-0603-4 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 30300 FC CN NTM 5440111 1.00 GE423 I: 21300 FC FAA AD PART 6 OR 91 1.00 POST 10335SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD(54-0080)BETWEEN RIB 6 AND RIB 7. 1993-228-154(B) POST 02434FAA ADNOTE: THRESHOLD COUNTED FROM MOD 10335 EMBODIMENT. 2000-10-18ISB 54-0073PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BEREMOVEDACCESS: 413GL* 0.17423GL* 0.17541107-0603-5 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 24000 FC CN NTM 5440111 1.00 PW423 I: 18200 FC FAA AD PART 6 OR 91 1.00 POST 10335SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD(54-0080)BETWEEN RIB 6 AND RIB 7. 1993-228-154(B)FAA ADNOTE: THRESHOLD COUNTED FROM MOD 10335 EMBODIMENT. 2000-10-18ISB 54-0073PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BEREMOVEDACCESS: 413GL* 0.17423GL* 0.17541107-0603-6 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 30300 FC CN NTM 5440111 1.00 GE423 I: 21300 FC FAA AD PART 6 OR 91 1.00 POST 10335SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD(54-0080)BETWEEN RIB 6 AND RIB 7. 1993-228-154(B) PRE 02434* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)541107-0603-6 * * * * * C O N T I N U E * * * * *NOTE: THRESHOLD COUNTED FROM MOD 10335 EMBODIMENT. FAA AD2000-10-18PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE ISB 54-0073REMOVEDACCESS: 413GL* 0.17423GL* 0.17543001-0602-1 415 SIDE SKIN RIB 1-18 MEC DET T: 11200 FC ALI EASA AD1 0.25 B2416 OR FAA AD 2006-00711 0.25 FROM 0 FC/FH425 DETAILED INSPECTION OF SIDE SKIN PANELS 12700 FH FAA AD1 0.25 TO LOV426 BETWEEN RIB 1 AND RIB 18. I: 8400 FC 2007-04-111 0.25473 OR1 0.25474 PREP.: COWLS TO BE OPENED. 9500 FH ALI REFERENCE: 1 0.25483 543001-01-11 0.254841 0.25543001-0602-2 415 SIDE SKIN RIB 1-18 MEC DET T: 10100 FC ALI EASA AD1 0.30 B4-100416 OR FAA AD 2006-00711 0.30 FROM 0 FC/FH425 DETAILED INSPECTION OF SIDE SKIN PANELS 14000 FH FAA AD1 0.30 TO LOV426 BETWEEN RIB 1 AND RIB 18. I: 7600 FC 2007-04-111 0.30473 OR1 0.30474 PREP.: COWLS TO BE OPENED. 10500 FH ALI REFERENCE: 1 0.30483 543001-01-21 0.304841 0.30543001-0602-3 415 SIDE SKIN RIB 1-18 MEC DET T: 8800 FC ALI EASA AD1 0.30 B4-200416 OR FAA AD 2006-00711 0.30 C4425 DETAILED INSPECTION OF SIDE SKIN PANELS 20400 FH FAA AD1 0.30 F4426 BETWEEN RIB 1 AND RIB 18. I: 6600 FC 2007-04-111 0.30 FROM 0 FC/FH473 OR1 0.30 TO LOV474 PREP.: COWLS TO BE OPENED 15300 FH ALI REFERENCE: 1 0.30483 543001-01-31 0.304841 0.30543001-0602-4 415 SIDE SKIN RIB 1-18 NDT SDI T: 22400 FH AD NTM 5130001 0.30 GE425 I: SEE ISB ISB PART 11 0.30 PRE 02434DETAILED AND SPECIAL DETAILED INSPECTION OF INNER AD EUPRE (54-0046)DOUBLER AROUND THE FIRE EXTINGUISHER BOTTLE ACCESS 1992-082-131(B)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)543001-0602-4 * * * * * C O N T I N U E * * * * *DOOR, BETWEEN RIB 13 AND RIB 15 FAA AD 93-05-04ISB 54-0070ACCESS: 473AL* 0.01484AR* 0.01543002-0602-4 415 SIDE SKIN AT RIB 8 MEC DET T: 5350 FC AD AD EU-2008-0181 1 0.30 PRE 10431416 I: 4300 FC ISB ISB 54-00751 0.30 (54-0081)425 DETAILED INSPECTION OF PYLON SIDE PANELS AT1 0.30426 RIB 8 (UPPER SECTION).1 0.30543002-0602-5 415 SIDE SKIN AT RIB 8 NDT SDI T: 12900 FC AD NTM 544003 PART 1 0.30 POST 10431416 I: 21600 FC ISB 61 0.30 (54-0081)425 SPECIAL DETAILED INSPECTION AND DETAILED INSPECTION AD EU-2008-0181 1 0.30426 ON PYLON SIDE PANELS AT RIB 8 (UPPER SECTION). ISB 54-00751 0.30NOTE: THRESHOLD COUNTED FROM MOD 10431 EMBODIMENTACCESS: 413CL 413DL* 0.41414CR 414DR* 0.48423CL 423DL* 0.41424CR 424DR* 0.48544007-0604-1 471 LINKS PYLON-WING RIB 12 NDT SDI I: 27300 FC MRB S AMM SSI 5440071 40.00 B2481 NTM 5440001 40.00SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4TO WING AT RIB 12, WITH LINKS REMOVED INCLUDING ZONES472/482:PREP: ENGINE AND LINKS REMOVEDACCESS: 471AL 472AR* 0.61481AL 482AR* 0.62544007-0604-2 471 LINKS PYLON-WING RIB 12 NDT SDI I: 22600 FC MRB S AMM SSI 5440071 40.00 B4-100481 NTM 5440001 40.00SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4TO WING AT RIB 12, WITH LINKS REMOVED INCLUDING ZONES472/482* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)544007-0604-2 * * * * * C O N T I N U E * * * * *PREP: ENGINE AND LINKS REMOVEDACCESS: 471AL 472AR* 0.61481AL 482AR* 0.62544007-0604-3 471 LINKS PYLON-WING RIB 12 NDT SDI I: 19200 FC MRB S AMM SSI 5440071 40.00 B4-200481 NTM 5440001 40.00 C4SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4F4TO WING AT RIB 12, WITH LINKS REMOVED INCLUDING ZONES472/482PREP: ENGINE AND LINKS REMOVEDACCESS: 471AL 472AR* 0.61481AL 482AR* 0.62544009-0604-1 473 LINKS PYLON-WING RIB 18 NDT SDI I: 27300 FC MRB S AMM SSI 5440091 2.00 B2483 NTM 5440001 2.00SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4TO WING AT RIB 18 INCLUDING ZONES 474/484ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03544009-0604-2 473 LINKS PYLON-WING RIB 18 NDT SDI I: 22600 FC MRB S AMM SSI 5440091 2.00 B4-100483 NTM 5440001 2.00SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4TO WING AT RIB 18 INCLUDING ZONES 474/484ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03544009-0604-3 473 LINKS PYLON-WING RIB 18 NDT SDI I: 19200 FC MRB S AMM SSI 5440091 2.00 B4-200483 NTM 5440001 2.00 C4SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4F4TO WING AT RIB 18 INCLUDING ZONES 474/484PREP.: ENGINE AND LINKS REMOVED.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 20APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)544009-0604-3 * * * * * C O N T I N U E * * * * *ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03544011-0603-1 413 THRUST REV.COWL FITTING MEC DET I: ISB ISB AMM SSI 5440112 3.00 GE423 54-060 MRB S CN2 3.00 PRE 2434DETAILED INSPECTION OF THRUST REVERSER COWL 90-222-116(B)PRE 6770HINGE FITTINGS INCLUDING ZONES 414, 415/416, 424 AND FAA AD(54-065)425/426. 2000-10-01ISB 54-060ACCESS: 451AL 452AR* 0.02461AL 462AR* 0.02544012-0603-1 413 THRUST REV. COWL FITTING MEC DET I: ISB ISB AMM SSI 5440122 2.50 PW423 54-063 MRB S CN2 2.50 POST 2434DETAILED INSPECTION OF THRUST REVERSER COWL 90-222-116(B)PRE 6442HINGE FITTINGS INCLUDING ZONES 414, 415/416, 424 AND FAA AD(54-064)425/426. 2000-10-01ISB 54-063ACCESS: 451AL 452AR* 0.02461AL 462AR* 0.02544200-0603-1 415 PYLON - ENGINE FWD ATTACHMENT FITTING MEC DET T: 5 YE CPCP AMM 7100001 0.50 ALL416 I: 5 YE MRB S1 0.50425 DETAILED INSPECTION OF ENGINE FWD ATTACHMENT AND MRB REFERENCE: 1 0.50426 PYLON LOWER SPAR IN AREA OF FWD ATTACH FITTINGS1 0.50544200-C603-1PREP.: ENGINE TO BE REMOVED544200-0603-2 410 PYLON - ENGINE AFT ATTACHMENT FITTING MEC DET T: 5 YE CPCP AMM 7100001 0.30 ALL420 I: 5 YE MRB S1 0.30DETAILED INSPECTION OF ENGINE AFT ATTACHMENT AND MRB REFERENCE:PYLON LOWER SPAR IN AREA OF AFT ATTACH FITTING544200-C603-2PREP.: ENGINE TO BE REMOVEDSTRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 21APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)544200-0603-4 410 PYLON - ENGINE FWD ATTACHMENT FITTING MEC DET I: 5 YE CPCP AMM SSI 5440031 0.50 B4-200420 OR MRB S AMM SSI 5440041 0.50 C4DETAILED INSPECTION OF FWD ATTACHMENT FITTING 6600 FC AMM 710000F4INCLUDING BOLT AND SPIGOT HOLESPREP.: ENGINE TO BE REMOVED546001-0606-1 415 PYLON FITTING NDT SDI T: 25000 FC ALI NTM 5440011 0.50 B2416 OR FAA AD PART 41 0.50 PRE 02434425 SPECIAL DETAILED INSPECTION OF PYLON ENGINE 28500 FH EASA AD1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4300 FC 2006-00711 0.50 TO 48000 FC451 PANEL. OR FAA AD1 0.50452 4900 FH 2007-04-111 0.504611 0.50462 ALI REFERENCE: 1 0.50546001-01-1ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-2 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 5440011 0.50 B2416 OR FAA AD PART 41 0.50 POST 02434425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 35300 FH EASA AD1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 6200 FC 2006-00711 0.50 TO 48000 FC451 PANEL. OR FAA AD1 0.50452 7000 FH 2007-04-111 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0607-4. ALI REFERENCE: 1 0.50546001-01-3ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-3 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 5440011 0.50 B4-100416 OR FAA AD PART 41 0.50 PRE 02434425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 33300 FH EASA AD1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4600 FC 2006-00711 0.50 TO 40000 FC451 PANEL. OR FAA AD1 0.50452 6400 FH 2007-04-111 0.50* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 22APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546001-0606-3 * * * * * C O N T I N U E * * * * *461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE: 1 0.50462 TASK 546001-0607-6. 546001-01-51 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-4 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 5440011 0.50 B4-100416 OR FAA AD PART 41 0.50 POST 02434425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 43100 FH EASA AD1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC 2006-00711 0.50 TO LOV451 PANEL. OR FAA AD1 0.50452 5800 FH 2007-04-111 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0607-8. ALI REFERENCE: 1 0.50546001-01-7ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-5 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 5440011 0.50 B4-200416 OR FAA AD PART 41 0.50 C4425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 55700 FH EASA AD1 0.50 F4426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 5200 FC 2006-00711 0.50 PRE 02434451 PANEL. OR FAA AD1 0.50 FROM 0 FC/FH452 12000 FH 2007-04-111 0.50 TO 34000 FC461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0607-9. ALI REFERENCE: 1 0.50546001-01-8ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-6 415 PYLON FITTING NDT SDI T: 30000 FC ALI NTM 5440011 0.50 B4-200416 OR FAA AD PART 41 0.50 C4425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 69600 FH EASA AD1 0.50 F4426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC 2006-00711 0.50 POST 02434* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 23APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546001-0606-6 * * * * * C O N T I N U E * * * * *451 PANEL. OR FAA AD1 0.50 FROM 0 FC/FH452 9700 FH 2007-04-111 0.50 TO LOV461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0608-2. ALI REFERENCE: 1 0.50546001-01-10ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-7 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B2416 OR FAA AD PART 41 0.50 PRE 02434425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 4800 FH EASA AD1 0.50 FROM 48000 FC426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-00711 0.50 TO LOV451 PANEL. FAA AD1 0.50452 2007-04-111 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0607-3. ALI REFERENCE: 1 0.50546001-01-2ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-8 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B2416 OR FAA AD PART 41 0.50 POST 02434425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 4800 FH EASA AD1 0.50 FROM 48000 FC426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-00711 0.50 TO LOV451 PANEL. FAA AD1 0.50452 2007-04-111 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0607-5. ALI REFERENCE: 1 0.50546001-01-4ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0606-9 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B4-100416 OR FAA AD PART 41 0.50 PRE 02434* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 24APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546001-0606-9 * * * * * C O N T I N U E * * * * *425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 5800 FH EASA AD1 0.50 FROM 40000 FC426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-00711 0.50 TO LOV451 PANEL. FAA AD1 0.50452 2007-04-111 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0607-7. ALI REFERENCE: 1 0.50546001-01-6ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0607-1 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B4-200416 OR FAA AD PART 41 0.50 C4425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 9700 FH EASA AD1 0.50 F4426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-00711 0.50 PRE 02434451 PANEL. FAA AD1 0.50 FROM 34000 FC452 2007-04-111 0.50 TO LOV461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS1 0.50462 TASK 546001-0608-1. ALI REFERENCE: 1 0.50546001-01-9ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0607-2 415 PYLON FITTING NDT SDI T: 25000 FC ALI NTM 5440011 0.50 B2416 OR CN PART 61 0.50 PRE 02434425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 28500 FH FAA AD CN 2006-0071(B) 1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4300 FC FAA AD 96-13-11 1 0.50 TO 48000 FC451 PANEL. OR1 0.50452 4900 FH ALI REFERENCE: 1 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-11 0.50462 TASK 546001-0606-1.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 25APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546001-0607-3 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B2416 OR CN PART 61 0.50 PRE 02434425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 4800 FH FAA AD CN 2006-0071(B) 1 0.50 FROM 48000 FC426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13-11 1 0.50 TO LOV451 PANEL.1 0.50452 ALI REFERENCE: 1 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-21 0.50462 TASK 546001-0606-7.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0607-4 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 5440011 0.50 B2416 OR CN PART 61 0.50 POST 02434425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 35300 FH FAA AD CN 2006-0071(B) 1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 6200 FC FAA AD 96-13-11 1 0.50 TO 48000 FC451 PANEL. OR1 0.50452 7000 FH ALI REFERENCE: 1 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-31 0.50462 TASK 546001-0606-2.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0607-5 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B2416 OR CN PART 61 0.50 POST 02434425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 4800 FH FAA AD CN 2006-0071(B) 1 0.50 FROM 48000 FC426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13-11 1 0.50 TO LOV451 PANEL.1 0.50452 ALI REFERENCE: 1 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-41 0.50462 TASK 546001-0606-8.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 26APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546001-0607-6 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 5440011 0.50 B4-100416 OR CN PART 61 0.50 PRE 02434425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 33300 FH FAA AD CN 2006-0071(B) 1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4600 FC FAA AD 96-13-11 1 0.50 TO 40000 FC451 PANEL. OR1 0.50452 6400 FH ALI REFERENCE: 1 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-51 0.50462 TASK 546001-0606-3.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0607-7 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B4-100416 OR CN PART 61 0.50 PRE 02434425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 5800 FH FAA AD CN 2006-0071(B) 1 0.50 FROM 40000 FC426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13-11 1 0.50 TO LOV451 PANEL.1 0.50452 ALI REFERENCE: 1 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-61 0.50462 TASK 546001-0606-9.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0607-8 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 5440011 0.50 B4-100416 OR CN PART 61 0.50 POST 02434425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 43100 FH FAA AD CN 2006-0071(B) 1 0.50 FROM 0 FC/FH426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC FAA AD 96-13-11 1 0.50 TO LOV451 PANEL. OR1 0.50452 5800 FH ALI REFERENCE: 1 0.50461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-71 0.50462 TASK 546001-0606-4.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 27APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546001-0607-9 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 5440011 0.50 B4-200416 OR CN PART 61 0.50 C4425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 55700 FH FAA AD CN 2006-0071(B) 1 0.50 F4426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 5200 FC FAA AD 96-13-11 1 0.50 PRE 02434451 PANEL. OR1 0.50 FROM 0 FC/FH452 12000 FH ALI REFERENCE: 1 0.50 TO 34000 FC461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-81 0.50462 TASK 546001-0606-5.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0608-1 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 5440011 0.50 B4-200416 OR CN PART 61 0.50 C4425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 9700 FH FAA AD CN 2006-0071(B) 1 0.50 F4426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13-11 1 0.50 PRE 02434451 PANEL.1 0.50 FROM 34000 FC452 ALI REFERENCE: 1 0.50 TO LOV461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-91 0.50462 TASK 546001-0607-1.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01546001-0608-2 415 PYLON FITTING NDT SDI T: 30000 FC ALI NTM 5440011 0.50 B4-200416 OR CN PART 61 0.50 C4425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 69600 FH FAA AD CN 2006-0071(B) 1 0.50 F4426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC FAA AD 96-13-11 1 0.50 POST 02434451 PANEL. OR1 0.50 FROM 0 FC/FH452 9700 FH ALI REFERENCE: 1 0.50 TO LOV461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-101 0.50462 TASK 546001-0606-6.1 0.50ACCESS: 451AL* 0.01452AR* 0.01461AL* 0.01462AR* 0.01STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 28APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)R 546014-0606-1 471 PYLON ATTACH FITTING MEC DET T: 29000 FC ALI EASA AD1 0.25 B2472 OR FAA AD 2006-00711 0.25 FROM 0 FC/FH481 DETAILED INSPECTION OF PYLON TO WING ATTACH 33000 FH FAA AD1 0.25 TO 48000 FC482 FITTING LUGS AND LINKS AT PYLON RIB 12. I: 2900 FC 2007-04-111 0.25ORNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 3300 FH ALI REFERENCE:546014-0607-1 AND 546014-0608-1 546014-01-1ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35R 546014-0606-2 471 PYLON ATTACH FITTING MEC DET I: 1800 FC ALI EASA AD1 0.25 B2472 OR FAA AD 2006-00711 0.25 FROM 48000 FC481 DETAILED INSPECTION OF PYLON TO WING ATTACH 2000 FH FAA AD1 0.25 TO LOV482 FITTING LUGS AND LINKS AT PYLON RIB 12. 2007-04-111 0.25NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK ALI REFERENCE:546014-0607-2 AND 546014-0608-2 546014-01-2ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35R 546014-0606-3 471 PYLON ATTACH FITTING MEC DET T: 29000 FC ALI EASA AD1 0.25 B4-100472 OR FAA AD 2006-00711 0.25 FROM 0 FC/FH481 DETAILED INSPECTION OF PYLON TO WING ATTACH 40300 FH FAA AD1 0.25 TO 40000 FC482 FITTING LUGS AND LINKS AT PYLON RIB 12. I: 4300 FC 2007-04-111 0.25ORNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 6000 FH ALI REFERENCE:546014-0607-3 AND 546014-0608-3 546014-01-3ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35R 546014-0606-4 471 PYLON ATTACH FITTING MEC DET I: 1800 FC ALI EASA AD1 0.25 B4-100472 OR FAA AD 2006-00711 0.25 FROM 40000 FC481 DETAILED INSPECTION OF PYLON TO WING ATTACH 2500 FH1 0.25 TO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 29APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546014-0606-4 * * * * * C O N T I N U E * * * * *482 FITTING LUGS AND LINKS AT PYLON RIB 12. FAA AD1 0.252007-04-11NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK546014-0607-4 AND 546014-0608-4 ALI REFERENCE:546014-01-4ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35R 546014-0606-5 471 PYLON ATTACH FITTING MEC DET T: 29000 FC ALI EASA AD1 0.25 B4-200472 OR FAA AD 2006-00711 0.25 C4481 DETAILED INSPECTION OF PYLON TO WING ATTACH 67300 FH FAA AD1 0.25 F4482 FITTING LUGS AND LINKS AT PYLON RIB 12. I: 1800 FC 2007-04-111 0.25 FROM 0 FC/FHORTO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 4200 FH ALI REFERENCE:546014-0607-5 AND 546014-0608-5 546014-01-5ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35R 546014-0607-1 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 5440021 0.25 B2472 OR FAA AD PART 41 0.25 FROM 0 FC/FH481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 33000 FH EASA AD1 0.25 TO 48000 FC482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 7000 FC 2006-00711 0.25OR FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 8000 FH 2007-04-11546014-0606-1 AND 546014-0608-1ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-1ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0607-2 471 PYLON ATTACH FITTING NDT SDI I: 5900 FC ALI NTM 5440001 0.25 B2472 OR FAA AD PART 41 0.25 FROM 48000 FC* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 30APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546014-0607-2 * * * * * C O N T I N U E * * * * *481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 6700 FH EASA AD1 0.25 TO LOV482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-00711 0.25FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11546014-0606-2 AND 546014-0608-2.ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-2ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0607-3 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 5440001 0.25 B4-100472 OR FAA AD PART 41 0.25 FROM 0 FC/FH481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 40300 FH EASA AD1 0.25 TO 40000 FC482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 7700 FC 2006-00711 0.25OR FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 10700 FH 2007-04-11546014-0606-3 AND 546014-0608-3.ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-3ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0607-4 471 PYLON ATTACH FITTING NDT SDI I: 5900 FC ALI NTM 5440001 0.25 B4-100472 OR FAA AD PART 41 0.25 FROM 40000 FC481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 8200 FH EASA AD1 0.25 TO LOV482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-00711 0.25FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11546014-0606-4 AND 546014-0608-4.ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-4ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 31APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546014-0607-4 * * * * * C O N T I N U E * * * * *482AR* 0.35546014-0607-5 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 5440001 0.25 B4-200472 OR FAA AD PART 41 0.25 C4481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 67300 FH EASA AD1 0.25 F4482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 5900 FC 2006-00711 0.25 FROM 0 FC/FHOR FAA ADTO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 13700 FH 2007-04-11546014-0606-5 AND 546014-0608-5.ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-5ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0608-1 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 5440021 0.25 B2472 OR FAA AD PART 61 0.25 FROM 0 FC/FH481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 33000 FH EASA AD1 0.25 TO 48000 FC482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 10800 FC 2006-00711 0.25OR FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 12300 FH 2007-04-11546014-0606-1 AND 546014-0607-1.ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-03-1ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0608-2 471 PYLON ATTACH FITTING NDT SDI I: 8800 FC ALI NTM 5440021 0.25 B2472 OR CN PART 61 0.25 FROM 48000 FC481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 10000 FH FAA AD EASA AD1 0.25 TO LOV482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-00711 0.25FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11546014-0606-2 AND 546014-0607-2.ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 32APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546014-0608-2 * * * * * C O N T I N U E * * * * *PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-03-2ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0608-3 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 5440021 0.25 B4-100472 OR CN PART 61 0.25 FROM 0 FC/FH481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 40300 FH FAA AD EASA AD1 0.25 TO 40000 FC482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 8900 FC 2006-00711 0.25OR FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 12300 FH 2007-04-11546014-0606-3 AND 546014-0607-3.ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-03-3ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0608-4 471 PYLON ATTACH FITTING NDT SDI I: 8800 FC ALI NTM 5440021 0.25 B4-100472 OR CN PART 61 0.25 FROM 40000 FC481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 12200 FH FAA AD EASA AD1 0.25 TO LOV482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-00711 0.25FAA ADNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11546014-0606-4 AND 546014-0607-4.ALI REFERENCE:PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-03-4ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35546014-0608-5 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 5440021 0.25 B4-200472 OR CN PART 61 0.25 C4481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 67300 FH FAA AD1 0.25 F4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 33APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)546014-0608-5 * * * * * C O N T I N U E * * * * *482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 8800 FC EASA AD1 0.25 FROM 0 FC/FHOR 2006-0071TO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 20400 FH FAA AD546014-0606-5 AND 546014-0607-5. 2007-04-11PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION ALI REFERENCE:546014-03-5ACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35548021-0603-1 410 PYLON INTERNAL SURFACE MEC DET T: 9 YE CPCP MRB REFERENCE: 2 5.00 ALL420 I: 5 YE 548021-C603-12 5.00470 DETAILED INSPECTION OF PYLON INTERNAL2 5.00480 STRUCTURE FROM RIB 1 TO RIB 18 AND FROM LOWER SPAR TO2 5.00UPPER SPAR.NOTE: THIS TASK CAN BE PERFORMED AT OPPORTUNITYOF ENGINE REMOVAL.PREP.: PRECOOLER TO BE REMOVED.ACCESS: 473AL 474AR* 0.02483AL 484AR* 0.02548023-0603-1 410 PYLON LOWER SPAR MEC DET T: 9 YE CPCP MRB REFERENCE: 2 TBD ALL420 I: 2,5 YE 548023-C603-12 TBD470 DETAILED INSPECTION OF PYLON LOWER SPAR UPPER2 TBD480 SURFACE FROM RIB 8 TO 18, INCLUDING JUNCTION WITH2 TBDRIBS AND LATERAL PANELSACCESS: 473AL 474AR* 0.02483AL 484AR* 0.02548031-0603-1 415 PYLON EXTERNAL SURFACE MEC DET T: 10 YE CPCP MRB REFERENCE: 1 0.50 ALL416 I: 5 YE 543101-C602-11 0.50425 DETAILED INSPECTION OF PYLON BOX EXTERNAL SURFACE 548031-C603-11 0.50426 FROM RIB 1 TO RIB 18 AND FROM LOWER SPAR TO UPPER1 0.50473 SPAR.1 0.50* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 34APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)548031-0603-1 * * * * * C O N T I N U E * * * * *4741 0.50483 PREP.:COWLS OPENED, THERMAL INSULATION1 0.50484 TO BE REMOVED1 0.50ACCESS: 451AL 452AR 473AL* 0.04461AL 462AR 484AR* 0.04548041-0603-1 473 PYLON TO WING FWD ATTACHMENT MEC DET T: 9 YE CPCP AMM SSI 5410031 1.00 PRE 03521474 I: 5 YE MRB S1 1.00 (54-0059)483 DETAILED INSPECTION OF PYLON TO WING FORWARD MRB REFERENCE: 1 1.00 PRE 04530484 ATTACHMENT.1 1.00 (54-0058)548041-C603-1PREP.:ENGINE REMOVED LINKS AND BOLTS REMOVAL(AT RIB 12)ACCESS: 473BL* 0.54474BR* 0.49483BL* 0.54484BR* 0.49548041-0603-2 473 PYLON TO WING FWD ATTACHMENT MEC DET T: 9 YE CPCP MRB REFERENCE: 1 1.00 POST 03521474 I: 9 YE 548041-C603-21 1.00 (54-0059)483 DETAILED INSPECTION OF PYLON TO WING FORWARD1 1.00 OR484 ATTACHMENT.1 1.00 POST 04530(54-0058)PREP.:ENGINE REMOVED LINKS AND BOLTS REMOVAL(AT RIB 12)ACCESS: 473BL* 0.54474BR* 0.49483BL* 0.54484BR* 0.49548051-0603-1 473 PYLON TO WING AFT ATTACHMENT MEC DET T: 7.5 YE CPCP MRB REFERENCE: 1 10.00 POST 02434474 I: 5 YE 548051-C603-11 10.00 PRE 10262483 DETAILED INSPECTION OF PYLON TO WING REAR1 10.00 PRE 10263484 ATTACHMENT.1 10.00 (54-0078)PREP.1:ENGINE TO BE REMOVED* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 35APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)548051-0603-1 * * * * * C O N T I N U E * * * * *PREP.2:LINKS, BOLTS AND BEARING TO BE REMOVED ATRIB 18.NOTE 1: APPLICATION OF SB 54-0059 IS RECOMMENDED(REPLACEMENT OF ORIGINAL BOLTS BYINCONEL 718 BOLTS)ACCESS: 473BL* 0.54474BR* 0.49483BL* 0.54484BR* 0.49548051-0603-2 470 PYLON TO WING AFT ATTACHMENT MEC DET T: 7.5 YE CPCP MRB REFERENCE: 1 10.00 POST 02434480 I: 7.5 YE 548051-C603-21 10.00 PRE 10262DETAILED INSPECTION OF PYLON TO WING REARPOST 10263ATTACHMENT.(54-0078)NOTE 01: LINKS BOLTS AND BEARING TO BE REMOVEDAT RIB 18NOTE 02: ENGINE TO BE REMOVEDNOTE 03: APPLICATION OF SB 54-0059 IS RECOMMENDED(REPLACEMENT OF ORIGINAL BOLTS BYINCONEL 718 BOLTS)ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03548051-0603-3 470 PYLON TO WING AFT ATTACHMT MEC DET T: 10 YE CPCP MRB REFERENCE: 1 10.00 POST 02434473 I: 10 YE 548051-C603-31 10.00 POST 10262474 DETAILED INSPECTION OF PYLON TO WING REAR1 10.00480 ATTACHMENT.1 10.004831 10.00484 NOTE 01: LINKS BOLTS AND BEARING TO BE REMOVED1 10.00AT RIB 18NOTE 02: ENGINE TO BE REMOVEDNOTE 03: APPLICATION OF SB 54-0059 IS RECOMMENDED(REPLACEMENT OF ORIGINAL BOLTS BY* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 36APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)548051-0603-3 * * * * * C O N T I N U E * * * * *INCONEL 718 BOLTS)ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03549001-0603-1 415 PYLON MEC SDI T: 10000 FH ISB ISB 54-00721 0.25 ALL416 I: 5000 FH1 0.25425 SPECIAL DETAILED INSPECTION OF TEMPERATURE SENSORS1 0.25426 FOR POSIBLE CHAFING AGAINST THE PYLON FORWARD1 0.25SHACKLES AND LUGSACCESS: 471AL* 0.35472AR* 0.26481AL* 0.27482AR* 0.35549002-0603-1 415 PYLON NDT SDI T: 15000 FH ISB NTM 5440051 0.50 POST 02434416 I: 15000 FH PART 61 0.50 PRE 11109425 SPECIAL DETAILED AND DETAILED INSPECTION OF THE ISB 54-0961 0.50 (54-0094)426 LOWER SIDE OF RIB 5 IN THE PYLON BOX.1 0.50PREP.: PRECOOLER TO BE REMOVED.ACCESS: 413GL* 0.17423GL* 0.17* * * * * E N D * * * * *STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION:3-54 PAGE 37APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551001-0602-1 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 2700 FC CPCP AMM SSI 5510011 0.50 B2ATTACHMENT MRB SMRB REFERENCE:DETAILED INSPECTION OF HORIZONTAL STABILIZERTRIM ACTUATOR ATTACH ARMS, SUPPORTING STRUCTURE AND 551001-C602-1STABILIZER FRONT SPAR.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACEONLY IN INTERVALS NOT EXCEEDING 9 YEARSACCESS: 312AR* 0.01551001-0602-2 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 2500 FC CPCP AMM SSI 5510011 0.50 B4-100ATTACHMENT MRB SMRB REFERENCE:DETAILED INSPECTION OF HORIZONTAL STABILIZERTRIM ACTUATOR ATTACH ARMS, SUPPORTING STRUCTURE AND 551001-C602-1STABILIZER FRONT SPAR.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACEONLY IN INTERVALS NOT EXCEEDING 9 YEARS.ACCESS: 312AR* 0.01551001-0602-3 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 1900 FC CPCP AMM SSI 5510011 0.50 B4-200ATTACHMENT MRB SC4MRB REFERENCE: F4DETAILED INSPECTION OF HORIZONTAL STABILIZERTRIM ACTUATOR ATTACH ARMS, SUPPORTING STRUCTURE AND 551001-C602-1STABILIZER FRONT SPAR.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACEONLY IN INTERVALS NOT EXCEEDING 9 YEARS.ACCESS: 312AR* 0.01551002-0604-1 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 27300 FC MRB S AMM SSI 5510021 4.00 B2ATTACHMENT NTM 555112PART 4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551002-0604-1 * * * * * C O N T I N U E * * * * *DETAILED OR NDT INSPECTION OF HORIZONTAL STABILIZER NTM 555112TRIM ACTUATOR ATTACH ARM LUGS AND SUPPORT FITTINGS. PART 6PREP.: ATTACH ARMS REMOVED.ACCESS: 312AR* 0.01551002-0604-2 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 22600 FC MRB S AMM SSI 5510021 4.00 B4-100ATTACHMENT NTM 555112PART 4DETAILED OR NDT INSPECTION OF HORIZONTAL STABILIZER NTM 555112TRIM ACTUATOR ATTACH ARM LUGS AND SUPPORT FITTINGS. PART 6PREP.: ATTACH ARMS REMOVED.ACCESS: 312AR* 0.01551002-0604-3 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 19200 FC MRB S AMM SSI 5510021 4.00 B4-200ATTACHMENT NTM 555112C4PART 4F4DETAILED OR NDT INSPECTION OF HORIZONTAL STABILIZER NTM 555112TRIM ACTUATOR ATTACH ARM LUGS AND SUPPORT FITTINGS. PART 6PREP.: ATTACH ARMS REMOVED.ACCESS: 312AR* 0.01551003-0604-1 334 LATERAL HINGE SUPP.FITTING MEC DET I: 27300 FC MRB S AMM SSI 5510031 0.33 B23441 0.33DETAILED INSPECTION OF LATERAL HINGE SUPPORTFITTING AT HORIZONTAL STABILIZER REAR SPAR RIB 4 ANDSUPPORTING STRUCTURE.ACCESS: 334AT* 0.38344AT* 0.38551003-0604-2 334 LATERAL HINGE SUPP.FITTING MEC DET I: 22600 FC MRB S AMM SSI 5510031 0.33 B4-1003441 0.33DETAILED INSPECTION OF LATERAL HINGE SUPPORT* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551003-0604-2 * * * * * C O N T I N U E * * * * *FITTING AT HORIZONTAL STABILIZER REAR SPAR RIB 4 ANDSUPPORTING STRUCTURE.ACCESS: 334AT* 0.38344AT* 0.38551003-0604-3 334 LATERAL HINGE SUPP.FITTING MEC DET I: 19200 FC MRB S AMM SSI 5510031 0.33 B4-2003441 0.33 C4DETAILED INSPECTION OF LATERAL HINGE SUPPORTF4FITTING AT HORIZONTAL STABILIZER REAR SPAR RIB 4 ANDSUPPORTING STRUCTURE.ACCESS: 334AT* 0.38344AT* 0.38551004-0603-1 319 ATTACHMENT LUG AT FR 91 NDT SDI I: 1200 FC ISB NTM 5319481 10.00 PRE 07715PART 6(53-0270)SPECIAL DETAILED INSPECTION OF FRAME 91, UPPER AND CNLOWER FRAME LUGS, LH AND RH. 1990-020-102(B)FAA AD 91-05-12NOTE: THIS TASK IS ONLY APPLICABLE FOR LUGS MADE OF ISB 53-02692014 MATERIALACCESS: 313AL* 0.14551009-0604-1 319 CENTER TORQUE BOX MEC DET I: 27300 FC MRB S AMM SSI 5510091 0.33 B2DETAILED INSPECTION OF STRUCTURE OF HORIZONTALSTABILIZER CENTER TORQUE BOX- THROUGH LIGHTENING HOLES IN SPARS -ACCESS: 312AR 313AL* 0.15551009-0604-2 319 CENTER TORQUE BOX MEC DET I: 22600 FC MRB S AMM SSI 5510091 0.33 B4-100DETAILED INSPECTION OF STRUCTURE OF HORIZONTALSTABILIZER CENTER TORQUE BOX- THROUGH LIGHTENING HOLES IN SPARS -* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551009-0604-2 * * * * * C O N T I N U E * * * * *ACCESS: 312AR 313AL* 0.15551009-0604-3 319 CENTER TORQUE BOX MEC DET I: 19200 FC MRB S AMM SSI 5510091 0.33 B4-200C4DETAILED INSPECTION OF STRUCTURE OF HORIZONTALF4STABILIZER CENTER TORQUE BOX- THROUGH LIGHTENING HOLES IN SPARS -ACCESS: 312AR 313AL* 0.15551015-0602-1 319 SKIN SPLICES HORIZ. STAB. MEC DET I: 10700 FC MRB S AMM SSI 5510151 0.33 B2DETAILED INSPECTION OF SKIN SPLICES ON UPPERHORIZONTAL STABILIZER CENTER TORQUE BOX.ACCESS: 312AR* 0.01551015-0602-2 319 SKIN SPLICES HORIZ. STAB. MEC DET I: 10000 FC MRB S AMM SSI 5510151 0.33 B4-100DETAILED INSPECTION OF SKIN SPLICES ON UPPERHORIZONTAL STABILIZER CENTER TORQUE BOX.ACCESS: 312AR* 0.01551015-0602-3 319 SKIN SPLICES HORIZ. STAB. MEC DET I: 7900 FC MRB S AMM SSI 5510151 0.33 B4-200C4DETAILED INSPECTION OF SKIN SPLICES ON UPPERF4HORIZONTAL STABILIZER CENTER TORQUE BOX.ACCESS: 312AR* 0.01551023-0604-1 333 REAR SPAR WEB HORIZ.STAB. MEC DET I: 27300 FC MRB S AMM SSI 5510231 0.33 B23431 0.33DETAILED INSPECTION REAR SPAR WEB AFT FACE OFHORIZONTAL STABILIZER BETWEEN RIBS 3 AND 6ACCESS: 334AT* 0.38344AT* 0.38STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551023-0604-2 333 REAR SPAR WEB HORIZ.STAB. MEC DET I: 22600 FC MRB S AMM SSI 5510231 0.33 B4-1003431 0.33DETAILED INSPECTION REAR SPAR WEB AFT FACE OFHORIZONTAL STABILIZER BETWEEN RIBS 3 AND 6ACCESS: 334AT* 0.38344AT* 0.38551023-0604-3 333 REAR SPAR WEB HORIZ.STAB. MEC DET I: 19200 FC MRB S AMM SSI 5510231 0.33 B4-2003431 0.33 C4DETAILED INSPECTION REAR SPAR WEB AFT FACE OFF4HORIZONTAL STABILIZER BETWEEN RIBS 3 AND 6ACCESS: 334AT* 0.38344AT* 0.38551025-0604-1 333 HORIZ.STAB.AT RIB 4 MEC DET I: 27300 FC MRB S AMM SSI 5510251 0.33 B23431 0.33DETAILED INSPECTION OF MACHINED FITTING AT AFTEND OF HORIZONTAL STABILIZER RIB 4 ATTACHED TOFORWARD FACE OF REAR SPAR- THROUGH LIGHTENING HOLES IN SPAR -ACCESS: 334AT* 0.38344AT* 0.38551025-0604-2 333 HORIZ.STAB.AT RIB 4 MEC DET I: 22600 FC MRB S AMM SSI 5510251 0.33 B4-1003431 0.33DETAILED INSPECTION OF MACHINED FITTING AT AFTEND OF HORIZONTAL STABILIZER RIB 4 ATTACHED TOFORWARD FACE OF REAR SPAR- THROUGH LIGHTENING HOLES IN SPAR -ACCESS: 334AT* 0.38344AT* 0.38551025-0604-3 333 HORIZ.STAB.AT RIB 4 MEC DET I: 19200 FC MRB S AMM SSI 5510251 0.33 B4-2003431 0.33 C4DETAILED INSPECTION OF MACHINED FITTING AT AFTF4END OF HORIZONTAL STABILIZER RIB 4 ATTACHED TOFORWARD FACE OF REAR SPAR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551025-0604-3 * * * * * C O N T I N U E * * * * *- THROUGH LIGHTENING HOLES IN SPAR -ACCESS: 334AT* 0.38344AT* 0.38551028-0604-1 333 HORIZ.STAB.SPLICE RIB 3 & 4 NDT SDI I: 17700 FC MRB S AMM SSI 5510281 0.33 B2343 NTM 5511121 0.33DETAILED AND SPECIAL DETAILED INSPECTION INTERNAL PART 4HORIZONTAL STABILIZER OUTER PANEL SPLICES TO CENTERTORQUE BOX AT UPPER SKIN BETWEEN RIBS 3 AND 4 ANDBETWEEN STRINGER 10 AND FRONT SPARACCESS: 333CT* 0.35343CT* 0.35551028-0604-2 333 HORIZ.STAB.SPLICE RIB 3 & 4 NDT SDI I: 17700 FC MRB S AMM SSI 5510281 0.33 B4-100343 NTM 5511121 0.33DETAILED AND SPECIAL DETAILED INSPECTION INTERNAL PART 4HORIZONTAL STABILIZER OUTER PANEL SPLICES TO CENTERTORQUE BOX AT UPPER SKIN BETWEEN RIBS 3 AND 4 ANDBETWEEN STRINGER 10 AND FRONT SPARACCESS: 333CT* 0.35343CT* 0.35551028-0604-3 333 HORIZ.STAB.SPLICE RIB 3 & 4 NDT SDI I: 15100 FC MRB S AMM SSI 5510281 0.33 B4-200343 NTM 5511121 0.33 C4DETAILED AND SPECIAL DETAILED INSPECTION INTERNAL PART 4F4HORIZONTAL STABILIZER OUTER PANEL SPLICES TO CENTERTORQUE BOX AT UPPER SKIN BETWEEN RIBS 3 AND 4 ANDBETWEEN STRINGER 10 AND FRONT SPAR551029-0603-1 319 HORIZONTAL STABILIZER REAR SPAR MEC DET I: 6800 FC CPCP AMM SSI 5510291 0.33 B2MRB SDETAILED INSPECTION OF HORIZONTAL STABILIZER MRB REFERENCE:HINGE BEARING SUPPORT FITTINGS AND UPPER AND LOWERATTACH FITTINGS AND STABILIZER REAR SPAR, AFT FACE 551029-C603-1AT RIB 3.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551029-0603-1 * * * * * C O N T I N U E * * * * *NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACE.ACCESS: 313AL* 0.14551029-0603-2 319 HORIZONTAL STABILIZER REAR SPAR MEC DET I: 6200 FC CPCP AMM SSI 5510291 0.33 B4-100MRB SDETAILED INSPECTION OF HORIZONTAL STABILIZER MRB REFERENCE:HINGE BEARING SUPPORT FITTINGS AND UPPER AND LOWERATTACH FITTINGS AND STABILIZER REAR SPAR, AFT FACE 551029-C603-1FROM RIBS 3LH TO 3RHNOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACHEONLY IN INTERVALS NOT EXCEEDING 9 YEARS.551029-0603-3 319 HORIZONTAL STABILIZER REAR SPAR MEC DET I: 4900 FC CPCP AMM SSI 5510291 0.33 B4-200MRB SC4DETAILED INSPECTION OF HORIZONTAL STABILIZER MRB REFERENCE: F4HINGE BEARING SUPPORT FITTINGS AND UPPER AND LOWERATTACH FITTINGS AND STABILIZER REAR SPAR, AFT FACE 551029-C603-1FROM RIBS 3LH TO 3RHNOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2OR G3 AFTER INSPECTION TO EXTERNAL SURFACE.551030-0604-1 319 HORIZ.STAB. STRUCTURE MEC DET I: 27300 FC MRB S AMM SSI 5510301 0.33 B2DETAILED INSPECTION OF HORIZONTAL STABILIZERSTRUCTURE AROUND HINGE BEARING SUPPORT FITTINGSACCESS: 313AL 334AT 344AT* 0.89551030-0604-2 319 HORIZ.STAB. STRUCTURE MEC DET I: 22600 FC MRB S AMM SSI 5510301 0.33 B4-100DETAILED INSPECTION OF HORIZONTAL STABILIZERSTRUCTURE AROUND HINGE BEARING SUPPORT FITTINGSACCESS: 313AL 334AT 344AT* 0.89STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)551030-0604-3 319 HORIZ.STAB. STRUCTURE MEC DET I: 19200 FC MRB S AMM SSI 5510301 0.33 B4-200C4DETAILED INSPECTION OF HORIZONTAL STABILIZERF4STRUCTURE AROUND HINGE BEARING SUPPORT FITTINGSACCESS: 313AL 334AT 344AT* 0.89551033-0603-1 319 STABILIZERS-THS CENTER BOX NDT SDI T: 11400 FC ISB AMM SSI 5510311 14.00 PRE 01692I: 6000 FC MRB S NTM 513000SPECIAL DETAILED INSPECTION OF INTEGRAL TOP SKIN OF NTM 513010THE THS LEVEL. NTM 516000NTM 551112NOTE: 01. THS SUPPORT FITTING TO BE REMOVED CN02. ALTERNATIVE METHOD COULD BE USED WITHOUT 1989-157-099(B)THS SUPPORT FITTING REMOVED. FAA AD 90-22-06ISB 55-0035552004-0603-1 335 ELEVATOR MEC DET I: 9 YE CPCP AMM SSI 5520031 1.00 ALL345 MRB S AMM SSI 5520041 1.00DETAILED INSPECTION OF HORIZONTAL STABILIZER AMM SSI 552005ELEVATOR FRONT SPAR FORWARD FACE INCLUDING HINGEFITTINGS. MRB REFERENCE:ACCESS: 334AT 334BT 334CT 334DT 334ET 334FT 552004-C603-1* 6.10334GT 334HT 334JT 334KT 334LT 335AB335AT 335BB 335BT 335CB 335CT 335DB335DT 335EB 335ET344AT 344BT 344CT 344DT 344ET 344FT* 6.12344GT 344HT 344JT 344KT 344LT 345AB345AT 345BB 345BT 345CB 345CT 345DB345DT 345EB 345ET552007-0602-1 335 ELEVATOR TRAILING EDGE MEC DET I: 30 MO MRB S1 0.20 PRE 055693451 0.20DETAILED INSPECTION OF ELEVATOR TRAILING EDGEFOR CORROSION.STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)553005-0602-1 323 SKIN SPLICE-VERTICAL STAB. MEC DET I: 11100 FC MRB S AMM SSI 5530051 0.20 B2DETAILED INSPECTION OF EXTERNAL SKIN SPLICEAT VERTICAL STABILIZER RIB 16.553005-0602-2 323 SKIN SPLICE-VERTICAL STAB. MEC DET I: 10300 FC MRB S AMM SSI 5530051 0.20 B4-100DETAILED INSPECTION OF EXTERNAL SKIN SPLICEAT VERTICAL STABILIZER RIB 16.553005-0602-3 323 SKIN SPLICE-VERTICAL STAB. MEC DET I: 8900 FC MRB S AMM SSI 5530051 0.20 B4-200C4DETAILED INSPECTION OF EXTERNAL SKIN SPLICEF4AT VERTICAL STABILIZER RIB 16.553017-0603-1 323 VERTICAL STABILIZER SKIN MEC DET T: 20000 FC ISB CN 83-102-53(B) 1 1.00 PRE 03172I: 1500 FC FAA AD 86-19-02 (55-0024)DETAILED INSPECTION OF VERTICAL STABILIZER ISB 55-026ATTACH FITTINGS LH AND RH FOR CRACKS.ACCESS: 311AZ 311BZ 312AR* 0.51555021-0603-1 330 ELEVATOR HINGE ARM NO.1 & 7 MEC DET I: 5 YE MRB S1 0.20 PRE 032263401 0.20 (D2396)DETAILED INSPECTION OF ELEVATOR HINGE ARMSNO.1 AND 7.ACCESS: 334AB 334BT 334EB 335AB 335AT 335ET* 0.76344AB 344BT 344EB 345AB 345AT 345ET* 0.75556001-0606-1 333 HORIZONTAL STABILIZER TOP SKIN NDT SDI T: SEE SB ALI NTM 5511121 7.50 ALL343 I: SEE SB CN PART 61 7.50 SB 55-0036SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER FAA AD CN 2006-0071(B) FROM 0 FC/FHCENTER BOX INTEGRAL SKIN JUST OUTBOARD OF RIB 3, FROM ISB FAA AD 96-13-11 TO LOVTHE REAR SPAR TO STRINGER 10 LH/RH. ISB 55-0036ACCESS: 333CT 333DT ALI REFERENCE: * 0.65343CT 343DT 556001-01-1* 0.65STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)556002-0602-1 323 VERTICAL STABILIZER SKIN MEC DET T: 37000 FC ALI EASA AD1 TBD B2OR 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF VERTICAL STABILIZER SKIN 41800 FH FAA ADTO LOVPANELS LH/RH FROM FRONT TO REAR SPAR AND FROM I: 6000 FC 2007-04-11FIN/FUSELAGE FAIRING TO TIP RIB 12, EXTERNAL SURFACE. OR6700 FH ALI REFERENCE:556002-01-1556002-0602-2 323 VERTICAL STABILIZER SKIN MEC DET T: 34000 FC ALI EASA AD1 TBD B4-100OR 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF VERTICAL STABILIZER SKIN 46200 FH FAA ADTO LOVPANELS LH/RH FROM FRONT TO REAR SPAR AND FROM I: 6000 FC 2007-04-11FIN/FUSELAGE FAIRING TO TIP RIB 12, EXTERNAL SURFACE. OR8100 FH ALI REFERENCE:556002-01-2556002-0602-3 323 VERTICAL STABILIZER SKIN MEC DET T: 28000 FC ALI EASA AD1 TBD B4-200OR 2006-0071C4DETAILED INSPECTION OF VERTICAL STABILIZER SKIN 61800 FH FAA ADF4PANELS LH/RH FROM FRONT TO REAR SPAR AND FROM I: 6000 FC 2007-04-11FROM 0 FC/FHFIN/FUSELAGE FAIRING TO TIP RIB 12, EXTERNAL SURFACE. ORTO LOV13200 FH ALI REFERENCE:556002-01-3556003-0606-1 323 VERTICAL STABILIZER ATTACHMENT MEC DET ST: 34000 FC ALI CN 2006-0071(B) 1 0.50 B2OR FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 38400 FHTO 48000 FCCENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH SI: 4400 FC ALI REFERENCE:INCLUSIVE RIVETING TO SKIN. OR 556003-01-15000 FHACCESS: 323AL 323AR 323BL 323BR* 1.62556003-0606-2 323 VERTICAL STABILIZER ATTACHMENT MEC DET I: 3300 FC ALI CN 2006-0071(B) 1 0.50 B2OR FAA AD 96-13-11 FROM 48000 FCDETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 3700 FHTO LOVCENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH ALI REFERENCE:INCLUSIVE RIVETING TO SKIN. 556003-01-2ACCESS: 323AL 323AR 323BL 323BR* 1.62STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)556003-0606-3 323 VERTICAL STABILIZER ATTACHMENT MEC DET ST: 31000 FC ALI CN 2006-0071(B) 1 0.50 B4-100OR FAA AD 96-13-11 FROM 0 FC/FHDETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 42200 FHTO 40000 FCCENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH SI: 4900 FC ALI REFERENCE:INCLUSIVE RIVETING TO SKIN. OR 556003-01-36700 FHACCESS: 323AL 323AR 323BL 323BR* 1.62556003-0606-4 323 VERTICAL STABILIZER ATTACHMENT MEC DET I: 3100 FC ALI CN 2006-0071(B) 1 0.50 B4-100OR FAA AD 96-13-11 FROM 40000 FCDETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 4200 FHTO LOVCENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH ALI REFERENCE:INCLUSIVE RIVETING TO SKIN. 556003-01-4ACCESS: 323AL 323AR 323BL 323BR* 1.62556003-0606-5 323 VERTICAL STABILIZER ATTACHMENT MEC DET ST: 26000 FC ALI CN 2006-0071(B) 1 0.50 B4-200OR FAA AD 96-13-11 C4DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 57500 FHF4CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH SI: 3900 FC ALI REFERENCE: FROM 0 FC/FHINCLUSIVE RIVETING TO SKIN. OR 556003-01-5TO 34000 FC8600 FHACCESS: 323AL 323AR 323BL 323BR* 1.62556003-0606-6 323 VERTICAL STABILIZER ATTACHMENT MEC DET I: 2600 FC ALI CN 2006-0071(B) 1 0.50 B4-200OR FAA AD 96-13-11 C4DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 5700 FHF4CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH ALI REFERENCE: FROM 34000 FCINCLUSIVE RIVETING TO SKIN. 556003-01-6TO LOVACCESS: 323AL 323AR 323BL 323BR* 1.62556004-0606-1 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 27000 FC ALI EASA AD1 1.00 B2OR FAA AD 2006-0071PRE 01236DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 30500 FH FAA ADFROM 0 FC/FHSTRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 6000 FC 2007-04-11TO LOVANGLES, FROM RIB 1 TO RIB 12. OR6700 FH ALI REFERENCE:ACCESS: 311AZ 311BZ 312AR 556004-01-1* 0.51STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)556004-0606-2 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 27000 FC ALI EASA AD1 1.00 B2OR FAA AD 2006-0071POST 01236DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 30500 FH FAA ADFROM 0 FC/FHSTRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 12700 FC 2007-04-11TO LOVANGLES, FROM RIB 1 TO RIB 12. OR14300 FH ALI REFERENCE:ACCESS: 311AZ 311BZ 312AR 556004-01-4* 0.51556004-0606-3 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 24500 FC ALI EASA AD1 1.00 B4-100OR FAA AD 2006-0071PRE 01236DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 33300 FH FAA ADFROM 0 FC/FHSTRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 5500 FC 2007-04-11TO LOVANGLES, FROM RIB 1 TO RIB 12. OR7400 FH ALI REFERENCE:ACCESS: 311AZ 311BZ 312AR 556004-01-2* 0.51556004-0606-4 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 24500 FC ALI EASA AD1 1.00 B4-100OR FAA AD 2006-0071POST 01236DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 33300 FH FAA ADFROM 0 FC/FHSTRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 11800 FC 2007-04-11TO LOVANGLES, FROM RIB 1 TO RIB 12. OR16000 FH ALI REFERENCE:ACCESS: 311AZ 311BZ 312AR 556004-01-5* 0.51556004-0606-5 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 19500 FC ALI EASA AD1 1.00 B4-200OR FAA AD 2006-0071C4DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 43000 FH FAA ADF4STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 4600 FC 2007-04-11PRE 01236ANGLES, FROM RIB 1 TO RIB 12. ORFROM 0 FC/FH10100 FH ALI REFERENCE: TO LOVACCESS: 311AZ 311BZ 312AR 556004-01-3* 0.51556004-0606-6 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 19500 FC ALI EASA AD1 1.00 B4-200OR FAA AD 2006-0071C4DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 43000 FH FAA ADF4STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 9900 FC 2007-04-11POST 01236ANGLES, FROM RIB 1 TO RIB 12. ORFROM 0 FC/FH21800 FH ALI REFERENCE: TO LOVACCESS: 311AZ 311BZ 312AR 556004-01-6* 0.51STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)556005-0604-1 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 58200 FC ALI NTM 5551151 TBD B2343 OR PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER 65700 FH EASA ADTO LOVREAR SPAR WEB JOINING PART AT RIB 3, RIVETING UPPER I: 7600 FC 2006-0071AREA BETWEEN RIB 3 AND RIB 4 LH/RH. OR FAA AD8600 FH 2007-04-11NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEENRIB 4 AND RIB 5. ALI REFERENCE:556005-01-1ACCESS: 333CT 333DT 334AT* 1.03343CT 343DT 344AT* 1.03556005-0604-2 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 50300 FC ALI NTM 5551151 TBD B4-100343 OR PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER 68400 FH EASA ADTO LOVREAR SPAR WEB JOINING PART AT RIB 3, RIVETING UPPER I: 6800 FC 2006-0071AREA BETWEEN RIB 3 AND RIB 4 LH/RH. OR FAA AD9200 FH 2007-04-11NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEENRIB 4 AND RIB 5. ALI REFERENCE:556005-01-2ACCESS: 333CT 333DT 334AT* 1.03343CT 343DT 344AT* 1.03556005-0604-3 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 40200 FC ALI NTM 5551151 TBD B4-200343 OR PART 61 TBD C4SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER 88800 FH EASA ADF4REAR SPAR WEB JOINING PART AT RIB 3, RIVETING UPPER I: 5500 FC 2006-0071FROM 0 FC/FHAREA BETWEEN RIB 3 AND RIB 4 LH/RH. OR FAA ADTO LOV12200 FH 2007-04-11NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEENRIB 4 AND RIB 5. ALI REFERENCE:556005-01-3ACCESS: 333CT 333DT 334AT* 1.03343CT 343DT 344AT* 1.03556006-0604-1 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 48000 FC ALI NTM 5551161 TBD B2343 OR PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54200 FH EASA ADTO LOVHORIZONTAL STABILIZER REAR SPAR WEB RIVETING UPPER I: 7200 FC 2006-0071AREA BETWEEN RIB 3 AND RIB 4 LH/RH OR FAA AD8100 FH 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)556006-0604-1 * * * * * C O N T I N U E * * * * *NOTE: GRACE PERIOD = 1000 FC ALI REFERENCE:556006-01-1ACCESS: 333CT 333DT 334AT* 1.03343CT 343DT 344AT* 1.03556006-0604-2 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 40000 FC ALI NTM 5551161 TBD B4-100343 OR PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54400 FH EASA ADTO LOVHORIZONTAL STABILIZER REAR SPAR WEB RIVETING UPPER I: 6400 FC 2006-0071AREA BETWEEN RIB 3 AND RIB 4 LH/RH OR FAA AD8700 FH 2007-04-11NOTE: GRACE PERIOD = 1000 FCALI REFERENCE:ACCESS: 333CT 333DT 334AT 556006-01-2* 1.03343CT 343DT 344AT* 1.03556006-0604-3 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 34000 FC ALI NTM 5551161 TBD B4-200343 OR PART 61 TBD C4SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 75100 FH EASA ADF4HORIZONTAL STABILIZER REAR SPAR WEB RIVETING UPPER I: 5200 FC 2006-0071FROM 0 FC/FHAREA BETWEEN RIB 3 AND RIB 4 LH/RH OR FAA ADTO LOV11400 FH 2007-04-11NOTE: GRACE PERIOD = 1000 FCALI REFERENCE:ACCESS: 333CT 333DT 334AT 556006-01-3* 1.03343CT 343DT 344AT* 1.03556007-0604-1 319 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 48000 FC ALI NTM 5551171 TBD B2OR PART 6FROM 0 FC/FHSPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54200 FH EASA ADTO LOVHORIZONTAL STABILIZER CENTER BOX UPPER SKIN REAR CAP I: 18700 FC 2006-0071RIVETING AT ATTACHMENT TO REAR SPAR BETWEEN RIB 2 AND OR FAA ADRIB 3 LH/RH. 21100 FH 2007-04-11NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN ALI REFERENCE:RIB 2 AND RIB 3, LH/RH. 556007-01-1NOTE 1: GRACE PERIOD = 1000 FCACCESS: 313AL* 0.14STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)556007-0604-2 319 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 40000 FC ALI NTM 5551171 TBD B4-100OR PART 6FROM 0 FC/FHSPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54400 FH EASA ADTO LOVHORIZONTAL STABILIZER CENTER BOX UPPER SKIN REAR CAP I: 16600 FC 2006-0071RIVETING AT ATTACHMENT TO REAR SPAR BETWEEN RIB 2 AND OR FAA ADRIB 3 LH/RH. 22500 FH 2007-04-11NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN ALI REFERENCE:RIB 2 AND RIB 3, LH/RH. 556007-01-2NOTE 1: GRACE PERIOD = 1000 FCACCESS: 313AL* 0.14556007-0604-3 319 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 34000 FC ALI NTM 5551171 TBD B4-200OR PART 6C4SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 75100 FH EASA ADF4HORIZONTAL STABILIZER CENTER BOX UPPER SKIN REAR CAP I: 13500 FC 2006-0071FROM 0 FC/FHRIVETING AT ATTACHMENT TO REAR SPAR BETWEEN RIB 2 AND OR FAA ADTO LOVRIB 3 LH/RH. 29800 FH 2007-04-11NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN ALI REFERENCE:RIB 2 AND RIB 3, LH/RH. 556007-01-3NOTE 1: GRACE PERIOD = 1000 FCACCESS: 313AL* 0.14556008-0604-1 300 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 55100 FC ALI EASA AD1 TBD B2OR 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL 62200 FH FAA ADTO LOVBOX UPPER SKIN EXTERNAL SURFACE BETWEEN RIB 3 AND I: 43800 FC 2007-04-11RIB 4 AND BETWEEN REAR SPAR AND STRINGER 11 LH/RH. OR49400 FH ALI REFERENCE:556008-01-1556008-0604-2 300 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 47700 FC ALI EASA AD1 TBD B4-100OR 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL 64800 FH FAA ADTO LOVBOX UPPER SKIN EXTERNAL SURFACE BETWEEN RIB 3 AND I: 38900 FC 2007-04-11RIB 4 AND BETWEEN REAR SPAR AND STRINGER 11 LH/RH. OR52900 FH ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)556008-0604-2 * * * * * C O N T I N U E * * * * *556008-01-2556008-0604-3 300 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 38100 FC ALI EASA AD1 TBD B4-200OR 2006-0071C4DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL 84200 FH FAA ADF4BOX UPPER SKIN EXTERNAL SURFACE BETWEEN RIB 3 AND I: 31800 FC 2007-04-11FROM 0 FC/FHRIB 4 AND BETWEEN REAR SPAR AND STRINGER 11 LH/RH. ORTO LOV70200 FH ALI REFERENCE:556008-01-3556009-0604-1 319 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 48000 FC ALI EASA AD1 TBD B2OR 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF HORIZONTAL STABILIZER REAR 54200 FH FAA ADTO LOVSPAR WEB JOINING PART AT RIB 3, RIVETING AREA BETWEEN I: 10400 FC 2007-04-11RIB 2 AND RIB 3, LH/RH OR11700 FH ALI REFERENCE:ACCESS: 313AL 556009-01-1* 0.14556009-0604-2 319 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100OR 2006-0071FROM 0 FC/FHDETAILED INSPECTION OF HORIZONTAL STABILIZER REAR 54300 FH FAA ADTO LOVSPAR WEB JOINING PART AT RIB 3, RIVETING AREA BETWEEN I: 9200 FC 2007-04-11RIB 2 AND RIB 3, LH/RH OR12600 FH ALI REFERENCE:ACCESS: 313AL 556009-01-2* 0.14556009-0604-3 319 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200OR 2006-0071C4DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR 75100 FH FAA ADF4SPAR WEB JOINING PART AT RIB 3, RIVETING AREA BETWEEN I: 7500 FC 2007-04-11FROM 0 FC/FHRIB 2 AND RIB 3, LH/RH ORTO LOV16700 FH ALI REFERENCE:ACCESS: 313AL 556009-01-3* 0.14558011-0603-1 323 VERTICAL STAB.-SPAR BOX MEC DET T: 15 YE CPCP MRB REFERENCE: 1 0.70 ALLI: 9 YE 558011-C603-1DETAILED INSPECTION OF VERTICAL STABILIZERINTERNAL STRUCTURE FROM RIB 12 TO 26.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)558011-0603-1 * * * * * C O N T I N U E * * * * *ACCESS: 322BL 322CL 324AT 325CR 325DL 325DR* 8.52325EL 325ER 325FL 325GL 325HL 325JL325KL558021-0603-1 322 VERTICAL STABILIZER - FRONT SPAR MEC GVI I: 9 YE CPCP MRB REFERENCE: 1 0.25 ALL324 558021-C603-11 0.25GENERAL VISUAL INSPECTION OF VERTICAL STABILIZERFRONT SPAR FORWARD FACE INCLUDING TIP.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION(EXCLUDING ANTENNA AND ANTENNA CONNECTION).ACCESS: 322AL 322BL 322CL* 5.98324AT 324BT* 1.10558041-0603-1 323 FUSELAGE EXTERNAL SURFACE VERTICAL MEC DET T: 5 YE CPCP AMM SSI 5550031 1.30 ALLSTABILIZER RIB 1 I: 5 YE MRB S AMM SSI 555005SIL SIL 55-033DETAILED INSPECTION OF FIN TO FUSELAGEATTACHMENT FITTINGS AND VERTICAL STABILIZER RIB 1 MRB REFERENCE:UPPER AND LOWER SURFACE INCLUDING FORKED LINKS ANDTRANSVERSE LOAD FITTINGS. 558041-C603-1NOTE 1: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION, EXCLUDING THECONICAL FIN TO FUSELAGE ATTACHMENT BOLTSATTACHMENT BOLTSNOTE 2: CHECK THE CORRECT ALIGNMENT OF THE TORQUEMARKSACCESS: 311AZ 311BZ 312AR 323AL 323AR 323BR* 1.98325BL558061-0603-1 326 RUDDER - INTERNAL STRUCTURE MEC BSI T: 15 YE CPCP NTM 5140001 2.00 ALLI: 9 YE PART 1NDT INSPECTION OF RUDDER INTERNAL STRUCTURE THROUGHLIGHTENING HOLES. MRB REFERENCE:558061-C603-1* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)558061-0603-1 * * * * * C O N T I N U E * * * * *NOTE: BOROSCOPE INSPECTIONACCESS: 325AL 325AR 325BL 325BR 325CL 325CR* 11.24325DL 325DR 325EL 325ER 325FL 325GL325HL 325JL 325KL 326AL 326AR 326BL326BR 326CL 326CR 326DL 326DR 326EL326ER 326FL 326GL 326HL 326JL 326KL326LL558065-0603-1 326 RUDDER FRONT SPAR MEC GVI T: 15 YE CPCP MRB REFERENCE: 1 0.50 ALLI: 9 YE 558065-C603-1GENERAL VISUAL INSPECTION OF RUDDER FRONT SPARFORWARD FACE .NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 325AL 325AR 325BL 325CL 325DL 325EL* 8.69325FL 325GL 325HL 325JL 325KL 326AL326AR 326BL 326BR 326CL 326CR 326DL326DR 326EL 326ER 326FL 326GL 326HL326JL 326KL 326LL558081-0603-1 325 VERTICAL STABILIZER TRAILING EDGE MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 0.50 ALL558081-C603-1GENERAL VISUAL INSPECTION OF VERTICAL STABILIZERTRAILING EDGE.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 325AL 325BL 325CL 325DL 325EL 325FL* 3.32325GL 325HL 325JL 325KL558085-0603-1 325 RUDDER HINGE ARMS AND FITTINGS MEC DET I: 5 YE CPCP AMM SSI 5530011 1.25 ALL326 MRB S AMM SSI 5530031 1.25DETAILED INSPECTION OF RUDDER HINGE ARMS 1 TO AMM SSI 5530097 AND ATTACH FITTINGS OF RUDDER HINGE ARMS AND AMM SSI 553013HYDRAULIC ACTUATORS INCLUDING SUPPORT STRUCTURE ON AMM SSI 553015VERTICAL STABILIZER REAR SPAR AND RUDDER FRONT SPAR. AMM SSI 554001* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)558085-0603-1 * * * * * C O N T I N U E * * * * *AMM SSI 554003NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, AMM SSI 554009G2 OR G3 AFTER INSPECTION AMM SSI 554011AMM SSI 554013ACCESS: 325BL 325DL 325FL 325HL 325KL AMM SSI 555007* 1.21326BL 326DL 326FL 326HL 326KL AMM SSI 555009* 1.10AMM SSI 555011AMM SSI 555013AMM SSI 555015AMM SSI 555017AMM SSI 555019SIL 55-013MRB REFERENCE:558085-C603-A558085-C603-B558089-0603-1 325 VERT.STAB.-MACHINED PLATES MEC DET I: 5 YE CPCP MRB REFERENCE: 1 0.80 ALL558089-C603-1DETAILED INSPECTION OF INTEGRAL MACHINEDPLATES ON VERTICAL STABILIZER REAR SPAR AFT FACEBETWEEN RIB 11 AND RIB 16.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTIONACCESS: 325DL* 0.21558193-0603-1 335 ELEVATOR INTERN. STRUCTURE MEC DET T: 15 YE CPCP MRB REFERENCE: 1 1.00 ALL345 I: 9 YE 558193-C603-11 1.00DETAILED INSPECTION OF HORIZONTAL STABILIZERELEVATOR INTERNAL STRUCTURE THROUGH LIGHTENING HOLES.ACCESS: 334AT 334BT 334CT 334DT 334ET 334FT* 6.10334GT 334HT 334JT 334KT 334LT 335AB335AT 335BB 335BT 335CB 335CT 335DB335DT 335EB 335ET344AT 344BT 344CT 344DT 344ET 344FT* 6.12344GT 344HT 344JT 344KT 344LT 345AB345AT 345BB 345BT 345CB 345CT 345DB* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)558193-0603-1 * * * * * C O N T I N U E * * * * *345DT 345EB 345ET558215-0603-1 334 HINGE ARMS, FITTING MEC DET I: 8200 FC CPCP AMM SSI 5510051 0.50 ALL344 OR 5 YE MRB S AMM SSI 5510071 0.50DETAILED INSPECTION OF FITTING ON HORIZONTALSTABILIZER REAR SPAR AND HINGE ARMS FOR ELEVATORS AT MRB REFERENCE:RIBS 6, 9, 10, 11, 14, 17 AND 20.558215-C603-1NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 ANDG2 AFTER INSPECTIONACCESS: 334AB 334BB 334BT 334CB 334CT 334DB* 5.60334DT 334EB 334ET 334FT 334GT 334HT334JT 334KT 334LT344AB 344BB 344BT 344CB 344CT 344DB* 5.59344DT 344EB 344ET 344FT 344GT 344HT344JT 344KT 344LT* * * * * E N D * * * * *STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION:3-55 PAGE 20APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571001-0602-1 541 TOP SKIN AT FRONT SPAR MEC DET T: 20600 FC ALI CN 2006-0071(B) 1 0.20 B2641 I: 12400 FC FAA AD 96-13-11 1 0.20 B4-100DETAILED INSPECTION OF TOP SKIN AT ATTACHMENTS TOFROM 0 FC/FHFRONT SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENCE: TO LOV571001-01-1571001-0602-2 541 TOP SKIN AT FRONT SPAR MEC DET T: 20000 FC ALI CN 2006-0071(B) 1 0.20 B4-200641 I: 12000 FC FAA AD 96-13-11 1 0.20 C4DETAILED INSPECTION OF TOP SKIN AT ATTACHMENTS TOF4FRONT SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENCE: FROM 0 FC/FH571001-01-2TO LOV571002-0602-1 541 TOP SKIN AT CENTER / AFT SPAR MEC DET T: 20600 FC ALI CN 2006-0071(B) 1 0.20 B2542 I: 12400 FC FAA AD 96-13-11 1 0.20 B4-100641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO1 0.20 FROM 0 FC/FH642 CENTER SPAR AND REAR SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENCE: 1 0.20 TO LOV571002-01-1571002-0602-2 541 TOP SKIN AT CENTER / AFT SPAR MEC DET T: 20000 FC ALI CN 2006-0071(B) 1 0.20 B4-200542 I: 12000 FC FAA AD 96-13-11 1 0.20 C4641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO1 0.20 F4642 CENTER SPAR AND REAR SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENCE: 1 0.20 FROM 0 FC/FH571002-01-2TO LOV571003-0602-1 541 TOP SKIN AT RIB 2 TO 9 MEC DET T: 20600 FC ALI CN 2006-0071(B) 1 0.20 B2542 I: 12400 FC FAA AD 96-13-11 1 0.20 B4-100641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO1 0.20 FROM 0 FC/FH642 RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- AND REAR ALI REFERENCE: 1 0.20 TO LOVSPAR. 571003-01-1571003-0602-2 541 TOP SKIN AT RIB 2 TO 9 MEC DET T: 20000 FC ALI CN 2006-0071(B) 1 0.20 B4-200542 I: 12000 FC FAA AD 96-13-11 1 0.20 C4641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO1 0.20 F4642 RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- AND REAR ALI REFERENCE: 1 0.20 FROM 0 FC/FHSPAR. 571003-01-2TO LOV571005-0602-1 542 BOTTOM SKIN AT REAR SPAR MEC DET T: 13200 FC ALI CN 2006-0071(B) 1 0.20 B2642 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 14900 FHTO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571005-0602-1 * * * * * C O N T I N U E * * * * *REAR SPAR, RIB 1 TO RIB 3 INCLUSIVE. I: 3300 FC ALI REFERENCE:OR 571005-01-13700 FH571005-0602-2 542 BOTTOM SKIN AT REAR SPAR MEC DET T: 12800 FC ALI CN 2006-0071(B) 1 0.20 B4-100642 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 17400 FHTO LOVREAR SPAR, RIB 1 TO RIB 3 INCLUSIVE. I: 3200 FC ALI REFERENCE:OR 571005-01-24300 FH571005-0602-3 542 BOTTOM SKIN AT REAR SPAR MEC DET T: 12000 FC ALI CN 2006-0071(B) 1 0.20 B4-200642 OR FAA AD 96-13-11 1 0.20 C4DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 26500 FHF4REAR SPAR, RIB 1 TO RIB 3 INCLUSIVE. I: 3000 FC ALI REFERENCE: FROM 0 FC/FHOR 571005-01-3TO LOV6600 FH571006-0602-1 541 BOTTOM SKIN AT FRONT- AND CENTER SPAR MEC DET T: 22400 FC ALI CN 2006-0071(B) 1 0.20 B2542 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FH641 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT 25300 FH1 0.20 TO LOV642 TO FRONT AND CENTER SPARS BETWEEN RIB 1 AND RIB 9 I: 10100 FC ALI REFERENCE: 1 0.20INCLUSIVE, AND AT ATTACHMENT TO REAR SPAR, RIB 3 AND OR 571006-01-1RIB 9 INCLUSIVE. 11400 FH571006-0602-2 541 BOTTOM SKIN AT FRONT- AND CENTER SPAR MEC DET T: 21700 FC ALI CN 2006-0071(B) 1 0.20 B4-100542 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FH641 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT 29700 FH1 0.20 TO LOV642 TO FRONT AND CENTER SPARS BETWEEN RIB 1 AND RIB 9 I: 9800 FC ALI REFERENCE: 1 0.20INCLUSIVE, AND AT ATTACHMENT TO REAR SPAR, RIB 3 AND OR 571006-01-2RIB 9 INCLUSIVE. 13400 FH571006-0602-3 541 BOTTOM SKIN AT FRONT- AND CENTER SPAR MEC DET T: 20400 FC ALI CN 2006-0071(B) 1 0.20 B4-200542 OR FAA AD 96-13-11 1 0.20 C4641 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT 46300 FH1 0.20 F4642 TO FRONT AND CENTER SPARS BETWEEN RIB 1 AND RIB 9 I: 9200 FC ALI REFERENCE: 1 0.20 FROM 0 FC/FHINCLUSIVE, AND AT ATTACHMENT TO REAR SPAR, RIB 3 AND OR 571006-01-3TO LOVRIB 9 INCLUSIVE. 20900 FHSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571007-0602-1 541 BOTTOM SKIN AND JOINT STRAPS MEC DET T: 18300 FC ALI CN 2006-0071(B) 1 0.20 B2542 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FH641 DETAILED INSPECTION OF BOTTOM SKIN AND JOINT STRAPS 20700 FH1 0.20 TO LOV642 ATTACHMENT TO RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- I: 11000 FC ALI REFERENCE: 1 0.20AND REAR SPAR. OR 571007-01-112400 FH571007-0602-2 541 BOTTOM SKIN AND JOINT STRAPS MEC DET T: 17500 FC ALI CN 2006-0071(B) 1 0.20 B4-100542 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FH641 DETAILED INSPECTION OF BOTTOM SKIN AND JOINT STRAPS 24000 FH1 0.20 TO LOV642 ATTACHMENT TO RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- I: 10500 FC ALI REFERENCE: 1 0.20AND REAR SPAR. OR 571007-01-214400 FH571007-0602-3 541 BOTTOM SKIN AND JOINT STRAPS MEC DET T: 16600 FC ALI CN 2006-0071(B) 1 0.20 B4-200542 OR FAA AD 96-13-11 1 0.20 C4641 DETAILED INSPECTION OF BOTTOM SKIN AND JOINT STRAPS 37700 FH1 0.20 F4642 ATTACHMENT TO RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- I: 10000 FC ALI REFERENCE: 1 0.20 FROM 0 FC/FHAND REAR SPAR. OR 571007-01-3TO LOV22700 FH571009-0602-1 500 WING - TOP SKIN PANEL NUMBER 3 MEC DET T: 14800 FC ISB ISB 57-2101 1.00 ALL600 I: 2500 FC1 1.00DETAILED INSPECTION OF WING TOP SKIN PANELNUMBER 3.ACCESS: 581EB 581FB 581GB 581HB* 0.19681EB 681FB 681GB 681HB* 0.19571013-0602-1 540 ACCESS DOOR AND BOTTOM SKIN MEC DET I: 6700 FC MRB S AMM SSI 5710131 0.50 B26401 0.50DETAILED INSPECTION OF EXTERNAL BOTTOM SKINAT DOOR CUTOUTS AND PUMP APERTURES AND ACCESS DOORSBETWEEN RIBS 1 AND 9.571013-0603-1 540 BOTTOM SKIN AND ACCESS DOORS AT CUTOUTS MEC DET I: 5 YE MRB S AMM SSI 5710131 0.30 ALL6401 0.30DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUT-OUTS BETWEEN RIBS 2 AND 9* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571013-0603-1 * * * * * C O N T I N U E * * * * *NOTE: DOOR OPENEDACCESS: 541AB 541BB 541CB 542CB 542DB 542EB* 9.00641AB 641BB 641CB 642CB 642DB 642EB* 9.00571013-0604-1 540 ACCESS DOOR AND BOTTOM SKIN MEC DET I: 17700 FC MRB S AMM SSI 5710131 1.50 B26401 1.50DETAILED INSPECTION OF FUEL PUMP APERTURESBETWEEN RIB 1 AND 2.PREP.: FUEL PUMPS REMOVED571014-0602-1 540 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 6500 FC MRB S AMM SSI 5710141 0.50 B4-1006401 0.50DETAILED INSPECTION OF EXTERNAL BOTTOMSKIN AT DOOR CUTOUTS AND PUMP APERTURES BETWEENRIBS 1 AND 9.571014-0602-2 540 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 6100 FC MRB S AMM SSI 5710141 0.50 B4-2006401 0.50 C4DETAILED INSPECTION OF EXTERNAL BOTTOMF4SKIN AT DOOR CUTOUTS AND PUMP APERTURES BETWEENRIBS 1 AND 9.571014-0604-1 540 FUEL PUMP APERTURES MEC DET I: 17700 FC MRB S AMM SSI 5710141 1.50 B4-1006401 1.50DETAILED INSPECTION OF FUEL PUMP APERTURESBETWEEN RIB 1 AND 2PREP.: FUEL PUMPS REMOVED.571014-0604-2 540 FUEL PUMP APERTURES MEC DET I: 15100 FC MRB S AMM SSI 5710141 1.50 B4-2006401 1.50 C4DETAILED INSPECTION OF FUEL PUMP APERTURESF4BETWEEN RIB 1 AND 2.PREP.: FUEL PUMPS REMOVED.STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571015-0603-1 542 ATTACH.OF FLAP TRACK 2 MEC DET I: 6000 FC MRB S AMM SSI 5710151 0.33 ALL6421 0.33DETAILED INSPECTION OF FLAP TRACK NO.2ATTACHMENT AT RIB 5 AND FALSE SPARACCESS: 532AF 532AM* 0.67632AF 632AM* 0.67571016-0604-1 541 WING RIB 7 TO 8 MEC DET I: 7700 FC MRB S AMM SSI 5710161 0.30 B26411 0.30DETAILED INSPECTION OF INTERNAL STRUCTURE TOPAND BOTTOM FROM RIBS 7 TO 8 IN PYLON ATTACHMENT AREAACCESS: 541CB* 1.50641CB* 1.50571016-0604-2 541 WING RIB 7 TO 8 MEC DET I: 7400 FC MRB S AMM SSI 5710161 0.30 B4-1006411 0.30DETAILED INSPECTION OF INTERNAL STRUCTURE TOPAND BOTTOM FROM RIBS 7 TO 8 IN PYLON ATTACHMENT AREAACCESS: 541CB* 1.50641CB* 1.50571016-0604-3 541 WING RIB 7 TO 8 MEC DET I: 7000 FC MRB S AMM SSI 5710161 0.30 B4-2006411 0.30 C4DETAILED INSPECTION OF INTERNAL STRUCTURE TOPF4AND BOTTOM FROM RIBS 7 TO 8 IN PYLON ATTACHMENT AREAACCESS: 541CB* 1.50641CB* 1.50571017-0602-1 523 TOP SKIN AT PYLON ATTACHMENT MEC DET T: 20600 FC ALI CN 2006-0071(B) 1 0.10 B2541 I: 6200 FC FAA AD 96-13-11 1 0.10 B4-100623 DETAILED INSPECTION OF TOP REINFORCING AND ADJACENT1 0.10 FROM 0 FC/FH641 SKIN AT ENGINE PYLON ATTACHMENT TO RIB 7 AND RIB 8 ALI REFERENCE: 1 0.10 TO LOVAND FRONT SPAR. 571017-01-1571017-0602-2 523 TOP SKIN AT PYLON ATTACHMENT MEC DET T: 20000 FC ALI CN 2006-0071(B) 1 0.10 B4-200541 I: 6000 FC FAA AD 96-13-11 1 0.10 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571017-0602-2 * * * * * C O N T I N U E * * * * *623 DETAILED INSPECTION OF TOP REINFORCING AND ADJACENT ALI REFERENCE: 1 0.10 F4641 SKIN AT ENGINE PYLON ATTACHMENT TO RIB 7 AND RIB 8 571017-01-21 0.10 FROM 0 FC/FHAND FRONT SPAR.TO LOV571018-0603-1 523 BOTTOM EXTERNAL REINFORCING NDT SDI T: 13400 FC ALI NTM 5741101 3.50 B2541 OR PART 41 3.50 FROM 0 FC/FH623 SPECIAL DETAILED INSPECTION OF BOTTOM EXTERNAL 15100 FH CN 2006-0071(B) 1 3.50 TO LOV641 REINFORCING AND ADJACENT SKIN AT PYLON ATTACHMENT RIB I: 6700 FC FAA AD 96-13-11 1 3.507 TO RIB 8 AND FRONT SPAR TO INCLUDE PYLON FORWARD ORPICK UP FITTING AND SUPPORT STRUCTURE. 7600 FH ALI REFERENCE:571018-01-1ACCESS: 512AT 512LB 523AB* 0.41471AL 471BL 472AR 472BR 473BL 474BR* 1.90612AT 612LB 623AB* 0.40481AL 481BL 482AR 482BR 483BL 484BR* 1.93571018-0603-2 523 BOTTOM EXTERNAL REINFORCING NDT SDI T: 13000 FC ALI NTM 5741101 3.50 B4-100541 OR PART 41 3.50 FROM 0 FC/FH623 SPECIAL DETAILED INSPECTION OF BOTTOM EXTERNAL 17800 FH CN 2006-0071(B) 1 3.50 TO LOV641 REINFORCING AND ADJACENT SKIN AT PYLON ATTACHMENT RIB I: 6500 FC FAA AD 96-13-11 1 3.507 TO RIB 8 AND FRONT SPAR TO INCLUDE PYLON FORWARD ORPICK UP FITTING AND SUPPORT STRUCTURE. 8900 FH ALI REFERENCE:571018-01-2ACCESS: 512AT 512LB 523AB* 0.41471AL 471BL 472AR 472BR 473BL 474BR* 1.90612AT 612LB 623AB* 0.40481AL 481BL 482AR 482BR 483BL 484BR* 1.93571018-0603-3 523 BOTTOM EXTERNAL REINFORCING NDT SDI T: 12200 FC ALI NTM 5741101 3.50 B4-200541 OR PART 41 3.50 C4623 SPECIAL DETAILED INSPECTION OF BOTTOM EXTERNAL 27700 FH CN 2006-0071(B) 1 3.50 F4641 REINFORCING AND ADJACENT SKIN AT PYLON ATTACHMENT RIB I: 6100 FC FAA AD 96-13-11 1 3.50 FROM 0 FC/FH7 TO RIB 8 AND FRONT SPAR TO INCLUDE PYLON FORWARD ORTO LOVPICK UP FITTING AND SUPPORT STRUCTURE. 13800 FH ALI REFERENCE:571018-01-3ACCESS: 512AT 512LB 523AB* 0.41471AL 471BL 472AR 472BR 473BL 474BR* 1.90612AT 612LB 623AB* 0.40481AL 481BL 482AR 482BR 483BL 484BR* 1.93STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571019-0604-1 541 FRONT SPAR AND ATTACHMENTS MEC DET I: 17700 FC MRB S AMM SSI 5710191 0.30 B26411 0.30DETAILED INSPECTION OF FRONT SPAR ANDATTACHMENTS, AFT FACE, FROM RIBS 1 TO 9 INCLUSIVEACCESS: 541AB 541BB 541CB 542EB* 6.00641AB 641BB 641CB 642EB* 6.00571019-0604-2 541 FRONT SPAR AND ATTACHMENTS MEC DET I: 17700 FC MRB S AMM SSI 5710191 0.30 B4-1006411 0.30DETAILED INSPECTION OF FRONT SPAR ANDATTACHMENTS, AFT FACE, FROM RIBS 1 TO 9 INCLUSIVEACCESS: 541AB 541BB 541CB 542EB* 6.00641AB 641BB 641CB 642EB* 6.00571019-0604-3 541 FRONT SPAR AND ATTACHMENTS MEC DET I: 15100 FC MRB S AMM SSI 5710191 0.30 B4-2006411 0.30 C4DETAILED INSPECTION OF FRONT SPAR ANDF4ATTACHMENTS, AFT FACE, FROM RIBS 1 TO 9 INCLUSIVEACCESS: 541AB 541BB 541CB 542EB* 6.00641AB 641BB 641CB 642EB* 6.00571020-0603-1 470 WING TO PYLON SPIGOT MEC DET I: 4 YE ISB ISB 57-01012 1.00 PRE 035544802 1.00DETAILED INSPECTION OF WING TO PYLON THRUSTLOAD SPIGOT SLEEVE FOR CORROSIONNOTE 01: SPIGOT SLEEVE REMOVEDNOTE 02: AFTER REWORK IN ACCORDANCE WITH SB 57 - 101,INTERVAL CAN BE EXTENDED TO 8 YEACCESS: 471AL 471BL 472AR 472BR* 0.88481AL 481BL 482AR 482BR* 0.91571021-0604-1 541 CENTER SPAR FORWARD FACE MEC DET I: 17700 FC MRB S AMM SSI 5710211 0.30 B26411 0.30DETAILED INSPECTION OF CENTER SPAR FORWARDFACE AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571021-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 541CB* 1.50641CB* 1.50571021-0604-2 541 CENTER SPAR FORWARD FACE MEC DET I: 17700 FC MRB S AMM SSI 5710211 0.30 B4-1006411 0.30DETAILED INSPECTION OF CENTER SPAR FORWARDFACE AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8ACCESS: 541CB* 1.50641CB* 1.50571021-0604-3 541 CENTER SPAR FORWARD FACE MEC DET I: 15100 FC MRB S AMM SSI 5710211 0.30 B4-2006411 0.30 C4DETAILED INSPECTION OF CENTER SPAR FORWARDF4FACE AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8ACCESS: 541CB* 1.50641CB* 1.50571022-0604-1 541 CENTER SPAR FORWARD FACE MEC DET I: 27300 FC MRB S AMM SSI 5710221 0.30 B26411 0.30DETAILED INSPECTION OF CENTER SPAR FORWARDFACE AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 ANDBETWEEN RIBS 8 AND 9.ACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571022-0604-2 541 CENTER SPAR FORWARD FACE MEC DET I: 22600 FC MRB S AMM SSI 5710221 0.30 B4-1006411 0.30DETAILED INSPECTION OF CENTER SPAR FORWARDFACE AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 ANDBETWEEN RIBS 8 AND 9.ACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571022-0604-3 541 CENTER SPAR FORWARD FACE MEC DET I: 19200 FC MRB S AMM SSI 5710221 0.30 B4-2006411 0.30 C4DETAILED INSPECTION OF CENTER SPAR FORWARDF4FACE AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 ANDBETWEEN RIBS 8 AND 9.ACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571023-0604-1 542 CENTER SPAR AFT FACE MEC DET I: 17700 FC MRB S AMM SSI 5710231 0.30 B26421 0.30DETAILED INSPECTION OF CENTER SPAR AFT FACEAND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8ACCESS: 542DB 542EB* 3.00642DB 642EB* 3.00571023-0604-2 542 CENTER SPAR AFT FACE MEC DET I: 17700 FC MRB S AMM SSI 5710231 0.30 B4-1006421 0.30DETAILED INSPECTION OF CENTER SPAR AFT FACEAND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8ACCESS: 542DB 542EB* 3.00642DB 642EB* 3.00571023-0604-3 542 CENTER SPAR AFT FACE MEC DET I: 15100 FC MRB S AMM SSI 5710231 0.30 B4-2006421 0.30 C4DETAILED INSPECTION OF CENTER SPAR AFT FACEF4AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8ACCESS: 542DB 542EB* 3.00642DB 642EB* 3.00571024-0604-1 542 CENTER SPAR AFT FACE MEC DET I: 27300 FC MRB S AMM SSI 5710241 0.30 B26421 0.30DETAILED INSPECTION OF CENTER SPAR AFT FACEAND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 ANDBETWEEN RIBS 8 AND 9ACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571024-0604-2 542 CENTER SPAR AFT FACE MEC DET I: 22600 FC MRB S AMM SSI 5710241 0.30 B4-1006421 0.30DETAILED INSPECTION OF CENTER SPAR AFT FACEAND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 ANDBETWEEN RIBS 8 AND 9ACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50571024-0604-3 542 CENTER SPAR AFT FACE MEC DET I: 19200 FC MRB S AMM SSI 5710241 0.30 B4-2006421 0.30 C4DETAILED INSPECTION OF CENTER SPAR AFT FACEF4AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 ANDBETWEEN RIBS 8 AND 9ACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50571025-0604-1 542 REAR SPAR FORWARD FACE MEC DET I: 27300 FC MRB S AMM SSI 5710251 0.30 B26421 0.30DETAILED INSPECTION OF REAR SPAR FORWARD FACEFROM RIBS 1 TO 3ACCESS: 542CB* 1.50642CB* 1.50571025-0604-2 542 REAR SPAR FORWARD FACE MEC DET I: 22600 FC MRB S AMM SSI 5710251 0.30 B4-1006421 0.30DETAILED INSPECTION OF REAR SPAR FORWARD FACEFROM RIBS 1 TO 3ACCESS: 542CB* 1.50642CB* 1.50571025-0604-3 542 REAR SPAR FORWARD FACE MEC DET I: 19200 FC MRB S AMM SSI 5710251 0.30 B4-2006421 0.30 C4DETAILED INSPECTION OF REAR SPAR FORWARD FACEF4FROM RIBS 1 TO 3ACCESS: 542CB* 1.50642CB* 1.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571026-0604-1 542 REAR SPAR FORWARD FACE MEC DET I: 17700 FC MRB S AMM SSI 5710261 0.30 B26421 0.30DETAILED INSPECTION OF REAR SPAR FORWARD FACEFROM RIBS 3 TO 9ACCESS: 542DB 542EB* 3.00642DB 642EB* 3.00571026-0604-2 542 REAR SPAR FORWARD FACE MEC DET I: 17700 FC MRB S AMM SSI 5710261 0.30 B4-1006421 0.30DETAILED INSPECTION OF REAR SPAR FORWARD FACEFROM RIBS 3 TO 9ACCESS: 542DB 542EB* 3.00642DB 642EB* 3.00571026-0604-3 542 REAR SPAR FORWARD FACE MEC DET I: 15100 FC MRB S AMM SSI 5710261 0.30 B4-2006421 0.30 C4DETAILED INSPECTION OF REAR SPAR FORWARD FACEF4FROM RIBS 3 TO 9ACCESS: 542DB 542EB* 3.00642DB 642EB* 3.00571027-0604-1 541 RIB 7,8 HALF RIBS AND ATTA. MEC DET I: 27300 FC MRB S AMM SSI 5710271 0.30 B26411 0.30DETAILED INSPECTION OF RIBS 7 AND 8, HALF RIBSAND ATTACHMENTS TO BOTTOM SKIN, FRONT SPAR AND CENTERSPARACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571027-0604-2 541 RIB 7,8 HALF RIBS AND ATTA. MEC DET I: 22600 FC MRB S AMM SSI 5710271 0.30 B4-1006411 0.30DETAILED INSPECTION OF RIBS 7 AND 8, HALF RIBSAND ATTACHMENTS TO BOTTOM SKIN, FRONT SPAR AND CENTERSPARACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571027-0604-3 541 RIB 7,8 HALF RIBS AND ATTA. MEC DET I: 19200 FC MRB S AMM SSI 5710271 0.30 B4-2006411 0.30 C4DETAILED INSPECTION OF RIBS 7 AND 8, HALF RIBSF4AND ATTACHMENTS TO BOTTOM SKIN, FRONT SPAR AND CENTERSPARACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571028-0602-1 571 REAR SPAR AND BOTTOM ANGLE MEC DET I: 6700 FC ALI CN 2006-0071(B) 1 0.50 B2671 OR FAA AD 96-13-11 1 0.50 FROM 0 FC/FHDETAILED INSPECTION OF REAR SPAR AND BOTTOM ANGLE 7600 FHTO LOVMEMBER, AFT FACE BETWEEN RIB 1 AND RIB 3. ALI REFERENCE:571028-01-1PREP.: MAIN LANDING GEAR DOORS OPEN.571028-0602-2 571 REAR SPAR AND BOTTOM ANGLE MEC DET I: 6500 FC ALI CN 2006-0071(B) 1 0.50 B4-100671 OR FAA AD 96-13-11 1 0.50 FROM 0 FC/FHDETAILED INSPECTION OF REAR SPAR AND BOTTOM ANGLE 8800 FHTO LOVMEMBER, AFT FACE BETWEEN RIB 1 AND RIB 3. ALI REFERENCE:571028-01-2PREP.: MAIN LANDING GEAR DOORS OPEN.571028-0602-3 571 REAR SPAR AND BOTTOM ANGLE MEC DET I: 6100 FC ALI CN 2006-0071(B) 1 0.50 B4-200671 OR FAA AD 96-13-11 1 0.50 C4DETAILED INSPECTION OF REAR SPAR AND BOTTOM ANGLE 13500 FHF4MEMBER, AFT FACE BETWEEN RIB 1 AND RIB 3. ALI REFERENCE: FROM 0 FC/FH571028-01-3TO LOVPREP.: MAIN LANDING GEAR DOORS OPEN.571029-0604-1 542 RIB 4,5,6 AND ATT.TO SKIN MEC DET I: 7700 FC MRB S AMM SSI 5710291 0.30 B26421 0.30DETAILED INSPECTION OF RIBS 4,5,6 ANDATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPARACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00571029-0604-2 542 RIB 4,5,6 AND ATT.TO SKIN MEC DET I: 7400 FC MRB S AMM SSI 5710291 0.30 B4-1006421 0.30* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571029-0604-2 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF RIBS 4,5,6 ANDATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPARACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00571029-0604-3 542 RIB 4,5,6 AND ATT.TO SKIN MEC DET I: 7000 FC MRB S AMM SSI 5710291 0.30 B4-2006421 0.30 C4DETAILED INSPECTION OF RIBS 4,5,6 ANDF4ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPARACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00571030-0604-1 542 RIB 2,3,7,8 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710301 0.30 B26421 0.30DETAILED INSPECTION OF RIBS 2,3,7,8 ANDATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPARACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50571030-0604-2 542 RIB 2,3,7,8 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710301 0.30 B4-1006421 0.30DETAILED INSPECTION OF RIBS 2,3,7,8 ANDATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPARACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50571030-0604-3 542 RIB 2,3,7,8 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710301 0.30 B4-2006421 0.30 C4DETAILED INSPECTION OF RIBS 2,3,7,8 ANDF4ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPARACCESS: 542CB 542DB 542EB* 4.50642CB 642DB 642EB* 4.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571031-0602-1 541 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 18600 FC ALI CN 2006-0071(B) 1 0.20 B2641 I: 11200 FC FAA AD 96-13-11 1 0.20 B4-100DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TOFROM 0 FC/FHSTRINGERS BETWEEN FRONT- AND CENTER SPAR, RIB 1 ALI REFERENCE: TO LOVTO RIB 9. 571031-01-1571031-0602-2 541 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 17500 FC ALI CN 2006-0071(B) 1 0.20 B4-200641 I: 10500 FC FAA AD 96-13-11 1 0.20 C4DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TOF4STRINGERS BETWEEN FRONT- AND CENTER SPAR, RIB 1 ALI REFERENCE: FROM 0 FC/FHTO RIB 9. 571031-01-2TO LOV571033-0602-1 541 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 13200 FC ALI CN 2006-0071(B) 1 0.20 B2641 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED EXTERNAL INSPECTION OF BOTTOM SKIN 14900 FHTO LOVAND RIVETS AT STRINGER RUNOUTS AFT OF FRONT SPAR I: 3300 FC ALI REFERENCE:FROM RIB 2 TO 8 INCLUSIVE. OR 571033-01-13700 FH571033-0602-2 541 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 12800 FC ALI CN 2006-0071(B) 1 0.20 B4-100641 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 17500 FHTO LOVSTRINGER RUNOUTS AFT OF FRONT SPAR RIB 2 TO RIB 8 I: 3200 FC ALI REFERENCE:INCLUSIVE. OR 571033-01-24400 FH571033-0602-3 541 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 12400 FC ALI CN 2006-0071(B) 1 0.20 B4-200641 OR FAA AD 96-13-11 1 0.20 C4DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 28100 FHF4STRINGER RUNOUTS AFT OF FRONT SPAR RIB 2 TO RIB 8 I: 3100 FC ALI REFERENCE: FROM 0 FC/FHINCLUSIVE. OR 571033-01-3TO LOV7000 FH571035-0602-1 542 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 18600 FC ALI CN 2006-0071(B) 1 0.20 B2642 I: 11200 FC FAA AD 96-13-11 1 0.20 B4-100DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TOFROM 0 FC/FHSTRINGERS BETWEEN CENTER- AND REAR SPAR, RIB 1 TO ALI REFERENCE: TO LOVRIB 9. 571035-01-1STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571035-0602-2 542 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 17500 FC ALI CN 2006-0071(B) 1 0.50 B4-200642 I: 10500 FC FAA AD 96-13-11 1 0.50 C4DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TOF4STRINGERS BETWEEN CENTER- AND REAR SPAR, RIB 1 TO ALI REFERENCE: FROM 0 FC/FHRIB 9. 571035-01-2TO LOV571036-0602-1 541 BOTTOM SKIN AND STRINGERS MEC DET I: 10100 FC MRB S AMM SSI 5710361 0.20 B26411 0.20DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT AND CENTER SPAR ANDRIBS 1 TO 9571036-0602-2 541 BOTTOM SKIN AND STRINGERS MEC DET I: 9900 FC MRB S AMM SSI 5710361 0.20 B4-1006411 0.20DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT AND CENTER SPAR ANDRIBS 1 TO 9571036-0602-3 541 BOTTOM SKIN AND STRINGERS MEC DET I: 9200 FC MRB S AMM SSI 5710361 0.20 B4-2006411 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDF4STRINGERS BETWEEN FRONT AND CENTER SPAR ANDRIBS 1 TO 9571036-0604-1 541 BOTTOM SKIN AND STRINGERS MEC DET I: 27300 FC MRB S AMM SSI 5710361 0.30 B26411 0.30DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT AND CENTER SPAR FROM RIBS 1TO 9ACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571036-0604-2 541 BOTTOM SKIN AND STRINGERS MEC DET I: 22600 FC MRB S AMM SSI 5710361 0.30 B4-1006411 0.30DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT AND CENTER SPAR FROM RIBS 1TO 9ACCESS: 541AB 541BB 541CB* 4.50* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571036-0604-2 * * * * * C O N T I N U E * * * * *641AB 641BB 641CB* 4.50571036-0604-3 541 BOTTOM SKIN AND STRINGERS MEC DET I: 19200 FC MRB S AMM SSI 5710361 0.30 B4-2006411 0.30 C4DETAILED INSPECTION OF BOTTOM SKIN ANDF4STRINGERS BETWEEN FRONT AND CENTER SPAR FROM RIBS 1TO 9ACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571037-0603-1 512 WING BOTTOM SKIN PANEL NUMBER 1 NDT SDI T: 5600 FC ISB NTM 5131041 1.00 PRE 04959612 I: 900 FC PART 11 1.00 (57-0132)SPECIAL DETAILED INSPECTION OF WING BOTTOM SKIN PANEL NTM 570001PRE 10086NUMBER 1 (REBATED SECTION). PART 6(57-0188)ISB 57-130ACCESS: 472AR 512LB* 0.39481AL 612LB* 0.39571037-0603-2 512 WING BOTTOM SKIN PANEL NUMBER 1 NDT SDI T: 5600 FC ISB NTM 5131041 1.00 POST 04959612 I: 900 FC PART 11 1.00 (57-0132)SPECIAL DETAILED INSPECTION OF WING BOTTOM SKIN PANEL NTM 570001PRE 10086NUMBER 1 (REBATED SECTION). PART 6(57-0188)ISB 57-130NOTENOTE: TASK VALID FOR RETROFIT 04959 - HOLESFILLED WITH AERODYNAMIC FILLER.ACCESS: 472AR 512LB* 0.39481AL 612LB* 0.39571037-0603-3 512 WING BOTTOM SKIN PANEL NUMBER 1 NDT SDI T: 18400 FC ISB NTM 5131041 1.00 POST 04959612 I: 900 FC PART 11 1.00 (57-0132)SPECIAL DETAILED INSPECTION OF WING BOTTOM SKIN PANEL NTM 570001PRE 10086NUMBER 1 (REBATED SECTION). PART 6(57-0188)ISB 57-130NOTENOTE: TASK VALID FOR RETROFIT 04959 - HOLESFILLED WITH INTERFERENCE FIT BOLTSACCESS: 472AR 512LB* 0.39* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571037-0603-3 * * * * * C O N T I N U E * * * * *481AL 612LB* 0.39571039-0604-1 541 RIB 2 - 6 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710391 0.30 B26411 0.30DETAILED INSPECTION OF RIBS 2 TO 6 ANDATTACHMENTS TO SKIN,FRONT SPAR AND CENTER SPARACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571039-0604-2 541 RIB 2 - 6 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710391 0.30 B4-1006411 0.30DETAILED INSPECTION OF RIBS 2 TO 6 ANDATTACHMENTS TO SKIN,FRONT SPAR AND CENTER SPARACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571039-0604-3 541 RIB 2 - 6 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710391 0.30 B4-2006411 0.30 C4DETAILED INSPECTION OF RIBS 2 TO 6 ANDF4ATTACHMENTS TO SKIN,FRONT SPAR AND CENTER SPARACCESS: 541AB 541BB 541CB* 4.50641AB 641BB 641CB* 4.50571040-0602-1 542 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 22500 FC ALI CN 2006-0071(B) 1 0.20 B2642 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF BOTTOM SKIN AND STRINGERS 25400 FHTO LOVBETWEEN CENTER- AND REAR SPAR AND RIB 1 TO RIB 9. I: 13500 FC ALI REFERENCE:OR 571040-01-115200 FH571040-0602-2 542 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 21600 FC ALI CN 2006-0071(B) 1 0.20 B4-100642 OR FAA AD 96-13-11 1 0.20 FROM 0 FC/FHDETAILED INSPECTION OF BOTTOM SKIN AND STRINGERS 29400 FHTO LOVBETWEEN CENTER- AND REAR SPAR AND RIB 1 TO RIB 9. I: 13000 FC ALI REFERENCE:OR 571040-01-2* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571040-0602-2 * * * * * C O N T I N U E * * * * *17700 FH571040-0602-3 542 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 20500 FC ALI CN 2006-0071(B) 1 0.20 B4-200642 OR FAA AD 96-13-11 1 0.20 C4DETAILED INSPECTION OF BOTTOM SKIN AND STRINGERS 45300 FHF4BETWEEN CENTER- AND REAR SPAR AND RIB 1 TO RIB 9. I: 12300 FC ALI REFERENCE: FROM 0 FC/FHOR 571040-01-3TO LOV27200 FH571041-0604-1 540 UPPER PART OF RIB 9 MEC DET I: 27300 FC MRB S AMM SSI 5710411 0.30 B26401 0.30DETAILED INSPECTION OF UPPER PART OF RIB 9 ANDATTACHMENTS TO TOP SKIN,FRONT SPAR AND REAR SPARACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00571041-0604-2 540 UPPER PART OF RIB 9 MEC DET I: 22600 FC MRB S AMM SSI 5710411 0.30 B4-1006401 0.30DETAILED INSPECTION OF UPPER PART OF RIB 9 ANDATTACHMENTS TO TOP SKIN,FRONT SPAR AND REAR SPARACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00571041-0604-3 540 UPPER PART OF RIB 9 MEC DET I: 19200 FC MRB S AMM SSI 5710411 0.30 B4-2006401 0.30 C4DETAILED INSPECTION OF UPPER PART OF RIB 9 ANDF4ATTACHMENTS TO TOP SKIN,FRONT SPAR AND REAR SPARACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00571042-0604-1 540 LOWER PART OF RIB 9 MEC DET I: 17700 FC MRB S AMM SSI 5710421 0.30 B26401 0.30DETAILED INSPECTION OF LOWER PART OF RIB 9 ANDATTACHMENTS TO BOTTOM SKIN BETWEEN FRONT SPAR ANDREAR SPAR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571042-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00571042-0604-2 540 LOWER PART OF RIB 9 MEC DET I: 17700 FC MRB S AMM SSI 5710421 0.30 B4-1006401 0.30DETAILED INSPECTION OF LOWER PART OF RIB 9 ANDATTACHMENTS TO BOTTOM SKIN BETWEEN FRONT SPAR ANDREAR SPARACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00571042-0604-3 540 LOWER PART OF RIB 9 MEC DET I: 15100 FC MRB S AMM SSI 5710421 0.30 B4-2006401 0.30 C4DETAILED INSPECTION OF LOWER PART OF RIB 9 ANDF4ATTACHMENTS TO BOTTOM SKIN BETWEEN FRONT SPAR ANDREAR SPARACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00571045-0602-1 543 TOP SKIN ATTACHMENT TO FRONT SPAR MEC DET T: 20300 FC ALI CN 2006-0071(B) 1 0.20 B2643 I: 12200 FC FAA AD 96-13-11 1 0.20 B4-100DETAILED INSPECTION OF TOP SKIN ATTACHMENT IN FRONTPOST 01868SPAR, REAR SPAR AND RIB 9 TO RIB 15 INCLUSIVE. ALI REFERENCE: POST 01869571045-01-1ORPOST 02101(57-0079)FROM 0 FC/FHTO LOV571045-0602-2 543 TOP SKIN ATTACHMENT TO FRONT SPAR MEC DET T: 20000 FC ALI CN 2006-0071(B) 1 0.20 B4-200643 I: 12000 FC FAA AD 96-13-11 1 0.20 C4DETAILED INSPECTION OF TOP SKIN ATTACHMENT IN FRONTF4SPAR, REAR SPAR AND RIB 9 TO RIB 15 INCLUSIVE. ALI REFERENCE: POST 01868571045-01-2POST 01869ORPOST 02101(57-0079)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571045-0602-2 * * * * * C O N T I N U E * * * * *FROM 0 FC/FHTO LOV571047-0602-1 543 BOTTOM SKIN RIBS 9 TO 15 MEC DET T: 13400 FC ALI EASA AD1 0.20 B2643 OR 2006-00711 0.20 FROM 0 FC/FHDETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 15100 FH FAA ADTO LOVTO FRONT SPAR AND REAR SPAR, RIB 9 TO RIB 15, AND TO I: 6700 FC 2007-04-11RIB 10 TO RIB 14 INCLUSIVE. OR7600 FH ALI REFERENCE:571047-01-1571047-0602-2 543 BOTTOM SKIN RIBS 9 TO 15 MEC DET T: 12800 FC ALI EASA AD1 0.20 B4-100643 OR 2006-00711 0.20 FROM 0 FC/FHDETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 17500 FH FAA ADTO LOVTO FRONT SPAR AND REAR SPAR, RIB 9 TO RIB 15, AND TO I: 6400 FC 2007-04-11RIB 10 TO RIB 14 INCLUSIVE. OR8700 FH ALI REFERENCE:571047-01-2571047-0602-3 543 BOTTOM SKIN RIBS 9 TO 15 MEC DET T: 12000 FC ALI EASA AD1 0.20 B4-200643 OR 2006-00711 0.20 C4DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 27200 FH FAA ADF4TO FRONT SPAR AND REAR SPAR, RIB 9 TO RIB 15, AND TO I: 6000 FC 2007-04-11FROM 0 FC/FHRIB 10 TO RIB 14 INCLUSIVE. ORTO LOV13600 FH ALI REFERENCE:571047-01-3571049-0602-1 543 ACCESS DOORS BOTT.SKIN MEC DET I: 10100 FC MRB S AMM SSI 5710491 0.20 B26431 0.20DETAILED EXTERNAL INSPECTION OF ACCESS DOORS ANDBOTTOM SKIN AT ACCESS DOOR CUTOUTS BETWEENRIBS 10 TO 13571049-0602-2 543 ACCESS DOORS BOTT.SKIN MEC DET I: 9700 FC MRB S AMM SSI 5710491 0.20 B4-1006431 0.20DETAILED EXTERNAL INSPECTION OF ACCESS DOORS ANDBOTTOM SKIN AT ACCESS DOOR CUTOUTS BETWEENRIBS 10 TO 13STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 20APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571049-0602-3 543 ACCESS DOORS BOTT.SKIN MEC DET I: 9000 FC MRB S AMM SSI 5710491 0.20 B4-2006431 0.20 C4DETAILED EXTERNAL INSPECTION OF ACCESS DOORS ANDF4BOTTOM SKIN AT ACCESS DOOR CUTOUTS BETWEENRIBS 10 TO 13571049-0603-1 543 ACCESS DOORS, BOTTOM SKIN MEC DET I: 5 YE MRB S AMM SSI 5710491 0.30 ALL6431 0.30DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUT-OUTS BETWEEN RIBS 10 AND 13ACCESS: 543AB 543BB 543CB* 4.50643AB 643BB 643CB* 4.50571051-0604-1 543 FRONT SPAR AND ATT.TO RIBS MEC DET I: 17700 FC MRB S AMM SSI 5710511 0.30 B26431 0.30DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDATTACHMENTS TO RIBS BETWEEN RIB 9 AND 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571051-0604-2 543 FRONT SPAR AND ATT.TO RIBS MEC DET I: 15100 FC MRB S AMM SSI 5710511 0.30 B4-1006431 0.30DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDATTACHMENTS TO RIBS BETWEEN RIB 9 AND 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571051-0604-3 543 FRONT SPAR AND ATT.TO RIBS MEC DET I: 15100 FC MRB S AMM SSI 5710511 0.30 B4-2006431 0.30 C4DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDF4ATTACHMENTS TO RIBS BETWEEN RIB 9 AND 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571053-0604-1 543 REAR SPAR AND ATT.TO RIBS MEC DET I: 27300 FC MRB S AMM SSI 5710531 0.30 B26431 0.30* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 21APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571053-0604-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF REAR SPAR FORWARD FACEAND ATTACHMENTS TO RIBS BETWEEN RIBS 9 AND 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571053-0604-2 543 REAR SPAR AND ATT.TO RIBS MEC DET I: 22600 FC MRB S AMM SSI 5710531 0.30 B4-1006431 0.30DETAILED INSPECTION OF REAR SPAR FORWARD FACEAND ATTACHMENTS TO RIBS BETWEEN RIBS 9 AND 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571053-0604-3 543 REAR SPAR AND ATT.TO RIBS MEC DET I: 19200 FC MRB S AMM SSI 5710531 0.30 B4-2006431 0.30 C4DETAILED INSPECTION OF REAR SPAR FORWARD FACEF4AND ATTACHMENTS TO RIBS BETWEEN RIBS 9 AND 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571055-0602-1 543 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 20300 FC ALI CN 2006-0071(B) 1 0.20 B2550 I: 12200 FC FAA AD 96-13-11 1 0.20 B4-100643 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO1 0.20 FROM 0 FC/FH650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO ALI REFERENCE: 1 0.20 TO LOVRIB 15. 571055-01-1571055-0602-2 543 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 20000 FC ALI CN 2006-0071(B) 1 0.20 B4-200550 I: 12000 FC FAA AD 96-13-11 1 0.20 C4643 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TOMENTS1 0.20 F4650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO ALI REFERENCE: 1 0.20 FROM 0 FC/FHRIB 15. 571055-01-2TO LOV571057-0602-1 543 BOTTOM SKIN AT STRINGER MEC DET T: 13400 FC ALI EASA AD1 0.20 B2550 OR 2006-00711 0.20 FROM 0 FC/FH643 DETAILED INSPECTION OF BOTTOM SKIN AT STRINGER 15300 FH FAA AD1 0.20 TO LOV650 RUNOUTS, RIB 9 TO RIB 15. I: 6700 FC 2007-04-111 0.20* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 22APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571057-0602-1 * * * * * C O N T I N U E * * * * *OR ALI REFERENCE:7600 FH 571057-01-1571057-0602-2 543 BOTTOM SKIN AT STRINGER MEC DET T: 12800 FC ALI EASA AD1 0.20 B4-100550 OR 2006-00711 0.20 FROM 0 FC/FH643 DETAILED INSPECTION OF BOTTOM SKIN AT STRINGER 17800 FH FAA AD1 0.20 TO LOV650 RUNOUTS, RIB 9 TO RIB 15. I: 6400 FC 2007-04-111 0.20OR8900 FH ALI REFERENCE:571057-01-2571057-0602-3 543 BOTTOM SKIN AT STRINGER MEC DET T: 12000 FC ALI EASA AD1 0.20 B4-200550 OR 2006-00711 0.20 C4643 DETAILED INSPECTION OF BOTTOM SKIN AT STRINGER 27800 FH FAA AD1 0.20 F4650 RUNOUTS, RIB 9 TO RIB 15. I: 6000 FC 2007-04-111 0.20 FROM 0 FC/FHORTO LOV13900 FH ALI REFERENCE:571057-01-3571058-0602-1 543 BOTTOM SKIN MEC DET I: 10100 FC ALI EASA AD1 0.20 B2550 OR 2006-00711 0.20 FROM 0 FC/FH643 DETAILED INSPECTION OF EXTERNAL BOTTOM SKIN AND 11400 FH FAA AD1 0.20 TO LOV650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO 2007-04-111 0.20RIB 15.ALI REFERENCE:571058-01-1571058-0602-2 543 BOTTOM SKIN MEC DET I: 9600 FC ALI EASA AD1 0.20 B4-100550 OR 2006-00711 0.20 FROM 0 FC/FH643 DETAILED INSPECTION OF EXTERNAL BOTTOM SKIN AND 13100 FH FAA AD1 0.20 TO LOV650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO 2007-04-111 0.20RIB 15.ALI REFERENCE:571058-01-2571058-0602-3 543 BOTTOM SKIN MEC DET I: 9000 FC ALI EASA AD1 0.20 B4-200550 OR 2006-00711 0.20 C4643 DETAILED INSPECTION OF EXTERNAL BOTTOM SKIN AND 20400 FH1 0.20 F4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 23APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571058-0602-3 * * * * * C O N T I N U E * * * * *650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO FAA AD1 0.20 FROM 0 FC/FHRIB 15. 2007-04-11TO LOVALI REFERENCE:571058-01-3571058-0604-1 543 BOTTOM SKIN AND STRINGERS MEC DET I: 27300 FC MRB S AMM SSI 5710581 0.30 B26431 0.30DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT SPAR AND REAR SPAR FROM RIBS9 TO 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571058-0604-2 543 BOTTOM SKIN AND STRINGERS MEC DET I: 22600 FC MRB S AMM SSI 5710581 0.30 B4-1006431 0.30DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT SPAR AND REAR SPAR FROM RIBS9 TO 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571058-0604-3 543 BOTTOM SKIN AND STRINGERS MEC DET I: 19200 FC MRB S AMM SSI 5710581 0.30 B4-2006431 0.30 C4DETAILED INSPECTION OF BOTTOM SKIN ANDF4STRINGERS BETWEEN FRONT SPAR AND REAR SPAR FROM RIBS9 TO 15ACCESS: 543AB 543BB 543CB 543DB 550BB* 7.50643AB 643BB 643CB 643DB 650BB* 7.50571059-0604-1 543 RIB 10 - 15 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710591 0.30 B26431 0.30DETAILED INSPECTION OF RIBS 10 TO 15INCLUSIVE, AND ATTACHMENTS TO SKINACCESS: 543AB 543BB 543CB 543DB 550BB 550DB* 9.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 24APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571059-0604-1 * * * * * C O N T I N U E * * * * *643AB 643BB 643CB 643DB 650BB 650DB* 9.00571059-0604-2 543 RIB 10 - 15 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710591 0.30 B4-1006431 0.30DETAILED INSPECTION OF RIBS 10 TO 15INCLUSIVE, AND ATTACHMENTS TO SKINACCESS: 543AB 543BB 543CB 543DB 550BB 550DB* 9.00643AB 643BB 643CB 643DB 650BB 650DB* 9.00571059-0604-3 543 RIB 10 - 15 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710591 0.30 B4-2006431 0.30 C4DETAILED INSPECTION OF RIBS 10 TO 15F4INCLUSIVE, AND ATTACHMENTS TO SKINACCESS: 543AB 543BB 543CB 543DB 550BB 550DB* 9.00643AB 643BB 643CB 643DB 650BB 650DB* 9.00571061-0603-1 543 ATTACH.OF FLAP TRACKS 3 & 4 MEC DET I: 6000 FC MRB S AMM SSI 5710611 0.30 ALL6431 0.30DETAILED INSPECTION OF FORWARD EXTERNALPICK-UP ATTACHMENTS OF FLAP TRACK 3 AND 4 AT RIB 11AND 15.ACCESS: 533AF 534AF* 0.67633AF 634AF* 0.67571062-0602-1 543 FLAP TRACKS 3 AND 4 ATTACH. MEC DET I: 6000 FC MRB S AMM SSI 5710621 0.30 ALL6431 0.30DETAILED INSPECTION OF ATTACHMENTS OF FLAPTRACKS TO REAR SPAR AT TRACK 3 AND 4.NOTE: FLAP EXTENDED571064-0604-1 543 FORWARD FLAP TRACK ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5710641 0.30 B26431 0.30DETAILED INSPECTION OF PICK UP ATTACHMENTS OFFLAP TRACKS NO. 3 AND 4 AT RIBS 11 AND 15* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 25APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571064-0604-1 * * * * * C O N T I N U E * * * * *ACCESS: 543AB 543BB 550BB 550DB* 6.00643AB 643BB 650BB 650DB* 6.00571064-0604-2 543 FORWARD FLAP TRACK ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710641 0.30 B4-1006431 0.30DETAILED INSPECTION OF PICK UP ATTACHMENTS OFFLAP TRACKS NO. 3 AND 4 AT RIBS 11 AND 15ACCESS: 543AB 543BB 550BB 550DB* 6.00643AB 643BB 650BB 650DB* 6.00571064-0604-3 543 FORWARD FLAP TRACK ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710641 0.30 B4-2006431 0.30 C4DETAILED INSPECTION OF PICK UP ATTACHMENTS OFF4FLAP TRACKS NO. 3 AND 4 AT RIBS 11 AND 15ACCESS: 543AB 543BB 550BB 550DB* 6.00643AB 643BB 650BB 650DB* 6.00571065-0602-1 550 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710651 0.20 B26501 0.20DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETSAT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS FROMRIB 15 TO 27 INCLUSIVE571065-0602-2 550 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710651 0.20 B4-1006501 0.20DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETSAT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS FROMRIB 15 TO 27 INCLUSIVE571065-0602-3 550 TOP SKIN MEC DET I: 11200 FC MRB S AMM SSI 5710651 0.20 B4-2006501 0.20 C4DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETSF4AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS FROMRIB 15 TO 27 INCLUSIVESTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 26APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571067-0602-1 550 BOTTOM SKIN MEC DET I: 9700 FC MRB S AMM SSI 5710671 0.20 B26501 0.20DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDRIVETS AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBSFROM RIB 15 TO 27 INCLUSIVE571067-0602-2 550 BOTTOM SKIN MEC DET I: 9500 FC MRB S AMM SSI 5710671 0.20 B4-1006501 0.20DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDRIVETS AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBSFROM RIB 15 TO 27 INCLUSIVE571067-0602-3 550 BOTTOM SKIN MEC DET I: 9100 FC MRB S AMM SSI 5710671 0.20 B4-2006501 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDF4RIVETS AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBSFROM RIB 15 TO 27 INCLUSIVE571069-0603-1 550 ACCESS DOORS, BOTTOM SKIN MEC DET I: 5 YE MRB S AMM SSI 5710691 0.20 B26501 0.20DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 13 AND 22NOTE: IN CASE OF FINDING AND IF A/C IS POST MOD 1824PERFORM AT THE SAME TIME INSPECTION OF OTHERDOORS/CUTOUTS LISTED IN TASK REF 571069-0604-1ACCESS: 543DB 550BB 550DB 550EB 550FB 550GB* 12.00550KB 550LB643DB 650BB 650DB 650EB 650FB 650GB* 12.00650KB 650LB571069-0604-1 550 ACCESS DOORS AND BOTT.SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710691 0.30 B26501 0.30 POST 1824DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUT-OUTS BETWEEN RIBS 17 AND 18AND BETWEEN RIBS 19 AND 22NOTE: DOOR OPENEDACCESS: 550FB 550GB 550KB 550LB* 6.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 27APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571069-0604-1 * * * * * C O N T I N U E * * * * *650FB 650GB 650KB 650LB* 6.00571070-0602-1 550 ACCESS DOORS AND BOTTOM SKIN AT CUTOUTS MEC DET I: 9700 FC MRB S AMM SSI 5710701 0.20 B26501 0.20DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUTOUTS,FROM RIB 13 TO 27571070-0602-2 550 ACCESS DOORS AND BOTTOM SKIN AT CUTOUTS MEC DET I: 9500 FC MRB S AMM SSI 5710701 0.20 B4-1006501 0.20DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUTOUTS,FROM RIB 13 TO 27571070-0602-3 550 ACCESS DOORS AND BOTTOM SKIN AT CUTOUTS MEC DET I: 9100 FC MRB S AMM SSI 5710701 0.20 B4-2006501 0.20 C4DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMF4SKIN AT ACCESS DOOR CUTOUTS,FROM RIB 13 TO 27571070-0603-1 550 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 5 YE MRB S AMM SSI 5710701 0.30 ALL6501 0.30DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUTOUTS BETWEEN RIB 22 AND 27.NOTE: THIS TASK COVERS THE PRE MOD 1824 CASE BETWEENRIBS 23 AND 26.ACCESS: 550LB 550MB 550NB 550PB 550QB* 7.50650LB 650MB 650NB 650PB 650QB* 7.50571070-0604-1 550 ACCESS DOORS, BOTTOM SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710701 0.30 B26501 0.30DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMSKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 23 AND 26NOTE: DOOR OPENEDACCESS: 550MB 550NB 550PB* 4.50650MB 650NB 650PB* 4.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 28APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571070-0604-2 550 ACCESS DOORS, BOTTOM SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710701 0.30 B4-1006501 0.30 POST 01824DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM(57-0060)SKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 23 AND 26NOTE: DOOR OPENEDACCESS: 550MB 550NB 550PB* 4.50650MB 650NB 650PB* 4.50571070-0604-3 550 ACCESS DOORS, BOTTOM SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710701 0.30 B4-2006501 0.30 C4DETAILED INSPECTION OF ACCESS DOORS AND BOTTOMF4SKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 23 AND 26POST 01824(57-0060)NOTE: DOOR OPENEDACCESS: 550MB 550NB 550PB* 4.50650MB 650NB 650PB* 4.50571071-0604-1 550 FRONT SPAR AND RIBS ATTACH MEC DET I: 17700 FC MRB S AMM SSI 5710711 0.30 B26501 0.30DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDATTACHMENTS OF RIBS FROM RIB 15 TO 27 INCLUSIVEACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571071-0604-2 550 FRONT SPAR AND RIBS ATTACH MEC DET I: 17700 FC MRB S AMM SSI 5710711 0.30 B4-1006501 0.30DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDATTACHMENTS OF RIBS FROM RIB 15 TO 27 INCLUSIVEACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 29APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571071-0604-3 550 FRONT SPAR AND RIBS ATTACH MEC DET I: 15100 FC MRB S AMM SSI 5710711 0.30 B4-2006501 0.30 C4DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDF4ATTACHMENTS OF RIBS FROM RIB 15 TO 27 INCLUSIVEACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571072-0603-1 550 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 5 YE MRB S AMM SSI 5710721 0.30 B46501 0.30 C4DETAILED INSPECTION OF WING BOTTOM SKIN ATF4ACCESS DOOR CUTOUTS BETWEEN RIBS 13 AND 22NOTE: THIS TASK COVERS THE PRE MOD 1824 CASE BETWEENRIBS 19 AND 22.ACCESS: 543DB 550BB 550DB 550EB 550FB 550GB* 12.00550KB 550LB643DB 650BB 650DB 650EB 650FB 650GB* 12.00650KB 650LB571072-0604-2 550 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 19200 FC MRB S AMM SSI 5710721 0.30 B46501 0.30 C4DETAILED INSPECTION OF WING BOTTOM SKIN ATF4ACCESS DOOR CUTOUTS BETWEEN RIBS 17 AND 18 ANDPOST 1824BETWEEN RIBS 19 AND 22POST 2300NOTE: DOORS OPENEDACCESS: 550FB 550GB 550KB 550LB* 6.00650FB 650GB 650KB 650LB* 6.00571073-0604-1 550 REAR SPAR AND RIBS ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5710731 0.30 B26501 0.30DETAILED INSPECTION OF REAR SPAR FORWARD FACEAND ATTACHMENTS OF RIBS FROM RIBS 15 TO 27 INCLUSIVEACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 30APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571073-0604-1 * * * * * C O N T I N U E * * * * *650KB 650LB 650MB 650NB 650PB 650QB571073-0604-2 550 REAR SPAR AND RIBS ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710731 0.30 B4-1006501 0.30DETAILED INSPECTION OF REAR SPAR FORWARD FACEAND ATTACHMENTS OF RIBS FROM RIBS 15 TO 27 INCLUSIVEACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571073-0604-3 550 REAR SPAR AND RIBS ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710731 0.30 B4-2006501 0.30 C4DETAILED INSPECTION OF REAR SPAR FORWARD FACEF4AND ATTACHMENTS OF RIBS FROM RIBS 15 TO 27 INCLUSIVEACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571075-0604-1 550 RIB 16-27 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710751 0.50 B26501 0.50DETAILED INSPECTION OF RIBS 16 TO 27 ANDATTACHMENTS TO SKINACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571075-0604-2 550 RIB 16-27 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710751 0.50 B4-1006501 0.50DETAILED INSPECTION OF RIBS 16 TO 27 ANDATTACHMENTS TO SKINACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 31APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571075-0604-2 * * * * * C O N T I N U E * * * * *650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571075-0604-3 550 RIB 16-27 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710751 0.50 B4-2006501 0.50 C4DETAILED INSPECTION OF RIBS 16 TO 27 ANDF4ATTACHMENTS TO SKINACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571077-0602-1 550 TOP SKIN AT STRINGER ATTACH MEC DET I: 11400 FC MRB S AMM SSI 5710771 0.30 B26501 0.30DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETSAT ATTACHMENTS TO STRINGERS BETWEEN FRONT SPAR ANDREAR SPAR AND RIBS 15 TO 27571077-0602-2 550 TOP SKIN AT STRINGER ATTACH MEC DET I: 11400 FC MRB S AMM SSI 5710771 0.30 B4-1006501 0.30DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETSAT ATTACHMENTS TO STRINGERS BETWEEN FRONT SPAR ANREAR SPAR AND RIBS 15 TO 27571077-0602-3 550 TOP SKIN AT STRINGER ATTACH MEC DET I: 11200 FC MRB S AMM SSI 5710771 0.30 B4-2006501 0.30 C4DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETSF4AT ATTACHMENTS TO STRINGERS BETWEEN FRONT SPAR ANDREAR SPAR AND RIBS 15 TO 27571080-0602-1 550 BOTTOM SKIN AT STRINGER RUN-OUTS AND MEC DET I: 9700 FC MRB S AMM SSI 5710791 0.30 B2650 ATTACHMENTS AMM SSI 5710801 0.30DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDRIVETS AT STRINGER ATTACHMENTS AND RUN-OUTS BETWEENFRONT SPAR AND REAR SPAR, FROM RIB 15 TO 27STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 32APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571080-0602-2 550 BOTTOM SKIN AT STRINGER RUN-OUTS AND MEC DET I: 9500 FC MRB S AMM SSI 5710791 0.30 B4-100650 ATTACHMENTS AMM SSI 5710801 0.30DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDRIVETS AT STRINGER ATTACHMENTS AND RUN-OUTS BETWEENFRONT SPAR AND REAR SPAR, FROM RIB 15 TO 27571080-0602-3 550 BOTTOM SKIN AT STRINGER RUN-OUTS AND MEC DET I: 9100 FC MRB S AMM SSI 5710791 0.30 B4-200650 ATTACHMENTS AMM SSI 5710801 0.30 C4F4DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ANDRIVETS AT STRINGER ATTACHMENTS AND RUN-OUTS BETWEENFRONT SPAR AND REAR SPAR, FROM RIB 15 TO 27571080-0604-1 550 BOTTOM SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710801 0.50 B26501 0.50DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT SPAR AND REAR SPAR, FROM RIB15 TO 27ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571080-0604-2 550 BOTTOM SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710801 0.50 B4-1006501 0.50DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT SPAR AND REAR SPAR, FROM RIB15 TO 27ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571080-0604-3 550 BOTTOM SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710801 0.50 B4-2006501 0.50 C4DETAILED INSPECTION OF BOTTOM SKIN ANDF4STRINGERS BETWEEN FRONT SPAR AND REAR SPAR, FROM RIB15 TO 27* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 33APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571080-0604-3 * * * * * C O N T I N U E * * * * *ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB* 18.00550KB 550LB 550MB 550NB 550PB 550QB650DB 650EB 650FB 650GB 650HB 650JB* 18.00650KB 650LB 650MB 650NB 650PB 650QB571083-0603-1 550 ATTACH.OF FLAP TRACK 5 & 6 MEC DET I: 6000 FC MRB S AMM SSI 5710831 0.30 ALL6501 0.30DETAILED INSPECTION OF FWD EXTERNAL PICK-UPATTACHMENTS OF FLAP TRACKS 5 AND 6 AT RIBS 18 AND 22ACCESS: 535AF 536AF* 0.67635AF 636AF* 0.67571084-0602-1 550 FLAP TRACK 5 AND 6 ATTACH. MEC DET I: 3000 FC MRB S AMM SSI 5710841 0.30 ALL6501 0.30DETAILED INSPECTION OF NO.5 AND 6 FLAPTRACK ATTACHMENTS TO REAR SPARNOTE: FLAP EXTENDED571085-0602-1 560 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710851 0.20 B26601 0.20DETAILED EXTERNAL INSPECTION OF TOP SKIN ATATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROMRIB 27 TO 29 INCLUSIVE571085-0602-2 560 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710851 0.20 B4-1006601 0.20DETAILED EXTERNAL INSPECTION OF TOP SKIN ATATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROMRIB 27 TO 29 INCLUSIVE571085-0602-3 560 TOP SKIN MEC DET I: 11200 FC MRB S AMM SSI 5710851 0.20 B4-2006601 0.20 C4DETAILED EXTERNAL INSPECTION OF TOP SKIN ATF4ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROMRIB 27 TO 29 INCLUSIVESTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 34APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571086-0604-1 550 FORWARD FLAP TRACK ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5710861 0.30 B26501 0.30DETAILED INSPECTION OF INTERNAL FORWARDPICK-UP ATTACHMENTS OF FLAP TRACKS NO.5 AND 6 AT RIBS18 AND 22ACCESS: 550FB 550GB 550KB 550LB* 6.00650FB 650GB 650KB 650LB* 6.00571086-0604-2 550 FORWARD FLAP TRACK ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710861 0.30 B4-1006501 0.30DETAILED INSPECTION OF INTERNAL FORWARDPICK-UP ATTACHMENTS OF FLAP TRACKS NO.5 AND 6 AT RIBS18 AND 22ACCESS: 550FB 550GB 550KB 550LB* 6.00650FB 650GB 650KB 650LB* 6.00571086-0604-3 550 FORWARD FLAP TRACK ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710861 0.30 B4-2006501 0.30 C4DETAILED INSPECTION OF INTERNAL FORWARDF4PICK-UP ATTACHMENTS OF FLAP TRACKS NO.5 AND 6 AT RIBS18 AND 22ACCESS: 550FB 550GB 550KB 550LB* 6.00650FB 650GB 650KB 650LB* 6.00571087-0602-1 560 BOTTOM SKIN MEC DET I: 9700 FC MRB S AMM SSI 5710871 0.20 B26601 0.20DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ATATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROMRIB 27 TO 29571087-0602-2 560 BOTTOM SKIN MEC DET I: 9500 FC MRB S AMM SSI 5710871 0.20 B4-1006601 0.20DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AT REFERENCE:ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROMRIB 27 TO 29STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 35APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571087-0602-3 560 BOTTOM SKIN MEC DET I: 9100 FC MRB S AMM SSI 5710871 0.20 B4-2006601 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN ATF4ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROMRIB 27 TO 29571091-0604-1 560 FRONT AND REAR SPAR AND RIBS ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5710911 0.30 B2660 AMM SSI 5710931 0.30DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDREAR SPAR FORWARD FACE AND ATTACHMENTS OF RIBS FROMRIB 27 TO 29 INCLUSIVE.ACCESS: 560AB 560BB* 3.00660AB 660BB* 3.00571091-0604-2 560 FRONT AND REAR SPAR AND RIBS ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710911 0.30 B4-100660 AMM SSI 5710931 0.30DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDREAR SPAR FORWARD FACE AND ATTACHMENTS OF RIBS FROMRIB 27 TO 29 INCLUSIVE.ACCESS: 560AB 560BB* 3.00660AB 660BB* 3.00571091-0604-3 560 FRONT AND REAR SPAR AND RIBS ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710911 0.30 B4-200660 AMM SSI 5710931 0.30 C4DETAILED INSPECTION OF FRONT SPAR AFT FACE ANDF4REAR SPAR FORWARD FACE AND ATTACHMENTS OF RIBS FROMRIB 27 TO 29 INCLUSIVE.ACCESS: 560AB 560BB* 3.00660AB 660BB* 3.00571097-0602-1 560 BOTTOM SKIN MEC DET I: 6400 FC MRB S AMM SSI 5710891 0.20 B2660 AMM SSI 5710971 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN AND RIVETS AT STRINGER ATTACHMENTS BETWEEN FRONTSPAR AND REAR SPAR INCLUDING APPERTURES, BETWEEN RIBS27 AND 29STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 36APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571097-0602-2 560 BOTTOM SKIN MEC DET I: 6300 FC MRB S AMM SSI 5710891 0.20 B4-100660 AMM SSI 5710971 0.20DETAILED EXTERNAL INSPECTION OF BOTTOM SKINAND RIVETS AT STRINGER ATTACHMENTS BETWEEN FRONT SPARAND REAR SPAR INCLUDING APPERTURES, BETWEEN RIBS 27AND 29571097-0602-3 560 BOTTOM SKIN MEC DET I: 6200 FC MRB S AMM SSI 5710891 0.20 B4-200660 AMM SSI 5710971 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOM SKINF4AND RIVETS AT STRINGER ATTACHMENTS BETWEEN FRONT SPARAND REAR SPAR INCLUDING APPERTURES, BETWEEN RIBS 27AND 29571097-0604-1 560 BOTTOM SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710891 0.30 B2660 AMM SSI 5710971 0.30DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT SPAR AND REAR SPAR INCLUDINGAPERTURES FROM RIBS 27 TO 29ACCESS: 560AB 560BB* 3.00660AB 660BB* 3.00571097-0604-2 560 BOTTOM SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710891 0.30 B4-100660 AMM SSI 5710971 0.30DETAILED INSPECTION OF BOTTOM SKIN ANDSTRINGERS BETWEEN FRONT SPAR AND REAR SPAR INCLUDINGAPERTURES FROM RIBS 27 TO 29ACCESS: 560AB 560BB* 3.00660AB 660BB* 3.00571097-0604-3 560 BOTTOM SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710891 0.30 B4-200660 AMM SSI 5710971 0.30 C4DETAILED INSPECTION OF BOTTOM SKIN ANDF4STRINGERS BETWEEN FRONT SPAR AND REAR SPAR INCLUDINGAPERTURES FROM RIBS 27 TO 29ACCESS: 560AB 560BB* 3.00660AB 660BB* 3.00STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 37APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571099-0603-1 500 CRACKED HOLES REPAIRED BY COLD WORK NDT SDI I: ISB ISB NTM 5711271 TBD ALL600 57-206 PART 11 TBDSPECIAL DETAILED INSPECTION OF CRACKED HOLES REPAIRED PART 4BY COLD WORKING. PART 6CN2000-434-321(B)ISB 57-206571100-0603-1 530 FLAP TRACK 2 TO 6 CARRIAGE DRIVE MEC DET I: 5 YE CPCP MRB REFERENCE: 0 N/A ALL630 ASSEMBLIES 571100-C603-10 N/ADETAILED INSPECTION OF FLAP TRACK 2 TO 6CARRIAGE DRIVE ASSEMBLIES, INCLUDING TAB DRIVE LEVERMOUNTINGS AND YOKE ASSEMBLIES.PREP.: FLAP TRACK FAIRINGS REMOVED.571103-0604-1 532 FLAP TRACK 2 BEAM INTERIOR NDT SDI I: 27300 FC CPCP AMM SSI 5711031 0.30 B2632 OR MRB S NTM 5741111 0.30SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE OF 10 YE PART 7FLAP TRACK BEAM N° 2.MRB REFERENCE:NOTE: 01. SCREW JACK REMOVED02. FLAPS FULLY EXTENDED, FLAP TRACK FAIRING 571103-C604-1DETACHEDBOROSCOPE NOTE 1: FLEXIBLE BOROSCOPE DOES NOT REQUIRESCREW YACK REMOVAL.(NTM 57.41.11 PART 7)BOROSCOPE NOTE 2: RIGID BOROSCOPE REQUESTS SCREWJACK REMOVALACCESS: 532AF 532AM* 0.67632AF 632AM* 0.67571103-0604-2 532 FLAP TRACK 2 BEAM INTERIOR NDT SDI I: 22600 FC CPCP AMM SSI 5711031 0.30 B4-100632 OR MRB S NTM 5741111 0.30SPECIAL DETAILED INSPECTION OF FLAP TRACK 2 BEAM 10 YE PART 7INTERIORNOTE: 01. SCREW JACK REMOVED* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 38APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571103-0604-2 * * * * * C O N T I N U E * * * * *02. FLAPS FULLY EXTENDED, FLAP TRACK FAIRING 571103-C604-1DETACHEDBOROSCOPE NOTE 1: FLEXIBLE BOROSCOPE DOES NOT REQUIRESCREW YACK REMOVAL.(NTM 57.41.11 PART 7)BOROSCOPE NOTE 2: RIGID BOROSCOPE REQUESTS SCREWJACK REMOVALACCESS: 532AF 532AM* 0.67632AF 632AM* 0.67571103-0604-3 532 FLAP TRACK 2 BEAM INTERIOR NDT SDI I: 19200 FC CPCP AMM SSI 5711031 0.30 B4-200632 OR MRB S NTM 5741111 0.30 C4SPECIAL DETAILED INSPECTION OF FLAP TRACK 2 BEAM 10 YE PART 7F4INTERIORMRB REFERENCE:NOTE: 01. SCREW JACK REMOVED02. FLAPS FULLY EXTENDED, FLAP TRACK FAIRING 571103-C604-1DETACHEDBOROSCOPE NOTE 1: FLEXIBLE BOROSCOPE DOES NOT REQUIRESCREW YACK REMOVAL.(NTM 57.41.11 PART 7)BOROSCOPE NOTE 2: RIGID BOROSCOPE REQUESTS SCREWJACK REMOVALACCESS: 532AF 532AM* 0.67632AF 632AM* 0.67571105-0604-1 530 FLAP TRACK 3, 4, 5 AND 6 BEAM INTERIOR NDT SDI I: 27300 FC CPCP AMM SSI 5711051 0.50 B2630 OR MRB S AMM SSI 5711071 0.50SPECIAL DETAILED INSPECTION OF FLAP TRACK 3, 4, 5 AND 10 YE AMM SSI 5711096 BEAM INTERIOR. AMM SSI 571111NTM 574111BOROSCOPE NOTES AS FOLLOWS: PART 7NOTE 1: FLEXIBLE BOROSCOPE DOES NOTREQUIRE SCREW JACK REMOVAL(NTM 57.41.11. PART 7)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 39APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571105-0604-1 * * * * * C O N T I N U E * * * * *NOTE 2: RIGID BOROSCOPE REQUESTS 571103-C604-1SCREW JACK REMOVAL 571105-C604-1NOTE 3: SCREW JACK REMOVEDNOTE 4: FLAPS FULLY EXTENDED, FLAP TRACK FAIRINGSDETACHEDACCESS: 533AF 533AM 534AF 534AM 535AF 535AM* 2.66536AF 536AM633AF 633AM 634AF 634AM 635AF 635AM* 2.66636AF 636AM571105-0604-2 533 FLAP TRACK 3, 4, 5 AND 6 BEAM INTERIOR NDT SDI I: 22600 FC CPCP AMM SSI 5711051 0.50 B4-100633 OR MRB S AMM SSI 5711071 0.50SPECIAL DETAILED INSPECTION OF FLAP TRACK 3, 4, 5 AND 10 YE AMM SSI 5711096 BEAM INTERIOR AMM SSI 571111NTM 574111BOROSCOPE NOTES: 01. FLEXIBLE BOROSCOPE DOES NOT PART 7REQUIRE SCREW JACK REMOVAL(NTM 57.41.11. PART 7) MRB REFERENCE:02. RIGID BOROSCOPE REQUESTSSCREW JACK REMOVAL 571103-C604-1571105-C604-1NOTE: 01. FLAPS FULLY EXTENDED, FLAP TRACK FAIRINGSDETACHEDACCESS: 533AF 533AM 534AF 534AM 535AF 535AM* 2.66536AF 536AM633AF 633AM 634AF 634AM 635AF 635AM* 2.66636AF 636AM571105-0604-3 533 FLAP TRACK 3, 4, 5 AND 6 BEAM INTERIOR NDT SDI I: 19200 FC CPCP AMM SSI 5711051 0.50 B4-200633 OR MRB S AMM SSI 5711071 0.50 C4SPECIAL DETAILED INSPECTION OF FLAP TRACK 3, 4, 5 AND 10 YE AMM SSI 571109F46 BEAM INTERIOR AMM SSI 571111NTM 574111BOROSCOPE NOTES: 01. FLEXIBLE BOROSCOPE DOES NOT PART 7REQUIRE SCREW JACK REMOVAL(NTM 57.41.11. PART 7) MRB REFERENCE:02. RIGID BOROSCOPE REQUESTSSCREW JACK REMOVAL 571103-C604-1571105-C604-1* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 40APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571105-0604-3 * * * * * C O N T I N U E * * * * *NOTE: 01. FLAPS FULLY EXTENDED, FLAP TRACK FAIRINGSDETACHEDACCESS: 533AF 533AM 534AF 534AM 535AF 535AM* 2.66536AF 536AM633AF 633AM 634AF 634AM 635AF 635AM* 2.66636AF 636AM571106-0604-1 533 FLAP TRACK 3, 4, 5 AND 6 BEAM EXTERIOR NDT SDI I: 17700 FC CPCP AMM SSI 5711061 2.00 B2633 OR MRB S AMM SSI 5711081 2.00 B4-100SPECIAL DETAILED INSPECTION TRACK NO. 3, 4, 5 AND 6 5 YE AMM SSI 571110BEAM EXTERIOR. AMM SSI 571112NTM 572511ACCESS: 533AF 533AM 534AF 534AM 535AF 535AM PART 4* 2.66536AF 536AM NTM 572512633AF 633AM 634AF 634AM 635AF 635AM PART 4* 2.66636AF 636AM NTM 572513PART 6571106-0604-3 533 FLAP TRACK 3, 4, 5 AND 6 BEAM EXTERIOR NDT SDI I: 15100 FC CPCP AMM SSI 5711061 2.00 B4-200633 OR MRB S AMM SSI 5711081 2.00 C4SPECIAL DETAILED INSPECTION OF TRACK NO. 3, 4, 5 AND 5 YE AMM SSI 571110F46 BEAM EXTERIOR. AMM SSI 571112NTM 572511ACCESS: 533AF 533AM 534AF 534AM 535AF 535AM PART 4* 2.66536AF 536AM NTM 572512633AF 633AM 634AF 634AM 635AF 635AM PART 4* 2.66636AF 636AM NTM 572513PART 6571113-0604-1 523 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711131 4.00 B26231 4.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 41APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571113-0604-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND ATTACHED STRUCTURE BETWEEN RIB 9 AND 17NOTE: HEAT SHIELD REMOVEDACCESS: 523CB 523DB 523EB 523FB 523GB 523HB* 0.98523JB 523KB 523LB 523MB623CB 623DB 623EB 623FB 623GB 623HB* 0.98623JB 623KB 623LB 623MB571113-0604-2 523 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711131 4.00 B4-1006231 4.00DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND ATTACHED STRUCTURE BETWEEN RIB 9 AND 17NOTE: HEAT SHIELD REMOVEDACCESS: 523CB 523DB 523EB 523FB 523GB 523HB* 0.98523JB 523KB 523LB 523MB623CB 623DB 623EB 623FB 623GB 623HB* 0.98623JB 623KB 623LB 623MB571113-0604-3 523 FRONT SPAR AND ATTACH.STRU. MEC DET I: 15100 FC MRB S AMM SSI 5711131 4.00 B4-2006231 4.00 C4DETAILED INSPECTION OF FRONT SPAR FORWARD FACEF4AND ATTACHED STRUCTURE BETWEEN RIB 9 AND 17NOTE: HEAT SHIELD REMOVEDACCESS: 523CB 523DB 523EB 523FB 523GB 523HB* 0.98523JB 523KB 523LB 523MB623CB 623DB 623EB 623FB 623GB 623HB* 0.98623JB 623KB 623LB 623MB571115-0604-1 512 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711151 4.00 B26121 4.00DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND ATTACHED STRUCTURE BETWEEN RIB 1 AND 9NOTE: HEAT SHIELD REMOVAL AT 24400 FC AND FURTHER* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 42APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571115-0604-1 * * * * * C O N T I N U E * * * * *INSPECTIONACCESS: 512AB 512BB 512CB 512DB 512EB 512FB* 1.72512GB 512HB 512JB 512KB 512LB 523AB523BB 523CB612AB 612BB 612CB 612DB 612EB 612FB* 1.69612GB 612HB 612JB 612KB 612LB 623AB623BB 623CB571115-0604-2 512 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711151 4.00 B4-1006121 4.00DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND ATTACHED STRUCTURE BETWEEN RIB 1 AND 9NOTE: HEAT SHIELD REMOVAL AT 24400 FC AND FURTHERINSPECTIONACCESS: 512AB 512BB 512CB 512DB 512EB 512FB* 1.72512GB 512HB 512JB 512KB 512LB 523AB523BB 523CB612AB 612BB 612CB 612DB 612EB 612FB* 1.69612GB 612HB 612JB 612KB 612LB 623AB623BB 623CB571115-0604-3 512 FRONT SPAR AND ATTACH.STRU. MEC DET I: 15100 FC MRB S AMM SSI 5711151 4.00 B4-2006121 4.00 C4DETAILED INSPECTION OF FRONT SPAR FORWARD FACEF4AND ATTACHED STRUCTURE BETWEEN RIB 1 AND 9NOTE: HEAT SHIELD REMOVAL AT 24400 FC AND FURTHERINSPECTIONACCESS: 512AB 512BB 512CB 512DB 512EB 512FB* 1.72512GB 512HB 512JB 512KB 512LB 523AB523BB 523CB612AB 612BB 612CB 612DB 612EB 612FB* 1.69612GB 612HB 612JB 612KB 612LB 623AB623BB 623CBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 43APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571117-0604-1 524 FRONT SPAR AND ATTACH.STRU. MEC DET I: 27300 FC MRB S AMM SSI 5711171 4.00 B26241 4.00DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND ATTACHED STRUCTURE BETWEEN RIB 17 AND 27NOTE: HEAT SHIELD REMOVEDACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KB571117-0604-2 524 FRONT SPAR AND ATTACH.STRU. MEC DET I: 22600 FC MRB S AMM SSI 5711171 4.00 B4-1006241 4.00DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND ATTACHED STRUCTURE BETWEEN RIB 17 AND 27NOTE: HEAT SHIELD REMOVEDACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KB571117-0604-3 524 FRONT SPAR AND ATTACH.STRU. MEC DET I: 19200 FC MRB S AMM SSI 5711171 4.00 B4-2006241 4.00 C4DETAILED INSPECTION OF FRONT SPAR FORWARD FACEF4AND ATTACHED STRUCTURE BETWEEN RIB 17 AND 27NOTE: HEAT SHIELD REMOVEDACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KB571118-0604-1 524 FRONT SPAR AND RIB ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5711181 0.20 B26241 0.20DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND RIB ATTACHMENTS BETWEEN RIB 27 AND 29ACCESS: 524KB* 0.22* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 44APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571118-0604-1 * * * * * C O N T I N U E * * * * *624KB* 0.22571118-0604-2 524 FRONT SPAR AND RIB ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5711181 0.20 B4-1006241 0.20DETAILED INSPECTION OF FRONT SPAR FORWARD FACEAND RIB ATTACHMENTS BETWEEN RIB 27 AND 29ACCESS: 524KB* 0.22624KB* 0.22571118-0604-3 524 FRONT SPAR AND RIB ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5711181 0.20 B4-2006241 0.20 C4DETAILED INSPECTION OF FRONT SPAR FORWARD FACEF4AND RIB ATTACHMENTS BETWEEN RIB 27 AND 29ACCESS: 524KB* 0.22624KB* 0.22571131-0604-1 572 FALSE SPAR SHROUD MEC DET I: 27300 FC MRB S AMM SSI 5711311 0.30 B26721 0.30DETAILED INSPECTION OF FALSE SPARSHROUD AFT FACE AND OTHER ATTACHMENTS BETWEEN RIB 5AND 6A.NOTE: FLAP EXTENDEDACCESS: 572GB 572LB* 0.11672GB 672LB* 0.14571131-0604-2 572 FALSE SPAR SHROUD MEC DET I: 22600 FC MRB S AMM SSI 5711311 0.30 B4-1006721 0.30DETAILED INSPECTION OF FALSE SPARSHROUD AFT FACE AND OTHER ATTACHMENTS BETWEEN RIB 5AND 6A.NOTE: FLAP EXTENDEDACCESS: 572GB 572LB* 0.11672GB 672LB* 0.14STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 45APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571131-0604-3 572 FALSE SPAR SHROUD MEC DET I: 19200 FC MRB S AMM SSI 5711311 0.30 B4-2006721 0.30 C4DETAILED INSPECTION OF FALSE SPARF4SHROUD AFT FACE AND OTHER ATTACHMENTS BETWEEN RIB 5AND 6A.NOTE: FLAP EXTENDEDACCESS: 572GB 572LB* 0.11672GB 672LB* 0.14571132-0604-1 575 ALL SPEED AILERON JACK LUGS MEC DET I: 27300 FC MRB S AMM SSI 5711321 0.20 B26751 0.20DETAILED INSPECTION OF JACK ATTACHMENT LUGSAND AILERON HINGE RIB ATTACHMENTS AT FALSE SPARBETWEEN RIB 6A AND 7AACCESS: 575CB 575CT* 0.22675CB 675CT* 0.22571132-0604-2 575 ALL SPEED AILERON JACK LUGS MEC DET I: 22600 FC MRB S AMM SSI 5711321 0.20 B4-1006751 0.20DETAILED INSPECTION OF JACK ATTACHMENT LUGSAND AILERON HINGE RIB ATTACHMENTS AT FALSE SPARBETWEEN RIB 6A AND 7AACCESS: 575CB 575CT* 0.22675CB 675CT* 0.22571132-0604-3 575 ALL SPEED AILERON JACK LUGS MEC DET I: 19200 FC MRB S AMM SSI 5711321 0.20 B4-2006751 0.20 C4DETAILED INSPECTION OF JACK ATTACHMENT LUGSF4AND AILERON HINGE RIB ATTACHMENTS AT FALSE SPARBETWEEN RIB 6A AND 7AACCESS: 575CB 575CT* 0.22675CB 675CT* 0.22571135-0604-1 575 ALL SPEED AILERON JACK BAY MEC DET I: 27300 FC MRB S AMM SSI 5711351 0.50 B26751 0.50DETAILED INSPECTION OF ALL SPEED AILERON JACK* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 46APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571135-0604-1 * * * * * C O N T I N U E * * * * *BAYACCESS: 575CB 575CT 576AB* 0.27675CB 675CT 676AB* 0.27571135-0604-2 575 ALL SPEED AILERON JACK BAY MEC DET I: 22600 FC MRB S AMM SSI 5711351 0.50 B4-1006751 0.50DETAILED INSPECTION OF ALL SPEED AILERON JACKBAYACCESS: 575CB 575CT 576AB* 0.27675CB 675CT 676AB* 0.27571135-0604-3 575 ALL SPEED AILERON JACK BAY MEC DET I: 19200 FC MRB S AMM SSI 5711351 0.50 B4-2006751 0.50 C4DETAILED INSPECTION OF ALL SPEED AILERON JACKF4BAYACCESS: 575CB 575CT 576AB* 0.27675CB 675CT 676AB* 0.27571136-0602-1 575 TOP SKIN AT RIBS 6A AND 7A. MEC DET I: 9000 FC MRB S AMM SSI 5711361 0.20 ALL6751 0.20DETAILED EXTERNAL INSPECTION OF TOPSKIN AND RIVETS AT ATTACHMENT TO RIBS 6A AND 7A571137-0604-1 575 RIB 5.PORT.AFT OF REAR SPAR MEC DET I: 17700 FC MRB S AMM SSI 5711371 0.20 B26751 0.20DETAILED INSPECTION OF RIB 5 PORTION AFT OFREAR SPARACCESS: 575AB* 0.04675AB* 0.04571137-0604-2 575 RIB 5.PORT.AFT OF REAR SPAR MEC DET I: 17700 FC MRB S AMM SSI 5711371 0.20 B4-1006751 0.20DETAILED INSPECTION OF RIB 5 PORTION AFT OFREAR SPAR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 47APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571137-0604-2 * * * * * C O N T I N U E * * * * *ACCESS: 575AB* 0.04675AB* 0.04571137-0604-3 575 RIB 5.PORT.AFT OF REAR SPAR MEC DET I: 15100 FC MRB S AMM SSI 5711371 0.20 B4-2006751 0.20 C4DETAILED INSPECTION OF RIB 5 PORTION AFT OFF4REAR SPARACCESS: 575AB* 0.04675AB* 0.04571139-0602-1 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6700 FC MRB S AMM SSI 5711391 0.20 B26751 0.20DETAILED EXTERNAL INSPECTION OF REARSPAR AFT FACE AND ATTACHED STRUCTURE FROM RIB 3 TO 5NOTE: FLAP EXTENDED571139-0602-2 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6500 FC MRB S AMM SSI 5711391 0.20 B4-1006751 0.20DETAILED EXTERNAL INSPECTION OF REARSPAR AFT FACE AND ATTACHED STRUCTURE FROM RIB 3 TO 5NOTE: FLAP EXTENDED571139-0602-3 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6100 FC MRB S AMM SSI 5711391 0.20 B4-2006751 0.20 C4DETAILED EXTERNAL INSPECTION OF REARF4SPAR AFT FACE AND ATTACHED STRUCTURE FROM RIB 3 TO 5NOTE: FLAP EXTENDED571139-0604-1 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711391 0.50 B26751 0.50DETAILED INSPECTION OF REAR SPAR AFT FACE ANDATTACHED STRUCTURE FROM RIB 3 TO 9 INCLUSIVEACCESS: 575AB 575AT 575BB 575EB 575FB* 0.26* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 48APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571139-0604-1 * * * * * C O N T I N U E * * * * *675AB 675AT 675BB 675EB 675FB* 0.26571139-0604-2 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711391 0.50 B4-1006751 0.50DETAILED INSPECTION OF REAR SPAR AFT FACE ANDATTACHED STRUCTURE FROM RIB 3 TO 9 INCLUSIVEACCESS: 575AB 575AT 575BB 575EB 575FB* 0.26675AB 675AT 675BB 675EB 675FB* 0.26571139-0604-3 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711391 0.50 B4-2006751 0.50 C4DETAILED INSPECTION OF REAR SPAR AFT FACE ANDF4ATTACHED STRUCTURE FROM RIB 3 TO 9 INCLUSIVEACCESS: 575AB 575AT 575BB 575EB 575FB* 0.26675AB 675AT 675BB 675EB 675FB* 0.26571141-0604-1 575 FALSE SPAR AND ATTACHMENTS MEC DET I: 27300 FC MRB S AMM SSI 5711411 0.30 B2675 AMM SSI 5711451 0.30DETAILED INSPECTION OF FALSE SPAR FORWARD FACEAND ATTACHMENTS BETWEEN RIB 5 AND 6A INCLUSIVE.INCLUDING RIB 5A AND ITS ATTACHMENTS.ACCESS: 575AB* 0.04675AB* 0.04571141-0604-2 575 FALSE SPAR AND ATTACHMENTS MEC DET I: 22600 FC MRB S AMM SSI 5711411 0.30 B4-100675 AMM SSI 5711451 0.30DETAILED INSPECTION OF FALSE SPAR FORWARD FACEAND ATTACHMENTS BETWEEN RIB 5 AND 6A INCLUSIVE.INCLUDING RIB 5A AND ITS ATTACHMENTS.ACCESS: 575AB* 0.04675AB* 0.04571141-0604-3 575 FALSE SPAR AND ATTACHMENTS MEC DET I: 19200 FC MRB S AMM SSI 5711411 0.30 B4-200675 AMM SSI 5711451 0.30 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 49APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571141-0604-3 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF FALSE SPAR FORWARD FACEF4AND ATTACHMENTS BETWEEN RIB 5 AND 6A INCLUSIVE.INCLUDING RIB 5A AND ITS ATTACHMENTS.ACCESS: 575AB* 0.04675AB* 0.04571146-0602-1 575 BOTT.SKIN AT RIB 5 AND 5A. MEC DET I: 3000 FC MRB S AMM SSI 5711461 0.20 ALL6751 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN AT ATTACHMENT TO RIBS 5 AND 5A,AFT OF REAR SPAR571147-0604-1 575 RIBS 6 TO 9 JACK BEAM AND ATTACHMENTS MEC DET I: 27300 FC MRB S AMM SSI 5711421 0.20 B2675 AMM SSI 5711471 0.20DETAILED INSPECTION OF RIBS 6, 6A, 7A, 8, 9AND THEIR ATTACHMENTS AFT OF REAR SPAR, INCLUDINGJACK BEAM AND SUPPORT STRUCTUREACCESS: 575AB 575BB 575DB 575EB 575FB 575GB* 0.37675AB 675BB 675DB 675EB 675FB 675GB* 0.37571147-0604-2 575 RIBS 6 TO 9 JACK BEAM AND ATTACHMENTS MEC DET I: 22600 FC MRB S AMM SSI 5711421 0.20 B4-100675 AMM SSI 5711471 0.20DETAILED INSPECTION OF RIBS 6, 6A, 7A, 8, 9AND THEIR ATTACHMENTS AFT OF REAR SPAR, INCLUDINGJACK BEAM AND SUPPORT STRUCTUREACCESS: 575AB 575BB 575DB 575EB 575FB 575GB* 0.37675AB 675BB 675DB 675EB 675FB 675GB* 0.37571147-0604-3 575 RIBS 6 TO 9 JACK BEAM AND ATTACHMENTS MEC DET I: 19200 FC MRB S AMM SSI 5711421 0.20 B4-200675 AMM SSI 5711471 0.20 C4DETAILED INSPECTION OF RIBS 6, 6A, 7A, 8, 9F4AND THEIR ATTACHMENTS AFT OF REAR SPAR, INCLUDINGJACK BEAM AND SUPPORT STRUCTUREACCESS: 575AB 575BB 575DB 575EB 575FB 575GB* 0.37675AB 675BB 675DB 675EB 675FB 675GB* 0.37STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 50APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571148-0602-1 575 BOTT.SKIN AFT OF REAR SPAR MEC DET I: 9000 FC MRB S AMM SSI 5711481 0.20 ALL6751 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN AT ATTACHMENTS OF RIBS,STIFFENERS,FALSE SPARAND INTERCOSTALS, AFT OF REAR SPAR BETWEEN RIB 5AAND 9571150-0602-1 575 TOP SKIN ACCESS DOOR MEC DET I: 9000 FC MRB S AMM SSI 5711501 0.20 ALL6751 0.20DETAILED EXTERNAL INSPECTION OF ACCESSDOORS AND TOP SKIN ACCESS DOOR APERTURES, AFT OF REARSPAR AND INBOARD OF RIB 6A571153-0602-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 3300 FC MRB S AMM SSI 5711531 0.20 B26811 0.20DETAILED VISUAL EXTERNAL INSPECTION OF REARSPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 9AND 19NOTE: FLAP FULLY EXTENDED571153-0602-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 3200 FC MRB S AMM SSI 5711531 0.20 B4-1006811 0.20DETAILED EXTERNAL INSPECTION OF REARSPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 9AND 19NOTE: FLAP EXTENDED571153-0602-3 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 3000 FC MRB S AMM SSI 5711531 0.20 B4-2006811 0.20 C4DETAILED EXTERNAL INSPECTION OF REARF4SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 9AND 19NOTE: FLAP FULLY EXTENDED571153-0604-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711531 0.30 B26811 0.30DETAILED INSPECTION OF REAR SPAR AFT FACE AND* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 51APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571153-0604-1 * * * * * C O N T I N U E * * * * *ATTACHED STRUCTURE BETWEEN RIB 9 AND 19ACCESS: 581CB 581DB 581EB 581FB 581GB* 0.22681CB 681DB 681EB 681FB 681GB* 0.22571153-0604-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711531 0.30 B4-1006811 0.30DETAILED INSPECTION OF REAR SPAR AFT FACE ANDATTACHED STRUCTURE BETWEEN RIB 9 AND 19ACCESS: 581CB 581DB 581EB 581FB 581GB* 0.22681CB 681DB 681EB 681FB 681GB* 0.22571153-0604-3 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711531 0.30 B4-2006811 0.30 C4DETAILED INSPECTION OF REAR SPAR AFT FACE ANDF4ATTACHED STRUCTURE BETWEEN RIB 9 AND 19ACCESS: 581CB 581DB 581EB 581FB 581GB* 0.22681CB 681DB 681EB 681FB 681GB* 0.22571155-0602-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6400 FC MRB S AMM SSI 5711551 0.20 B26811 0.20DETAILED VISUAL EXTERNAL INSPECTION OF REARSPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 19AND 22NOTE: FLAP FULLY EXTENDED571155-0602-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6300 FC MRB S AMM SSI 5711551 0.20 B4-1006811 0.20DETAILED EXTERNAL INSPECTION OF REARSPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 19AND 22NOTE: FLAP EXTENDEDSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 52APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571155-0602-3 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6100 FC MRB S AMM SSI 5711551 0.20 B4-2006811 0.20 C4DETAILED EXTERNAL INSPECTION OF REARF4SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 19AND 22NOTE: FLAP FULLY EXTENDED571155-0604-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711551 0.30 B26811 0.30DETAILED INSPECTION OF REAR SPAR AFT FACE ANDATTACHED STRUCTURE BETWEEN RIB 19 AND 27 INCLUSIVE(INCLUDING ZONE 591/691).ACCESS: 581HB 581JB 581KB 591AB 591BB 591CB* 0.25681HB 681JB 681KB 691AB 691BB 691CB* 0.33571155-0604-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711551 0.30 B4-1006811 0.30DETAILED INSPECTION OF REAR SPAR AFT FACE ANDATTACHED STRUCTURE BETWEEN RIB 19 AND 27 INCLUSIVE(INCLUDING ZONE 591/691).ACCESS: 581HB 581JB 581KB 591AB 591BB 591CB* 0.25681HB 681JB 681KB 691AB 691BB 691CB* 0.33571155-0604-3 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711551 0.30 B4-2006811 0.30 C4DETAILED INSPECTION OF REAR SPAR AFT FACE ANDF4ATTACHED STRUCTURE BETWEEN RIB 19 AND 27 INCLUSIVE(INCLUDING ZONE 591/691).ACCESS: 581HB 581JB 581KB 591AB 591BB 591CB* 0.25681HB 681JB 681KB 691AB 691BB 691CB* 0.33571156-0604-1 591 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711561 0.20 B26911 0.20DETAILED INSPECTION OF REAR SPAR AFT FACE ANDATTACHED STRUCTURE BETWEEN RIB 27 AND 29ACCESS: 591DB* 0.06* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 53APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571156-0604-1 * * * * * C O N T I N U E * * * * *691DB* 0.06571156-0604-2 591 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711561 0.20 B4-1006911 0.20DETAILED INSPECTION OF REAR SPAR AFT FACE ANDATTACHED STRUCTURE BETWEEN RIB 27 AND 29ACCESS: 591DB* 0.06691DB* 0.06571156-0604-3 591 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711561 0.20 B4-2006911 0.20 C4DETAILED INSPECTION OF REAR SPAR AFT FACE ANDF4ATTACHED STRUCTURE BETWEEN RIB 27 AND 29ACCESS: 591DB* 0.06691DB* 0.06571157-0602-1 542 BOTT.SKIN REINFORCING PLATE MEC DET I: 6700 FC MRB S AMM SSI 5711571 0.20 B26421 0.20DETAILED VISUAL EXTERNAL INSPECTION OF BOTTOMSKIN REINFORCING PLATE AT RIB 5571157-0602-2 542 BOTT.SKIN REINFORCING PLATE MEC DET I: 6500 FC MRB S AMM SSI 5711571 0.20 B4-1006421 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN REINFORCING PLATE AT RIB 5571157-0602-3 542 BOTT.SKIN REINFORCING PLATE MEC DET I: 6100 FC MRB S AMM SSI 5711571 0.20 B4-2006421 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOMF4SKIN REINFORCING PLATE AT RIB 5571159-0602-1 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 6700 FC MRB S AMM SSI 5711591 0.20 B26501 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN AT FUEL PUMP ATTACHMENT HOLES FROM RIB 14 TO 15* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 54APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571159-0602-1 * * * * * C O N T I N U E * * * * *NOTE: FUEL PUMP REMOVEDACCESS: 550AB 550CB* 0.09650AB 650CB* 0.09571159-0602-2 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 6400 FC MRB S AMM SSI 5711591 0.20 B4-1006501 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN AT FUEL PUMP ATTACHMENT HOLES FROM RIB 14 TO 15NOTE: FUEL PUMP REMOVEDACCESS: 550AB 550CB* 0.09650AB 650CB* 0.09571159-0602-3 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 6000 FC MRB S AMM SSI 5711591 0.20 B4-2006501 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOMF4SKIN AT FUEL PUMP ATTACHMENT HOLES FROM RIB 14 TO 15NOTE: FUEL PUMP REMOVEDACCESS: 550AB 550CB* 0.09650AB 650CB* 0.09571159-0604-1 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 27300 FC MRB S AMM SSI 5711591 0.50 B26501 0.50DETAILED INSPECTION OF BOTTOM SKIN AT FUELPUMP ATTACHMENT HOLES FROM RIB 14 TO 15ACCESS: 550BB* 1.50650BB* 1.50571159-0604-2 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 22600 FC MRB S AMM SSI 5711591 0.50 B4-1006501 0.50DETAILED INSPECTION OF BOTTOM SKIN AT FUELPUMP ATTACHMENT HOLES FROM RIB 14 TO 15* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 55APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571159-0604-2 * * * * * C O N T I N U E * * * * *ACCESS: 550BB* 1.50650BB* 1.50571159-0604-3 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 19200 FC MRB S AMM SSI 5711591 0.50 B4-2006501 0.50 C4DETAILED INSPECTION OF BOTTOM SKIN AT FUELF4PUMP ATTACHMENT HOLES FROM RIB 14 TO 15ACCESS: 550BB* 1.50650BB* 1.50571161-0604-1 523 FRONT SPAR JOINT PLATE INS. MEC DET I: 27300 FC MRB S AMM SSI 5711611 1.00 B26231 1.00DETAILED INSPECTION OF FRONT SPAR JOINT PLATEINSTALLATION AT RIB 9NOTE: HEAT SHIELD REMOVEDACCESS: 523CB* 0.13623CB* 0.13571161-0604-2 523 FRONT SPAR JOINT PLATE INS. MEC DET I: 22600 FC MRB S AMM SSI 5711611 1.00 B4-1006231 1.00DETAILED INSPECTION OF FRONT SPAR JOINT PLATEINSTALLATION AT RIB 9NOTE: HEAT SHIELD REMOVEDACCESS: 523CB* 0.13623CB* 0.13571161-0604-3 523 FRONT SPAR JOINT PLATE INS. MEC DET I: 19200 FC MRB S AMM SSI 5711611 1.00 B4-2006231 1.00 C4DETAILED INSPECTION OF FRONT SPAR JOINT PLATEF4INSTALLATION AT RIB 9NOTE: HEAT SHIELD REMOVEDACCESS: 523CB* 0.13* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 56APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571161-0604-3 * * * * * C O N T I N U E * * * * *623CB* 0.13571165-0604-1 575 BOTTOM SKIN AT ACCESS DOOR MEC DET I: 17700 FC MRB S AMM SSI 5711651 0.20 B26751 0.20DETAILED INSPECTION OF BOTTOM SKIN IN ACCESSDOOR AREA AFT OF REAR SPARNOTE: DOORS OPENEDACCESS: 575AB 575BB* 0.10675AB 675BB* 0.10571165-0604-2 575 BOTTOM SKIN AT ACCESS DOOR MEC DET I: 17700 FC MRB S AMM SSI 5711651 0.20 B4-1006751 0.20DETAILED INSPECTION OF BOTTOM SKIN IN ACCESSDOOR AREA AFT OF REAR SPARNOTE: DOORS OPENEDACCESS: 575AB 575BB* 0.10675AB 675BB* 0.10571165-0604-3 575 BOTTOM SKIN AT ACCESS DOOR MEC DET I: 15100 FC MRB S AMM SSI 5711651 0.20 B4-2006751 0.20 C4DETAILED INSPECTION OF BOTTOM SKIN IN ACCESSF4DOOR AREA AFT OF REAR SPARNOTE: DOORS OPENEDACCESS: 575AB 575BB* 0.10675AB 675BB* 0.10571167-0604-1 575 BOTTOM SKIN IN PYLON AREA MEC DET I: 27300 FC MRB S AMM SSI 5711671 0.20 B26751 0.20DETAILED INSPECTION OF BOTTOM SKIN INNERSURFACE IN PYLON FAIRING AREA AFT OF REAR SPARACCESS: 575BB* 0.06675BB* 0.06STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 57APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571167-0604-2 575 BOTTOM SKIN IN PYLON AREA MEC DET I: 22600 FC MRB S AMM SSI 5711671 0.20 B4-1006751 0.20DETAILED INSPECTION OF BOTTOM SKIN INNERSURFACE IN PYLON FAIRING AREA AFT OF REAR SPARACCESS: 575BB* 0.06675BB* 0.06571167-0604-3 575 BOTTOM SKIN IN PYLON AREA MEC DET I: 19200 FC MRB S AMM SSI 5711671 0.20 B4-2006751 0.20 C4DETAILED INSPECTION OF BOTTOM SKIN INNERF4SURFACE IN PYLON FAIRING AREA AFT OF REAR SPARACCESS: 575BB* 0.06675BB* 0.06571169-0602-1 575 BOTTOM SKIN IN BOOSTER BAY MEC DET I: 3000 FC MRB S AMM SSI 5711691 0.20 ALL6751 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN IN BOOSTER BAY REGION571173-0603-1 577 FLAP TRACK 1 BEAM EXTERIOR MEC DET I: 5 YE CPCP AMM SSI 5711731 0.30 ALL677 MRB S1 0.30DETAILED INSPECTION OF FLAP TRACK NO. 1 BEAM MRB REFERENCE:EXTERIOR571173-C603-1ACCESS: 577DT 577ET* 1.01677DT 677ET* 1.01571174-0603-1 577 FLAP TRACK 1 BEAM INTERIOR NDT BSI I: 5 YE CPCP AMM SSI 5711741 1.50 ALL677 MRB S NTM 5741111 1.50NDT INSPECTION OF FLAP TRACK NO.1 BEAM INTERIOR PART 7NOTE: TOP FRONT AND REAR ATTACH BOLTS OF AFT FITTING MRB REFERENCE:REMOVED571174-C603-1ACCESS: 577DT 577ET* 1.01677DT 677ET* 1.01STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 58APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571175-0603-1 571 WING INNER REAR SPAR AT BUILD SLOT NDT SDI T: 18000 FC CN NTM 5131041 1.00 B2671 I: 5000 FC FAA AD PART 11 1.00 PRE 11130SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105(57-221)WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1BOTTOM FACE BUILT SLOT. CN1994-207-168(B)ACCESS: 571AB FAA AD 95-24-04 * 0.10671AB ISB 57-0213* 0.10571175-0603-2 571 WING INNER REAR SPAR AT BUILD SLOT NDT SDI T: 19000 FC CN NTM 5131041 1.00 B4-100671 I: 6000 FC FAA AD PART 11 1.00 PRE 11130SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105(57-221)WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1BOTTOM FACE BUILT SLOT. CN1994-207-168(B)ACCESS: 571AB FAA AD 95-24-04 * 0.10671AB ISB 57-0213* 0.10571175-0603-3 571 WING INNER REAR SPAR AT BUILD SLOT NDT SDI T: 17000 FC CN NTM 5131041 1.00 B4-200671 I: 5000 FC FAA AD PART 11 1.00 C4SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105F4WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1PRE 11130BOTTOM FACE OF BUILD SLOT. CN(57-221)1994-207-168(B)ACCESS: 571AB FAA AD 95-24-04 * 0.10671AB ISB 57-0213* 0.10571175-0603-4 571 WING INNER REAR SPAR AT BUILD SLOT NDT SDI T: NOTE CN NTM 5131041 1.00 B2671 I: 5000 FC FAA AD PART 11 1.00 POST 11130SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105(57-221)WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1BOTTOM FACE OF BUILT SLOT. CN1994-207-168(B)NOTE: ON A/C ON WHICH SB 57-221 (MOD 11130) HAS FAA AD 95-24-04BEEN EMBODIED, NEXT INSPECTION IS DUE 33000 FC ISB 57-0213FROM TIME OF MOD EMBODIEMENT.ACCESS: 571AB* 0.10671AB* 0.10STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 59APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)571200-0603-1 520 WING LEADING EDGE - RIB 8 MEC DET T: 15000 FC ISB CN 83-102-53(B) 1 0.40 B2620 I: 3000 FC FAA AD 86-19-02 1 0.40 PRE 1307DETAILED INSPECTION OF BEND RADIUS OF THE ISB 57-0109LANDING ANGLE AT THE UPPER FLANGE OF THE NOSE RIBNO.8ACCESS: 523BB* 0.09623BB* 0.09571213-0603-1 543 WING - RIB 13 MEC DET T: 5800 FC ISB ISB 57-1811 1.00 PRE 8758643 I: 2900 FC1 1.00 (57-182)DETAILED INSPECTION OF WEB OF RIB 13 BETWEENSTRINGER 11 AND 12.ACCESS: 543CB 543DB* 3.00643CB 643DB* 3.00572003-0602-1 512 D-NOSE ASSEMBLY SKIN MEC DET I: 9000 FC MRB S AMM SSI 5720031 0.30 ALL6121 0.30DETAILED EXTERNAL INSPECTION OF D-NOSEASSEMBLY SKIN AND SUB SPAR, JACK AND TRACK APERTURE,JOINT PLATES, ATTACHMENTS AND FITTINGS AT INNERLEADING EDGENOTE: SLAT EXTENDED572004-0604-1 512 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720011 0.30 B2612 AMM SSI 5720041 0.30DETAILED INSPECTION OF INTERNAL D-NOSEASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS ANDINTERNAL SLAT FAIRING STRIP AT INNER LEADING EDGEACCESS: 512BB 512CB 512DB 512EB 512FB 512GB* 1.27512HB 512JB 512KB 512LB612BB 612CB 612DB 612EB 612FB 612GB* 1.24612HB 612JB 612KB 612LB572004-0604-2 512 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720011 0.30 B4-100612 AMM SSI 5720041 0.30DETAILED INSPECTION OF INTERNAL D-NOSEASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AND* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 60APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572004-0604-2 * * * * * C O N T I N U E * * * * *INTERNAL SLAT FAIRING STRIP AT INNER LEADING EDGEACCESS: 512BB 512CB 512DB 512EB 512FB 512GB* 1.27512HB 512JB 512KB 512LB612BB 612CB 612DB 612EB 612FB 612GB* 1.24612HB 612JB 612KB 612LB572004-0604-3 512 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720011 0.30 B4-200612 AMM SSI 5720041 0.30 C4DETAILED INSPECTION OF INTERNAL D-NOSEF4ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS ANDINTERNAL SLAT FAIRING STRIP AT INNER LEADING EDGEACCESS: 512BB 512CB 512DB 512EB 512FB 512GB* 1.27512HB 512JB 512KB 512LB612BB 612CB 612DB 612EB 612FB 612GB* 1.24612HB 612JB 612KB 612LB572015-0602-1 523 D-NOSE ASSY INTER.LEAD.EDGE MEC DET I: 3000 FC MRB S AMM SSI 5720151 0.20 ALL6231 0.20DETAILED EXTERNAL INSPECTION OF D-NOSEASSEMBLY SKIN AND SUB SPAR ATTACHMENTS, JACK ANDTRACK APERTURES, FITTINGS AND JOINT PLATES AT INTER-MEDIATE LEADING EDGE.PREP.: SLAT EXTENDED572016-0604-1 523 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720161 0.30 B26231 0.30DETAILED INSPECTION OF INTERNAL D-NOSEASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS ATINTERMEDIATE LEADING EDGEACCESS: 523AB 523BB 523CB 523DB 523EB 523FB* 1.11523GB 523HB 523JB 523KB 523LB 523MB623AB 623BB 623CB 623DB 623EB 623FB* 1.11623GB 623HB 623JB 623KB 623LB 623MBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 61APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572016-0604-2 523 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720161 0.30 B4-1006231 0.30DETAILED INSPECTION OF INTERNAL D-NOSEASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS ATINTERMEDIATE LEADING EDGEACCESS: 523AB 523BB 523CB 523DB 523EB 523FB* 1.11523GB 523HB 523JB 523KB 523LB 523MB623AB 623BB 623CB 623DB 623EB 623FB* 1.11623GB 623HB 623JB 623KB 623LB 623MB572016-0604-3 523 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720161 0.30 B4-2006231 0.30 C4DETAILED INSPECTION OF INTERNAL D-NOSEF4ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS ATINTERMEDIATE LEADING EDGEACCESS: 523AB 523BB 523CB 523DB 523EB 523FB* 1.11523GB 523HB 523JB 523KB 523LB 523MB623AB 623BB 623CB 623DB 623EB 623FB* 1.11623GB 623HB 623JB 623KB 623LB 623MB572021-0602-1 524 D-NOSE ASSY OUTER LEAD.EDGE MEC DET I: 9000 FC MRB S AMM SSI 5720211 0.20 ALL6241 0.20DETAILED EXTERNAL INSPECTION OF D-NOSEASSEMBLY SKIN AND SUB SPAR ATTACHMENTS, JACK ANDTRACK APERTURES, FITTINGS AND JOINT PLATES AT OUTERLEADING EDGENOTE: SLAT EXTENDED572022-0604-1 524 D-NOSE ASSY OUT.LEAD.EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720221 0.30 B26241 0.30DETAILED INSPECTION OF INTERNAL D-NOSEASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT OUTERLEADING EDGEACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 62APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572022-0604-2 524 D-NOSE ASSY OUT.LEAD.EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720221 0.30 B4-1006241 0.30DETAILED INSPECTION OF INTERNAL D-NOSEASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT OUTERLEADING EDGEACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KB572022-0604-3 524 D-NOSE ASSY OUT.LEAD.EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720221 0.30 B4-2006241 0.30 C4DETAILED INSPECTION OF INTERNAL D-NOSEF4ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT OUTERLEADING EDGEACCESS: 524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KB572063-0603-1 512 SLAT TRACK INNER LEADING EDGE MEC DET I: 6000 FC ALI CN 2006-0071(B) 1 0.50 ALL612 FAA AD 96-13-11 1 0.50 FROM 0 FC/FHDETAILED INSPECTION OF SLAT TRACK RIBS ANDTO LOVATTACHMENTS, INNER LEADING EDGE. ALI REFERENCE:572063-01-1ACCESS: 512BB 512EB 512FB 512JB 512KB* 0.69612BB 612EB 612FB 612JB 612KB* 0.69572065-0604-1 523 SLAT TRACK RIBS MEC DET I: 27300 FC MRB S AMM SSI 5720651 0.30 B26231 0.30DETAILED INSPECTION OF SLAT TRACK RIBS ANDATTACHMENTS OF INTERMEDIATE LEADING EDGEACCESS: 523BB 523CB 523EB 523FB 523HB 523JB* 0.92523LB 523MB623BB 623CB 623EB 623FB 623HB 623JB* 0.92623LB 623MBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 63APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572065-0604-2 523 SLAT TRACK RIBS MEC DET I: 22600 FC MRB S AMM SSI 5720651 0.30 B4-1006231 0.30DETAILED INSPECTION OF SLAT TRACK RIBS ANDATTACHMENTS OF INTERMEDIATE LEADING EDGEACCESS: 523BB 523CB 523EB 523FB 523HB 523JB* 0.92523LB 523MB623BB 623CB 623EB 623FB 623HB 623JB* 0.92623LB 623MB572065-0604-3 523 SLAT TRACK RIBS MEC DET I: 19200 FC MRB S AMM SSI 5720651 0.30 B4-2006231 0.30 C4DETAILED INSPECTION OF SLAT TRACK RIBS ANDF4ATTACHMENTS OF INTERMEDIATE LEADING EDGEACCESS: 523BB 523CB 523EB 523FB 523HB 523JB* 0.92523LB 523MB623BB 623CB 623EB 623FB 623HB 623JB* 0.92623LB 623MB572067-0604-1 524 SLAT TRACK OUTER LEAD.EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720671 0.30 B26241 0.30DETAILED INSPECTION OF SLAT TRACK RIBS ANDATTACHMENTS OF OUTER LEADING EDGEACCESS: 524BB 524CB 524EB 524FB 524GB 524HB* 1.10524KB624BB 624CB 624EB 624FB 624GB 624HB* 1.10624KB572067-0604-2 524 SLAT TRACK OUTER LEAD.EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720671 0.30 B4-1006241 0.30DETAILED INSPECTION OF SLAT TRACK RIBS AND:ATTACHMENTS OF OUTER LEADING EDGEACCESS: 524BB 524CB 524EB 524FB 524GB 524HB* 1.10524KB624BB 624CB 624EB 624FB 624GB 624HB* 1.10624KBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 64APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572067-0604-3 524 SLAT TRACK OUTER LEAD.EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720671 0.30 B4-2006241 0.30 C4DETAILED INSPECTION OF SLAT TRACK RIBS ANDF4ATTACHMENTS OF OUTER LEADING EDGEACCESS: 524BB 524CB 524EB 524FB 524GB 524HB* 1.10524KB624BB 624CB 624EB 624FB 624GB 624HB* 1.10624KB572069-0604-1 512 SLAT JACK AND PYLON RIBS MEC DET I: 27300 FC MRB S AMM SSI 5720691 0.20 B26121 0.20DETAILED INSPECTION OF SLAT JACK AND PYLONRIBS AND ATTACHMENTS OF INNER LEADING EDGEACCESS: 512BB 512CB 512DB 512GB 512HB 512JB* 0.92512KB612BB 612CB 612DB 612GB 612HB 612JB* 0.89612KB572069-0604-2 512 SLAT JACK AND PYLON RIBS MEC DET I: 22600 FC MRB S AMM SSI 5720691 0.20 B4-1006121 0.20DETAILED INSPECTION OF SLAT JACK AND PYLONRIBS AND ATTACHMENTS OF INNER LEADING EDGEACCESS: 512BB 512CB 512DB 512GB 512HB 512JB* 0.92512KB612BB 612CB 612DB 612GB 612HB 612JB* 0.89612KB572069-0604-3 512 SLAT JACK AND PYLON RIBS MEC DET I: 19200 FC MRB S AMM SSI 5720691 0.20 B4-2006121 0.20 C4DETAILED INSPECTION OF SLAT JACK AND PYLONF4RIBS AND ATTACHMENTS OF INNER LEADING EDGEACCESS: 512BB 512CB 512DB 512GB 512HB 512JB* 0.92512KB612BB 612CB 612DB 612GB 612HB 612JB* 0.89612KBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 65APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572071-0604-1 523 SLAT JACK RIBS INTER.L.EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720711 0.30 B26231 0.30DETAILED INSPECTION OF SLAT JACK RIBS ANDATTACHMENTS OF INTERMEDIATE LEADING EDGEACCESS: 523CB 523DB 523EB 523JB 523KB 523LB* 0.57623CB 623DB 623EB 623JB 623KB 623LB* 0.57572071-0604-2 523 SLAT JACK RIBS INTER.L.EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720711 0.30 B4-1006231 0.30DETAILED INSPECTION OF SLAT JACK RIBS ANDATTACHMENTS OF INTERMEDIATE LEADING EDGEACCESS: 523CB 523DB 523EB 523JB 523KB 523LB* 0.57623CB 623DB 623EB 623JB 623KB 623LB* 0.57572071-0604-3 523 SLAT JACK RIBS INTER.L.EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720711 0.30 B4-2006231 0.30 C4DETAILED INSPECTION OF SLAT JACK RIBS ANDF4ATTACHMENTS OF INTERMEDIATE LEADING EDGEACCESS: 523CB 523DB 523EB 523JB 523KB 523LB* 0.57623CB 623DB 623EB 623JB 623KB 623LB* 0.57572073-0604-1 524 SLAT JACK RIBS OUTER.L.EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720731 0.30 B26241 0.30DETAILED INSPECTION OF SLAT JACK RIBS ANDATTACHMENTS OF OUTER LEADING EDGEACCESS: 524CB 524DB 524EB 524HB 524JB 524KB* 0.76624CB 624DB 624EB 624HB 624JB 624KB* 0.76572073-0604-2 524 SLAT JACK RIBS OUTER.L.EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720731 0.30 B4-1006241 0.30DETAILED INSPECTION OF SLAT JACK RIBS ANDATTACHMENTS OF OUTER LEADING EDGEACCESS: 524CB 524DB 524EB 524HB 524JB 524KB* 0.76624CB 624DB 624EB 624HB 624JB 624KB* 0.76STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 66APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572073-0604-3 524 SLAT JACK RIBS OUTER.L.EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720731 0.30 B4-2006241 0.30 C4DETAILED INSPECTION OF SLAT JACK RIBS ANDF4ATTACHMENTS OF OUTER LEADING EDGEACCESS: 524CB 524DB 524EB 524HB 524JB 524KB* 0.76624CB 624DB 624EB 624HB 624JB 624KB* 0.76572075-0602-1 512 BOTTOM SKIN LEADING EDGE MEC DET I: 10100 FC MRB S AMM SSI 5720751 0.20 B26121 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN BETWEEN FRONT SPAR AND LEADING EDGE572075-0602-2 512 BOTTOM SKIN LEADING EDGE MEC DET I: 9900 FC MRB S AMM SSI 5720751 0.20 B4-1006121 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN BETWEEN FRONT SPAR AND LEADING EDGE572075-0602-3 512 BOTTOM SKIN LEADING EDGE MEC DET I: 9200 FC MRB S AMM SSI 5720751 0.20 B4-2006121 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOMF4SKIN BETWEEN FRONT SPAR AND LEADING EDGE572077-0602-1 523 BOTTOM SKIN INTER.LEAD.EDGE MEC DET I: 10100 FC MRB S AMM SSI 5720771 0.20 B26231 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN BETWEEN FRONT SPAR AND INTERMEDIATE LEADING EDGE572077-0602-2 523 BOTTOM SKIN INTER.LEAD.EDGE MEC DET I: 9700 FC MRB S AMM SSI 5720771 0.20 B4-1006231 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN BETWEEN FRONT SPAR AND INTERMEDIATE LEADING EDGE572077-0602-3 523 BOTTOM SKIN INTER.LEAD.EDGE MEC DET I: 9000 FC MRB S AMM SSI 5720771 0.20 B4-2006231 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOMF4SKIN BETWEEN FRONT SPAR AND INTERMEDIATE LEADING EDGESTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 67APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572079-0602-1 524 BOTTOM SKIN OUTER LEAD.EDGE MEC DET I: 9700 FC MRB S AMM SSI 5720791 0.20 B26241 0.20DETAILED VISUAL EXTERNAL INSPECTION OF BOTTOMSKIN BETWEEN FRONT SPAR AND OUTER LEADING EDGE572079-0602-2 524 BOTTOM SKIN OUTER LEAD.EDGE MEC DET I: 9500 FC MRB S AMM SSI 5720791 0.20 B4-1006241 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN BETWEEN FRONT SPAR AND OUTER LEADING EDGE572079-0602-3 524 BOTTOM SKIN OUTER LEAD.EDGE MEC DET I: 9200 FC MRB S AMM SSI 5720791 0.20 B4-2006241 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOMF4SKIN BETWEEN FRONT SPAR AND OUTER LEADING EDGE572081-0602-1 581 BOTT.SKIN AFT OF REAR SPAR MEC DET I: 10100 FC MRB S AMM SSI 5720811 0.20 B26811 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN AFT OF REAR SPAR FROM RIB 9 TO 29572081-0602-2 581 BOTT.SKIN AFT OF REAR SPAR MEC DET I: 9700 FC MRB S AMM SSI 5720811 0.20 B4-1006811 0.20DETAILED EXTERNAL INSPECTION OF BOTTOMSKIN AFT OF REAR SPAR FROM RIB 9 TO 29572081-0602-3 581 BOTT.SKIN AFT OF REAR SPAR MEC DET I: 9000 FC MRB S AMM SSI 5720811 0.20 B4-2006811 0.20 C4DETAILED EXTERNAL INSPECTION OF BOTTOMF4SKIN AFT OF REAR SPAR FROM RIB 9 TO 29572085-0604-1 591 TRAILING EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720851 0.30 B26911 0.30DETAILED INSPECTION OF "A" FRAMES, TIE BEAM,CANTILEVERS AND HINGE BRACKETS IN TRAILING EDGEACCESS: 591BB 591CB 591DB* 0.15691BB 691CB 691DB* 0.22STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 68APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572085-0604-2 591 TRAILING EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720851 0.30 B4-1006911 0.30DETAILED INSPECTION OF "A" FRAMES, TIE BEAM,CANTILEVERS AND HINGE BRACKETS IN TRAILING EDGEACCESS: 591BB 591CB 591DB* 0.15691BB 691CB 691DB* 0.22572085-0604-3 591 TRAILING EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720851 0.30 B4-2006911 0.30 C4DETAILED INSPECTION OF "A" FRAMES, TIE BEAM,F4CANTILEVERS AND HINGE BRACKETS IN TRAILING EDGEACCESS: 591BB 591CB 591DB* 0.15691BB 691CB 691DB* 0.22572089-0604-1 581 AIRBRAKE AND SPOILER HINGE MEC DET I: 27300 FC MRB S AMM SSI 5720891 0.30 B26811 0.30DETAILED INSPECTION OF AIRBRAKE AND SPOILERHINGE AND JACK RIBS AT TRAILING EDGEACCESS: 581CB 581DB 581EB 581FB 581GB 581HB* 0.35581JB 581KB681CB 681DB 681EB 681FB 681GB 681HB* 0.35681JB 681KB572089-0604-2 581 AIRBRAKE AND SPOILER HINGE MEC DET I: 22600 FC MRB S AMM SSI 5720891 0.30 B4-1006811 0.30DETAILED INSPECTION OF AIRBRAKE AND SPOILERHINGE AND JACK RIBS AT TRAILING EDGEACCESS: 581CB 581DB 581EB 581FB 581GB 581HB* 0.35581JB 581KB681CB 681DB 681EB 681FB 681GB 681HB* 0.35681JB 681KB572089-0604-3 581 AIRBRAKE AND SPOILER HINGE MEC DET I: 19200 FC MRB S AMM SSI 5720891 0.30 B4-2006811 0.30 C4DETAILED INSPECTION OF AIRBRAKE AND SPOILERF4HINGE AND JACK RIBS AT TRAILING EDGE* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 69APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572089-0604-3 * * * * * C O N T I N U E * * * * *ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB* 0.35581JB 581KB681CB 681DB 681EB 681FB 681GB 681HB* 0.35681JB 681KB572090-0603-1 570 OUT.SHROUD BOX HNG.BRACKETS MEC DET T: 5000 FC ISB CN1 4.00 PRE 06661670 I: 1000 FC 1998-449-265(B) 1 4.00 (57-0143)DETAILED INSPECTION OF OUTER SHROUD BOX AFT FAA AD 90-11-05HINGE BRACKETS. ISB 57-0142PREP: FLAPS EXTENDEDINNER AIRBRAKES DEPLOYEDACCESS: 577CT 577DT* 1.13677CT 677DT* 1.13572090-0604-1 575 LOWER SKIN PANEL INBOARD OF RIB 9 AND NDT SDI T: SEE SB AD NTM 5700011 1.50 ALL675 AFT OF REAR SPAR I: SEE SB SB PART 61 1.50 SB 57-0177NTM 573319SPECIAL DETAILED INSPECTION OF BOTTOM SKIN PANEL PART 2INBOARD OF RIB 9 AND AFT OF REAR SPAR. AD 2008-06-18SB 57-0177ACCESS: 575FB* 0.09675FB* 0.09572090-0604-2 575 LOWER SKIN PANEL INBOARD OF RIB 9 AND MEC DET T: SEE SB AD AD 2008-06-181 0.30 ALL675 AFT OF REAR SPAR I: SEE SB SB SB 57-01771 0.30DETAILED VISUAL INSPECTION OF BOTTOM SKIN PANELINBOARD OF RIB 9 AND AFT OF REAR SPAR.ACCESS: 575FB* 0.09675FB* 0.09572091-0604-1 572 INNER AIRBRAKE HINGE BOLTS MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL672 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF INNER AIRBRAKE HINGE 572091-C604-1BOLTS SINGLE HINGE POSITIONS.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 70APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572091-0604-1 * * * * * C O N T I N U E * * * * *PREP: FLAPS EXTENDEDREMOVE MOVABLE HINGE BRACKET FAIRINGS AND BOLTS572092-0604-1 572 INNER AIRBRAKE HINGE BOLTS NDT SDI I: 17700 FC MRB S AMM SSI 5720921 2.00 B2672 NTM 5754121 2.00SPECIAL DETAILED INSPECTION OF INNER AIRBRAKE HINGE PART 8BOLTS (DOUBLE HINGE POSITION).NOTE: DOUBLE HINGE BOLTS REMOVED572092-0604-2 572 INNER AIRBRAKE HINGE BOLTS NDT SDI I: 17700 FC MRB S AMM SSI 5720921 2.00 B4-100672 NTM 5754121 2.00SPECIAL DETAILED INSPECTION OF INNER AIRBRAKE HINGE PART 8BOLTS (DOUBLE HINGE POSITION).NOTE: DOUBLE HINGE BOLTS REMOVED572092-0604-3 572 INNER AIRBRAKE HINGE BOLTS NDT SDI I: 15100 FC MRB S AMM SSI 5720921 2.00 B4-200672 NTM 5754121 2.00 C4SPECIAL DETAILED INSPECTION OF INNER AIRBRAKE HINGE PART 8F4BOLTS (DOUBLE HINGE POSITIONS).NOTE: DOUBLE HINGE BOLTS REMOVED572093-0604-1 582 AIRBRAKES, SPOILER ACTUATOR BRACKETS NDT SDI T: 48000 FC ALI NTM 5720931 TBD ALL583 I: 5500 FC PART 61 TBD FROM 0 FC/FH584 SPECIAL DETAILED INSPECTION OF OUTER AIRBRAKES AND EASA AD1 TBD TO LOV682 SPOILER 3 ACTUATOR BRACKET LUGS. 2006-00711 TBD683 FAA AD1 TBD684 PREP.: DETACH JACK ATTACHMENT 2007-04-111 TBDALI REFERENCE:572093-01-1572094-0604-1 582 AIRBRAKES, SPOILER ACTUATOR BRACKETS NDT SDI T: 48000 FC ALI NTM 5720941 TBD ALL583 I: 10000 FC PART 81 TBD FROM 0 FC/FH584 SPECIAL DETAILED INSPECTION OF OUTER AIRBRAKES AND EASA AD1 TBD TO LOV682 SPOILER 3 JACK ATTACHMENT PIN. 2006-00711 TBD* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 71APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572094-0604-1 * * * * * C O N T I N U E * * * * *683 FAA AD1 TBD684 PREP.: DETACH JACK ATTACHMENT 2007-04-111 TBDALI REFERENCE:572094-01-1572095-0604-1 576 ALL SPEED AILERON MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL676 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF ALL SPEED AILERON 572095-C604-1HINGE BOLTS.PREP: REMOVE BOLTSACCESS: 575CB 575CT 575GB 576AB 576BB 576CB* 0.61576DB 576EB675CB 675CT 675GB 676AB 676BB 676CB* 0.61676DB 676EB572099-0604-1 581 AIRBRAKES AND SPOILERS MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL681 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF AIRBRAKE AND SPOILER 572099-C604-1HINGE BOLTSPREP: EXTEND FLAPS, SPOILERS AND AIRBRAKESACCESS: 581AT 581BT 581CT 581ET* 0.10681AT 681BT 681CT 681ET* 0.10572103-0604-1 592 LOW SPEED AILERON MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL692 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF LOW SPEED AILERON HINGE 572103-C604-1BOLTSPREP: REMOVE BOLTSACCESS: 591AB 591BB 591CB 591DB 591EB 591FB* 0.70591GB 591HB 592AT 592BB691AB 691AT 691BB 691BT 691CB 691DB* 1.00691EB 691FB 691GB 691HB 692AT 692BBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 72APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572105-0604-1 591 LOW SPEED AILERON MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL691 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF LOW SPEED AILERON 572105-C604-1CANTILEVERS CENTRE AND OUTER FAILSAFE ATTACHMENTBOLTSPREP: REMOVE BOLTSACCESS: 591CB 591DB* 0.09691CB 691DB* 0.16572107-0603-1 581 QUADRANT AIRBRAKE CONTROL MEC DET I: 6000 FC MRB S AMM SSI 5721071 0.20 ALL6811 0.20DETAILED INSPECTION OF QUADRANT AIRBRAKECONTROL AT RIB 14ACCESS: FLAPS EXTENDED572109-0604-1 577 FLAP MEC DET T: 20 YE CPCP1 TBD ALL677 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572109-C604-1OF THE NO.1 TRACK BEAM FORWARD ATTACHMENTPREP: LOWER THE FLAPSREMOVE BOLTS AND BUSH572111-0604-1 577 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL677 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572111-C604-1OF THE BEAM NO.1 AFT ATTACHMENTPREP: LOWER THE FLAPSREMOVE BOLTS AND BUSH572113-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL632 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF FAILSAFE BOLT OF THE 572113-C604-1NO.2 FLAP TRACK BEAM FORWARD ATTACHMENTPREP: REMOVE FIXED FAIRING AND BOLTSSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 73APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572115-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL632 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF THE FAILSAFE PINS OF 572115-C604-1THE NO.2 FLAP TRACK BEAM FORWARD ATTACHMENTPREP: REMOVE FIXED FAIRING AND PINS572117-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL632 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF FAILSAFE BOLT AND BUSH 572117-C604-1OF THE NO.2 FLAP TRACK FRONT CARRIAGE TO REARCARRIAGE ATTACHMENTPREP: LOWER THE FLAPSREMOVE BOLT AND BUSH572119-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL632 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572119-C604-1OF THE NO.2 FLAP TAB ROD TO REAR CARRIAGE ATTACHMENTNOTE: LOWER THE FLAPSREMOVE BOLT AND BUSH572121-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL632 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572121-C604-1OF THE NO.2 FLAP TAB ROD AT THE TAB CONNECTIONPREP: LOWER THE FLAPSREMOVE BOLT AND BUSH572123-0604-1 533 BOLT FWD FLAP TRACK NO.3 NDT SDI I: 27300 FC MRB S AMM SSI 5721231 1.00 B2633 NTM 5741111 1.00SPECIAL DETAILED INSPECTION OF FAILSAFE BOLT OF TRACK PART 8BEAM NO.3 FORWARD ATTACHMENTNOTE: BOLT REMOVEDACCESS: 533AF* 0.33633AF* 0.33STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 74APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572123-0604-2 533 BOLT FWD FLAP TRACK NO.3 NDT SDI I: 22600 FC MRB S AMM SSI 5721231 1.00 B4-100633 NTM 5741111 1.00SPECIAL DETAILED INSPECTION OF FAILSAFE BOLT OF TRACK PART 8BEAM NO.3 FORWARD ATTACHMENTNOTE: BOLT REMOVEDACCESS: 533AF* 0.33633AF* 0.33572123-0604-3 533 BOLT FWD FLAP TRACK NO.3 NDT SDI I: 19200 FC MRB S AMM SSI 5721231 1.00 B4-200633 NTM 5741111 1.00 C4SPECIAL DETAILED INSPECTION OF FAILSAFE BOLT OF TRACK PART 8F4BEAM NO.3 FORWARD ATTACHMENTNOTE: BOLT REMOVEDACCESS: 533AF* 0.33633AF* 0.33572125-0604-1 530 BOLT FORWARD FLAP TRACK NO4/5/6 NDT SDI I: 17700 FC MRB S AMM SSI 5721251 1.50 B2630 NTM 5741111 1.50SPECIAL DETAILED INSPECTION OF FAILSAFE BOLTS OF PART 8TRACK BEAMS 4,5,6 FWD ATTACHMENTNOTE: BOLTS REMOVEDACCESS: 534AF 535AF 536AF* 1.00634AF 635AF 636AF* 1.00572125-0604-2 530 BOLT FORWARD FLAP TRACK NO4/5/6 NDT SDI I: 17700 FC MRB S AMM SSI 5721251 1.50 B4-100630 NTM 5741111 1.50SPECIAL DETAILED INSPECTION OF FAILSAFE BOLTS OF PART 8TRACK BEAMS 4,5,6 FWD ATTACHMENTNOTE: BOLTS REMOVEDACCESS: 534AF 535AF 536AF* 1.00634AF 635AF 636AF* 1.00STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 75APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572125-0604-3 530 BOLT FORWARD FLAP TRACK NO4/5/6 NDT SDI I: 15100 FC MRB S AMM SSI 5721251 1.50 B4-200630 NTM 5741111 1.50 C4SPECIAL DETAILED INSPECTION OF FAILSAFE BOLTS OF PART 8F4TRACK BEAMS 4,5,6 FWD ATTACHMENTNOTE: BOLTS REMOVEDACCESS: 534AF 535AF 536AF* 1.00634AF 635AF 636AF* 1.00572127-0604-1 533 FLAP TRACK BEAMS MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL534 I: 10 YE MRB S1 TBD535 DETAILED INSPECTION OF FAILSAFE PINS OF THE NO 572127-C604-11 TBD633 3,4 AND 5 FLAP TRACK BEAMS FORWARD ATTACHMENT.1 TBD6341 TBD635 PREP: REMOVE FIXED FAIRING AND PINS1 TBD572129-0604-1 536 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL636 I: 10 YE MRB S1 TBDDETAILED INSPECTION OF FAILSAFE PINS OF THE 572129-C604-1NO.6 FLAP TRACK BEAMS FORWARD ATTACHMENTPREP: REMOVE FIXED FAIRINGS AND PINS572131-0604-1 533 FLAP MEC DET T: 20 YE CPCP MRB REFERENCE: 1 TBD ALL534 I: 10 YE MRB S1 TBD535 DETAILED INSPECTION OF PIN AND HOLLOW PIN OF 572131-C604-11 TBD536 THE FLAP TRACK 3, 4, 5 AND 6 CARRIAGES1 TBD6331 TBD634 PREP REMOVE THE FIXED FAIRING AND PINS1 TBD6351 TBD6361 TBD572199-0603-1 513 FORWARD WING MEC DET T: 10 YE CPCP MRB REFERENCE: 1 TBD ALL613 I: 5 YE MRB S1 TBDDETAILED INSPECTION OF THE OUTER WING TOP SKIN 572199-C603-1UPPER SURFACE FORWARD OF FRONT SPAR AT WING ROOT AREAUNDER FORWARD WING TO FUSELAGE FAIRINGPREP.: FORWARD WING TO FUSELAGE FAIRINGS TO BEREMOVEDSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 76APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)572512-0603-1 500 WING FLAP TRACKS MEC DET I: 12000 FC ISB ISB 57-0911 2.00 PRE 29736001 2.00DETAILED INSPECTION OF FLAP TRACK NO. 3, 4,5 AND 6.PREP: REMOVE MOVABLE FAIRINGS AT REAR ENDSET FLAPS TO RET (1ST NOTCH) POSITION572512-0603-2 532 WING FLAP TRACKS NDT SDI I: ISB ISB NTM 5725111 3.00 ALL632 57-116 PART 41 3.00SPECIAL DETAILED INSPECTION OF FLAP BEAM NO. 2 SIDE NTM 572512AND BASE MEMBERS FOR CRACKS PART 4CNACCESS: 532AF 532AM 1986-187-076(B) * 0.67632AF 632AM FAA AD 95-21-09 * 0.67ISB 57-116572512-0603-3 500 WING FLAP TRACKS MEC DET T: 6000 FC ISB ISB 57-2191 1.00 PRE 2973600 I: 4000 FC1 1.00 PRE 11058DETAILED INSPECTION OF FLAP TRACK NO.2(57-220)PREP: REMOVE MOVABLE FAIRINGS AT FLAP TRACK NO.2SET FLAPS TO THE RET (1ST NOTCH) POSITION572512-0603-4 500 WING FLAP TRACKS MEC DET T: 12000 FC ISB ISB 57-2191 1.00 PRE 2973600 I: 12000 FC1 1.00 POST 11058DETAILED INSPECTION OF FLAP TRACK NO.2(57-220)PREP: REMOVE MOVABLE FAIRINGS AT FLAP TRACK NO.2SET FLAPS TO THE RET (1ST NOTCH) POSITION574111-0603-1 470 REAR ATTACH.-WING TO PYLON NDT SDI I: 6000 FH ISB NTM 5741111 0.50 ALL480 PART 41 0.50SPECIAL DETAILED INSPECTION OF LUGS OF WING TO PYLON ISB 57-115REAR ATTACHMENT FITTING FOR CRACKSACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 77APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)574112-0603-1 470 PYLON SPIGOT FITTING NDT SDI I: 6000 FH ISB NTM 5741121 0.50 ALL480 PART 41 0.50SPECIAL DETAILED INSPECTION OF PYLON SPIGOT FITTING ISB 57-115FOR CRACKSACCESS: 471BL 472BR* 0.27481BL 482BR* 0.29574113-0603-1 471 WINGS-PYLON THRUST AND SIDELOAD FITTING MEC DET T: 2800 FC AD AD EASA AD1 0.50 ALL481 I: 2800 FC ISB 2007-02431 0.50DETAILED INSPECTION OF PYLON THRUST AND AD 2009-01-08SIDELOAD FITTING (SPIGOT) CN1997-358-232(B)PREP: BLEED AIR DUCT TO BE REMOVED ISB 57-0232ACCESS: 471BL 472BR* 0.27481BL 482BR* 0.29574211-0602-1 571 ATTACHMENT - MAIN GEAR NDT SDI I: 400 FC ISB NTM 5733101 0.50 PRE 02437671 ISB 57-0851 0.50 (57-0088)SPECIAL DETAILED INSPECTION OF MLG ACTUATING CYLINDERATTACHMENT FITTING BOLTS (LOCATED ON TOP SKIN BETWEENRIB 5 AND REAR SPAR)R 574212-0602-1 571 WINGS - TRAILING EDGE MEC DET T: 400 FC AD AD 2006-12-131 0.16 POST 11932671 I: 400 FC CN CN 2009-00811 0.16 (57-0235)DETAILED INSPECTION OF MAIN LANDING GEAR RIB 5 EUAD EUAD F-2003-318ATTACHMENT FITTING LOWER FLANGE FOR CRACKS. FAA AD FAA ADISB 2000-05-07PREP.:REMOVE MAIN LANDING GEAR ACTUATING CYLINDER OIT ISB 57A0246ASSEMBLY AND DISCONNECT HYDRAULIC PIPES. OIT9991.0017 09ACCESS: 575AB* 0.04675AB* 0.04R 574212-0602-2 571 WINGS - TRAILING EDGE NDT SDI T: 400 FC AD NTM 5131041 2.00 POST 11932671 I: 400 FC CN PART 11 2.00 (57-0235)SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR EUAD NTM 516000RIB 5 ATTACHMENT FITTING LOWER FLANGE. FAA AD PART 1ISB NTM 516001PREP.:REMOVE MAIN LANDING GEAR ACTUATING CYLINDER OIT PART 1* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 78APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)574212-0602-2 * * * * * C O N T I N U E * * * * *ASSEMBLY AND DISCONNECT HYDRAULIC PIPES. AD 2006-12-13CN 2009-0081ACCESS: 575AB EUAD F-2003-318 * 0.04675AB FAA AD* 0.042000-05-07ISB 57A0246OIT9991.0017 09R 574212-0602-3 571 WINGS - TRAILING EDGE MEC DET T: SEE ISB EUAD EUAD F-2005-113 1 2.00 PRE 11932671 I: SEE ISB FAA AD FAA AD1 2.00 (57-0235)DETAILED INSPECTION OF MAIN LANDING GEAR RIB 5 ISB 2006-12-13ATTACHMENT FITTING LOWER FLANGE FOR CRACKS. ISB 57A0234PREP.:REMOVE MAIN LANDING GEAR ACTUATING CYLINDERASSEMBLY AND DISCONNECT HYDRAULIC PIPES.ACCESS: 575AB* 0.04675AB* 0.04R 574212-0602-4 571 WINGS - TRAILING EDGE NDT SDI T: SEE ISB EUAD NTM 5131041 2.00 PRE 11932671 I: SEE ISB FAA AD PART 11 2.00 (57-0235)SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR RIB ISB NTM 5742125 ATTACHMENT FITTING LOWER FLANGE. PART 6EUAD F-2005-113PREP.:REMOVE MAIN LANDING GEAR ACTUATING CYLINDER FAA ADASSEMBLY AND DISCONNECT HYDRAULIC PIPES. 2006-12-13ISB 57A0234ACCESS: 575AB* 0.04675AB* 0.04574300-0603-1 581 SPOILER JACK ATTACHMENTS MEC DET T: ISB ISB AMM 276151/4031 6.00 PRE 05132681 57-133 ISB 57-1331 6.00 (57-0134)DETAILED INSPECTION OF THE BEAM ASSEMBLY I: 3000 FHATTACHMENT BOLTS OF OUTER AIRBRAKE AND SPOILER FORLOOSENESS OR FAILUREACCESS: 581CB 581DB 581EB 581FB 581GB 581HB* 0.35581JB 581KB681CB 681DB 681EB 681FB 681GB 681HB* 0.35* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 79APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)574300-0603-1 * * * * * C O N T I N U E * * * * *681JB 681KB575001-0603-1 511 SLAT TRACK 1 NDT SDI I: 11100 FC MRB S AMM SSI 5750011 2.00 ALL611 NTM 5758101 2.00SPECIAL DETAILED INSPECTION OF SLAT TRACK NO.1 AT PART 6LOCATION OF FIRST LOWER ROLLER WHEN RETRACTEDNOTE: SLAT EXTENDED575005-0603-1 511 SLAT TRACK 3 NDT SDI I: 11100 FC MRB S AMM SSI 5750051 2.00 ALL611 NTM 5758111 2.00SPECIAL DETAILED INSPECTION OF SLAT TRACK NO.3 AT PART 6LOCATION OF FIRST LOWER ROLLER WHEN RETRACTEDNOTE: SLAT EXTENDED575009-0604-1 511 SLAT RIB LOWER LUG NDT SDI I: 17700 FC MRB S AMM SSI 5750091 2.00 B2611 NTM 5758101 2.00SPECIAL DETAILED INSPECTION OF SLAT RIB LOWER LUG AT PART 6ATTACHMENT TO TRACKS 1 AND 3 NTM 575811PART 6NOTE: SLAT EXTENDED,TRACK AND BEARING HOUSING REMOVED575009-0604-2 511 SLAT RIB LOWER LUG NDT SDI I: 17700 FC MRB S AMM SSI 5750091 2.00 B4-100611 NTM 5758101 2.00SPECIAL DETAILED INSPECTION OF SLAT RIB LOWER LUG AT PART 6ATTACHMENT TO TRACKS 1 AND 3 NTM 575811PART 6NOTE: SLAT EXTENDED,TRACK AND BEARING HOUSING REMOVED575009-0604-3 511 SLAT RIB LOWER LUG NDT SDI I: 15100 FC MRB S AMM SSI 5750091 2.00 B4-200611 NTM 5758101 2.00 C4SPECIAL DETAILED INSPECTION OF SLAT RIB LOWER LUG AT PART 6F4ATTACHMENT TO TRACKS 1 AND 3* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 80APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575009-0604-3 * * * * * C O N T I N U E * * * * *NTM 575811NOTE: SLAT EXTENDED,TRACK AND BEARING HOUSING REMOVED PART 6575010-0603-1 511 SLAT 1 TRACKS 1 TO 3 NDT SDI T: 10 YE CPCP NTM 5750101 TBD ALL611 I: 5 YE PART 81 TBDSPECIAL DETAILED INSPECTION OF SLAT 1 TRACKS 1 TO 3MRB REFERENCE:NOTE: SLAT EXTENDED, SUCCESSIVE REMOVAL OF PINS AND 575010-C603-1SLEEVES.575011-0602-1 511 SLAT RIB LUGS & SKIN MEC DET I: 8300 FC MRB S AMM SSI 5750111 0.20 ALL6111 0.20DETAILED INSPECTION OF SLAT RIB UPPERLUGS AT ATTACHMENT TO TRACKS 1 AND 3NOTE: SLAT EXTENDED575013-0603-1 511 SLAT RIB LOWER LUG MEC DET I: 11100 FC MRB S AMM SSI 5750131 0.33 ALL6111 0.33DETAILED INSPECTION OF SLAT RIB LOWER LUG ATATTACHMENT TO TRACK 2.NOTE: SLAT EXTENDED, DETACH FAIRING PLATE575015-0604-1 511 SLAT RIB UPPER LUG-TRACK 2 NDT SDI I: 27300 FC MRB S AMM SSI 5750151 1.00 B2611 NTM 5758121 1.00SPECIAL DETAILED INSPECTION OF SLAT RIB UPPER LUG PART 6ATTACHMENT TO TRACK NO.2NOTE: SLAT IN EXTENDED POSITION, TRACK DETACHEDFROM LUGS AND BEARING HOUSING REMOVED575015-0604-2 511 SLAT RIB UPPER LUG-TRACK 2 NDT SDI I: 22600 FC MRB S AMM SSI 5750151 1.00 B4-100611 NTM 5758121 1.00SPECIAL DETAILED INSPECTION OF SLAT RIB UPPER LUG PART 6* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 81APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575015-0604-2 * * * * * C O N T I N U E * * * * *ATTACHMENT TO TRACK NO.2NOTE: SLAT IN EXTENDED POSITION, TRACK DETACHEDFROM LUGS AND BEARING HOUSING REMOVED575015-0604-3 511 SLAT RIB UPPER LUG-TRACK 2 NDT SDI I: 19200 FC MRB S AMM SSI 5750151 1.00 B4-200611 NTM 5758121 1.00 C4SPECIAL DETAILED INSPECTION OF SLAT RIB UPPER LUG PART 6F4ATTACHMENT TO TRACK NO.2NOTE: SLAT IN EXTENDED POSITION, TRACK DETACHEDFROM LUGS AND BEARING HOUSING REMOVED575017-0603-1 511 SLAT RIB LUGS AT ATT. MEC DET I: 11100 FC MRB S AMM SSI 5750171 0.33 ALL6111 0.33DETAILED INSPECTION OF SLAT RIB LUGS ATATTACHMENT TO JACKS 1 AND 2.NOTE: SLAT EXTENDED, DETACH FORK ATTACHMENT575021-0604-1 511 SLAT SKIN, AREA OF TRACK 2 NDT SDI T: 36500 FC ALI NTM 5758131 1.00 ALL611 I: 9000 FC PART 61 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF SLAT 1 SKIN AT TRACK EASA ADTO LOVRIB 2. 2006-0071FAA ADPREP.: SLAT EXTENDED 2007-04-11ALI REFERENCE:575021-01-1575023-0603-1 511 SLAT 1 LOWER SKIN NDT SDI I: 11100 FC MRB S AMM SSI 5750231 1.00 ALL611 NTM 5758141 1.00SPECIAL DETAILED INSPECTION OF SLAT LOWER SKIN IN PART 6AREA OF LOWER GIRDER OF AUXILIARY SPAR AT RIB 20STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 82APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575027-0602-1 511 LUGS OF HINGE BRACK. SLAT 1 MEC DET I: 5500 FC MRB S AMM SSI 5750271 0.20 ALL6111 0.20DETAILED INSPECTION OF EXTERNAL LUGS OFHINGE BRACKET AT RIB 21 OF SLAT 1NOTE: SLAT EXTENDED575051-0604-1 521 SLAT RIB LUGS MEC DET I: 27300 FC MRB S AMM SSI 5750511 0.20 B26211 0.20DETAILED INSPECTION OF SLAT RIB LUGS ATATTACHMENT TO TRACKS 4 TO 7 AND JACKS 3 AND 4.NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGSAND FORK ATTACHMENT AT JACK RIB LUGS DETACHED575051-0604-2 521 SLAT RIB LUGS MEC DET I: 22600 FC MRB S AMM SSI 5750511 0.20 B4-1006211 0.20DETAILED INSPECTION OF SLAT RIB LUGS ATATTACHMENT TO TRACKS 4 TO 7 AND JACKS 3 AND 4.NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGSAND FORK ATTACHMENT AT JACK RIB LUGS DETACHED575051-0604-3 521 SLAT RIB LUGS MEC DET I: 19200 FC MRB S AMM SSI 5750511 0.20 B4-2006211 0.20 C4DETAILED INSPECTION OF SLAT RIB LUGS ATF4ATTACHMENT TO TRACKS 4 TO 7 AND JACKS 3 AND 4.NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGSAND FORK ATTACHMENT AT JACK RIB LUGS DETACHED575061-0604-1 521 SLAT SKIN, AREA OF TRACK 5 AND 6 NDT SDI T: 27000 FC ALI NTM 5759101 2.00 ALL621 I: 2800 FC PART 61 2.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF SLAT 2 SKIN IN AREA OF EASA ADTO LOVTRACK RIBS 5, 6 AND 7 AT THE ATTACHMENT OF THE LOWER 2006-0071GIRDER. FAA AD2007-04-11PREP.: SLAT EXTENDEDALI REFERENCE:575061-01-1STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 83APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575081-0604-1 522 SLAT RIB LUGS AT ATTACHMENT MEC DET I: 27300 FC MRB S AMM SSI 5750811 0.20 B26221 0.20DETAILED INSPECTION OF SLAT RIB LUGS ATATTACHMENT TO TRACKS 8 TO 11 AND JACKS 5 AND 6NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGSAND FORK ATTACHMENTS AT JACK RIB LUGS DETACHED575081-0604-2 522 SLAT RIB LUGS AT ATTACHMENT MEC DET I: 22600 FC MRB S AMM SSI 5750811 0.20 B4-1006221 0.20DETAILED INSPECTION OF SLAT RIB LUGS ATATTACHMENT TO TRACKS 8 TO 11 AND JACKS 5 AND 6NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGSAND FORK ATTACHMENTS AT JACK RIB LUGS DETACHED575081-0604-3 522 SLAT RIB LUGS AT ATTACHMENT MEC DET I: 19200 FC MRB S AMM SSI 5750811 0.20 B4-2006221 0.20 C4DETAILED INSPECTION OF SLAT RIB LUGS ATF4ATTACHMENT TO TRACKS 8 TO 11 AND JACKS 5 AND 6NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGSAND FORK ATTACHMENTS AT JACK RIB LUGS DETACHED575082-0604-1 521 SLAT 2 AND SLAT 3 NDT SDI T: 10 YE EUAD NTM 5750821 TBD ALL522 I: 5 YE PART 21 TBD621 SPECIAL DETAILED INSPECTION OF SLAT 2 AND 3, SLEEVES EUAD 2006-00711 TBD622 UPPER AND LOWER LUG, ECCENTRIC BOLT AT TRACKS 4 TO 111 TBDMRB REFERENCE:PREP.: SLAT EXTENDET, SUCCESSIVE REMOVAL OF PINS 575082-C604-1AND SLEEVES.575087-0604-1 522 SLAT SKIN, AREA OF TRACK 9 NDT SDI T: 27000 FC ALI NTM 5759121 1.00 ALL622 I: 2800 FC PART 61 1.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF SLAT 3 SKIN IN AREA OF EASA ADTO LOVHORIZONTAL FLANGES OF TRACK RIBS 8, 9 AND 10 AT THE 2006-0071ATTACHMENT OF THE LOWER GIRDER. FAA AD2007-04-11PREP.: SLAT EXTENDEDALI REFERENCE:575087-01-1STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 84APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575088-0604-1 521 SLAT SKIN, AREA OF TRACKS AND JACKS NDT SDI T: 35000 FC ALI NTM 5750881 TBD ALL522 I: 6000 FC PART 61 TBD FROM 0 FC/FH621 SPECIAL DETAILED INSPECTION OF TRAILING EDGE SKIN AT EASA AD1 TBD TO LOV622 TRACK 5, 6, 9 AND 10 AND JACK 4 AND 5. INSPECT FOR 2006-00711 TBDCRACKS FROM FASTENER HOLE TO THE EDGE OF SKIN. (25 CM FAA ADON BOTH SIDES OF JACKS AND TRACKS) 2007-04-11PREP.: SLAT EXTENDED ALI REFERENCE:575088-01-1575101-0604-1 574 LUGS FWD HINGE FLAP TRACK 1 NDT SDI I: 17700 FC MRB S AMM SSI 5751011 2.00 B2674 NTM 5751101 2.00SPECIAL DETAILED INSPECTION OF LUGS OF FORWARD HINGE PART 4BRACKET OF INNER FLAP AT TRACK 1575101-0604-2 574 LUGS FWD HINGE FLAP TRACK 1 NDT SDI I: 17700 FC MRB S AMM SSI 5751011 2.00 B4-100674 NTM 5751101 2.00SPECIAL DETAILED INSPECTION OF LUGS OF FORWARD HINGE PART 4BRACKET OF INNER FLAP AT TRACK 1575101-0604-3 574 LUGS FWD HINGE FLAP TRACK 1 NDT SDI I: 15100 FC MRB S AMM SSI 5751011 2.00 B4-200674 NTM 5751101 2.00 C4SPECIAL DETAILED INSPECTION OF LUGS OF FORWARD HINGE PART 4F4BRACKET OF INNER FLAP AT TRACK 1575103-0604-1 574 LUGS FWD HINGE FLAP TRACK 2 NDT SDI I: 27300 FC MRB S AMM SSI 5751031 2.00 B2674 NTM 5751111 2.00SPECIAL DETAILED INSPECTION OF LUG OF FWD HINGE PART 6BRACKET OF INNER FLAP AT TRACK 2PREP: FLAP AND TAB REMOVED, BEARING HOUSING REMOVED575103-0604-2 574 LUGS FWD HINGE FLAP TRACK 2 NDT SDI I: 22600 FC MRB S AMM SSI 5751031 2.00 B4-1006741 2.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 85APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575103-0604-2 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION OF LUG OF FWD HINGE NTM 575111BRACKET OF INNER FLAP AT TRACK 2 PART 6PREP: FLAP AND TAB REMOVED, BEARING HOUSING REMOVED575103-0604-3 574 LUGS FWD HINGE FLAP TRACK 2 NDT SDI I: 19200 FC MRB S AMM SSI 5751031 2.00 B4-200674 NTM 5751111 2.00 C4SPECIAL DETAILED INSPECTION OF LUG OF FWD HINGE PART 6F4BRACKET OF INNER FLAP AT TRACK 2PREP: FLAP AND TAB REMOVED, BEARING HOUSING REMOVED575104-0604-1 574 FLAP AND TABS - INNER NDT SDI T: 37000 FC ALI NTM 5751041 TBD ALL674 I: 5000 FC PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF INNER FLAP ATTACHMENT EASA ADTO LOVOF TAB BRACKET AT HINGE 5.(RIB 14) 2006-0071FAA ADPREP.: FAIRING TO BE REMOVED 2007-04-11ALI REFERENCE:575104-01-1575105-0604-1 574 LUGS REAR SUPPORT FLAP TR.2 NDT SDI I: 17700 FC MRB S AMM SSI 5751051 2.00 B2674 NTM 5751121 2.00SPECIAL DETAILED INSPECTION OF LUGS OF REAR SUPPORT PART 4BRACKET OF INNER FLAP AT TRACK 2NOTE: FLAP EXTENDED, LINK DETACHED AND FLAP LIFTED575105-0604-2 574 LUGS REAR SUPPORT FLAP TR.2 NDT SDI I: 17700 FC MRB S AMM SSI 5751051 2.00 B4-100674 NTM 5751121 2.00SPECIAL DETAILED INSPECTION OF LUGS OF REAR SUPPORT PART 4BRACKET OF INNER FLAP AT TRACK 2NOTE: FLAP EXTENDED, LINK DETACHED AND FLAP LIFTEDSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 86APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575105-0604-3 574 LUGS REAR SUPPORT FLAP TR.2 NDT SDI I: 15100 FC MRB S AMM SSI 5751051 2.00 B4-200674 NTM 5751121 2.00 C4SPECIAL DETAILED INSPECTION OF LUGS OF REAR SUPPORT PART 4F4BRACKET OF INNER FLAP AT TRACK 2NOTE: FLAP EXTENDED, LINK DETACHED AND FLAP LIFTED575107-0602-1 574 LUGS OF LINK FOR CONNECTION MEC DET I: 11100 FC MRB S AMM SSI 5751071 0.20 ALL6741 0.20DETAILED EXTERNAL INSPECTION OF LUGSOF LINK FOR CONNECTION OF INNER FLAP TO FLAP TRACK 2NOTE: FLAP EXTENDED575109-0604-1 574 CONNECT.BETW.INN.FLAP TAB MEC DET I: 27300 FC MRB S AMM SSI 5751091 0.20 B26741 0.20DETAILED INSPECTION OF CONNECTIONS BETWEENINNER FLAP TAB AND INNER FLAP(EXCEPT AT TRACK 2)NOTE: FLAP EXTENDED, FAIRING REMOVED575109-0604-2 574 CONNECT.BETW.INN.FLAP TAB MEC DET I: 22600 FC MRB S AMM SSI 5751091 0.20 B4-1006741 0.20DETAILED INSPECTION OF CONNECTIONS BETWEENINNER FLAP TAB AND INNER FLAP(EXCEPT AT TRACK 2)NOTE: FLAP EXTENDED, FAIRING REMOVED575109-0604-3 574 CONNECT.BETW.INN.FLAP TAB MEC DET I: 19200 FC MRB S AMM SSI 5751091 0.20 B4-2006741 0.20 C4DETAILED INSPECTION OF CONNECTIONS BETWEENF4INNER FLAP TAB AND INNER FLAP(EXCEPT AT TRACK 2)NOTE: FLAP EXTENDED, FAIRING REMOVED575115-0602-1 574 FLAP LOWER SKIN MEC DET I: 5500 FC MRB S AMM SSI 5751151 0.20 ALL6741 0.20* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 87APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575115-0602-1 * * * * * C O N T I N U E * * * * *DETAILED EXTERNAL INSPECTIONOF INNER FLAP LOWER SKIN AROUND REAR SUPPORT BRACKETAT TRACK 2NOTE: FLAP EXTENDED575119-0604-1 574 RIVETING OF LOWER SKIN MEC DET I: 27300 FC MRB S AMM SSI 5751191 0.20 B26741 0.20DETAILED INSPECTION OF RIVETING OF LOWER SKINOF INNER FLAP TO RIBS 21A, 23A AND 25A BELOW FAIRINGAT TRACK 1NOTE: FLAP EXTENDED, FAIRING REMOVED575119-0604-2 574 RIVETING OF LOWER SKIN MEC DET I: 22600 FC MRB S AMM SSI 5751191 0.20 B4-1006741 0.20DETAILED INSPECTION OF RIVETING OF LOWER SKINOF INNER FLAP TO RIBS 21A, 23A AND 25A BELOW FAIRINGAT TRACK 1NOTE: FLAP EXTENDED, FAIRING REMOVED575119-0604-3 574 RIVETING OF LOWER SKIN MEC DET I: 19200 FC MRB S AMM SSI 5751191 0.20 B4-2006741 0.20 C4DETAILED INSPECTION OF RIVETING OF LOWER SKINF4OF INNER FLAP TO RIBS 21A, 23A AND 25A BELOW FAIRINGAT TRACK 1NOTE: FLAP EXTENDED, FAIRING REMOVED575121-0602-1 574 FLAP UPPER SKIN MEC DET I: 11100 FC MRB S AMM SSI 5751211 0.20 ALL6741 0.20DETAILED EXTERNAL INSPECTION OFRIVETING OF UPPER SKIN OF INNER FLAP BETWEEN RIBS 21AAND 23A FORWARD OF FRONT SPARNOTE: FLAP EXTENDEDSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 88APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575122-0603-1 574 FLAP LOWER SKIN MEC DET I: 8300 FC MRB S AMM SSI 5751221 0.50 ALL6741 0.50DETAILED INSPECTION OF RIVETING OF LOWER SKINOF INNER FLAP TO RIB 20D NEAR INBOARD TAB HINGEBRACKET.PREP.: FLAP EXTENDED, INBOARD HINGE FAIRING REMOVED.575123-0602-1 574 INNER FLAP TAB CONNECTION MEC DET I: 5500 FC MRB S AMM SSI 5751231 0.30 ALL6741 0.30DETAILED EXTERNAL INSPECTION OF CONNECTIONOF INNER FLAP TAB TO INNER FLAP AT TRACK 2 AND AREAOF LOWER LUG OF DRIVE BRACKET OF INNER FLAP TAB.PREP.: FLAP EXTENDED575125-0602-1 574 INNER FLAP RIB 1C MEC DET I: 3000 FC ISB ISB 57-02151 0.10 PRE 047706741 0.10 (57-0201)DETAILED INSPECTION OF THE INNER FLAP RIB 1C.575126-0602-1 574 FLAPS AND TABS - INNER NDT SDI T: SEE ISB CN NTM 5140001 1.50 PRE 13031674 I: 1000 FC FAA AD PART 71 1.50 ORSPECIAL DETAILED INSPECTION OF NOSE RIB 7 OF THE ISB NTM 575108PRE 13241INNER FLAP FOR CRACKS. PART 6(57-0245)CN F-2005-198NOTE: INNER FLAP REMOVED CN 2006-0179FAA AD2006-13-04ISB 57-0240575127-0602-1 587 INBOARD CENTER FLAP TAB HINGE BRACKETS MEC DET T: 5300 FC ISB ISB 57-02141 0.10 PRE 04770687 I: 750 FC1 0.10 (57-0205)DETAILED INSPECTION OF ALL INBOARD CENTER FLAPTAB ATTACHMENT BRACKETS.575127-0602-2 587 INBOARD CENTER FLAP TAB HINGE BRACKETS NDT SDI T: 6000 FC AD NTM 5751271 1.00 PRE 13400687 I: 850 FC ISB PART 61 1.00 (57-0252)SPECIAL DETAILED INSPECTION OF CENTRE HINGE BRACKET AD EU-2007-0299 PRE 04770OF CENTER FLAP INBOARD TAB ISB 57-0250(57-0205)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 89APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575127-0602-2 * * * * * C O N T I N U E * * * * *PREP: FLAPS EXTENDED.575127-0602-3 587 INBOARD CENTER FLAP TAB HINGE BRACKETS NDT SDI T: 6000 FC AD NTM 5751271 1.00 PRE 13400687 I: 850 FC ISB PART 61 1.00 (57-0252)SPECIAL DETAILED INSPECTION OF CENTRE HINGE BRACKET AD EU-2007-0299 POST 04770OF CENTER FLAP INBOARD TAB ISB 57-0250(57-0205)PREP: FLAPS EXTENDED.575153-0602-1 587 LUGS OF LINK SUPP.BRACKET MEC DET I: 11100 FC MRB S AMM SSI 5751532 1.00 ALL6872 1.00DETAILED INSPECTION OF LUGS OF LINKSUPPORT BRACKETS OF CENTER FLAP AND ATTACHMENTSTO RIBS AT FLAP TRACKS 3 AND 4NOTE: FLAP EXTENDED575167-0602-1 587 CENTER FLAP LOWER SKIN MEC DET I: 5500 FC MRB S AMM SSI 5751671 0.30 ALL6871 0.30DETAILED INSPECTION OF EDGE OF CUTOUTIN LOWER SKIN OF CENTER FLAP FORWARD OF FRONT SPARAT FLAP TRACKS 3 AND 4NOTE: FLAP EXTENDED575169-0602-1 587 CENTER FLAP LOWER SKIN MEC DET I: 11100 FC MRB S AMM SSI 5751691 0.30 ALL6871 0.30DETAILED INSPECTION OF LOWER SKIN ANDDOUBLER OF CENTER FLAP BETWEEN FRONT SPAR AND REARSPAR AT TRACKS 3 AND 4, 200MM INBOARD AND OUTBOARD OFTRACK LINENOTE: FLAP EXTENDED575171-0603-1 587 LUGS OF CONNECTING LINK NDT SDI T: 49000 FC ALI NTM 5752102 10.00 ALL687 I: 4100 FC PART 4 AND 62 10.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF LUGS OF CONNECTING EASA ADTO LOVLINKS BETWEEN CENTER FLAP AND TRACKS 3 AND 4. 2006-0071* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 90APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575171-0603-1 * * * * * C O N T I N U E * * * * *FAA ADPREP.: FLAP REMOVED AND LINKS DETACHED 2007-04-11ALI REFERENCE:575171-01-1575175-0602-1 587 CENTER FLAP TAB LUGS MEC DET I: 5500 FC MRB S AMM SSI 5751751 0.30 ALL6871 0.30DETAILED INSPECTION OF LUGS CONNECTINGCENTER FLAP TABS TO TAB DRIVE RODSNOTE: FLAP EXTENDED575203-0602-1 588 LUGS OF LINK SUPP.BRACKET MEC DET I: 11100 FC MRB S AMM SSI 5752032 0.30 ALL6882 0.30DETAILED INSPECTION OF LUGS OF LINKSUPPORT BRACKETS OF OUTER FLAP AND ATTACHMENTS TORIBS AT FLAP TRACKS 5 AND 6NOTE: FLAP EXTENDED575217-0602-1 588 OUTER FLAP LOWER SKIN MEC DET I: 11100 FC MRB S AMM SSI 5752171 0.20 ALL6881 0.20DETAILED INSPECTION OF EDGES OF CUTOUTSIN LOWER SKIN OF OUTER FLAP FORWARD OF FRONT SPAR ATFLAP TRACKS 5 AND 6NOTE: FLAP EXTENDED575221-0602-1 588 OUTER FLAP LOWER SKIN MEC DET I: 2700 FC MRB S AMM SSI 5752211 0.30 ALL6881 0.30DETAILED INSPECTION OF LOWER SKIN ANDDOUBLER OF OUTER FLAP BETWEEN FRONT SPAR AND REARSPAR AT TRACKS NO.5 AND 6, 200MM INBOARD AND OUTBOARDOF TRACK LINE575223-0603-1 588 LUGS OF CONNECTING LINK NDT SDI T: 49000 FC ALI NTM 5753102 10.00 ALL688 I: 4100 FC PART 4 AND 62 10.00 FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 91APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575223-0603-1 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION OF LUGS OF CONNECTING EASA ADTO LOVLINKS BETWEEN OUTER FLAP AND TRACKS 5 AND 6. 2006-0071FAA ADPREP.: FLAP REMOVED AND LINKS DETACHED 2007-04-11ALI REFERENCE:575223-01-1575227-0602-1 588 OUTER FLAP TAB LUGS MEC DET I: 5500 FC MRB S AMM SSI 5752271 0.30 ALL6881 0.30DETAILED INSPECTION OF LUGS CONNECTINGOUTER FLAP TABS TO TAB DRIVE RODS575251-0604-1 576 ALL SPEED AILERON LUGS MEC DET I: 27300 FC MRB S AMM SSI 5752511 0.20 B26761 0.20DETAILED INSPECTION OF UPPER AND LOWER LUGS OFINNER HINGE BRACKET OF ALL SPEED AILERONNOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHTPOSITIONACCESS: 575CB 575CT 575GB 576AB 576BB 576CB* 0.61576DB 576EB675CB 675CT 675GB 676AB 676BB 676CB* 0.61676DB 676EB575251-0604-2 576 ALL SPEED AILERON LUGS MEC DET I: 22600 FC MRB S AMM SSI 5752511 0.20 B4-1006761 0.20DETAILED INSPECTION OF UPPER AND LOWER LUGS OFINNER HINGE BRACKET OF ALL SPEED AILERONNOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHTPOSITIONACCESS: 575CB 575CT 575GB 576AB 576BB 576CB* 0.61576DB 576EB675CB 675CT 675GB 676AB 676BB 676CB* 0.61676DB 676EBSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 92APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575251-0604-3 576 ALL SPEED AILERON LUGS MEC DET I: 19200 FC MRB S AMM SSI 5752511 0.20 B4-2006761 0.20 C4DETAILED INSPECTION OF UPPER AND LOWER LUGS OFF4INNER HINGE BRACKET OF ALL SPEED AILERONNOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHTPOSITIONACCESS: 575CB 575CT 575GB 576AB 576BB 576CB* 0.61576DB 576EB675CB 675CT 675GB 676AB 676BB 676CB* 0.61676DB 676EB575253-0604-1 576 ALL SPEED AILERON LUGS MEC DET I: 17700 FC MRB S AMM SSI 5752531 0.20 B26761 0.20DETAILED INSPECTION OF OUTBOARD LUGS OF OUTERHINGE BRACKET OF ALL SPEED AILERON AND ATTACHMENT TOREAR SPARACCESS: 575GB 576FB* 0.19675GB 676FB* 0.19575253-0604-2 576 ALL SPEED AILERON LUGS MEC DET I: 17700 FC MRB S AMM SSI 5752531 0.20 B4-1006761 0.20DETAILED INSPECTION OF OUTBOARD LUGS OF OUTERHINGE BRACKET OF ALL SPEED AILERON AND ATTACHMENT TOREAR SPARACCESS: 575GB 576FB* 0.19675GB 676FB* 0.19575253-0604-3 576 ALL SPEED AILERON LUGS MEC DET I: 15100 FC MRB S AMM SSI 5752531 0.20 B4-2006761 0.20 C4DETAILED INSPECTION OF OUTBOARD LUGS OF OUTERF4HINGE BRACKET OF ALL SPEED AILERON AND ATTACHMENT TOREAR SPARACCESS: 575GB 576FB* 0.19675GB 676FB* 0.19STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 93APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575271-0604-1 592 LOW SPEED AILERON LUGS MEC DET I: 27300 FC MRB S AMM SSI 5752711 0.20 B26921 0.20DETAILED INSPECTION OF UPPER AND LOWER LUGS OFINNER HINGE BRACKET OF LOW SPEED AILERONNOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHTPOSITIONACCESS: 591BB 592AB 592BB 592CB 592DB 592EB* 0.49691BB 692AB 692BB 692CB 692DB 692EB* 0.50575271-0604-2 592 LOW SPEED AILERON LUGS MEC DET I: 22600 FC MRB S AMM SSI 5752711 0.20 B4-1006921 0.20DETAILED INSPECTION OF UPPER AND LOWER LUGS OFINNER HINGE BRACKET OF LOW SPEED AILERONNOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHTPOSITIONACCESS: 591BB 592AB 592BB 592CB 592DB 592EB* 0.49691BB 692AB 692BB 692CB 692DB 692EB* 0.50575271-0604-3 592 LOW SPEED AILERON LUGS MEC DET I: 19200 FC MRB S AMM SSI 5752711 0.20 B4-2006921 0.20 C4DETAILED INSPECTION OF UPPER AND LOWER LUGS OFF4INNER HINGE BRACKET OF LOW SPEED AILERONNOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHTPOSITIONACCESS: 591BB 592AB 592BB 592CB 592DB 592EB* 0.49691BB 692AB 692BB 692CB 692DB 692EB* 0.50575273-0604-1 592 LOW SPEED AILERON LUGS MEC DET I: 27300 FC MRB S AMM SSI 5752731 0.20 B26921 0.20DETAILED INSPECTION OF LOW SPEED AILERON LUGSOF CENTER AND OUTER HINGE BRACKETS AND ATTACHMENT TOREAR SPAR, PLUS LUGS OF LINKS AT OUTER HINGEACCESS: 591DB 592FB 592GB 592HB* 0.24691DB 692FB 692GB 692HB* 0.24STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 94APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575273-0604-2 592 LOW SPEED AILERON LUGS MEC DET I: 22600 FC MRB S AMM SSI 5752731 0.20 B4-1006921 0.20DETAILED INSPECTION OF LOW SPEED AILERON LUGSOF CENTER AND OUTER HINGE BRACKETS AND ATTACHMENT TOREAR SPAR, PLUS LUGS OF LINKS AT OUTER HINGEACCESS: 591DB 592FB 592GB 592HB* 0.24691DB 692FB 692GB 692HB* 0.24575273-0604-3 592 LOW SPEED AILERON LUGS MEC DET I: 19200 FC MRB S AMM SSI 5752731 0.20 B4-2006921 0.20 C4DETAILED INSPECTION OF LOW SPEED AILERON LUGSF4OF CENTER AND OUTER HINGE BRACKETS AND ATTACHMENT TOREAR SPAR, PLUS LUGS OF LINKS AT OUTER HINGEACCESS: 591DB 592FB 592GB 592HB* 0.24691DB 692FB 692GB 692HB* 0.24575293-0602-1 585 UPPER SKIN OF SPOILERS AND SPEEDBRAKES MEC DET T: 17000 FC ALI EASA AD1 0.20 ALL586 I: 2700 FC 2006-00711 0.20 FROM 0 FC/FH685 DETAILED INSPECTION OF SPEEDBRAKES AND SPOILERS FAA AD1 0.20 TO LOV686 UPPER SKIN. 2007-04-111 0.20NOTE: SPOILER EXTENDET ALI REFERENCE:575293-01-1575313-0604-1 573 INNER AIRBRAKES LUGS MEC DET I: 27300 FC MRB S AMM SSI 5753131 1.00 B26731 1.00DETAILED INSPECTION OF UPPER AND LOWER LUGS OFCENTER HINGE BRAKES OF BOTH INNER AIRBRAKESNOTE: FLAP EXTENDED AND HINGE BRACKET FAIRINGREMOVED, AIRBRAKES IN DOWN AND UPWARD POSITION575313-0604-2 573 INNER AIRBRAKES LUGS MEC DET I: 22600 FC MRB S AMM SSI 5753131 1.00 B4-1006731 1.00DETAILED INSPECTION OF UPPER AND LOWER LUGS OFCENTER HINGE BRAKES OF BOTH INNER AIRBRAKESNOTE: FLAP EXTENDED AND HINGE BRACKET FAIRINGREMOVED, AIRBRAKES IN DOWN AND UPWARD POSITIONSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 95APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)575313-0604-3 573 INNER AIRBRAKES LUGS MEC DET I: 19200 FC MRB S AMM SSI 5753131 1.00 B4-2006731 1.00 C4DETAILED INSPECTION OF UPPER AND LOWER LUGS OFF4CENTER HINGE BRAKES OF BOTH INNER AIRBRAKESNOTE: FLAP EXTENDED AND HINGE BRACKET FAIRINGREMOVED, AIRBRAKES IN DOWN AND UPWARD POSITION575315-0602-1 573 INNER AIRBRAKES LUGS MEC DET I: 5500 FC MRB S AMM SSI 5753151 0.50 ALL6731 0.50DETAILED INSPECTION OF LUGS OF OUTERHINGES OF BOTH INNER AIRBRAKESNOTE: FLAP EXTENDED, AIRBRAKES EXTENDED AND INRETRACTED POSITION575412-0602-1 572 INNER AIRBRAKES - CENTER HINGE NDT SDI T: 16000 FC CN NTM 5131042 1.00 PRE 11602672 I: 8200 FC FAA AD PART 12 1.00 (57-0231)SPECIAL DETAILED INSPECTION OF CENTER HINGE BRACKETS ISB NTM 513105OF INNER AIRBRAKES NO. 1 AND NO. 2. PART 1CNPREP.: REMOVE DETACHABLE SECTION OF FAIRINGS AT 97-080-211(B)CENTER HINGE POSITION OF INNER AIRBRAKES FAA AD 98-04-10ISB 57-0229575612-0603-1 592 AILERON - LOW SPEED LH/RH NDT SDI I: 6000 FH ISB ISB 57-00721 6.00 MSN 003-0126921 6.00SPECIAL DETAILED INSPECTION OF LOW SPEED AILERON RIBSAND TOP SKIN BETWEEN RIB 8 AND 15 FOR CRACKS (WITHAILERON IN HORIZONTAL POSITION)576001-0606-1 541 FRONT SPAR BOTTOM BOOM, RIB 1 TO 6 NDT SDI T: SEE ISB ALI NTM 5700001 5.00 ALL641 I: SEE ISB ISB PART 61 5.00 SB 57-0184SPECIAL DETAILED INSPECTION OF FRONT SPAR BOTTOM BOOM NTM 570001FROM 0 FC/FHBETWEEN RIB 1 AND RIB 6. PART 6TO LOVNTM 571123PREP.: REMOVE PAINT FINISH PART 4EASA AD2006-0071FAA AD2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 96APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576001-0606-1 * * * * * C O N T I N U E * * * * *ISB 57-0184ALI REFERENCE:576001-01-1576002-0606-1 540 WING - FRONT SPAR BOTTOM BOOM NDT SDI T: SEE ISB ALI NTM 5711231 7.00 ALL640 I: SEE ISB ISB PART 41 7.00 SB 57-0147DETAILED OR SPECIAL DETAILED INSPECTION OF THE FRONT EASA ADFROM 0 FC/FHSPAR BOTTOM BOOM BETWEEN RIBS 6 AND 7 AND RIBS 8 AND 2006-0071TO LOV9. FAA AD2007-04-11PREP.: AIRCRAFT TO BE DEFUELED. ISB 57-0149ACCESS: 542EB ALI REFERENCE: * 1.50642EB 576002-01-1* 1.50576003-0606-1 540 FRONT AND REAR SPAR BOTTOM BOOM, RIB 9 NDT SDI T: SEE ISB ALI NTM 5711151 2.00 ALL640 I: SEE ISB ISB PART 41 2.00 SB 57-0152SPECIAL DETAILED INSPECTION OF FASTENER HOLES INBOARD CN 2006-0071(B) FROM 0 FC/FHAND OUTBOARD OF RIB 9 ON THE FRONT AND REAR SPAR FAA AD 96-13-11 TO LOVBOTTOM BOOMS. ISB 57-0152PREP.: AIRCRAFT TO BE DEFUELED. ALI REFERENCE:576003-01-1ACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00576004-0606-1 550 OUTER WING FRONT SPAR NDT SDI ST: 33500 FC ALI NTM 5711201 6.00 B2650 OR PART 41 6.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 38200 FH CN 2006-0071(B) TO 48000 FCBOTTOM BOOM BETWEEN RIB 21 AND RIB 24. SI: 11800 FC FAA AD 96-13-11OR13400 FH ALI REFERENCE:576004-01-1576004-0606-2 550 OUTER WING FRONT SPAR NDT SDI I: 10300 FC ALI NTM 5711201 6.00 B2650 OR PART 41 6.00 FROM 48000 FCSPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 11700 FH CN 2006-0071(B) TO LOVBOTTOM BOOM BETWEEN RIB 21 AND RIB 24. FAA AD 96-13-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 97APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576004-0606-2 * * * * * C O N T I N U E * * * * *ALI REFERENCE:576004-01-2576004-0606-3 550 OUTER WING FRONT SPAR NDT SDI ST: 30000 FC ALI NTM 5711201 6.00 B4-100650 OR PART 41 6.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 41700 FH CN 2006-0071(B) TO 40000 FCBOTTOM BOOM BETWEEN RIB 21 AND RIB 24. SI: 10000 FC FAA AD 96-13-11OR13900 FH ALI REFERENCE:576004-01-3576004-0606-4 550 OUTER WING FRONT SPAR NDT SDI I: 9000 FC ALI NTM 5711201 6.00 B4-100650 OR PART 41 6.00 FROM 40000 FCSPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 12500 FH CN 2006-0071(B) TO LOVBOTTOM BOOM BETWEEN RIB 21 AND RIB 24. FAA AD 96-13-11ALI REFERENCE:576004-01-4576004-0606-5 550 OUTER WING FRONT SPAR NDT SDI ST: 26500 FC ALI NTM 5711201 6.00 B4-200650 OR PART 41 6.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 61500 FH CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. SI: 7800 FC FAA AD 96-13-11 FROM 0 FC/FHORTO 34000 FC18100 FH ALI REFERENCE:576004-01-5576004-0606-6 550 OUTER WING FRONT SPAR NDT SDI I: 7800 FC ALI NTM 5711201 6.00 B4-200650 OR PART 41 6.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 18100 FH CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. FAA AD 96-13-11 FROM 34000 FCTO LOVALI REFERENCE:576004-01-6576005-0606-1 540 OUTER WING FRONT AND REAR SPAR TOP BOOM NDT SDI T: SEE SB ALI NTM REF: SEE1 13.00 ALL640 RIB 9 I: SEE SB CN ISB1 13.00 SB 57-0155FAA AD CN 2006-0071(B) FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 98APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576005-0606-1 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION (HF-EC) OF REAR FRONT AND ISB FAA AD 96-13-11 TO LOVREAR SPAR TOP BOOMS INBOARD AND OUTBOARD OF RIB 9. ISB 57-0155PREP: AIRCRAFT TO BE DEFUELED. ALI REFERENCE:576005-01-1ACCESS: 542EB 543AB* 3.00642EB 643AB* 3.00576006-0606-2 470 BOTTOM SKIN ADJACENT TO PYLON REAR MEC DET T: SEE SB ALI CN 2006-0071(B) 1 1.00 ALL480 ATTACHMENT FITTING I: SEE SB CN FAA AD 96-13-11 1 1.00 SB 57-0148FAA AD ISB 57-0176FROM 0 FC/FHDETAILED INSPECTION OF WINGS BOTTOM SKIN ADJACENT TO ISBTO LOVPYLON REAR ATTACHMENT FITTING. ALI REFERENCE:576006-01-1ACCESS: 473BL 474BR* 1.02483BL 484BR* 1.03576007-0606-1 542 OUTER WING FRONT SPAR MEC DET ST: 36000 FC ALI CN 2006-0071(B) 1 5.00 B2642 OR CN FAA AD 96-13-11 1 5.00 FROM 0 FC/FHDETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 40700 FH FAA ADTO 48000 FCREAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO SI: 7400 FC ALI REFERENCE:BOTTOM BOOM. OR 576007-01-18400 FHACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00576007-0606-2 542 OUTER WING FRONT SPAR MEC DET I: 5700 FC ALI CN 2006-0071(B) 1 5.00 B2642 OR CN FAA AD 96-13-11 1 5.00 FROM 48000 FCDETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 6400 FH FAA ADTO LOVREAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO ALI REFERENCE:BOTTOM BOOM. 576007-01-2ACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00576007-0606-3 542 OUTER WING FRONT SPAR MEC DET ST: 30000 FC ALI CN 2006-0071(B) 1 5.00 B4-100642 OR CN FAA AD 96-13-11 1 5.00 FROM 0 FC/FHDETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 40800 FH FAA ADTO 40000 FCREAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO SI: 6300 FC ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 99APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576007-0606-3 * * * * * C O N T I N U E * * * * *BOTTOM BOOM. OR 576007-01-38600 FHACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00576007-0606-4 542 OUTER WING FRONT SPAR MEC DET I: 5000 FC ALI CN 2006-0071(B) 1 5.00 B4-100642 OR CN FAA AD 96-13-11 1 5.00 FROM 40000 FCDETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 6800 FH FAA ADTO LOVREAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO ALI REFERENCE:BOTTOM BOOM. 576007-01-4ACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00576007-0606-5 542 OUTER WING FRONT SPAR MEC DET ST: 25000 FC ALI CN 2006-0071(B) 1 5.00 B4-200642 OR CN FAA AD 96-13-11 1 5.00 C4DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 55200 FH FAA ADF4REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO SI: 5200 FC ALI REFERENCE: FROM 0 FC/FHBOTTOM BOOM. OR 576007-01-5TO 34000 FC11500 FHACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00576007-0606-6 542 OUTER WING FRONT SPAR MEC DET I: 4300 FC ALI CN 2006-0071(B) 1 5.00 B4-200642 OR CN FAA AD 96-13-11 1 5.00 C4DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 9500 FH FAA ADF4REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO ALI REFERENCE: FROM 34000 FCBOTTOM BOOM. 576007-01-6TO LOVACCESS: 542CB 542DB* 3.00642CB 642DB* 3.00576008-0606-1 540 CENTER SPAR SEALING ANGLE MEC SDI T: SEE SB ALI NTM 5711281 2.00 ALL640 I: SEE SB CN PART 61 2.00 SB 57-0146SPECIAL DETAILED INSPECTION OF VERTICAL FLANGE OF FAA AD CN 2006-0071(B) FROM 0 FC/FHSEALING ANGLE OUTBOARD OF RIB 8. ISB FAA AD 96-13-11 TO LOVISB 57-0146PREP.: AIRCRAFT TO BE DEFUELED.ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 100APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576008-0606-1 * * * * * C O N T I N U E * * * * *ACCESS: 541CB 542DB 542EB 576008-01-1* 4.50641CB 642DB 642EB* 4.50576009-0606-1 550 OUTER WING REAR SPAR NDT SDI ST: 37500 FC ALI NTM 5711221 12.00 B2650 OR CN PART 41 12.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 42700 FH FAA AD CN 2006-0071(B) TO 48000 FCBOTTOM BOOM BETWEEN RIB 18 AND RIB 24. SI: 10500 FC FAA AD 96-13-11ORACCESS: 550GB 550LB 12000 FH ALI REFERENCE: * 3.00650GB 650LB 576009-01-1* 3.00576009-0606-2 550 OUTER WING REAR SPAR NDT SDI ST: 32500 FC ALI NTM 5711221 12.00 B4-100650 OR CN PART 41 12.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45200 FH FAA AD CN 2006-0071(B) TO 40000 FCBOTTOM BOOM BETWEEN RIB 18 AND RIB 24. SI: 7500 FC FAA AD 96-13-11ORACCESS: 550GB 550LB 10400 FH ALI REFERENCE: * 3.00650GB 650LB 576009-01-3* 3.00576009-0606-3 550 OUTER WING REAR SPAR NDT SDI ST: 28500 FC ALI NTM 5711221 12.00 B4-200650 OR CN PART 41 12.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 66100 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. SI: 5500 FC FAA AD 96-13-11 FROM 0 FC/FHORTO 34000 FCACCESS: 550GB 550LB 12700 FH ALI REFERENCE: * 3.00650GB 650LB 576009-01-5* 3.00576009-0606-4 550 OUTER WING REAR SPAR NDT SDI I: 7500 FC ALI NTM 5711221 12.00 B2650 OR CN PART 41 12.00 FROM 48000 FCSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 8500 FH FAA AD CN 2006-0071(B) TO LOVBOTTOM BOOM BETWEEN RIB 18 AND RIB 24. FAA AD 96-13-11ACCESS: 550GB 550LB ALI REFERENCE: * 3.00650GB 650LB 576009-01-2* 3.00576009-0606-5 550 OUTER WING REAR SPAR NDT SDI I: 6500 FC ALI NTM 5711221 12.00 B4-100650 OR CN PART 41 12.00 FROM 40000 FCSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 9000 FH FAA AD CN 2006-0071(B) TO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 101APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576009-0606-5 * * * * * C O N T I N U E * * * * *BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. FAA AD 96-13-11ACCESS: 550GB 550LB ALI REFERENCE: * 3.00650GB 650LB 576009-01-4* 3.00576009-0606-6 550 OUTER WING REAR SPAR NDT SDI I: 5500 FC ALI NTM 5711221 12.00 B4-200650 OR CN PART 41 12.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 12700 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. FAA AD 96-13-11 FROM 34000 FCTO LOVACCESS: 550GB 550LB ALI REFERENCE: * 3.00650GB 650LB 576009-01-6* 3.00576010-0606-1 540 REAR SPAR BOTTOM BOOM NDT SDI T: SEE SB ALI NTM 5711161 6.00 ALL640 I: SEE SB CN PART 41 6.00 SB 57-0147SPECIAL DETAILED INSPECTION OF REAR SPAR BOTTOM BOOM FAA AD CN 2006-0071(B) FROM 0 FC/FHBETWEEN RIB 1 AND RIB 9 IN BOTH AREAS INBOARD AND ISB FAA AD 96-13-11 TO LOVOUTBOARD OF MAIN LANDING GEAR REINFORCING PLATE. ISB 57-0147PREP.: AIRCRAFT TO BE DEFUELED ALI REFERENCE:576010-01-1ACCESS: 542DB 542EB* 3.00642DB 642EB* 3.00576011-0606-1 541 OUTER WING BOTTOM SKIN NDT SDI ST: 41000 FC ALI NTM 5730101 1.30 B2542 OR CN PART 21 1.30 FROM 0 FC/FH543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 46300 FH FAA AD CN 2006-0071(B) 1 1.30 TO 48000 FC641 JOINT AT RIB 9. SI: 5500 FC FAA AD 96-13-11 1 1.30642 OR1 1.30643 6200 FH ALI REFERENCE: 1 1.30576011-01-1ACCESS: 542EB* 1.50543AB* 1.50642EB* 1.50643AB* 1.50576011-0606-2 541 OUTER WING BOTTOM SKIN NDT SDI ST: 35000 FC ALI NTM 5730101 1.30 B4-100542 OR CN PART 21 1.30 FROM 0 FC/FH543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 47900 FH FAA AD CN 2006-0071(B) 1 1.30 TO 40000 FC* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 102APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576011-0606-2 * * * * * C O N T I N U E * * * * *641 JOINT AT RIB 9. SI: 5000 FC FAA AD 96-13-11 1 1.30642 OR1 1.30643 6800 FH ALI REFERENCE: 1 1.30576011-01-3ACCESS: 542EB* 1.50543AB* 1.50642EB* 1.50643AB* 1.50576011-0606-3 541 OUTER WING BOTTOM SKIN NDT SDI ST: 29500 FC ALI NTM 5730101 1.30 B4-200542 OR CN PART 21 1.30 C4543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 67000 FH FAA AD CN 2006-0071(B) 1 1.30 F4641 SKIN JOINT AT RIB 9. SI: 4200 FC FAA AD 96-13-11 1 1.30 FROM 0 FC/FH642 OR1 1.30 TO 34000 FC643 9500 FH ALI REFERENCE: 1 1.30576011-01-5ACCESS: 542EB* 1.50543AB* 1.50642EB* 1.50643AB* 1.50576011-0606-4 541 OUTER WING BOTTOM SKIN NDT SDI I: 2800 FC ALI NTM 5730101 1.30 B2542 OR CN PART 21 1.30 FROM 48000 FC543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 3200 FH FAA AD CN 2006-0071(B) 1 1.30 TO LOV641 SKIN JOINT AT RIB 9. FAA AD 96-13-11 1 1.306421 1.30643 ALI REFERENCE: 1 1.30576011-01-2ACCESS: 542EB* 1.50543AB* 1.50642EB* 1.50643AB* 1.50576011-0606-5 541 OUTER WING BOTTOM SKIN NDT SDI I: 2400 FC ALI NTM 5730101 1.30 B4-100542 OR CN PART 21 1.30 FROM 40000 FC543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 3300 FH FAA AD CN 2006-0071(B) 1 1.30 TO LOV641 SKIN JOINT AT RIB 9. FAA AD 96-13-11 1 1.306421 1.30643 ALI REFERENCE: 1 1.30576011-01-4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 103APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576011-0606-5 * * * * * C O N T I N U E * * * * *ACCESS: 542EB* 1.50543AB* 1.50642EB* 1.50643AB* 1.50576011-0606-6 541 OUTER WING BOTTOM SKIN NDT SDI I: 2000 FC ALI NTM 5730101 1.30 B4-200542 OR CN PART 21 1.30 C4543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 4500 FH FAA AD CN 2006-0071(B) 1 1.30 F4641 SKIN JOINT AT RIB 9. FAA AD 96-13-11 1 1.30 FROM 34000 FC6421 1.30 TO LOV643 ALI REFERENCE: 1 1.30576011-01-6ACCESS: 542EB* 1.50543AB* 1.50642EB* 1.50643AB* 1.50576012-0606-1 540 BOTTOM SKIN STRINGERS ADJACENT RIB 14 NDT SDI T: SEE SB ALI NTM 5713101 1.50 ALL640 I: SEE SB CN PART 61 1.50 SB 57-0148SPECIAL DETAILED INSPECTION OF WINGS BOTTOM SKIN FAA AD CN 2006-0071(B) FROM 0 FC/FHSTRINGER 10 TO STRINGER 17 RUNOUTS, STRINGERS ISB FAA AD 96-13-11 TO LOVADJECENT TO RIB 14. ISB 57-0148PREP.: AIRCRAFT TO BE DEFUELED. ALI REFERENCE:576012-01-1ACCESS: 543DB 550BB* 3.00643DB 650BB* 3.00576013-0604-1 500 OUTER WING BOTTOM SKIN MEC DET ST: 28000 FC ALI CN 2006-0071(B) 1 2.00 B2600 OR CN FAA AD 96-13-11 1 2.00 PRE 08253DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 31600 FH FAA AD(57-0175)MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 2900 FC ALI REFERENCE: FROM 0 FC/FHHOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, OR 576013-01-1TO 48000 FCAND RIB 14 AND RIB 22. 3300 FHNOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-1576013-0604-2 500 OUTER WING BOTTOM SKIN MEC DET I: 2600 FC ALI CN 2006-0071(B) 1 2.00 B2600 OR CN FAA AD 96-13-11 1 2.00 PRE 08253* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 104APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576013-0604-2 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 2900 FH FAA AD ALI REFERENCE: (57-0175)MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN 576013-01-2FROM 48000 FCHOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13,TO LOVAND RIB 14 AND RIB 22.NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-2576013-0604-3 500 OUTER WING BOTTOM SKIN MEC DET ST: 24000 FC ALI CN 2006-0071(B) 1 2.00 B4-100600 OR CN FAA AD 96-13-11 1 2.00 PRE 08253DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 32900 FH FAA AD(57-0175)MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 2200 FC ALI REFERENCE: FROM 0 FC/FHHOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, OR 576013-01-3TO 40000 FCAND RIB 14 AND RIB 22. 3000 FHNOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-3576013-0604-4 500 OUTER WING BOTTOM SKIN MEC DET I: 2200 FC ALI CN 2006-0071(B) 1 2.00 B4-100600 OR CN FAA AD 96-13-11 1 2.00 PRE 08253DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 3000 FH FAA AD(57-0175)MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN ALI REFERENCE: FROM 40000HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, 576013-01-4TO LOVAND RIB 14 AND RIB 22.NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-4576013-0604-5 500 OUTER WING BOTTOM SKIN MEC DET ST: 19000 FC ALI CN 2006-0071(B) 1 2.00 B4-200600 OR CN FAA AD 96-13-11 1 2.00 C4DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 43100 FH FAA ADF4MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 1900 FC ALI REFERENCE: PRE 08253HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, OR 576013-01-5(57-0175)AND RIB 14 AND RIB 22. 4300 FHFROM 0 FC/FHTO 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-5576013-0604-6 500 OUTER WING BOTTOM SKIN MEC DET I: 1900 FC ALI CN 2006-0071(B) 1 2.00 B4-200600 OR CN FAA AD 96-13-11 1 2.00 C4DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 4300 FH FAA ADF4MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN ALI REFERENCE: PRE 08253HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, 576013-01-6(57-0175)* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 105APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576013-0604-6 * * * * * C O N T I N U E * * * * *AND RIB 14 AND RIB 22.FROM 34000 FCTO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-6576013-0606-1 500 OUTER WING BOTTOM SKIN NDT SDI ST: 28000 FC ALI NTM 5730111 3.00 B2600 OR CN PART 61 3.00 PRE 08253SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 31600 FH FAA AD CN 2006-0071(B) (57-0175)AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 5800 FC FAA AD 96-13-11 FROM 0 FC/FHHOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND ORTO 48000 FCRIB 14 AND RIB 22. 6500 FH ALI REFERENCE:576013-02-1NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-1576013-0606-2 500 OUTER WING BOTTOM SKIN NDT SDI I: 5100 FC ALI NTM 5730111 3.00 B2600 OR CN PART 61 3.00 PRE 08253SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 5800 FH FAA AD CN 2006-0071(B) (57-0175)AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN FAA AD 96-13-11 FROM 48000 FCHOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, ANDTO LOVRIB 14 AND RIB 22. ALI REFERENCE:576013-02-2NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-2576013-0606-3 500 OUTER WING BOTTOM SKIN NDT SDI ST: 24000 FC ALI NTM 5730111 3.00 B4-100600 OR CN PART 61 3.00 PRE 08253SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 32900 FH FAA AD CN 2006-0071(B) (57-0175)AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 5000 FC FAA AD 96-13-11 FROM 0 FC/FHHOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND ORTO 40000 FCRIB 14 AND RIB 22. 6800 FH ALI REFERENCE:576013-02-3NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-3576013-0606-4 500 OUTER WING BOTTOM SKIN NDT SDI I: 4400 FC ALI NTM 5730111 3.00 B4-100600 OR CN PART 61 3.00 PRE 08253SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 6000 FH FAA AD CN 2006-0071(B) (57-0175)AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN FAA AD 96-13-11 FROM 40000HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, ANDTO LOVRIB 14 AND RIB 22. ALI REFERENCE:576013-02-4NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-4STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 106APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576013-0606-5 500 OUTER WING BOTTOM SKIN NDT SDI ST: 19000 FC ALI NTM 5730111 3.00 B4-200600 OR CN PART 61 3.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 43100 FH FAA AD CN 2006-0071(B) F4AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 3800 FC FAA AD 96-13-11 PRE 08253HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND OR(57-0175)RIB 14 AND RIB 22. 8600 FH ALI REFERENCE: FROM 0 FC/FH576013-02-5TO 34000 FCNOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-5576013-0606-6 500 OUTER WING BOTTOM SKIN NDT SDI I: 3700 FC ALI NTM 5730111 3.00 B4-200600 OR CN PART 61 3.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 8400 FH FAA AD CN 2006-0071(B) F4AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN FAA AD 96-13-11 PRE 08253HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND(57-0175)RIB 14 AND RIB 22. ALI REFERENCE: FROM 34000 FC576013-02-6TO LOVNOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-6576014-0606-1 540 BOTTOM SKIN AT MAGNETIC LEVEL INDICATOR NDT SDI T: SEE SB ALI NDT 5730101 1.50 ALL640 I: SEE SB CN PART 61 1.50 SB 57-0153VISUAL OR SPECIAL DETAILED INSPECTION OF OUTER WING FAA AD CN 2006-0071(B) FROM 0 FC/FHBOTTOM SKIN AT MAGNETIC LEVEL INDICATOR (MLI) AND ISB FAA AD 96-13-11 TO LOVSLAT CAN DRAIN HOLE BETWEEN RIB 8 AND RIB 9. ISB 57-0153ALI REFERENCE:576014-01-1576016-0606-1 540 WING-REAR SPAR NDT SDI T: SEE SB ALI NTM 5711121 5.00 ALL640 I: SEE SB CN PART 41 5.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF REAR SPAR AT SELECTED FAA AD CN 2006-0071(B) TO LOVBOLT LOCATION FOR ATTACHMENT OF MLG FORWARD PICK UP ISB FAA AD 96-13-11FITTING AND MLG RIB 5 AFT OF REAR SPAR. ISB 57-0157PREP.: AIRCRAFT TO BE DEFUELED. ALI REFERENCE:576016-01-1ACCESS: 542CB* 1.50642CB* 1.50576017-0606-1 540 WING - STRUCTURE AROUND MANHOLES NDT SDI T: SEE SB ALI NTM 5733151 2.50 B2640 I: SEE SB CN PART 61 2.50 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF MANHOLE SURROUND FAA AD CN 2006-0071(B) TO LOV* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 107APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576017-0606-1 * * * * * C O N T I N U E * * * * *STRUCTURE BETWEEN RIB 2 AND RIB 11. ISB FAA AD 96-13-11ISB 57-0230PREP.: TANKS TO BE DEFUELED.ALI REFERENCE:ACCESS: 541AB 541BB 541CB 542CB 542DB 542EB 576017-01-1* 10.50543AB641AB 641BB 641CB 642CB 642DB 642EB* 10.50643AB576021-0606-1 523 OUTER WING TOP SKIN MEC DET ST: 26500 FC ALI CN 2006-0071(B) 1 5.00 B2524 SI: 3300 FC CN FAA AD 96-13-11 1 5.00 FROM 0 FC/FH623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD1 5.00 TO 48000 FC624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENCE: 1 5.00576021-01-1576021-0606-2 523 OUTER WING TOP SKIN MEC DET ST: 26500 FC ALI CN 2006-0071(B) 1 5.00 B4-100524 SI: 3400 FC CN FAA AD 96-13-11 1 5.00 FROM 0 FC/FH623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD1 5.00 TO 40000 FC624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENCE: 1 5.00576021-01-2576021-0606-3 523 OUTER WING TOP SKIN MEC DET ST: 25000 FC ALI CN 2006-0071(B) 1 5.00 B4-200524 SI: 3900 FC CN FAA AD 96-13-11 1 5.00 C4623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD1 5.00 F4624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENCE: 1 5.00 FROM 0 FC/FH576021-01-3TO 34000 FC576021-0606-4 523 OUTER WING TOP SKIN MEC DET I: 2600 FC ALI CN 2006-0071(B) 1 5.00 B2524 CN FAA AD 96-13-11 1 5.00 FROM 48000 FC623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD1 5.00 TO LOV624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENCE: 1 5.00576021-01-4576021-0606-5 523 OUTER WING TOP SKIN MEC DET I: 2600 FC ALI CN 2006-0071(B) 1 5.00 B4-100524 CN FAA AD 96-13-11 1 5.00 FROM 40000 FC623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD1 5.00 TO LOV624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENCE: 1 5.00576021-01-5STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 108APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576021-0606-6 523 OUTER WING TOP SKIN MEC DET I: 2600 FC ALI CN 2006-0071(B) 1 5.00 B4-200524 CN FAA AD 96-13-11 1 5.00 C4623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD1 5.00 F4624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENCE: 1 5.00 FROM 34000 FC576021-01-6TO LOV576029-0605-1 541 OUTER WING FRONT SPAR NDT SDI ST: 36500 FC ALI NTM 5711231 14.00 B2641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 41200 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHBOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 SI: 3000 FC FAA AD 96-13-11 TO 48000 FCAND RIB 9 OR3400 FH ALI REFERENCE:NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-1AS TASK 576029-0606-1ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0605-2 541 OUTER WING FRONT SPAR NDT SDI I: 2000 FC ALI NTM 5711231 14.00 B2641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 2200 FH FAA AD CN 2006-0071(B) FROM 48000 FCBOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 FAA AD 96-13-11 TO LOVAND RIB 9ALI REFERENCE:NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-2AS TASK 576029-0606-2ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0605-3 541 OUTER WING FRONT SPAR NDT SDI ST: 40500 FC ALI NTM 5711231 14.00 B4-100641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 55500 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHBOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 SI: N/A FAA AD 96-13-11 TO 40000 FCAND RIB 9ALI REFERENCE:NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-3AS TASK 576029-0606-3ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 109APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576029-0605-4 541 OUTER WING FRONT SPAR NDT SDI I: 5700 FC ALI NTM 5711231 14.00 B4-100641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 7800 FH FAA AD CN 2006-0071(B) FROM 40000 FCBOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 FAA AD 96-13-11 TO LOVAND RIB 9ALI REFERENCE:NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-4AS TASK 576029-0606-4ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0605-5 541 OUTER WING FRONT SPAR NDT SDI ST: 34000 FC ALI NTM 5711231 14.00 B4-200641 OR CN PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 77200 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 SI: N/A FAA AD 96-13-11 POST 01868AND RIB 9FROM 0 FC/FHALI REFERENCE: TO 34000 FCNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-5AS TASK 576029-0606-5ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0605-6 541 OUTER WING FRONT SPAR NDT SDI I: 4700 FC ALI NTM 5711231 14.00 B4-200641 OR CN PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 10700 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 FAA AD 96-13-11 POST 01868AND RIB 9FROM 34000 FCALI REFERENCE: TO LOVNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-6AS TASK 576029-0606-6ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0606-1 541 OUTER WING FRONT SPAR NDT SDI ST: 36500 FC ALI NTM 5711231 14.00 B2641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF 2 BOLTS JUST INBOARD 41200 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHOF RIB 7 OF OUTER WING FRONT SPAR. SI: 3000 FC FAA AD 96-13-11 TO 48000 FCORNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 3400 FH ALI REFERENCE:* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 110APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576029-0606-1 * * * * * C O N T I N U E * * * * *TASK 576029-0605-1 576029-02-1ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0606-2 541 OUTER WING FRONT SPAR NDT SDI I: 2000 FC ALI NTM 5711231 14.00 B2641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF 2 BOLTS JUST INBOARD 2200 FH FAA AD CN 2006-0071(B) FROM 48000 FCOF RIB 7 OF OUTER WING FRONT SPAR. FAA AD 96-13-11 TO LOVNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE:TASK 576029-0605-2 576029-02-2ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0606-3 541 OUTER WING FRONT SPAR NDT SDI ST: 40500 FC ALI NTM 5711231 14.00 B4-100641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 55500 FH FAA AD CN 2006-0071(B) FROM 0 FC/FHOF RIB 7 OF OUTER WING FRONT SPAR. SI: N/A FAA AD 96-13-11 TO 40000 FCNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE:TASK 576029-0605-3 576029-02-3ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0606-4 541 OUTER WING FRONT SPAR NDT SDI I: 5700 FC ALI NTM 5711231 14.00 B4-100641 OR CN PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 7800 FH FAA AD CN 2006-0071(B) FROM 40000 FCOF RIB 7 OF OUTER WING FRONT SPAR. FAA AD 96-13-11 TO LOVNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE:TASK 576029-0605-4 576029-02-4ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 111APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576029-0606-5 541 OUTER WING FRONT SPAR NDT SDI ST: 34000 FC ALI NTM 5711231 14.00 B4-200641 OR CN PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 77200 FH FAA AD CN 2006-0071(B) F4OF RIB 7 OF OUTER WING FRONT SPAR. SI: N/A FAA AD 96-13-11 POST 01868FROM 0 FC/FHNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE: TO 34000 FCTASK 576029-0605-5 576029-02-5ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576029-0606-6 541 OUTER WING FRONT SPAR NDT SDI I: 4700 FC ALI NTM 5711231 14.00 B4-200641 OR CN PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 10700 FH FAA AD CN 2006-0071(B) F4OF RIB 7 OF OUTER WING FRONT SPAR. FAA AD 96-13-11 POST 01868FROM 34000 FCNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE: TO LOVTASK 576029-0605-6 576029-02-6ACCESS: 541CB 542EB* 3.00641CB 642EB* 3.00576031-0606-1 543 OUTER WING FRONT SPAR NDT SDI T: 33500 FC ALI NTM1 4.50 B2550 OR CN 571119 PART 41 4.50 POST 01868 OR643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 37800 FH FAA AD CN 2006-0071(B) 1 4.50 POST 02101650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. I: 3500 FC FAA AD 96-13-11 1 4.50 (57-0079) ANDORPRE 023383900 FH ALI REFERENCE: FROM 0 FC/FH576031-01-1TO 48000 FC576031-0606-2 543 OUTER WING FRONT SPAR NDT SDI I: 1900 FC ALI NTM1 4.50 B2550 OR CN 571119 PART 41 4.50 POST 01868 OR643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 2100 FH FAA AD CN 2006-0071(B) 1 4.50 POST 02101650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. FAA AD 96-13-11 1 4.50 (57-0079) ANDPRE 02338ALI REFERENCE: FROM 48000 FC576031-01-2TO LOV576031-0606-3 543 OUTER WING FRONT SPAR NDT SDI T: 34000 FC ALI NTM1 4.50 B4-100550 OR CN 571119 PART 41 4.50 POST 01868 OR643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 46600 FH FAA AD CN 2006-0071(B) 1 4.50 POST 02101* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 112APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576031-0606-3 * * * * * C O N T I N U E * * * * *650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. I: 3500 FC FAA AD 96-13-11 1 4.50 (57-0079) ANDORPRE 023384800 FH ALI REFERENCE: FROM 0 FC/FH576031-01-3TO 40000 FC576031-0606-4 543 OUTER WING FRONT SPAR NDT SDI I: 1650 FC ALI NTM1 4.50 B4-100550 OR CN 571119 PART 41 4.50 POST 01868 OR643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 2300 FH FAA AD CN 2006-0071(B) 1 4.50 POST 02101650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. FAA AD 96-13-11 1 4.50 (57-0079) ANDPRE 02338ALI REFERENCE: FROM 40000 FC576031-01-4TO LOV576031-0606-5 543 OUTER WING FRONT SPAR NDT SDI T: 28000 FC ALI NTM1 4.50 B4-200550 OR CN 571119 PART 41 4.50 C4643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 63500 FH FAA AD CN 2006-0071(B) 1 4.50 F4650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. I: 3500 FC FAA AD 96-13-11 1 4.50 POST 01868 ORORPOST 021017900 FH ALI REFERENCE: (57-0079) AND576031-01-5PRE 02338FROM 0 FC/FHTO 34000 FC576031-0606-6 543 OUTER WING FRONT SPAR NDT SDI I: 1400 FC ALI NTM1 4.50 B4-200550 OR CN 571119 PART 41 4.50 C4643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 3200 FH FAA AD CN 2006-0071(B) 1 4.50 F4650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. FAA AD 96-13-11 1 4.50 POST 01868 ORPOST 02101ALI REFERENCE: (57-0079) AND576031-01-6PRE 02338FROM 34000 FCTO LOV576035-0606-1 542 OUTER WING REAR SPAR NDT SDI T: 36000 FC ALI NTM1 14.00 B2642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 40700 FH EASA ADPRE (53-0282)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 6700 FC 2006-0071FROM 0 FC/FHMAIN LANDING GEAR REINFORCING . OR FAA ADTO 48000 FC7600 FH 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 113APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576035-0606-1 * * * * * C O N T I N U E * * * * *ACCESS: 542DB 542EB ALI REFERENCE: * 3.00642DB 642EB 576035-01-1* 3.00576035-0606-2 542 OUTER WING REAR SPAR NDT SDI I: 3700 FC ALI NTM1 14.00 B2642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 4200 FH EASA ADPRE (53-0282)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071FROM 48000 FCMAIN LANDING GEAR REINFORCING . FAA ADTO LOV2007-04-11ACCESS: 542DB 542EB* 3.00642DB 642EB ALI REFERENCE: * 3.00576035-01-2576035-0606-3 542 OUTER WING REAR SPAR NDT SDI T: 36000 FC ALI NTM1 14.00 B2642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 40700 FH EASA ADPOST (53-0282)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 5700 FC 2006-0071FROM 0 FC/FHMAIN LANDING GEAR REINFORCING . OR FAA ADTO 48000 FC6400 FH 2007-04-11ACCESS: 542DB 542EB* 3.00642DB 642EB ALI REFERENCE: * 3.00576035-01-3576035-0606-4 542 OUTER WING REAR SPAR NDT SDI I: 3100 FC ALI NTM1 14.00 B2642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 3500 FH EASA ADPOST (53-0282)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071FROM 48000 FCMAIN LANDING GEAR REINFORCING . FAA ADTO LOV2007-04-11ACCESS: 542DB 542EB* 3.00642DB 642EB ALI REFERENCE: * 3.00576035-01-4576035-0606-5 542 OUTER WING REAR SPAR NDT SDI T: 33500 FC ALI NTM1 14.00 B4-100642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH EASA ADPRE (53-0291)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 5300 FC 2006-0071FROM 0 FC/FHMAIN LANDING GEAR REINFORCING . OR FAA ADTO 40000 FC7300 FH 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 114APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576035-0606-5 * * * * * C O N T I N U E * * * * *ACCESS: 542DB 542EB ALI REFERENCE: * 3.00642DB 642EB 576035-01-5* 3.00576035-0606-6 542 OUTER WING REAR SPAR NDT SDI I: 3200 FC ALI NTM1 14.00 B4-100642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 4400 FH EASA ADPRE (53-0291)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071FROM 40000 FCMAIN LANDING GEAR REINFORCING . FAA ADTO LOV2007-04-11ACCESS: 542DB 542EB* 3.00642DB 642EB ALI REFERENCE: * 3.00576035-01-6576035-0606-7 542 OUTER WING REAR SPAR NDT SDI T: 33500 FC ALI NTM1 14.00 B4-100642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH EASA ADPOST (53-0291)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 4500 FC 2006-0071FROM 0 FC/FHMAIN LANDING GEAR REINFORCING . OR FAA ADTO 40000 FC6200 FH 2007-04-11ACCESS: 542DB 542EB* 3.00642DB 642EB ALI REFERENCE: * 3.00576035-01-7576035-0606-8 542 OUTER WING REAR SPAR NDT SDI I: 2700 FC ALI NTM1 14.00 B4-100642 OR FAA AD 571116 PART 41 14.00 POST 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 3700 FH EASA ADPOST (53-0291)BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071FROM 40000 FCMAIN LANDING GEAR REINFORCING . FAA ADTO LOV2007-04-11ACCESS: 542DB 542EB* 3.00642DB 642EB ALI REFERENCE: * 3.00576035-01-8576035-0606-9 542 OUTER WING REAR SPAR NDT SDI T: 27000 FC ALI NTM1 14.00 B4-200642 OR FAA AD 571116 PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 61300 FH EASA ADF4BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 4200 FC 2006-0071POST 01868MAIN LANDING GEAR REINFORCING . OR FAA ADPRE (53-0291)9500 FH 2007-04-11FROM 0 FC/FH* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 115APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576035-0606-9 * * * * * C O N T I N U E * * * * *ACCESS: 542DB 542EB ALI REFERENCE: * 3.00 TO 34000 FC642DB 642EB 576035-01-9* 3.00576035-0607-1 542 OUTER WING REAR SPAR NDT SDI I: 2800 FC ALI NTM1 14.00 B4-200642 OR FAA AD 571116 PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 6300 FH EASA ADF4BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071POST 01868MAIN LANDING GEAR REINFORCING . FAA ADPRE (53-0291)2007-04-11FROM 34000 FCACCESS: 542DB 542EB* 3.00 TO LOV642DB 642EB ALI REFERENCE: * 3.00576035-01-10576035-0607-2 542 OUTER WING REAR SPAR NDT SDI T: 27500 FC ALI NTM1 14.00 B4-200642 OR FAA AD 571116 PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 62400 FH EASA ADF4BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 3600 FC 2006-0071POST 01868MAIN LANDING GEAR REINFORCING . OR FAA ADPOST (53-0291)8200 FH 2007-04-11FROM 0 FC/FHACCESS: 542DB 542EB* 3.00 TO 34000 FC642DB 642EB ALI REFERENCE: * 3.00576035-01-11576035-0607-3 542 OUTER WING REAR SPAR NDT SDI I: 2400 FC ALI NTM1 14.00 B4-200642 OR FAA AD 571116 PART 41 14.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 5400 FH EASA ADF4BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071POST 01868MAIN LANDING GEAR REINFORCING . FAA ADPOST (53-0291)2007-04-11FROM 34000 FCACCESS: 542DB 542EB* 3.00 TO LOV642DB 642EB ALI REFERENCE: * 3.00576035-01-12576037-0606-1 543 OUTER WING REAR SPAR NDT SDI ST: 38000 FC ALI NTM1 4.50 B2550 OR FAA AD 571121 PART 41 4.50 POST 01868643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 43300 FH EASA AD1 4.50 OR650 BOTTOM BETWEEN RIB 9 AND RIB 18. SI: 7000 FC 2006-00711 4.50 POST 02100OR FAA AD(57-0078)ACCESS: 543BB 8000 FH 2007-04-11* 1.50 PRE 02338* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 116APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576037-0606-1 * * * * * C O N T I N U E * * * * *550DB ALI REFERENCE: * 1.50 FROM 0 FC/FH643BB 576037-01-1* 1.50 TO 48000 FC650DB* 1.50576037-0606-2 543 OUTER WING REAR SPAR NDT SDI I: 7000 FC ALI NTM1 4.50 B2550 OR FAA AD 571121 PART 41 4.50 POST 01868643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 8000 FH EASA AD1 4.50 OR650 BOTTOM BETWEEN RIB 9 AND RIB 18. 2006-00711 4.50 POST 02100FAA AD(57-0078)ACCESS: 543BB 2007-04-11* 1.50 PRE 02338550DB* 1.50 FROM 48000 FC643BB ALI REFERENCE: * 1.50 TO LOV650DB 576037-01-2* 1.50576037-0606-3 543 OUTER WING REAR SPAR NDT SDI ST: 33000 FC ALI NTM1 4.50 B4-100550 OR FAA AD 571121 PART 41 4.50 POST 01868643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH EASA AD1 4.50 OR650 BOTTOM BETWEEN RIB 9 AND RIB 18. SI: 7000 FC 2006-00711 4.50 POST 02100OR FAA AD(57-0078)ACCESS: 543BB 9700 FH 2007-04-11* 1.50 PRE 02338550DB* 1.50 FROM 0 FC/FH643BB ALI REFERENCE: * 1.50 TO 40000 FC650DB 576037-01-3* 1.50576037-0606-4 543 OUTER WING REAR SPAR NDT SDI I: 5400 FC ALI NTM1 4.50 B4-100550 OR FAA AD 571121 PART 41 4.50 POST 01868643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 7500 FH EASA AD1 4.50 OR650 BOTTOM BETWEEN RIB 9 AND RIB 18. 2006-00711 4.50 POST 02100FAA AD(57-0078)ACCESS: 543BB 2007-04-11* 1.50 PRE 02338550DB* 1.50 FROM 40000 FC643BB ALI REFERENCE: * 1.50 TO LOV650DB 576037-01-4* 1.50576037-0606-5 543 OUTER WING REAR SPAR NDT SDI ST: 27000 FC ALI NTM1 4.50 B4-200550 OR FAA AD 571121 PART 41 4.50 C4643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 62600 FH EASA AD1 4.50 F4650 BOTTOM BETWEEN RIB 9 AND RIB 18. SI: 7000 FC 2006-00711 4.50 POST 01868OROR* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 117APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576037-0606-5 * * * * * C O N T I N U E * * * * *ACCESS: 543BB 16200 FH FAA AD* 1.50 POST 02100550DB 2007-04-11* 1.50 (57-0078)643BB* 1.50 PRE 02338650DB ALI REFERENCE: * 1.50 FROM 0 FC/FH576037-01-5TO 34000 FC576037-0606-6 543 OUTER WING REAR SPAR NDT SDI I: 4700 FC ALI NTM1 4.50 B4-200550 OR FAA AD 571121 PART 41 4.50 C4643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 10900 FH EASA AD1 4.50 F4650 BOTTOM BETWEEN RIB 9 AND RIB 18. 2006-00711 4.50 POST 01868FAA ADORACCESS: 543BB 2007-04-11* 1.50 POST 02100550DB* 1.50 (57-0078)643BB ALI REFERENCE: * 1.50 PRE 02338650DB 576037-01-6* 1.50 FROM 34000 FCTO LOV576041-0606-1 541 OUTER WING TOP BOOM NDT SDI T: 34000 FC ALI NTM1 1.30 B2542 I: 4400 FC CN 571124 PART 41 1.30 POST 01869543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND FAA AD CN 2006-0071(B) 1 1.30 OR641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13-11 1 1.30 POST 020996421 1.30 (57-0077)643 ALI REFERENCE: 1 1.30 FROM 0 FC/FH576041-01-1TO 48000 FCACCESS: 542EB 575FB 575GB* 1.68543AB 543CB 581CB* 3.04642EB 675FB 675GB* 1.68643AB 643CB 681CB* 3.04576041-0606-2 541 OUTER WING TOP BOOM NDT SDI I: 2300 FC ALI NTM1 1.30 B2542 CN 571124 PART 41 1.30 POST 01869543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071(B) 1 1.30 OR641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13-11 1 1.30 POST 020996421 1.30 (57-0077)643 ALI REFERENCE: 1 1.30 FROM 48000 FC576041-01-2TO LOVACCESS: 542EB 575FB 575GB* 1.68543AB 543CB 581CB* 3.04642EB 675FB 675GB* 1.68643AB 643CB 681CB* 3.04STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 118APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576041-0606-3 541 OUTER WING TOP BOOM NDT SDI T: 29000 FC ALI NTM1 1.30 B4-100542 I: 5800 FC CN 571124 PART 41 1.30 POST 01869543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071(B) 1 1.30 OR641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13-11 1 1.30 POST 020996421 1.30 (57-0077)643 ALI REFERENCE: 1 1.30 FROM 0 FC/FH576041-01-3TO 40000 FCACCESS: 542EB 575FB 575GB* 1.68543AB 543CB 581CB* 3.04642EB 675FB 675GB* 1.68643AB 643CB 681CB* 3.04R 576041-0606-4 541 OUTER WING TOP BOOM NDT SDI I: 3400 FC ALI NTM1 1.30 B4-100542 CN 571124 PART 41 1.30 POST 01869543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071(B) 1 1.30 OR641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13-11 1 1.30 POST 020996421 1.30 (57-0077)643 ALI REFERENCE: 1 1.30 FROM 40000 FC576041-01-6TO LOVACCESS: 542EB 575FB 575GB* 1.68543AB 543CB 581CB* 3.04642EB 675FB 675GB* 1.68643AB 643CB 681CB* 3.04R 576041-0606-5 541 OUTER WING TOP BOOM NDT SDI T: 25500 FC ALI NTM1 1.30 B4-200542 I: 5800 FC CN 571124 PART 41 1.30 C4543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071(B) 1 1.30 F4641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13-11 1 1.30 POST 018696421 1.30 OR643 ALI REFERENCE: 1 1.30 POST 02099576041-01-4(57-0077)ACCESS: 542EB 575FB 575GB* 1.68 FROM 0 FC/FH543AB 543CB 581CB* 3.04 TO 34000 FC642EB 675FB 675GB* 1.68643AB 643CB 681CB* 3.04R 576041-0606-6 541 OUTER WING TOP BOOM NDT SDI I: 3400 FC ALI NTM1 1.30 B4-200542 CN 571124 PART 41 1.30 C4543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071(B) 1 1.30 F4641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13-11 1 1.30 POST 018696421 1.30 OR643 ALI REFERENCE: 1 1.30 POST 02099* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 119APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576041-0606-6 * * * * * C O N T I N U E * * * * *ACCESS: 542EB 575FB 575GB 576041-01-5* 1.68 (57-0077)543AB 543CB 581CB* 3.04 FROM 34000 FC642EB 675FB 675GB* 1.68 TO LOV643AB 643CB 681CB* 3.04576047-0606-1 541 WING CENTER SPAR NDT SDI ST: 29000 FC ALI NTM 5711271 5.00 B2542 OR CN PART 41 5.00 POST 01868641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 32800 FH FAA AD AND PART 61 5.00 FROM 0 FC/FH642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM SI: 4500 FC CN 2006-0071(B) 1 5.00 TO 48000 FCBETWEEN RIB 1 AND RIB 6. OR FAA AD 96-13-115100 FHACCESS: 541AB 541BB ALI REFERENCE: * 3.00542CB 576047-01-1* 1.50641AB 641BB 576047-02-1* 3.00642CB* 1.50576047-0606-2 541 WING CENTER SPAR NDT SDI I: 3000 FC ALI NTM 5711271 5.00 B2542 OR CN PART 41 5.00 POST 01868641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 3400 FH FAA AD AND PART 61 5.00 FROM 48000 FC642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM CN 2006-0071(B) 1 5.00 TO LOVBETWEEN RIB 1 AND RIB 6. FAA AD 96-13-11ACCESS: 541AB 541BB ALI REFERENCE: * 3.00542CB 576047-01-2* 1.50641AB 641BB 576047-02-2* 3.00642CB* 1.50576047-0606-3 541 WING CENTER SPAR NDT SDI ST: 31000 FC ALI NTM 5711271 5.00 B4-100542 OR CN PART 41 5.00 POST 01868641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 42200 FH FAA AD AND PART 61 5.00 FROM 0 FC/FH642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM SI: 5200 FC CN 2006-0071(B) 1 5.00 TO 40000 FCBETWEEN RIB 1 AND RIB 6. OR FAA AD 96-13-117100 FHACCESS: 541AB 541BB ALI REFERENCE: * 3.00542CB 576047-01-3* 1.50641AB 641BB 576047-02-3* 3.00642CB* 1.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 120APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576047-0606-4 541 WING CENTER SPAR NDT SDI I: 3400 FC ALI NTM 5711271 5.00 B4-100542 OR CN PART 41 5.00 POST 01868641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 4600 FH FAA AD AND PART 61 5.00 FROM 40000 FC642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM CN 2006-0071(B) 1 5.00 TO LOVBETWEEN RIB 1 AND RIB 6. FAA AD 96-13-11ACCESS: 541AB 541BB ALI REFERENCE: * 3.00542CB 576047-01-4* 1.50641AB 641BB 576047-02-4* 3.00642CB* 1.50576047-0606-5 541 WING CENTER SPAR NDT SDI ST: 24000 FC ALI NTM 5711271 5.00 B4-200542 OR CN PART 41 5.00 C4641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 53000 FH FAA AD AND PART 61 5.00 F4642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM SI: 5200 FC CN 2006-0071(B) 1 5.00 POST 01868BETWEEN RIB 1 AND RIB 6. OR FAA AD 96-13-11 FROM 0 FC/FH11500 FHTO 34000 FCACCESS: 541AB 541BB ALI REFERENCE: * 3.00542CB 576047-01-5* 1.50641AB 641BB 576047-02-5* 3.00642CB* 1.50576047-0606-6 541 WING CENTER SPAR NDT SDI I: 3400 FC ALI NTM 5711271 5.00 B4-200542 OR CN PART 41 5.00 C4641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 7500 FH FAA AD AND PART 61 5.00 F4642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM CN 2006-0071(B) 1 5.00 POST 01868BETWEEN RIB 1 AND RIB 6. FAA AD 96-13-11 FROM 34000 FCTO LOVACCESS: 541AB 541BB ALI REFERENCE: * 3.00542CB 576047-01-6* 1.50641AB 641BB 576047-02-6* 3.00642CB* 1.50576051-0606-1 541 PYLON REAR ATTACHMENT NDT SDI ST: 33000 FC ALI NTM 5741131 2.00 B2542 OR CN PART 41 2.00 FROM 0 FC/FH641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 37300 FH FAA AD EASA AD1 2.00 TO 48000 FC642 DIAPHRAGM. SI: 3700 FC 2006-00711 2.00OR FAA ADACCESS: 541CB 4200 FH 2007-04-11* 1.50542DB* 1.50641CB ALI REFERENCE: * 1.50642DB 576051-01-1* 1.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 121APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576051-0606-2 541 PYLON REAR ATTACHMENT NDT SDI ST: 28000 FC ALI NTM 5741131 2.00 B4-100542 OR CN PART 41 2.00 FROM 0 FC/FH641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 38400 FH FAA AD EASA AD1 2.00 TO 40000 FC642 DIAPHRAGM. SI: 3200 FC 2006-00711 2.00OR FAA ADACCESS: 541CB 4400 FH 2007-04-11* 1.50542DB* 1.50641CB ALI REFERENCE: * 1.50642DB 576051-01-3* 1.50R 576051-0606-3 541 PYLON REAR ATTACHMENT NDT SDI ST: 24000 FC ALI NTM 5741131 2.00 B4-200542 OR EASA AD PART 41 2.00 C4641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 54500 FC FAA AD EASA AD1 2.00 F4642 DIAPHRAGM. SI: 2900 FC 2006-00711 2.00 FROM 0 FCOR FAA ADTO 34000 FCACCESS: 541CB 6600 FH 2007-04-11* 1.50542DB* 1.50641CB ALI REFERENCE: * 1.50642DB 576051-01-5* 1.50576051-0606-4 541 PYLON REAR ATTACHMENT NDT SDI I: 3500 FC ALI NTM 5741131 2.00 B2542 OR CN PART 41 2.00 FROM 48000 FC641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 3900 FH FAA AD CN 2006-0071(B) 1 2.00 TO LOV642 DIAPHRAGM. FAA AD 96-13-11 1 2.00ACCESS: 541CB ALI REFERENCE: * 1.50542DB 576051-01-2* 1.50641CB* 1.50642DB* 1.50R 576051-0606-5 541 PYLON REAR ATTACHMENT NDT SDI I: 3000 FC ALI NTM 5741131 2.00 B4-100542 OR CN PART 41 2.00 FROM 40000 FC641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 4100 FH FAA AD CN 2006-0071(B) 1 2.00 TO LOV642 DIAPHRAGM. FAA AD 96-13-11 1 2.00ACCESS: 541CB ALI REFERENCE: * 1.50542DB 576051-01-4* 1.50641CB* 1.50642DB* 1.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 122APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576051-0606-6 541 PYLON REAR ATTACHMENT NDT SDI I: 2600 FC ALI NTM 5741131 2.00 B4-200542 OR CN PART 41 2.00 C4641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 5900 FH FAA AD CN 2006-0071(B) 1 2.00 F4642 DIAPHRAGM. FAA AD 96-13-11 1 2.00 FROM 34000 FCTO LOVACCESS: 541CB ALI REFERENCE: * 1.50542DB 576051-01-6* 1.50641CB* 1.50642DB* 1.50576053-0605-1 540 WING TOP SKIN CENTER SPAR MEC DET T: SEE SB ALI CN 2006-0071(B) 1 1.00 ALL640 I: SEE SB CN FAA AD 96-13-11 1 1.00 SB 57-0158DETAILED OR NDT INSPECTION OF TOP SKIN FAA AD ISB 57-0158FROM 0 FC/FHAT CENTER SPAR JOINT BETWEEN RIB 1 AND RIB 7. ISBTO LOVALI REFERENCE:576053-01-1576055-0606-1 540 WINGS - FRONT SPAR BOTTOM BOOM NDT SDI T: SEE SB ALI NTM 5700001 13.00 ALL640 I: SEE SB CN PART 61 13.00 SB 57-0162SPECIAL DETAILED INSPECTION OF WING FRONT SPAR BOTTOM FAA AD NTM 570001FROM 0 FC/FHBOOM BETWEEN RIB 9 AND RIB 21, AND CENTER SPAR BOOM ISB PART 6TO LOVJOINT AT RIB 5. NTM 571119PART 4PREP.: AIRCRAFT TO BE DEFUELED CN 2006-0071(B)ACCESS: SEE SB FAA AD 96-13-11ISB 57-0162ALI REFERENCE:576055-01-1576056-0606-1 540 WINGS - FRONT AND REAR SPAR TOP BOOMS MEC SDI T: SEE SB ALI NTM 5700001 10.00 ALL640 I: SEE SB CN PART 61 10.00 SB 57-0164SPECIAL DETAILED INSPECTION OF THE WING FRONT AND FAA AD NTM 570001FROM 0 FC/FHREAR SPAR TOP BOOMS TO SKIN JOINT BETWEEN RIB 9 AND ISB PART 6TO LOVRIB 18. NTM 573314PART 6PREP.: AIRCRAFT TO BE DEFUELED. CN 2006-0071(B)FAA AD 96-13-11ISB 57-0164ALI REFERENCE:576056-01-1STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 123APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576057-0606-1 543 WING FRONT SPAR BETWEEN RIB 10 AND RIB NDT SDI T: SEE SB ALI NTM 5711251 2.00 B2643 11 I: SEE SB CN PART 41 2.00 SB 57-0151FAA AD CN 2006-0071(B) FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF THE BOTTOM BOOM ISB FAA AD 96-13-11 TO LOVATTACHMENT HOLES IN FRONT SPAR WEB BETWEEN RIB 10 AND ISB 57-0151RIB 11.ALI REFERENCE:ACCESS: 523EB 576057-01-1* 0.18623EB* 0.18576058-0606-1 542 WING TOP SKIN AT RIB 9 NDT SDI T: SEE ISB ALI NTM 5733181 15.00 ALL642 I: SEE ISB CN PART 41 15.00 SB 57-0193DETAILED AND SPECIAL DETAILED INSPECTION OF WING TOP FAA AD CN 2006-0071(B) FROM 0 FC/FHSKIN AND STRINGER JOINT AT RIB 9. ISB FAA AD 96-13-11 TO LOVISB 57-0193ACCESS: 542EB 543AB* 3.00642EB 643AB ALI REFERENCE: * 3.00576058-01-1576059-0606-1 543 WING SKIN JOINTS NDT SDI T: SEE SB ALI NTM 5700001 7.00 ALL550 I: SEE SB CN PART 61 7.00 SB 57-0119643 SPECIAL DETAILED INSPECTION OF BOTTOM SKIN TO REAR FAA AD NTM 5700011 7.00 FROM 0 FC/FH650 SPAR JOINT BETWEEN RIB 11 AND RIB 18. ISB PART 61 7.00 TO LOVNTM 571121ACCESS: 543BB 543CB 543DB PART 4* 4.50550BB 550CB 550DB 550EB 550FB 581CB CN 2006-0071(B) * 6.30581DB 581EB 581FB 581GB FAA AD 96-13-11643BB 643DB ISB 57-0119* 3.00650BB 650CB 650DB 650EB 650FB 681CB* 6.30681DB 681EB 681FB 681GB ALI REFERENCE:576059-01-1576060-0605-1 550 WING TOP SKIN MEC DET T: SEE SB ALI CN 2006-0071(B) 1 1.00 ALL650 I: SEE SB CN FAA AD 96-13-11 1 1.00 SB 57-0187DETAILED INSPECTION OF WING TOP SKIN AT FRONT FAA AD ISB 57-0187FROM 0 FC/FHSPAR BETWEEN RIB 1 AND RIB 7. ISBTO LOVALI REFERENCE:576060-01-1576062-0606-1 543 WING REAR SPAR BOTTOM BOOM NDT SDI T: 38000 FC ALI NTM 5711211 3.00 B2643 OR CN PART 41 3.00 PRE 01868* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 124APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576062-0606-1 * * * * * C O N T I N U E * * * * *SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 43300 FH FAA AD CN 2006-0071(B) PRE 02100BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. I: 7000 FC FAA AD 96-13-11 (57-0078)ORFROM 0 FC/FHACCESS: 543AB 8000 FH ALI REFERENCE: * 1.50 TO LOV643AB 576062-01-1* 1.50576062-0606-2 543 WING REAR SPAR BOTTOM BOOM NDT SDI T: 33000 FC ALI NTM 5711211 3.00 B4-100643 OR CN PART 41 3.00 PRE 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH FAA AD CN 2006-0071(B) PRE 02100BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. I: 7000 FC FAA AD 96-13-11 (57-0078)ORFROM 0 FC/FHACCESS: 543AB 9700 FH ALI REFERENCE: * 1.50 TO 40000 FC643AB 576062-01-2* 1.50576062-0606-3 543 WING REAR SPAR BOTTOM BOOM NDT SDI I: 5400 FC ALI NTM 5711211 3.00 B4-100643 OR CN PART 41 3.00 PRE 01868SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 7500 FH FAA AD CN 2006-0071(B) PRE 02100BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. FAA AD 96-13-11 (57-0078)FROM 40000 FCACCESS: 543AB ALI REFERENCE: * 1.50 TO LOV643AB 576062-01-3* 1.50576062-0606-4 543 WING REAR SPAR BOTTOM BOOM NDT SDI T: 27000 FC ALI NTM 5711211 3.00 B4-200643 OR CN PART 41 3.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 62600 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. I: 7000 FC FAA AD 96-13-11 PRE 01868ORPRE 02100ACCESS: 543AB 16200 FH ALI REFERENCE: * 1.50 (57-0078)643AB 576062-01-4* 1.50 FROM 0 FC/FHTO 34000 FC576062-0606-5 543 WING REAR SPAR BOTTOM BOOM NDT SDI I: 4700 FC ALI NTM 5711211 3.00 B4-200643 OR CN PART 41 3.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 10900 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. FAA AD 96-13-11 PRE 01868PRE 02100ACCESS: 543AB ALI REFERENCE: * 1.50 (57-0078)643AB 576062-01-5* 1.50 FROM 34000 FCTO LOVSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 125APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576063-0606-1 541 FRONT AND REAR SPAR BOTTOM BOOM NDT SDI T: 29000 FC ALI NTM 5713111 0.60 B4-100543 OR CN PART 41 0.60 PRE 10470550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 39700 FH FAA AD CN 2006-0071(B) 1 0.60 (57-0207)641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES I: 5400 FC FAA AD 96-13-11 1 0.60 FROM 0 FC/FH643 EXEPT AT STRINGER 19. OR1 0.60 TO 40000 FC650 7400 FH ALI REFERENCE: 1 0.60576063-01-1576063-0606-2 541 FRONT AND REAR SPAR BOTTOM BOOM NDT SDI I: 3100 FC ALI NTM 5713111 0.60 B4-100543 OR CN PART 41 0.60 PRE 10470550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 4200 FH FAA AD CN 2006-0071(B) 1 0.60 (57-0207)641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES FAA AD 96-13-11 1 0.60 FROM 40000 FC643 EXEPT AT STRINGER 19.1 0.60 TO LOV650 ALI REFERENCE: 1 0.60576063-01-2576063-0606-3 541 FRONT AND REAR SPAR BOTTOM BOOM NDT SDI T: 25000 FC ALI NTM 5713111 0.60 B4-200543 OR CN PART 41 0.60 C4550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 56700 FH FAA AD CN 2006-0071(B) 1 0.60 F4641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES I: 4500 FC FAA AD 96-13-11 1 0.60 PRE 10470643 EXEPT AT STRINGER 19. OR1 0.60 (57-0207)650 10200 FH ALI REFERENCE: 1 0.60 FROM 0 FC/FH576063-01-3TO 34000 FC576063-0606-4 541 FRONT AND REAR SPAR BOTTOM BOOM NDT SDI I: 2500 FC ALI NTM 5713111 0.60 B4-200543 OR CN PART 41 0.60 C4550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 5700 FH FAA AD CN 2006-0071(B) 1 0.60 F4641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES FAA AD 96-13-11 1 0.60 PRE 10470643 EXEPT AT STRINGER 19.1 0.60 (57-0207)650 ALI REFERENCE: 1 0.60 FROM 34000 FC576063-01-4TO LOV576064-0606-1 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI ST: 35000 FC ALI NTM 5713111 1.00 B2650 OR CN PART 41 1.00 PRE 10326SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 39500 FH FAA AD CN 2006-0071(B) (57-0203)BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB SI: 7000 FC FAA AD 96-13-11 FROM 0 FC/FH13 AND RIB 14. ORTO 48000 FC7900 FH ALI REFERENCE:576064-01-1STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 126APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576064-0606-2 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI I: 7000 FC ALI NTM 5713111 1.00 B2650 OR CN PART 41 1.00 PRE 10326SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 7900 FH FAA AD CN 2006-0071(B) (57-0203)BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB FAA AD 96-13-11 FROM 48000 FC13 AND RIB 14.TO LOVALI REFERENCE:576064-01-2576064-0606-3 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI ST: 31000 FC ALI NTM 5713111 1.00 B4-100650 OR CN PART 41 1.00 PRE 10326SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 42500 FH FAA AD CN 2006-0071(B) (57-0203)BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB SI: 7000 FC FAA AD 96-13-11 FROM 0 FC/FH13 AND RIB 14. ORTO 40000 FC9600 FH ALI REFERENCE:576064-01-3576064-0606-4 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI I: 5400 FC ALI NTM 5713111 1.00 B4-100650 OR CN PART 41 1.00 PRE 10326SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 7400 FH FAA AD CN 2006-0071(B) (57-0203)BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB FAA AD 96-13-11 FROM 40000 FC13 AND RIB 14.TO LOVALI REFERENCE:576064-01-4576064-0606-5 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI ST: 26000 FC ALI NTM 5713111 1.00 B4-200650 OR CN PART 41 1.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 59000 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB SI: 7000 FC FAA AD 96-13-11 PRE 1032613 AND RIB 14. OR(57-0203)15900 FH ALI REFERENCE: FROM 0 FC/FH576064-01-5TO 34000 FC576064-0606-6 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI I: 4700 FC ALI NTM 5713111 1.00 B4-200650 OR CN PART 41 1.00 C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 10700 FH FAA AD CN 2006-0071(B) F4BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB FAA AD 96-13-11 PRE 1032613 AND RIB 14.(57-0203)ALI REFERENCE: FROM 34000 FC576064-01-6TO LOVSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 127APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576065-0606-1 540 BOTTOM SKIN AT DRAIN VALVES MEC DET ST: 28000 FC ALI CN 2006-0071(B) 1 2.00 B2550 SI: 2900 FC CN FAA AD 96-13-11 1 2.00 FROM 0 FC/FH640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD1 2.00 TO 48000 FC650 WATER DRAIN VALVES BETWEEN RIB 5 AND 14 AND 15 AND ALI REFERENCE: 1 2.0022 AND AT MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 576065-01-1AND RIB 14.NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0607-1.576065-0606-2 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 2600 FC ALI CN 2006-0071(B) 1 3.00 B2550 CN FAA AD 96-13-11 1 3.00 FROM 48000 FC640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD1 3.00 TO LOV650 WATER DRAIN VALVES BETWEEN RIB 5 AND 14 AND 15 AND 22 ALI REFERENCE: 1 3.00AND AT MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 576065-01-2AND RIB 14.NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0607-2.576065-0606-3 540 BOTTOM SKIN AT DRAIN VALVES MEC DET ST: 24000 FC ALI CN 2006-0071(B) 1 2.00 B4-100550 SI: 2200 FC CN FAA AD 96-13-11 1 2.00 FROM 0 FC/FH640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD1 2.00 TO 40000 FC650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT ALI REFERENCE: 1 2.00MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14. 576065-01-3NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0607-3.576065-0606-4 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 2200 FC ALI CN 2006-0071(B) 1 3.00 B4-100550 CN FAA AD 96-13-11 1 3.00 FROM 40000 FC640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD1 3.00 TO LOV650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT ALI REFERENCE: 1 3.00MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14. 576065-01-4NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0607-4.576065-0606-5 540 BOTTOM SKIN AT DRAIN VALVES MEC DET ST: 19000 FC ALI CN 2006-0071(B) 1 2.00 B4-200550 SI: 1900 FC CN FAA AD 96-13-11 1 2.00 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 128APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576065-0606-5 * * * * * C O N T I N U E * * * * *640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD ALI REFERENCE: 1 2.00 F4650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT 576065-01-51 2.00 FROM 0 FC/FHMAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.TO 34000 FCNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0607-5.576065-0606-6 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 1900 FC ALI CN 2006-0071(B) 1 3.00 B4-200550 CN FAA AD 96-13-11 1 3.00 C4640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD1 3.00 F4650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT ALI REFERENCE: 1 3.00 FROM 34000 FCMAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14. 576065-01-6TO LOVNOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0607-6.576065-0607-1 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI ST: 28000 FC ALI NTM 5730111 2.00 B2550 SI: 5800 FC CN PART 61 2.00 FROM 0 FC/FH640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071(B) 1 2.00 TO 48000 FC650 AT WATER DRAIN VALVES FROM RIB 5 TO RIB 14 FROM RIB FAA AD 96-13-11 1 2.0015 TO RIB 22 AND AT MAGNETIC LEVEL INDICATORS BETWEENRIB 13 AND RIB 14. ALI REFERENCE:576065-02-1NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0606-1.576065-0607-2 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI I: 5100 FC ALI NTM 5730111 3.00 B2550 CN PART 61 3.00 FROM 48000 FC640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071(B) 1 3.00 TO LOV650 AT WATER DRAIN VALVES FROM RIB 5 TO RIB 14, FROM RIB FAA AD 96-13-11 1 3.0015 TO RIB 22 AND AT MAGNETIC LEVEL INDICATORS BETWEENRIB 13 AND RIB 14. ALI REFERENCE:576065-02-2NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK576065-0606-2.576065-0607-3 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI ST: 24000 FC ALI NTM 5730111 2.00 B4-100550 SI: 5000 FC CN PART 61 2.00 FROM 0 FC/FH640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071(B) 1 2.00 TO 40000 FC* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 129APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576065-0607-3 * * * * * C O N T I N U E * * * * *650 AT WATER DRAIN VALVES BETWEEN RIB 5 TO 22 AND AT FAA AD 96-13-11 1 2.00MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.ALI REFERENCE:NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-3576065-0606-3.576065-0607-4 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI I: 4400 FC ALI NTM 5730111 3.00 B4-100550 CN PART 61 3.00 FROM 40000 FC640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071(B) 1 3.00 TO LOV650 AT WATER DRAIN VALVES BETWEEN RIB 5 TO 22 AND AT FAA AD 96-13-11 1 3.00MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.ALI REFERENCE:NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-4576065-0606-4.576065-0607-5 540 BOTTOM SKIN AT DRAIN VALVES MEC DET ST: 19000 FC ALI NTM 5730111 2.00 B4-200550 SI: 3800 FC CN PART 61 2.00 C4640 NDT INSPECTION OF OUTER WING BOTTOM FAA AD CN 2006-0071(B) 1 2.00 F4650 SKIN AT WATER DRAIN VALVES BETWEEN RIB 5 TO 22 AND AT FAA AD 96-13-11 1 2.00 FROM 0 FC/FHMAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.TO 34000 FCALI REFERENCE:NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-5576065-0606-5.576065-0607-6 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 3700 FC ALI NTM 5730111 3.00 B4-200550 CN PART 61 3.00 C4640 NDT INSPECTION OF OUTER WING BOTTOM FAA AD CN 2006-0071(B) 1 3.00 F4650 SKIN AT WATER DRAIN VALVES BETWEEN RIB 5 TO 22 AND AT FAA AD 96-13-11 1 3.00 FROM 34000 FCMAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.TO LOVALI REFERENCE:NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-6576065-0606-6.576066-0606-1 540 BOTTOM SKIN CENTER SPAR, RIBS 1-6 NDT SDI T: SEE SB ALI NTM 5711271 24.00 ALL640 I: SEE SB CN PART 4 AND 61 24.00 SB 57-0208SPECIAL DETAILED INSPECTION OF BOTTOM SKIN TO CENTER FAA AD CN 2006-0071(B) FROM 0 FC/FHSPAR JOINT BETWEEN RIB 1 AND RIB 6. (EXCLUDING RIB 5) FAA AD 96-13-11 TO LOVACCESS: 541AB 541BB 541CB 542CB 542DB ALI REFERENCE: * 7.50* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 130APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576066-0606-1 * * * * * C O N T I N U E * * * * *641AB 641BB 641CB 642CB 642DB 576066-01-1* 7.50576067-0606-1 550 BOTTOM SKIN MANHOLE, RIBS 11-21 NDT SDI T: 25500 FC ALI NTM 5733151 3.00 B2650 OR CN PART 61 3.00 FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 28800 FH FAA AD CN 2006-0071(B) TO 48000 FCMANHOLE SURROUNDS BETWEEN RIB 11 AND RIB 21. I: 8400 FC FAA AD 96-13-11ORACCESS: 543AB 543BB 543CB 543DB 550BB 550DB 9500 FH ALI REFERENCE: * 16.50550EB 550FB 550GB 550HB 550JB 576067-01-1643AB 643BB 643CB 643DB 650BB 650DB* 16.50650EB 650FB 650GB 650HB 650JB576067-0606-2 550 BOTTOM SKIN MANHOLE, RIBS 11-21 NDT SDI I: 7600 FC ALI NTM 5733151 3.00 B2650 OR CN PART 61 3.00 FROM 48000 FCSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 8600 FH FAA AD CN 2006-0071(B) TO LOVMANHOLE SURROUNDS BETWEEN RIB 11 AND RIB 21. FAA AD 96-13-11ACCESS: 543AB 543BB 543CB 543DB 550BB 550DB ALI REFERENCE: * 16.50550EB 550FB 550GB 550HB 550JB 576067-01-2643AB 643BB 643CB 643DB 650BB 650DB* 16.50650EB 650FB 650GB 650HB 650JB576068-0606-1 542 WING TOP SKIN, RIB 9 NDT SDI T: 30400 FC ALI NTM 5733111 1.50 B2543 I: 2800 FC CN PART 21 1.50 POST 01869642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 5733181 1.50 OR643 AND STRINGER JOINT AT RIB 9. PART 41 1.50 POST 02099CN 2006-0071(B) (57-0077)ACCESS: 542EB FAA AD 96-13-11 * 1.50 FROM 0 FC/FH543AB* 1.50 TO 48000 FC642EB ALI REFERENCE: * 1.50643AB 576068-01-1* 1.50576068-02-1576068-0606-2 542 WING TOP SKIN, RIB 9 NDT SDI I: 2500 FC ALI NTM 5733111 1.50 B2543 CN PART 21 1.50 POST 01869642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 5733181 1.50 OR643 AND STRINGER JOINT AT RIB 9. PART 41 1.50 POST 02099CN 2006-0071(B) (57-0077)ACCESS: 542EB FAA AD 96-13-11 * 1.50 FROM 48000 FC* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 131APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576068-0606-2 * * * * * C O N T I N U E * * * * *543AB ALI REFERENCE: * 1.50 TO LOV642EB 576068-01-4* 1.50643AB 576068-02-4* 1.50576068-0606-3 542 WING TOP SKIN, RIB 9 NDT SDI T: 34100 FC ALI NTM 5733111 1.50 B4-100543 I: 2800 FC CN PART 21 1.50 POST 01869642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 5733181 1.50 OR643 AND STRINGER JOINT AT RIB 9. PART 41 1.50 POST 02099CN 2006-0071(B) (57-0077)ACCESS: 542EB FAA AD 96-13-11 * 1.50 FROM 0 FC/FH543AB* 1.50 TO 40000 FC642EB ALI REFERENCE: * 1.50643AB 576068-01-2* 1.50576068-02-2576068-0606-4 542 WING TOP SKIN, RIB 9 NDT SDI I: 2500 FC ALI NTM 5733111 1.50 B4-100543 CN PART 21 1.50 POST 01869642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 5733181 1.50 OR643 AND STRINGER JOINT AT RIB 9. PART 41 1.50 POST 02099CN 2006-0071(B) (57-0077)ACCESS: 542EB FAA AD 96-13-11 * 1.50 FROM 40000 FC543AB* 1.50 TO LOV642EB ALI REFERENCE: * 1.50643AB 576068-01-5* 1.50576068-02-5576068-0606-5 542 WING TOP SKIN, RIB 9 NDT SDI T: 30200 FC ALI NTM 5733111 1.50 B4-200543 I: 2800 FC CN PART 21 1.50 C4642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 5733181 1.50 F4643 AND STRINGER JOINT AT RIB 9. PART 41 1.50 POST 01869CN 2006-0071(B) ORACCESS: 542EB FAA AD 96-13-11 * 1.50 POST 02099543AB* 1.50 (57-0077)642EB ALI REFERENCE: * 1.50 FROM 0 FC/FH643AB 576068-01-3* 1.50 TO 34000 FC576068-02-3576068-0606-6 542 WING TOP SKIN, RIB 9 NDT SDI I: 2500 FC ALI NTM 5733111 1.50 B4-200543 CN PART 21 1.50 C4* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 132APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576068-0606-6 * * * * * C O N T I N U E * * * * *642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 5733181 1.50 F4643 AND STRINGER JOINT AT RIB 9. PART 41 1.50 POST 01869CN 2006-0071(B) ORACCESS: 542EB FAA AD 96-13-11 * 1.50 POST 02099543AB* 1.50 (57-0077)642EB ALI REFERENCE: * 1.50 FROM 34000 FC643AB 576068-01-6* 1.50 TO LOV576068-02-6576069-0606-1 550 WINGS MANHOLE SURROUND STRUCTURE NDT SDI T: SEE SB ALI NTM 5733171 TBD ALL650 I: SEE SB CN PART 61 TBD SB 57-0211SPECIAL DETAILED INSPECTION OF MANHOLE SURROUND FAA AD CN 2006-0071(B) FROM 0 FC/FHSTRUCTURE IN FASTENER HOLES. FAA AD 96-13-11 TO LOVACCESS: 550KB 550LB ALI REFERENCE: * 3.00650KB 650LB 576069-01-1* 3.00576070-0606-1 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI ST: 29000 FC ALI NTM 5711271 8.50 B2542 RIB OR CN PART 41 8.50 FROM 0 FC/FH641 32800 FH FAA AD AND PART 61 8.50 TO 48000 FC642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SI: 4500 FC CN 2006-0071(B) 1 8.50SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 OR FAA AD 96-13-11AND HALF RIBS. 5100 FHALI REFERENCE:ACCESS: 541CB 576070-01-1* 1.50542DB 576070-02-1* 1.50641CB* 1.50642DB* 1.50576070-0606-2 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI I: 3000 FC ALI NTM 5711271 8.50 B2542 RIB OR CN PART 41 8.50 FROM 48000 FC641 3400 FH FAA AD AND PART 61 8.50 TO LOV642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM CN 2006-0071(B) 1 8.50SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 FAA AD 96-13-11AND HALF RIBS.ALI REFERENCE:ACCESS: 541CB 576070-01-2* 1.50542DB 576070-02-2* 1.50641CB* 1.50642DB* 1.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 133APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576070-0606-3 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI ST: 31000 FC ALI NTM 5711271 8.50 B4-100542 RIB OR CN PART 41 8.50 FROM 0 FC/FH641 42200 FH FAA AD AND PART 61 8.50 TO 40000 FC642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SI: 5200 FC CN 2006-0071(B) 1 8.50SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 OR FAA AD 96-13-11AND HALF RIBS. 7100 FHALI REFERENCE:ACCESS: 541CB 576070-01-3* 1.50542DB 576070-02-3* 1.50641CB* 1.50642DB* 1.50576070-0606-4 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI I: 3400 FC ALI NTM 5711271 8.50 B4-100542 RIB OR CN PART 41 8.50 FROM 40000 FC641 7100 FH FAA AD AND PART 61 8.50 TO LOV642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM CN 2006-0071(B) 1 8.50SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 FAA AD 96-13-11AND HALF RIBS.ALI REFERENCE:ACCESS: 541CB 576070-01-4* 1.50542DB 576070-02-4* 1.50641CB* 1.50642DB* 1.50576070-0606-5 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI ST: 24000 FC ALI NTM 5711271 8.50 B4-200542 RIB OR CN PART 41 8.50 C4641 53000 FH FAA AD AND PART 61 8.50 F4642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SI: 5200 FC CN 2006-0071(B) 1 8.50 FROM 0 FC/FHSKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 OR FAA AD 96-13-11 TO 34000 FCAND HALF RIBS. 11500 FHALI REFERENCE:ACCESS: 541CB 576070-01-5* 1.50542DB 576070-02-5* 1.50641CB* 1.50642DB* 1.50576070-0606-6 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI I: 3400 FC ALI NTM 5711271 8.50 B4-200542 RIB OR CN PART 41 8.50 C4641 7500 FH FAA AD AND PART 61 8.50 F4642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM CN 2006-0071(B) 1 8.50 FROM 34000 FCSKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 FAA AD 96-13-11 TO LOVAND HALF RIBS.* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 134APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576070-0606-6 * * * * * C O N T I N U E * * * * *ACCESS: 541CB ALI REFERENCE: * 1.50542DB 576070-01-6* 1.50641CB 576070-02-6* 1.50642DB* 1.50576071-0606-1 550 BOTTOM SKIN MEC DET T: SEE SB ALI NTM 5130051 1.50 B2650 I: SEE SB CN PART 11 1.50 SB 57-0225NDT OR DETAILED INSPECTION OF OUTER WING BOX BOTTOM FAA AD NTM 513010FROM 0 FC/FHSKIN, WATER DRAIN VALVE BETWEEN RIB 14 AND RIB 15. PART 1TO LOVNTM 573004PART 1CN 2006-0071(B)FAA AD 96-13-11ALI REFERENCE:576071-01-1576072-0606-1 542 TOP SKIN MEC DET T: 48000 FC ALI EASA AD1 TBD B2642 I: 4000 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF OUTER WING REAR SPAR TOP FAA ADTO LOVBOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2007-04-11NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE:TASK 576072-0606-2 576072-01-1576072-0606-2 542 TOP SKIN NDT SDI T: 48000 FC ALI NTM 5711281 TBD B2642 I: 4000 FC FAA AD PART 41 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR EASA ADTO LOVTOP BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2006-0071FAA ADNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 576072-0606-1ALI REFERENCE:576072-02-1576072-0606-3 542 TOP SKIN MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100642 I: 4000 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF OUTER WING REAR SPAR TOP FAA ADTO LOVBOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2007-04-11* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 135APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576072-0606-3 * * * * * C O N T I N U E * * * * *ALI REFERENCE:NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 576072-01-2TASK 576072-0606-4576072-0606-4 542 TOP SKIN NDT SDI T: 40000 FC ALI NTM 5711281 TBD B4-100642 I: 4000 FC FAA AD PART 41 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR EASA ADTO LOVTOP BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2006-0071FAA ADNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 576072-0606-3ALI REFERENCE:576072-02-2576072-0606-5 542 TOP SKIN MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200642 I: 4000 FC FAA AD 2006-00711 TBD C4DETAILED INSPECTION OF OUTER WING REAR SPAR TOP FAA ADF4BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2007-04-11FROM 0 FC/FHTO LOVNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENCE:TASK 576072-0606-6 576072-01-3576072-0606-6 542 TOP SKIN NDT SDI T: 34000 FC ALI NTM 5711281 TBD B4-200642 I: 4000 FC FAA AD PART 41 TBD C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR EASA ADF4TOP BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2006-0071FROM 0 FC/FHFAA ADTO LOVNOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11TASK 576072-0606-5ALI REFERENCE:576072-02-3576073-0606-1 550 OUTER WING TOP SKIN MEC DET T: 48000 FC ALI EASA AD1 TBD B2650 I: 6000 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF OUTER WING TOP SKIN AT FAA ADTO LOVATTACHMENT TO RIB FROM RIB 10 TO RIB 18 BETWEEN 2007-04-11FRONT AND REAR SPAR.ALI REFERENCE:576073-01-1STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 136APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)576073-0606-2 550 OUTER WING TOP SKIN MEC DET T: 40000 FC ALI EASA AD1 TBD B4-100650 I: 6000 FC FAA AD 2006-00711 TBD FROM 0 FC/FHDETAILED INSPECTION OF OUTER WING TOP SKIN AT FAA ADTO LOVATTACHMENT TO RIB FROM RIB 10 TO RIB 18 BETWEEN 2007-04-11FRONT AND REAR SPAR.ALI REFERENCE:576073-01-2576073-0606-3 550 OUTER WING TOP SKIN MEC DET T: 34000 FC ALI EASA AD1 TBD B4-200650 I: 6000 FC FAA AD 2006-00711 TBD C4DETAILED INSPECTION OF OUTER WING TOP SKIN AT FAA ADF4ATTACHMENT TO RIB FROM RIB 10 TO RIB 18 BETWEEN 2007-04-11FROM 0 FC/FHFRONT AND REAR SPAR.TO LOVALI REFERENCE:576073-01-3576074-0606-1 550 OUTER WING REAR SPAR NDT SDI T: 48000 FC ALI NTM 5711291 TBD B2650 I: 6000 FC CN PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FAA AD CN 2006-0071(B) TO LOVRIB 18 ATTACHMENT POST. FAA AD 96-13-11ACCESS: 550HB ALI REFERENCE: * 1.50650HB 576074-01-1* 1.50576074-0606-2 550 OUTER WING REAR SPAR NDT SDI T: 40000 FC ALI NTM 5711291 TBD B4-100650 I: 6000 FC CN PART 61 TBD FROM 0 FC/FHSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FAA AD CN 2006-0071(B) TO LOVRIB 18 ATTACHMENT POST. FAA AD 96-13-11ACCESS: 550HB ALI REFERENCE: * 1.50650HB 576074-01-2* 1.50576074-0606-3 550 OUTER WING REAR SPAR NDT SDI T: 34000 FC ALI NTM 5711291 TBD B4-200650 I: 6000 FC CN PART 61 TBD C4SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FAA AD CN 2006-0071(B) F4RIB 18 ATTACHMENT POST. FAA AD 96-13-11 FROM 0 FC/FHTO LOVACCESS: 550HB ALI REFERENCE: * 1.50650HB 576074-01-3* 1.50STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 137APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)578011-0602-1 540 SLAT TRACK CAN DRAIN HOLES MEC DET I: 5 YE CPCP MRB REFERENCE: 1 0.80 ALL550 578011-C602-11 0.80560 DETAILED INSPECTION OF SLAT CAN DRAIN HOLES.1 0.806401 0.806501 0.806601 0.80578013-0603-1 512 WING LEADING EDGE MEC GVI T: IMPL.AGE CPCP MRB REFERENCE: 1 2.00 ALL523 10 YE 578013-C603-11 2.00524 GENERAL VISUAL INSPECTION OF WING FRONT SPAR FORWARD I: 5 YE1 2.00612 FACE.1 2.006231 2.00624 NOTE: 01. ALUMINIUM SHIELD BETWEEN SLAT TRACK 3 TO 81 2.00REMOVED.02. APPLY TEMPORARY PROTECTION AFTER INSPECTIONPREP.: SLATS TO BE EXTENDEDACCESS: 512AB 512AT 512BB 512CB 512DB 512EB* 1.70512FB 512GB 512HB 512JB 512KB 512LB523AB 523BB 523CB 523DB 523EB 523FB* 1.11523GB 523HB 523JB 523KB 523LB 523MB524AB 524BB 524CB 524DB 524EB 524FB* 1.25524GB 524HB 524JB 524KB612AB 612AT 612BB 612CB 612DB 612EB* 1.67612FB 612GB 612HB 612JB 612KB 612LB623AB 623BB 623CB 623DB 623EB 623FB* 1.11623GB 623HB 623JB 623KB 623LB 623MB624AB 624BB 624CB 624DB 624EB 624FB* 1.25624GB 624HB 624JB 624KB578021-0602-1 181 WING LOWER SKIN MEC DET I: 30 MO CPCP MRB REFERENCE: 1 0.30 ALL182 MRB S1 0.30DETAILED INSPECTION OF WING LOWER SKIN BETWEEN 578021-C602-1FUSELAGE AND RIB 2 LH/RH.578021-0602-2 181 WING CENTER BOX - INBOARD AND OUTBOARD MEC DET I: ISB AD AD EASA AD2 6.00 ALL182 57-204 CN F-2008-02082 6.00DETAILED INSPECTION OF WING BOTTOM SKIN, ISB FAA AD 98-21-34INBOARD AND OUTBOARD OF THE RIB 1 EXTERNAL LOWER SB 57-0204SURFACE SPLICE BETWEEN FR. 40 AND FR. 47STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 138APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)578023-0603-1 511 WING LEADING EDGE MEC DET I: 5 YE CPCP MRB REFERENCE: 1 0.30 ALL611 578023-C603-11 0.30DETAILED INSPECTION OF EXTERNAL SURFACE OFSLAT NO 1.PREP.: SLATS TO BE EXTENDED.578031-0603-1 513 WING LEADING EDGE MEC DET T: IMPL.AGE CPCP MRB REFERENCE: 1 1.00 KRUEGER FLAP613 10 YE 578031-C603-11 1.00DETAILED INSPECTION OF FORWARD WING ROOT, I: 5 YEINTERNAL STRUCTURE.NOTE: APPLY TEMPORARY PROTECTION AFTER INSPECTIONPREP.: KRUEGER FLAPS TO BE EXTENDEDACCESS: 512AB 513AB 513AT* 0.72612AB 613AB 613AT* 0.43578101-0603-1 530 FLAP TRACK BEAMS NO 2 TO 6 MEC DET I: 5 YE CPCP MRB REFERENCE: 1 2.00 ALL630 578101-C603-11 2.00DETAILED INSPECTION OF FLAP TRACK BEAMS NUMBER2 TO 6, EXTERNAL SURFACE.NOTE: 01. LUBRICATION RECOMMENDED AS PER572500-0505-1.02. FLAPS MUST BE FULLY EXTENDED PRIOR TOINSPECTION, FLAP TRACK FAIRINGS MUST BEDETACHED.578255-0603-1 582 AIR BRAKES END RIBS MEC DET T: 15 YE CPCP MRB REFERENCE: 1 1.00 ALL682 I: 6 YE 578255-C603-11 1.00DETAILED INSPECTION OF INNER AND OUTER AIRBRAKES, SPAR END RIB, HINGES AND SERVO CONTROL FRONTATTACHMENT BRACKETS.PREP.: AIRBRAKES TO BE DEPLOYED.578261-0603-1 580 SPOILERS END RIBS MEC DET T: 15 YE CPCP MRB REFERENCE: 1 1.00 ALL680 IMPL.AGE 578261-C603-11 1.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 139APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)578261-0603-1 * * * * * C O N T I N U E * * * * *DETAILED INSPECTION OF INNER, CENTER AND OUTER I: 6 YESPOILER END RIB HINGES, LINKS AND SERVO CONTROLATTACHMENT BRACKETS.PREP.: SPOILER TO BE DEPLOYED.578261-0606-1 585 SPOILERS END RIBS NDT SDI T: 48000 FC ALI NTM 5782611 1.00 ALL586 I: 5500 FC FAA AD PART 61 1.00 FROM 0 FC/FH685 SPECIAL DETAILED INSPECTION OF SPOILER 1 AND 2 EASA AD1 1.00 TO LOV686 ACTUATOR BRACKET LUGS. 2006-00711 1.00FAA ADPREP: DETACH JACK ATTACHMENT. 2007-04-11ALI REFERENCE:578261-01-1578265-0603-1 580 AIRBRAKE AND SPOILER MEC DET I: 10 YE CPCP MRB REFERENCE: 1 1.00 POST 5132680 578265-C603-11 1.00DETAILED INSPECTION OF AIRBRAKES AND SPOILERSACTUATOR BEAM ATTACHMENT BOLTS.PREP.: AIRBRAKES/SPOILERS TO BE DEPLOYED. BOLTS TOBE REMOVED.GRACE PERIOD: 5 YEARS STARTING FROM THE ISSUANCE DATEOF CPCP REVISION 07.ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB* 0.35581JB 581KB681CB 681DB 681EB 681FB 681GB 681HB* 0.35681JB 681KB578271-0603-1 576 AILERONS END RIBS MEC DET T: IMPL.AGE CPCP MRB REFERENCE: 1 1.00 ALL592 15 YE 578271-C603-11 1.00676 DETAILED INSPECTION OF ALL SPEED AILERON AND I: 9 YE1 1.00692 LOW SPEED AILERON END RIBS, HINGES LINK, AND SERVO1 1.00CONTROL ATTACHMENT BRACKETS.PREP.: ALL SPEED AND LOW SPEED AILERON TO BE DEPLOYEDSTRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 140APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)578281-0603-1 570 FLAP END RIBS MEC DET T: IMPL.AGE CPCP MRB REFERENCE: 1 1.00 ALL580 15 YE 578281-C603-11 1.00670 DETAILED INSPECTION OF INNER, CENTER AND OUTER I: 9 YE1 1.00680 FLAP END RIBS.1 1.00PREP.: EXTEND FLAPS578301-0603-1 570 FLAP TAB HINGES MEC DET I: 4 YE CPCP MRB REFERENCE: 1 0.50 ALL580 578301-C603-11 0.50670 DETAILED INSPECTION OF FLAP TAB HINGES, DRIVE1 0.50680 MECHANISM AND BRACKETS.1 0.50PREP.: FLAP TAB FAIRINGS TO BE REMOVEDFLAPS TO BE EXTENDEDACCESS: 572AB 572CB 572GB 572LB 575AB 575BB* 3.68575CB 575DB 575FB 575GB 576AB 576BB576CB 576DB 576EB 576FB 577AB 577BB577ET 577FT 577GT581DB 581EB 581FB 581GB 581HB 581JB* 0.31581KB672AB 672CB 672GB 672LB 675AB 675BB* 3.72675CB 675DB 675FB 675GB 676AB 676BB676CB 676DB 676EB 676FB 677AB 677BB677ET 677FT 677GT681DB 681EB 681FB 681GB 681HB 681JB* 0.31681KB579001-0603-1 550 WING MEC DET T: 9 YE ISB ISB 57-02121 2.00 ALL650 I: 5 YE1 2.00DETAILED INSPECTION OF MAIN LANDING GEARATTACHMENT LUGS.ACCESS: OPEN THE MAIN LANDING GEAR DOORS.579002-0603-1 532 WING MEC DET T: 8200 FC ISB ISB 57-02371 2.00 ALL533 OR1 2.00534 DETAILED INSPECTION OF THE REAR ATTACHMENT 5 YE1 2.00535 BOLTS OF THE FLAP TRACKS 2 THRU 6 I: 8200 FC1 2.00536 OR1 2.00632 ACCESS: EXTEND THE FLAPS. 5 YE1 2.006331 2.00* * * * * C O N T I N U E D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 141APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)579002-0603-1 * * * * * C O N T I N U E * * * * *6341 2.006351 2.006361 2.00579003-0603-1 571 WING NDT SDI T: 18000 FC CN NTM 5131041 2.00 B2671 I: 700 FC FAA AD PART 11 2.00 PRE 11932SPECIAL DETAILED INSPECTION OF ATTACHMENT FITTING ISB NTM 574212(57-0235)GEAR RIB 5 PART 1CN 2002-620(B)ACCESS: REMOVE THE MLG ACTUATING CYLINDER ASSEMBLY FAA AD2000-05-07ISB 57A0234579003-0603-2 571 WING NDT SDI T: 14500 FC CN NTM 5131041 2.00 B4671 I: 700 FC FAA AD PART 11 2.00 PRE 11932SPECIAL DETAILED INSPECTION OF ATTACHMENT FITTING ISB NTM 574212(57-0235)GEAR RIB 5 PART 1CN 2002-620(B)ACCESS: REMOVE THE MLG ACTUATING CYLINDER ASSEMBLY FAA AD2000-05-07ISB 57A0234579004-0603-1 571 MAIN LANDING GEAR ATTACHMENT FITTING MEC DET T: 12000 FC ISB ISB 57-02511 0.50 PRE 13348671 I: 100 FC1 0.50 (57-0249)DETAILED VISUAL INSPECTION OF MAIN LANDING GEARRIB 5 AFT BEARING FORWARD LUG.NOTE: THIS TASK IS AN ALTERNATIVE TO 579004-0603-2.579004-0603-2 571 MAIN LANDING GEAR ATTACHMENT FITTING NDT SDI T: 12000 FC ISB NTM 5742111 2.00 PRE 13348671 I: 675 FC PART 41 2.00 (57-0249)SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR ISB 57-0251RIB 5 AFT BEARING FORWARD LUG.NOTE: THIS TASK IS AN ALTERNATIVE TO 579004-0603-1.* * * * * E N D * * * * *STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION:3-57 PAGE 142

# MAINTENANCE PLANNING DOCUMENT

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# INTRODUCTION

1. GENERAL

This section provides the General Visual Inspection (GVI) requirements for each aircraft zone to inspect

system and powerplant installations for security and general condition and structure for general

condition.

Inspections are to be accomplished at or before the stated intervals.

The inspections are specified by quoting the relevant zone number, zone description, access

requirements and intervals.

The extent of the inspections is defined by the preparation and access requirements.

The zone is to be inspected as visible with the relevant access open.

There are zones which will require more than one inspection at different Intervals, because the depth at

which the zone is to be examined may necessitate differing levels of accessibility.

The Zonal tasks must also inspect the general condition of any fairings. Panels, or other items which

are removed/opened to gain access to a particular zone.

The inspection tasks in this Zonal Program do not provide a complete summary of all structure and

systems items to be inspected in the affected zone. It is therefore considered that the person performing

the inspection has an adequate knowledge of the aircraft construction and of its system installation.

2. GUIDANCE FOR ACCOMPLISHMENT OF A ZONAL GVI

A Zonal GVI requires a visual examination to detect obvious unsatisfactory conditions and

discrepancies. It shall be performed from within touching distance unless otherwise noted, that being

the distance from the examiner’s eye to the area/item being inspected.

Flashlights and mirrors may be required to provide an adequate view of all surfaces.

There is no requirement for equipment removal or displacement unless this is specifically called for in

the access instructions. However, should unsatisfactory conditions be suspected, additional items may

need to be removed or displaced in order to permit proper assessment.

Paint and/or sealant removal is not necessary and should be avoided unless condition is suspect.

It is expected that the area to be inspected is clean enough to minimize the possibility that accumulated

dirt or grease might hide unsatisfactory conditions that would otherwise be obvious. Any cleaning that is

considered necessary should be performed in accordance with approved procedures in order to

minimize the possibility of the cleaning process itself introducing anomalies.

In general, the person performing the inspection is expected to identify degradation due to wear,

vibration, moisture, contamination, excessive heat, aging, etc. and make an assessment as to what

actions are appropriate to address the noted discrepancy. In making this assessment, the person

performing the inspection shall take into account potential influence on adjacent system installations,

particularly if these include wiring.

As a result of the CPCP requirement to control corrosion to Level 1 or better, operators shall report

corrosion findings to the manufacturer in accordance with the Structures Program Reporting System,

refer to Appendix 6 of the MRB Report.

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# The following list is intended to clarify the type of deterioration that constitutes a discrepancy that is

expected to be found and corrected. The list is not intended to be exhaustive and may be amended or

expanded as considered appropriate.

Structural Items/Assemblies

General

• Deformations e. g. bulging skin joint

• Corrosion

• Cracks

• Delamination or disbanding

• Obstructed drain holes

• Damage to hinges or latches

• Evidence of fluid spillage or pooled liquids

Accidental Damage

• Dents

• Impact marks

• Scratches or gouges

• Evidence of hail damage

• Evidence of lightning strike

• Evidence of foreign object damage (FOD) / bird strike

Fasteners

• General condition of fasteners

• Missing or broken fasteners

Surface Protection

• Damaged, detached or missing sealant

• Damaged, blistering or missing paint

• Severely discolored paint (evidence of corrosive fluid spillage)

• Accumulation of contaminants (dirt, grease, skydrol etc.)

Repairs

• Deterioration of previous repairs

Electrical installation

(also refer to AMM Chapter 20 Standard Practices)

Wire / Wire Harnesses

• Wire bundle/wire bundle or wire bundle/structure contact/chafing

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ISSUE:APR 01/10 ZONAL Page 3 

# • Wire bundle sagging or badly secured

• Wires damaged (large scale damage due to mechanical impact, overheat, localized chafing etc.)

• Lacing tape and/or ties missing/incorrectly installed

• Wiring protection sheath/conduit deformity or incorrectly installed

• End of sheath rubbing on end attachment device

• Grommet missing or damaged

• Dust and lint accumulation

• Surface contamination by metal shavings / swarf

• Contamination by liquids

• Deterioration of previous repairs

Connectors

• External corrosion on receptacles

• Backshell tail broken

• Rubber pad or packing on backshell missing

• No backshell wire securing device

• Fool proofing chain broken

• Missing or broken safety wire

• Discoloration/evidence of overheat on terminal lugs/blocks

• Torque stripe misalignment

Switches

• Rear protection cap damaged

Ground Points

• Corrosion

Bonding braid/bonding jumper

• Braid broken or disconnected

• Multiple strands corroded

• Multiple strands broken

Wiring clamps or brackets

• Corroded

• Broken/missing

• Bent or twisted

• Faulty attachment (bad attachment or fastener missing)

• Unstuck/detached

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# • Protection/cushion damaged

Supports (rails or tubes/conduit)

• Broken

• Deformed

• Fastener missing

• Missing edge protection on rims of feed through holes

• Racetrack cushion damaged

The following item could be considered to be covered by the ZIP if access to the electrical power center,

relay boxes etc. are added in the access requirements:

Circuit breakers, contactors or relays

• Signs of overheat

Hydraulic/Fuel/Water Waste/Oxygen/Fire Detection/Fire Suppression system installation

• Seepage/leakage of liquid

• Broken or incorrect wire locking

• Pipes badly secured

• Pipe/pipe or pipe/structure contact (check for chafing and restore separation)

• Missing or broken clamps

• Crushed / damaged pipes

• Broken/disconnected bonding leads / jumpers

• Deterioration of previous repairs

• Obstruction of smoke detectors

• Plugged or damaged distribution nozzles

Air systems installation

• Evidence of leakage on adjacent structure/components

• Crushed/split ducts

• Misaligned, missing or broken clamps

• Ducting badly secured

Mechanical systems installation

• Bent/crushed control rods

• Sagging control cables

• Excessively worn, frayed or kinked control cables

• Excessively worn fairleads

• Extruded bearing liners

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# • Broken or incorrect wire locking

• Significant corrosion on cables, threads

Cargo Systems

• Split/holed compartment liners

• Seal damage

• Excessively worn rollers (sign of jamming and resultant overheat)

• Missing/damaged stops/latches

• Damaged cargo net restraining attachments

Engines/Pylons

• Blade damage (e.g., nicks, cracks)

• Blades rub (on rubstrip)

• Vane damage

• Cowling damage

• Loose or migrating fasteners and bushings (due to vibration)

• Discoloration (due to heat damage)

• Foreign Object Damage (FOD)

• Damage due to birdstrike/ingestions

General

• Illegible labels

• Condensation in windows

• Window crazing

• Oil canning

WET AREAS - for floor structure

The wet area is defined as the area 0.5m (20") around any installed lavatory, galley or any door area

where the door is not deactivated.

Rules:

The wet area - WET AREA - definition applies independently from the A/C subtype (B2, B4, C4, F4,

etc.)

If during regular operation, sp illage of corrosive fluids in the entire cargo compartment or certain areas

of it is likely, then these areas are to be conservatively considered as - WET AREA -.

If a task is referred to be applicable to - WET AREA - these areas have to be identified by each operator

based on their cabin configuration and / or operational experience.

The layout and definition must be implemented into the operator's individual maintenance program.

# MAINTENANCE PLANNING DOCUMENT

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# If an operator chooses not to specify the dedicated - WET AREA -, then the complete area is to be

considered as - WET AREA -.

With respect General Introduction, operators shall consider all Zonal tasks in this Section are required

to support compliance with EWIS requirements. This practice overrides any requirement to identify each

task individually with (EZAP) in each task description.

3. RULES

Inspections are to be accomplished on each aircraft.

4. INSPECTIONS MORE FREQUENT THAN 500FH OR 4 MONTHS

As explained in the MRB Report of Section E Introduction, the routine content of inspections with

frequencies below 600 FH / 100 days shall be developed by the operator.

Therefore these tasks do not appear as maintenance tasks in the MPD, it is however recommended

that these inspections are considered by all operators, for inclusion in their routine maintenance

programs. Recommended intervals are provided for guidance where no similar inspections already exist

on comparable fleets.

It is recognised that these inspections are of a lesser intensity than a General Visual Inspection, since

they are to be performed 'from the ground, as far as visible'.

ZONE DESCRIPTION RECOMMENDED CALENDAR INTERVAL

100 Lower half of fuselage 36 hours

200 Upper half of fuselage 36 hours

300 Empennage and fuselage tail 36 hours

400 Power plants, nacelles and pylons 36 hours

500/600 Wings, L/H and R/H 36 hours

700 Landing gear & landing gear doors 36 hours

800 Doors 36 hours

123 Nose gear well 8 days

147/148 Main landing gear well and hydraulic

compartment 8 days

571/671 Main landing gear bay 8 days

5. NOTES

NOTE 1 to 9

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# Contents of MRBR Section E Notes are given as full text to the appropriate tasks in the MPD.

6. REPORTING SYSTEM

As a result of the CPCP requirement to control corrosion to Level 1 or better (Refer to Structure

Section), operators shall report corrosion findings to the manufacturer in accordance with the Structures

Reporting System. An example of the Structural Inspection Report is shown at the end of the Structure.APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-100-0402-1 100 LOWER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 1 C CPCP AMM SSI 5305011 3.00 ALLMRB S AMM SSI 533421GENERAL VISUAL INSPECTION OF: MRB Z AMM SSI 533523- RADOME FOR CONDITION AND DELAMINATION, AMM SSI 533723- EXTERNAL SKIN FROM FRAME 1 TO FRAME 80 BETWEENSTRINGER 33 LH AND 33 RH INCLUDING SERVICE DOORS, MRB REFERENCE:- SKIN AND STRUCTURE SURROUNDING FORWARD, REAR ANDBULK CARGO COMPARTMENT DOORS INCLUDING HINGES AND ZL-100HOOK ATTACHMENT FITTINGS. 533120-C602-1ACCESS: 811 812 813* 0.17ZL-100-0402-2 100 LOWER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 5 YE CPCP AMM SSI 5305011 2.50 POST 02727MRB S AMM SSI 533523ORGENERAL VISUAL INSPECTION OF EXTERNAL SKIN OF LOWERPOST 03245HALF OF FUSELAGE FROM FRAME 1 TO FRAME 80 WITH MRB REFERENCE:PARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINALLAP JOINTS FOR SEALING AND CORROSION. 533130-C602-1ZL-100-0402-3 100 LOWER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 30 MO CPCP MRB REFERENCE: 1 2.50 PRE 02727MRB Z ZL-100GENERAL VISUAL INSPECTION OF EXTERNAL SKIN OF LOWER 533130-C602-1HALF OF FUSELAGE FROM FRAME 1 TO FRAME 80 WITHPARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINALLAP JOINTS FOR SEALING AND CORROSION.ZL-110-0403-1 110 RADOME MEC GVI I: 2 C MRB Z MRB REFERENCE: 1 0.33 ALLZL-110VISUAL INSPECTION OF RADOME COMPONENT INSTALLATIONAND WIRING FOR GENERAL CONDITIONACCESS: 110AL* 0.01ZL-120-0403-1 120 ELECTRONICS-ELT.COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.00 ALLZL-120GENERAL VISUAL INSPECTION OF ELECTRONICS-, ELECTRICALCOMPARTMENT INCLUDING CONTROLS AND OXYGEN PIPES.(ZONES 121/122)ACCESS: 132AZ* 0.01ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 1APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-120-0403-3 120 ELECTRONICS-ELT.COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 1.00 ALLZL-120GENERAL VISUAL INSPECTION OF FLIGHT CONTROL, LANDINGGEAR EMERGENCY EXTENSION AND NLG-STEERING CONTROLINSTALLATIONS (ZONE 121/122)ACCESS: 121AF 121BF 121CF 121DF 121EF 121FF* 3.96121GF 121HF 121JF 121KF 121LF 121MF121NF 121PF 122AF 122BF 122CF 122DF122EF 122FF 122GF 122HF 122JF 122KF122LF 122MFZL-120-0403-4 120 ELECTRONICS-ELT.COMPARTMENT MEC GVI I: 9 YE CPCP MRB REFERENCE: 1 20.00 ALLMRB Z ZL-120GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE BELOW 531150-C603-1CABIN FLOOR LEVEL INCLUDING REAR FACE OF FORWARDPRESSURE BULKHEAD, IN ZONE 121, 122.PREP.: REMOVE INSULATIONACCESS: 131AZ 132AZ* 0.01ZL-130-0403-1 130 FWD CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 2.50 ALLZL-130GENERAL VISUAL INSPECTION OF:- FORWARD CARGO COMPARTMENT FOR GENERAL CONDITION(ZONES 131/132),- OXYGEN STORAGE AND PIPES AND CARGO COMPARTMENTFIRE EXTINGUISHER BOTTLES AND MOUNTS,- BLOW-IN AND BLOW-OUT PNELS (DECOMPRESSION PANELS)FOR PROPER INSTALLATION.ACCESS: 132BZ 132DZ* 0.20ZL-130-0403-2 130 FWD CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 2 15.00 ALLZL-130GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT(ZONES 131/132) INSTALLATIONS (FLIGHT CONTROLS,LANDING GEAR EMERGENCY EXTENSION, OXYGEN PIPES, ETC.)PREP.: REMOVE CEILING PANELS AND LININGS.ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 2APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-130-0403-3 131 FWD CARGO COMPARTMENT MEC GVI I: 9 YE CPCP MRB REFERENCE: 1 16.00 ALL132 MRB Z ZL-1301 16.00 EXCEPT137 GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531420-C603-11 16.00 F4,C4138 BETWEEN CABIN FLOOR AND CARGO FLOOR FRO FRAME 201 16.00TO FRAME 39 INCLUDING CABIN FLOOR STRUCTURENOTE: THIS TASK CAN BE PERFORMED AT SAME TIME ASSB 53-229, REQUIRING SIMILAR ACCESS.PREP.: REMOVE CEILING PANELS, LININGS, INSULATION.ACCESS: 131BZ 131CZ* 0.26132EZ* 0.13ZL-130-0403-4 131 FWD CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 20.00 C4132 MRB Z ZL-1301 20.00 F4137 GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531420-C603-11 20.00 NOTE138 BETWEEN CABIN FLOOR AND CARGO FLOOR FROM FRAME 20 531430-C603-11 20.00TO FRAME 39 INCLUDING CABIN FLOOR STRUCTURE.NOTE: THIS TASK CAN BE PERFORMED AT SAME TIME ASSB 53-0229, REQUIRING SIMILAR ACCESS.NOTE: ONLY APPLICABLE TO C4, IF A/C WAS USED IN FULLCARGO CONFIGURATION SINCE LAST INSPECTIONPREP.: REMOVE CEILING PANELS, LININGS AND INSULATION.ACCESS: 131BZ 131CZ* 0.26132EZ* 0.13ZL-130-0403-5 133 BAY UNDER FWD CARGO COMP. MEC GVI I: 4 YE CPCP MRB REFERENCE: 1 10.00 ALL134 MRB Z ZL-1301 10.00135 GENERAL VISUAL INSPECTION OF BAY UNDER CARGO 531440-C603-11 10.00136 FLOOR PANELS TO BOTTOM CENTER LINE FROM FRAME 201 10.00TO FRAME 39 INCLUDING ROLLER TRACKS.NOTE: FOR POST MOD 06699(SB 53-0215, 53-0216) A/C RIMAY BE INCREASED UP TO 5 YEARS01. INSPECT ZONE IN GENERAL INCLUDING FLIGHT CONTROLSPRESSURE SEALS, AIR DISTRIBUTION INSTALLATIONS.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 3APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-130-0403-5 * * * * * C O N T I N U E * * * * *(PRIOR TO REMOVAL OF INSULATION)02. REMOVE FLOOR PANELS AND INSULATION AND CLEAN AREA03. INSPECT INTERNAL STRUCTURE FOR GENERAL CONDITION.04. TPS TO BE APPLIED ON BILGHE AREAS FROM STRINGER41 LH/RH TO BOTTOM CENTER LINE FROM FRAME 19TO 39.05. APPLY TEMPORARY PROTECTION TYPE 1 AND TYPE 2AFTER INSPECTION.06. REINSTALL INSULATION.PREP.: REMOVE FLOOR PANELS AND INSULATION.ACCESS: 131ABF 131AEF 131AFF 131BF 131CF 131DF* 3.38131HF 131JF 131KF 131NF 131PF 131TF131WF 131XF132AF 132BF 132CF 132DF 132EF 132FF* 3.82132GF 132HF 132JF 132KF 132LF 132MF132NF131ABF 131AEF 131AFF 131BF 131CF 131DF* 3.38131HF 131JF 131KF 131NF 131PF 131TF131WF 131XF132AF 132BF 132CF 132DF 132EF 132FF* 3.82132GF 132HF 132JF 132KF 132LF 132MF132NFZL-130-0403-6 137 BAY BEHIND FWD CARGO COMP. MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.00 ALLZL-130GENERAL VISUAL INSPECTION OF BAY BETWEEN BULKHEAD OFFWD CARGO COMPARTMENT AND FWD PRESSURE BULKHEAD OFWING CENTER BOX IN GENERAL WITH PARTICULAR ATTENTIONTO WATER STORAGE SYSTEM AND ENGINE CONTROL CABLES FORWEAR AT PRESSURE SEALS. (INCL. ZONE 138)ACCESS: 131BZ 131CZ 132EZ* 0.39ZL-130-0403-7 137 BAY BEHIND FWD CARGO COMP. MEC GVI I: 9 YE MRB Z MRB REFERENCE: 1 5.00 ALLZL-130EXCL. F4GENERAL VISUAL INSPECTION OF STRUCTURE.(INCLUDING ZONE 138)PREP.: REMOVE INSULATION.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 4APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-130-0403-7 * * * * * C O N T I N U E * * * * *ACCESS: 131BZ 131CZ 132EZ* 0.39ZL-130-0403-8 131 FORWARD CARGO COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 1.50 B2132 I: 30 MO MRB Z ZL-1301 1.50 B4GENERAL VISUAL INSPECTION OF FLOOR STRUCTURE BELOW 532110-C603-1GALLEYS AND TOILETS FROM FRAME 26 TO FRAME 33.01. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2 ORG3 AFTER INSPECTION.02. TPS TO BE APPLIED AROUND GALLEYS AREAS (0.5 M/INCHES).PREP.: REMOVE CEILING PANELS IN GALLEY/TOILET AREA.ZL-130-0413-1 134 FRONT BAY UNDER FWD CARGO COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 2.50 TOILET KFLOOR I: 30 MO 531330-C603-1GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE AROUND WASTE WATER CONNECTION BOX BETWEENFR 26 AND FR 27 FROM STR 45 RH TO STR 48 RH.NOTE: TEMPORARY PROTECTION SYSTEMS TYPE 1 AND TYPE 2TO BE APPLIED.PREP.:CARGO FLOOR PANELS AND INSULATION TO BEREMOVEDACCESS: 811* 0.15ZL-130-0413-2 136 REAR BAY UNDER FWD CARGO COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 2.50 TOILETS H,K,L,MFLOOR I: 30 MO 531330-C603-1GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE AROUND WASTE WATER CONNECTION BOX BETWEENFR 30 AND FR 31 FROM STR 50 RH TO STR 54 RH.NOTE: TEMPORARY PROTECTION SYSTEMS TYPE 1 AND TYPE 2TO BE APPLIED.PREP.:CARGO FLOOR PANELS AND INSULATION TO BE* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 5APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-130-0413-2 * * * * * C O N T I N U E * * * * *REMOVED.ACCESS: 811* 0.15ZL-140-0403-1 141 WING CENTER BOX MEC GVI I: 2 C MRB Z MRB REFERENCE: 1 0.50 B2ZL-140GENERAL VISUAL INSPECTION OF WING CENTER BOXINCLUDING FUEL SYSTEM INSTALLATIONS.(INCLUDING ZONE 142)ACCESS: 147AZ 147DZ 148AZ 148DZ* 0.51ZL-140-0403-2 141 WING CENTER BOX MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 1.00 B2142 MRB Z ZL-1401 1.00GENERAL VISUAL INSPECTION OF WING CENTER BOX 531580-C603-1STRUCTURE.NOTE: FILLING COMPOUND EC 3524 A/B INSTALLED ON NONDRAINABLE AREAS (SOME B2) NOT TO BE REMOVED FORINSPECTION.ACCESS: 147AZ 147DZ 148AZ 148DZ 733 734* 0.71ZL-140-0403-3 141 WING CENTER BOX MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 1.00 B4142 MRB Z ZL-1401 1.00 C401. GENERAL VISUAL INSPECTION OF WING CENTER BOX 531580-C603-1F4STRUCTURE AND- FUEL SYSTEM INSTALLATION IN WING CENTER BOX- WING CENTER BOX STRUCTURE.02. CHECK CONTENT OF STRONTIUM CHROMATE CAPSULES(IF INSTALLED).NOTE: FILLING COMPOUND EC 3524 A/B INSTALLED ON NONDRAINABLE AREAS (SOME B2) NOT TO BE REMOVED FORINSPECTION.ACCESS: 147AZ 147DZ 147GZ 733* 0.39148AZ 148DZ 148GZ 734* 0.39ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 6APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-140-0403-4 143 AIR CONDITIONING COMPM. MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 0.75 ALLZL-140GENERAL VISUAL INSPECTION OF AIR CONDITIONINGCOMPARTMENT INCLUDING:- CONTROLS, DUCTING, WIRING,- VAPOR SEAL (CENTER FUEL TANK).(INCLUDING ZONE 144)ACCESS: 147BZ 147CZ 147DZ 147FZ 147GZ 147HZ* 0.21148DZ 148GZ 148HZZL-140-0403-5 143 AIR CONDITIONING COMPM. MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 0.50 ALL144 I: 5 YE MRB Z ZL-1401 0.50GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL 531583-C603-1STRUCTURE IN AIR CONDITIONING COMPARTMENT FROMFRAME 39 TO FRAME 47.NOTE: IMPROVED DRAINAGE IN ACCORDANCE WITH SB 53-0160IN RECOMMENDED.ACCESS: 143AF 143BF 143CF 143DF 147FZ 147GZ* 0.52147HZ 733148GZ 148HZ 734* 0.15ZL-140-0403-6 143 AIR CONDITIONING COMPARTM. MEC GVI I: 9 YE CPCP MRB REFERENCE: 2 25.00 B4144 MRB Z ZL-1402 25.00 C4GENERAL VISUAL INSPECTION OF WING BOX LOWER SECTION 531586-C603-1F4OF FRONT SPAR COVERED BY THE VAPOR SEAL.PREP.: DISPLACE VAPOR SEAL.ACCESS: 147BZ 147CZ 147FZ 147GZ 147HZ 148DZ* 0.18148GZ 148HZZL-140-0403-7 147 MLG BAY & HYDRAULIC COMPT. MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 5.00 ALLZL-140GENERAL VISUAL INSPECTION OF ZONE INCLUDING:- CONTROLS,- HYDRAULIC,- FUEL AND AIR CONDITIONING INSTALLATIONS.(INCLUDING ZONE 148).PREP.: REMOVE LININGS BETWEEN FR 47 AND FR 54 AND* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 7APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-140-0403-7 * * * * * C O N T I N U E * * * * *CEILING PANELS.ACCESS: 147BZ 147CZ 147DZ 147FZ 147GZ 147HZ* 0.89147LZ 147MZ 147NZ 147RZ 147SZ 147TZ147UZ 147VZ 147WZ 147XZ 148DZ 148GZ148HZ 148LZ 148MZ 148NZ 148RZ 148SZ148TZ 148UZ 148VZ 148WZ 148XZZL-140-0403-8 147 MLG BAY & HYDRAULIC COMPT. MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 2.00 PRE 03378148 OR 531590-C603-11 2.00 (29-0077)GENERAL VISUAL INSPECTION OF CONTROLS AND STRUCTURE 34100 FCINCLUDING MAIN LANDING GEAR DOOR HINGES. I: 2800 FCNOTE: FOR PREVENTION PURPOSE SB 53-0281APPLICATION IS RECOMMENDED.ACCESS: 147AF 147BF 147BZ 147CF 147CZ 147DZ* 0.53147FZ 147GZ 147HZ 147LZ 147MZ 147NZ147RZ 147SZ 147TZ 147UZ 147VZ 147WZ147XZ 733148AF 148DZ 148GZ 148HZ 148LZ 148MZ* 0.62148NZ 148RZ 148SZ 148TZ 148UZ 148VZ148WZ 148XZ 734ZL-140-0403-9 145 ZONE ABOVE WING CENTER BOX MEC GVI I: 9 YE CPCP MRB REFERENCE: 1 40.00 ALL146 MRB Z ZL-1401 40.00GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE FROM 531593-C603-1FRAME 39 TO FRAME 54 AND BETWEEN CABIN FLOOR ANDCENTER WING BOX UPPER SURFACE/PRESSURE FLOOR.PREP.: REMOVE PAX SEATS, FLOOR PANELS AND INSULATION,DISPLACE VAPOR SEAL (ABOVE CTR TANK UPPER-SKIN), IF INSTALLED(REF. SB 28-0033 AS APPLICABLE).ZL-140-0413-1 147 MLG BAY & HYDRAULIC COMPT. MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 2.00 POST 03378148 MRB Z ZL-1401 2.00 (29-0077)GENERAL VISUAL INSPECTION OF CONTROLS AND STRUCTURE 531590-C603-1INCLUDING MAIN LANDING GEAR DOOR HINGES.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 8APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-140-0413-1 * * * * * C O N T I N U E * * * * *NOTE: FOR PREVENTION PURPOSE SB 53-0281APPLICATION IS RECOMMENDED.ACCESS: 147AF 147BF 147CF 147FZ 147GZ 147HZ* 0.23733734* 0.10ZL-150-0403-1 151 AFT CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 2.00 ALLZL-150GENERAL VISUAL INSPECTION OF:- AFT CARGO COMPARTMENT FOR GENERAL CONDITION,- BLOW-IN AND BLOW-OUT PANELS (DECOMPRESSION PANELS)FOR PROPER INSTALLATION.(INCLUDING ZONE 152)ZL-150-0403-2 151 AFT CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 2 20.00 ALLZL-150GENERAL VISUAL INSPECTION OF INSTALLATIONS INCLUDINGFLIGHT CONTROLS, APU-BLEED AIR SUPPLY DUCTS.(INCLUDING ZONE 152)PREP.: REMOVE CEILING PANELS AND LININGS.ZL-150-0403-3 151 AFT CARGO COMPARTMENT MEC GVI T: 15 YE CPCP MRB REFERENCE: 2 40.00 ALL152 I: 9 YE MRB Z ZL-1502 40.00 EXCL. F4GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL 531610-C603-1STRUCTURE BETWEEN CABIN FLOOR AND CARGO FLOOR FROMFRAME 54 TO FRAME 64 INCLUDING CABIN FLOOR STRUCTURE.NOTE 01: THIS TASK CAN BE PERFORMED AT SAME TIME ASSB 53-0229, REQUIRING SIMILAR ACCESSPREP.: REMOVE CEILING PANELS, SIDE LININGS ANDINSULATION.ACCESS: 812* 0.01ZL-150-0403-4 151 AFT CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 2 40.00 C4152 MRB Z ZL-1502 40.00 F4GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL 531620-C603-1NOTE* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 9APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-150-0403-4 * * * * * C O N T I N U E * * * * *STRUCTURE BETWEEN CABIN FLOOR AND CARGO FLOOR FROMFRAME 54 TO FRAME 64 INCLUDING CABIN FLOOR STRUCTURE.NOTE 1 : THIS TASK CAN BE PERFORMED AT SAME TIME ASSB53-0229, REQUIRING SIMILAR ACCESS.NOTE 2 : ONLY APPLICABLE TO C4, IF A/C WAS USED INFULL CARGO CONFIGURATION SINCE LASTINSPECTION.PREP.: REMOVE CEILING PANELS, SIDE LININGS ANDINSULATION.ACCESS: 812* 0.01ZL-150-0403-5 153 BAY UNDER AFT CARGO COMPT MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 20.00 ALL154 I: 4 YE MRB Z ZL-1501 20.00GENERAL VISUAL INSPECTION OF: 531630-C603-101. INSPECT ZONE UNDER AFT CARGO COMPARTMENT,INCLUDING FLIGHT CONTROLS AND AIR DISTRIBUTIONINSTALLATIONS. (PRIOR TO REMOVAL OF INSULATION)02. REMOVE INSULATION AND INSPECT INTERNAL STRUCTUREBELOW CARGO FLOOR PANELS TO BOTTOM CENTER LINEFROM FRAME 54 TO FRAME 64 INCLUDING ROLLER TRACKSNOTE 1: TPS TO BE APPLIED ON BILGE AREAS FROMSTRINGER 49 LH/RH TO BOTTOM CENTER LINE FROMFRAME 54 TO 64.03.NOTE 2: APPLY TEMPORARY PROTECTION TYPE 1 OR TYPE 2AFTER INSPECTION.PREP.: REMOVE CARGO FLOOR PANELS AND BALL MATSINSULATION.ACCESS: 151BF 151CF 151GF 151HF 151MF 151NF* 14.03151SF 151TF 152AF 152BF 152CF 152DF152EF 152FF 152GF 152HF812* 0.01ZL-160-0403-1 161 BULK CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.00 ALLZL-160GENERAL VISUAL INSPECTION OF:- REAR (BULK) CARGO COMPARTMENT FOR GENERAL CONDITION* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 10APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-160-0403-1 * * * * * C O N T I N U E * * * * *- BLOW-IN AND BLOW-OUT PANELS (DECOMPRESSION PANELS)FOR PROPER INSTALLATION.(INCLUDES ZONE 162)ZL-160-0403-2 161 BULK CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 2 10.00 ALLZL-160GENERAL VISUAL INSPECTION INCLUDING FLIGHT CONTROLS,APU, BLEED AIR SUPPLY DUCT. (INCLUDING ZONE 162)PREP.: REMOVE CEILING PANELS AND LININGS.ZL-160-0403-3 161 BULK CARGO COMPARTMENT MEC GVI I: 9 YE CPCP MRB REFERENCE: 2 10.00 ALL162 MRB Z ZL-1602 10.00 EXCL. F4GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531730-C603-1BETWEEN CABIN FLOOR AND CARGO FLOOR FROM FRAMEFRAME 64 TO FRAME 70 INCLUDING CABIN FLOOR STRUCTURE.NOTE: THIS TASK CAN BE PERFORMED AT SAME TIME ASSB 53-0229, REQUIRING SIMILAR ACCESS.PREP.: REMOVE CEILING PANELS, SIDE LININGS ANDINSULATION.ACCESS: 813* 0.01ZL-160-0403-4 161 BULK CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 2 10.00 C4162 MRB Z ZL-1602 10.00 F4GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531730-C603-1NOTEBETWEEN CABIN FLOOR AND CARGO FLOOR FROM FRAMEFRAME 64 TO FRAME 70 INCLUDING CABIN FLOOR STRUCTURE.NOTE: THIS TASK CAN BE PERFORMED AT SAME TIME ASSB 53-0229, REQUIRING SIMILAR ACCESS.NOTE: ONLY APPLICABLE TO C4, IF A/C WAS USED IN FULLCARGO CONFIGURATION SINCE LAST INSPECTION.PREP.: REMOVE CEILING PANELS, SIDE LININGS ANDINSULATION.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 11APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-160-0403-4 * * * * * C O N T I N U E * * * * *ACCESS: 813* 0.01ZL-160-0403-5 163 BAY UNDER BULK CARGO COMPT. MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 8.00 ALL164 MRB Z ZL-1601 8.00GENERAL VISUAL INSPECTION OF FOLLOWING: 531750-C603-101. INSPECT BAY UNDER REAR (BULK) CARGO COMPARTMENTINCLUDING FLIGHT CONTROLS AND AIR EXTRACTIONCOMPONENTS. (PRIOR TO REMOVAL OF INSULATION)02. REMOVE INSULATION03. INSPECT INTERNAL STRUCTURE BELOW CARGO FLOORPANELS TO BOTTOM CENTER LINE FROM FRAME 64 TOFRAME 70.04. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 ANDTYPE 2 AFTER INSPECTION.05. INSTALL INSULATION.PREP.: REMOVE FLOOR PANELS AND INSULATION.ACCESS: 161AF 161BF 161CF 161DF 161EF 161FF* 1.63161GF162AF 162BF 162CF 162DF 162EF 162FF* 1.49162GF 813ZL-170-0403-1 171 AFT CABIN UNDERFLOOR COMPT. MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 2.00 ALLZL-170GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOORCOMPARTMENT INCLUDING FLIGHT CONTROLS, DUCTINGS ANDPRESSURE SEALS FOR GENERAL CONDITION.(INCLUDING ZONE 172)ACCESS: 162AZ* 0.01ZL-170-0403-2 171 AFT CABIN UNDERFLOOR COMPT. MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 5.00 ALL172 I: 5 YE MRB Z ZL-1701 5.00GENERAL VISUAL INSPECTION OF: 531830-C603-101. INSPECT FLIGHT CONTROLS BELOW FLOOR PANELS ANDINSTALLATIONS BEHIND 171AZ. (PRIOR TO REMOVAL OFINSULATION)02. INSPECT FUSELAGE INTERNAL STRUCTURE BELOW CABINFLOOR LEVEL TO BOTTOM CENTER LINE FROM FRAME 70* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 12APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-170-0403-2 * * * * * C O N T I N U E * * * * *UP TO AND INCLUDING REAR PRESSURE BULKHEAD LOWERFORWARD FACE.03. REMOVE INSULATION.04. INSPECT STRUCTURE FOR GENERAL CONDITION.05. REINSTALL INSULATION.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 ANDTYPE 2 AFTER INSPECTION.NOTE: TPS TO BE APPLIED ON BILGE AREAS FROM STRINGER40 LH/RH TO BOTTOM CENTER LINE FROM FRAME70 TO 80.PREP.: REMOVE FLOOR PANELS AND INSULATION.ACCESS: 171AF 171AZ* 0.16162AZ 172AF 172BF* 0.15ZL-200-0402-1 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 3.00 ALLZL-200EXCL. F4GENERAL VISUAL INSPECTION OF:- SKIN AND STRUCTURE SURROUNDING FWD, MID, AFTPASSENGER/CREW DOOR AND EMERGENCY EXITS INCLUDINGSCUFF PLATES, DOOR STOPS AND HOOK ATTACHMENTFITTINGS. (DOORS TO BE OPENED)- WINDOWS (ZONE 200).- FLIGHT DECK AREA (ZONE 211/212).ACCESS: 831 832 833 834 841 842* 0.80843 844ZL-200-0402-2 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 3.00 POST 02727MRB Z ZL-200ORGENERAL VISUAL INSPECTION OF EXTERNAL SKIN OF UPPER 533140-C602-1POST 03245HALF OF FUSELAGE FROM FRAME 1 TO FRAME 80 WITHPARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINALLAP JOINTS FOR SEALING AND CORROSIONZL-200-0402-3 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 30 MO CPCP MRB REFERENCE: 1 3.00 PRE 02727533140-C602-1PRE 03245GENERAL VISUAL INSPECTION OF EXTERNAL SKIN OF UPPER* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 13APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-200-0402-3 * * * * * C O N T I N U E * * * * *HALF OF FUSELAGE FROM FRAME 1 TO FRAME 80 WITHPARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINALLAP JOINTS FOR SEALING AND CORROSIONZL-200-0402-4 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 3.00 F4ZL-200GENERAL VISUAL INSPECTION OF:- SKIN AND STRUCTURE SURROUNDING FWD PASSENGER/CREWDOORS AND EMERGENCY EXITS INCLUDING SCUFF PLATES,DOOR STOPS AND HOOK ATTACHMENT FITTINGS.- WINDOWS (ZONE 200).- FLIGHT DECK AREA (ZONE 211/212).ACCESS: 831 834 841 844* 0.40ZL-210-0403-1 210 FLIGHT COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.50 ALLZL-210GENERAL VISUAL INSPECTION OF FLIGHT COMPARTMENTINCLUDING CONTROLS INSTALLATIONS AND OXYGEN PIPES ASFAR AS VISIBLE.ZL-210-0403-2 210 FLIGHT COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 10.00 ALLZL-210GENERAL VISUAL INSPECTION OF ZONE INSTALLATIONSINCLUDING LANDING GEAR EMERGENCY EXTENSION, ENGINECONTROLS, FLIGHT CONTROLS.NOTE: THE FOLLOWING PANELS HAVE NOT TO BE REMOVED:8VU, 9VU, 11VU, 20VU, 21VU, 22VU, 50VU, 130VUPREP.: REMOVE SEATS, FLOOR PANELS AND LININGS.ZL-210-0403-3 210 FLIGHT COMPARTMENT MEC GVI T: 15 YE CPCP MRB REFERENCE: 2 80.00 ALLI: 9 YE MRB Z ZL-210GENERAL VISUAL INSPECTION OF FUSELAGE UPPER LOBE 531140-C603-1INTERNAL STRUCTURE INCLUDING FLOOR STRUCTURE.NOTE: NO REMOVAL OF FLIGHT CONTROL PANEL, CONSOLES ORELECTRICAL PANELS. INSULATION TO BE LIFTED* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 14APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-210-0403-3 * * * * * C O N T I N U E * * * * *ENOUGH TO INSPECT THE STRUCTURE (THE FOLLOWINGPANELS HAVE NOT TO BE REMOVED: 8VU, 11VU, 20VU,21VU, 22VU, 50VU, 130VU).PREP.: REMOVE SEATS, FLOOR PANELREMOVE SIDE WALL AND CEILING PANELS ORELECTRICAL PANELSFLOOR PANELS AND LIFT INSULATION ENOUGH TOINSPECT THE STRUCTURE.ZL-220-0403-1 220 PASSENGER COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 8.00 ALLZL-220EXCL. F4GENERAL VISUAL INSPECTION OF CABIN INCLUDING SEATBELTS, BACK RESTS, OVERHEAD STOWAGE COMPARTMENT,GALLEYS AND TOILETS FOR GENERAL CONDITION (ANDBARRIER NET ATTACHMENTS FOR C4-203) IN ZONES 221/222,231/232, 241/242, 251/252, 261/262ZL-220-0403-2 220 PASSENGER COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 2 20.00 ALLZL-220GENERAL VISUAL INSPECTION OF:- LOWER DOOR FRAME- ZONE 220 INCL. INSTALLATIONS AND AIR DISTRIBUTION.PREP.: REMOVE LOWER SIDE PANELS, LOWER DOOR FRAMEPANELS AND INSULATION,ZL-220-0403-5 220 PASSENGER COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENCE: 2 3.00 ALL230 I: 5 YE MRB Z ZL-2202 3.00 EXCL. F4240 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE 532120-C603-12 3.00250 BELOW GALLEYS AND TOILETS AND DOOR ENTRANCE AREAS.2 3.002602 3.00PREP: REMOVE GALLEYS AND TOILETS AND FLOOR PANELSNOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.ZL-220-0403-6 220 PASSENGER COMPARTMENT MEC GVI T: 15 YE CPCP MRB REFERENCE: 2 4.00 ALL230 I: 9 YE MRB Z ZL-2202 95.00 EXCL. F4* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 15APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-220-0403-6 * * * * * C O N T I N U E * * * * *240 GENERAL VISUAL INSPECTION FUSELAGE UPPER LOBE 533230-C603-12 85.00250 INTERNAL STRUCTURE FROM FRAME 11/11.1 TO REAR 533240-C603-12 85.00260 PRESSURE BULKHEAD FORWARD FACE AND FLOOR STRUCTURE,2 95.00UP TO STRINGER 15 EXCLUDING SEAT TRACKS AND FROMSTRINGER 15 LH/RH TO CROWN CENTER LINE.THIS TASK CAN BE PERFORMED AT THE SAME TIME ASSB 53-0229 REQUIRING SIMILAR ACCESS.PREP.: REMOVE TOILET, GALLEY, FLOOR PANELSREMOVE SIDE WALL PANELS AND CEILING PANELS,REMOVE SIDE HATRACKS,LIFT INSULATION.ZL-220-0403-8 220 PASSENGER OVERHEAD COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 4.00 ALL230 ZL-2201 4.00 EXCL. F4240 GENERAL VISUAL INSPECTION OF ZONES 223/224,1 4.00250 233/234,243/244,253/254,263/264 INCLUDING1 4.00260 INSTALLATIONS.1 4.00NOTE: INSPECTION TO BE PERFORMED FROM LATERAL HATRACKINSTALLATION TO CENTRAL HATRACK INSTALLATIONPREP.: REMOVE CEILING PANELS.ZL-220-0403-9 220 PASSENGER COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENCE: 1 TBD ALL230 I: 5 YE 534101-C603-11 TBD EXCL. F4240 GENERAL VISUAL INSPECTION OF SEAT TRACKS 534110-C603-11 TBD250 BETWEEN FRAME 15A AND FRAME 80, EXCEPT 534120-C603-11 TBD260 BELOW GALLEY, TOILETS AND DOOR AREA. 534130-C603-11 TBDPREP.: REMOVE PASSENGER SEAT. (WITHOUT FLOOR PANELS) 534140-C603-1ZL-221-0403-1 220 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 3.00 F4ZL-221GENERAL VISUAL INSPECTION OF UPPER (MAIN) DECK CARGOCOMPARTMENT (ZONES 221/222, 231/232, 241/242,251/252, 261/262)ZL-221-0403-3 220 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENCE: 2 3.00 F4I: 5 YE MRB Z ZL-221* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 16APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-221-0403-3 * * * * * C O N T I N U E * * * * *GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE 532130-C603-1BELOW GALLEY AND TOILET AND DOOR ENTRANCE AREA.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.PREP.: REMOVE GALLEY AND TOILET,REMOVE FLOOR PANELS IN GALLEY/TOILET AREA,REMOVE FLOOR PANELS IN DOOR ENTRANCE AREA.ZL-221-0403-4 220 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI T: 15 YE CPCP MRB REFERENCE: 2 20.00 F4230 I: 9 YE MRB Z ZL-2212 20.00240 GENERAL VISUAL INSPECTION FUSELAGE UPPER LOBE 533250-C603-12 20.00250 INTERNAL STRUCTURE FROM FRAME 11/11.1 TO REAR 533260-C603-12 20.00260 PRESSURE BULKHEAD FORWARD FACE AND FLOOR STRUCTURE,2 20.00UP TO STRINGER 15 EXCLUDING SEAT TRACKS AND FROMSTRINGER 15 LH/RH TO CROWN CENTER LINE.THIS TASK CAN BE PERFORMED AT THE SAME TIME ASSB 53-0229 REQUIRING SIMILAR ACCESS.PREP.: REMOVE TOILET, GALLEY, FLOOR PANELSREMOVE SIDE WALL PANELS AND CEILING PANELS,REMOVE SIDE HATRACKS,LIFT INSULATION.ZL-221-0403-6 220 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 2.00 F4ZL-221GENERAL VISUAL INSPECTION OF ZONES 223/224, 233/234,243/244,253/254,263/264 INCLUDING INSTALLATIONS.ZL-221-0403-7 230 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 3.00 F4ZL-221GENERAL VISUAL INSPECTION OF SKIN AND STRUCTURESURROUNDING MID AND AFT PAX/CREW DOORS AND EMERG.EXIT INCLUDING DOOR STOP FITTINGS.(INCLUDING ZONE 240, 250, 260)PREP.: REMOVE PAX/CREW DOORS AND EMERG. EXIT DOORS.ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 17APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-230-0403-1 230 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 4 40.00 ALLMRB Z ZL-230EXCL. F4GENERAL VISUAL INSPECTION OF ZONE 231/232 INCLUDING 534110-C603-1INSTALLATIONS,AIR DISTRIBUTION DUCTS AND SEAT TRACKS.PREP.: REMOVE PASSENGER SEATS,REMOVE SIDEWALL PANELS,REMOVE CEILING PANELS BETWEEN FRAME 28 TO 30,REMOVE INSULATION.ZL-230-0403-2 230 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 2 20.00 F4MRB Z C53-220-01-02GENERAL VISUAL INSPECTION OF ZONE 231/232 INCLUDING ZL-230INSTALLATIONS, AIR DISTRIBUTION DUCTS.PREP.: REMOVE SIDEWALL PANELS AND INSULATION.ZL-240-0403-1 240 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 4 60.00 ALLMRB Z ZL-240EXCL. F4GENERAL VISUAL INSPECTION OF ZONES 241/242, 145/146 534120-C603-1INCLUDING INSTALLATIONS, AIR DISTRIBUTION DUCTS ANDSEAT TRACKS.PREP.: REMOVE PAX SEATS, LININGS, LOWER SIDE PANELS,LOWER DOOR FRAME PANELS AND INSULATION IN AREAOF EMERGENCY DOORS,REMOVE CEILING PANELS BETWEEN FRAME 30 AND 36,FRAME 40 TO 42 AND FRAME 50 TO 52,REMOVE CARPET AND FLOOR PANELS TO GAIN ACCESSTO ZONE 145 AND 146 (ZONES 241/242).ACCESS: 241AGF 241AKF 241ASF 241ZF 242AAF 242AJF* 0.78ZL-240-0403-2 240 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 2 30.00 F4MRB Z C53-220-01-02GENERAL VISUAL INSPECTION OF ZONES 241/242, 145/146 ZL-240INCLUDING INSTALLATIONS, AIR DISTRIBUTION DUCTS.PREP.: REMOVE LININGS, LOWER SIDE PANELS, LOWER DOORFRAME PANELS,REMOVE CARGO LOADING SYSTEM AND FLOOR PANELS(ACCESS TO ZONES 145/146, 241/242),* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 18APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-240-0403-2 * * * * * C O N T I N U E * * * * *REMOVE INSULATION.ACCESS: 241AGF 241AKF 241ASF 241ZF 242AAF 242AJF* 0.78ZL-250-0403-1 250 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 2 40.00 ALLMRB Z ZL-250EXCL. F4GENERAL VISUAL INSPECTION OF ZONE 251/252 INCLUDING 534130-C603-1INSTALLATIONS, AIR DISTRIBUTION DUCTS AND SEATTRACKS.PREP.: REMOVE PASSENGER SEATS,REMOVE SIDEWALL PANELS AND INSULATION.ZL-250-0403-2 250 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 2 20.00 F4ZL-250GENERAL VISUAL INSPECTION OF ZONE 251/252 INCLUDINGINSTALLATIONS AND AIR DISTRIBUTION DUCTS.PREP.: REMOVE SIDEWALL PANELS AND INSULATION.ZL-260-0403-1 260 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENCE: 2 20.00 ALLMRB Z ZL-260EXCL. F4GENERAL VISUAL INSPECTION OF ZONE 261/262 INCLUDING 534140-C603-1INSTALLATIONS, AIR DISTRIBUTION DUCTS AND SEATTRACKS.PREP.: REMOVE LININGS AND LOWER SIDEWALL PANELS,REMOVE INSULATION.ZL-260-0403-2 260 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 2 20.00 F4ZL-260GENERAL VISUAL INSPECTION OF ZONE 261/262 INCLUDINGINSTALLATIONS AND AIR DISTRIBUTION DUCTS.PREP.: REMOVE SIDEWALL PANELS AND INSULATION.ZL-300-0402-1 310 EMPENNAGE AND FUSELAGE TAIL MEC GVI I: 1 C CPCP AMM SSI 5309071 1.00 ALLMRB S AMM SSI 533905* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 19APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-300-0402-1 * * * * * C O N T I N U E * * * * *GENERAL VISUAL INSPECTION OF ZONE INCLUDING: MRB Z AMM SSI 533907- TAIL CONE, AMM SSI 533917- APU AIR INTAKE AND EXHAUST AREA,- DRAIN HOLES, MRB REFERENCE:- LOWER FUSELAGE AT FRAME 80: BETWEEN STRINGERS34RH AND LH. ZL-300531940-C602-1ZL-300-0402-2 330 EMPENNAGE AND FUSELAGE TAIL MEC GVI I: 1 C CPCP MRB REFERENCE: 1 1.00 ALL340 MRB Z ZL-3001 1.00GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 531940-C602-1- HORIZONTAL STABILIZER TRAVEL APRON AREAAND FAIRINGS,- HORIZONTAL STABILIZER LEADING EDGE,- HORIZONTAL STABILIZER TIP,- ELEVATOR AND DRAIN HOLES,- FLIGHT CONTROLS AND INSTALLATIONS AS FAR AS VISIBLEZL-300-0402-3 320 EMPENNAGE AND FUSELAGE TAIL MEC GVI I: 1 C CPCP MRB REFERENCE: 1 1.00 ALLMRB Z ZL-300GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 531940-C602-1- VERTICAL STABILIZER LEADING EDGE,- DORSAL FIN,- VERTICAL STABILIZER TIP,- RUDDER,- DRAIN HOLES,- FLIGHT CONTROLS AND INSTALLATIONS AS FAR ASVISIBLE.ZL-300-0402-4 300 EMPENNAGE AND FUSELAGE TAIL MEC GVI T: 9 YE CPCP MRB REFERENCE: 1 4.00 ALLI: 4 YE MRB Z ZL-300GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 531940-C602-1- HORIZONTAL STABILIZER AFT OF FRONT SPAR,- VERTICAL STABILIZER AFT OF FRONT SPAR,- FUSELAGE TAIL SECTION FWD OF TAIL CONE.ZL-310-0403-1 310 TAIL CONE AREA MEC GVI I: 1 C MRB Z SIL 27-1021 1.50 ALLSILGENERAL VISUAL INSPECTION OF ZONE 311/312:* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 20APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-310-0403-1 * * * * * C O N T I N U E * * * * *- FLIGHT CONTROL INSTALLATIONS ZL-310- APU FUEL LINE- BLEED AIR SUPPLY DUCT- PRESSURE SEALS AND DRAIN VALVEINCLUDING LOWER PRESSURE DOME AREA FOR CONDITIONACCESS: 312AR* 0.01ZL-310-0403-2 311 TAIL CONE AREA, HORIZONTAL STABILIZER MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 0.50 ALL312 MRB Z ZL-3101 0.50319 GENERAL VISUAL INSPECTION OF FOLLOWING ZONES 531940-C603-11 0.50INCLUDING STRUCTURE: 551101-C603-1- HORIZ. AND VERT. STAB. ATTACHM. AREA,- HORIZONTAL STABILIZER CENTER SECTION BOX EXTERNALSTRUCTURE,- FUSELAGE INTERNAL STRUCTURE BETWEEN FR80 AND 92INCLUDING REAR PRESSURE BULKHEAD.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.ACCESS: 313AL* 0.14312AR* 0.01ZL-310-0403-3 310 TAIL CONE AREA, HORIZONTAL STABILIZER MEC GVI I: 9 YE CPCP MRB REFERENCE: 1 1.50 ALLMRB Z ZL-310GENERAL VISUAL INSPECTION OF STRUCTURE IN FOLLOWING 538829-C603-1ZONES: 551101-C603-1- TAIL CONE-APU AIR INTAKE AREA ZONE 313/314, 551110-C603-1- HORIZONTAL STABILIZER CENTER SECTION BOX INTERNALSTRUCTURE ZONE 319.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.(DO NOT SPRAY TEMPORARY PROTECTION AGAINSTFIRE WALLS. IN CASE OF FIRE THIS COULD CAUSEAN EXPLOSION.)ACCESS: 312AR 313AL* 0.15ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 21APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-310-0403-4 310 TAIL CONE-APU AREA MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.50 ALLZL-310GENERAL VISUAL INSPECTION OF FOLLOWING ZONES:- AIR INTAKE AREA ZONE 313/314,- ACCESSORY COMP. ZONE 315/316,- EXHAUST AREA ZONE 317/318,INCLUDING:- FLIGHT CONTROLS,- FIRE EXTINGUISHER AND MOUNTS,- APU INSTALLATIONS.ACCESS: 313AL 315AL 316AR 317AL* 0.20ZL-320-0403-1 320 VERTICAL STABILIZER AREA MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 3.00 ALLZL-320GENERAL VISUAL INSPECTION OF STRUCTURE IN FOLLOWINGZONES:- DORSAL FIN ZONE 321,- HF-ANTENNA ATTACHM. AREA ZONE 322,- LEADING EDGE ZONE 322,- SPAR BOX ZONE 323,- STABILIZER TIP ZONE 324,- TRAILNG EDGE ZONE 325.ACCESS: 311AZ 311BZ 312AR 321AL 322AL 322BL* 12.54322CL 324AT 324BT 325AL 325AR 325BL325CL 325DL 325EL 325FL 325GL 325HL325JL 325KLZL-320-0403-2 323 VERTICAL STAB.SPAR BOX MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 0.50 ALLMRB Z ZL-320GENERAL VISUAL INSPECTION OF ZONE INCLUDING 553101-C603-1FLIGHT CONTROL INSTALLATIONS FROM RIB 1 TO RIB12.ACCESS: 311AZ 311BZ 312AR 322AL 322BL 322CL* 9.80325AL 325BL 325CL 325DL 325EL 325FL325GL 325HL 325JL 325KLZL-320-0403-3 320 VERT.STAB.TRAIL.EDGE/RUDDER MEC GVI I: 2 C MRB Z MRB REFERENCE: 1 1.00 ALLZL-320GENERAL VISUAL INSPECTION OF ZONE INCLUDING FLIGHTCONTROL INSTALLATIONS AND ATTACHMENTS.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 22APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-320-0403-3 * * * * * C O N T I N U E * * * * *ACCESS: 325BL 325DL 325FL 325HL 325KL 326BL* 2.31326DL 326FL 326HL 326KLZL-320-0403-4 326 RUDDER MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 1.00 ALLZL-320GENERAL VISUAL INSPECTION OF ZONE INCLUDINGINTERNAL STRUCTURE.ACCESS: 325AL 325AR 325BL 325CL 325DL 325EL* 8.69325FL 325GL 325HL 325JL 325KL 326AL326AR 326BL 326BR 326CL 326CR 326DL326DR 326EL 326ER 326FL 326GL 326HL326JL 326KL 326LLZL-330-0403-1 330 HORIZONTAL STABILIZER MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 1.50 ALL340 MRB Z ZL-3301 1.50GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: 551120-C603-1- LEADING EDGE ZONE 331/341, 551130-C603-1- STABILIZER TIP ZONE 332/342, 551301-C603-1- SPAR BOX ZONE 333/343,- TRAILING EDGE ZONE 334/344,INCLUDING INTERNAL STRUCTURE.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.TO EXTERNAL SURFACE AND, BETWEEN RIB 3 AND 4,TO THE THS SPAR BOX INTERNAL STRUCTURE.ACCESS: 331AB 331BB 331CB 332AB 334AT 334BT* 11.44334CT 334DT 334ET 334FT 334GT 334HT334JT 334KT 334LT341AB 341BB 341CB 342AB 344AT 344BT* 11.44344CT 344DT 344ET 344FT 344GT 344HT344JT 344KT 344LTZL-330-0403-2 330 HORIZ.STAB.TRLG.EDGE/ELEVATOR MEC GVI I: 2 C MRB Z MRB REFERENCE: 1 1.00 ALL340 ZL-3301 1.00GENERAL VISUAL INSPECTION OF FOLLOWING ZONES:- TRAILING EDGE ZONE 334/344,- ELEVATOR ZONE 335/345,* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 23APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-330-0403-2 * * * * * C O N T I N U E * * * * *INCLUDING FLIGHT CONTROL INSTALLATIONS ANDATTACHMENTS.ACCESS: 334AT 334BT 334CT 334DT 334ET 334FT* 6.10334GT 334HT 334JT 334KT 334LT 335AB335AT 335BB 335BT 335CB 335CT 335DB335DT 335EB 335ET344AT 344BT 344CT 344DT 344ET 344FT* 6.12344GT 344HT 344JT 344KT 344LT 345AB345AT 345BB 345BT 345CB 345CT 345DB345DT 345EB 345ETZL-400-0402-1 415 PYLON BOX EXTERNAL SURFACE RIB 1 TO 18 MEC GVI T: 10 YE CPCP MRB REFERENCE: 1 1.00 ALL416 I: 5 YE MRB Z ZL-4001 1.00425 GENERAL VISUAL INSPECTION OF PYLON BOX EXTERNAL 543101-C602-11 1.00426 SURFACE FROM RIB 1 TO RIB 18 AND FROM LOWER SPAR TO1 1.00473 UPPER SPAR, PYLON AND ENGINE NACELLE STRUCTURE,1 1.00474 ACCESS PANELS AND DOORS.1 1.004831 1.00484 PREP: COWLS OPENED1 1.00ZL-410-0403-1 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.50 PRE 02434420 ZL-4101 1.50GENERAL VISUAL INSPECTION OF ZONES, INCLUDING:- FUEL CONTROLS,- ENGINE CONTROLS,- PNEUMATIC INSTALLATIONS,- HYDRAULIC INSTALLATIONS.ACCESS: 413AL 413BL 413EL 413FL 414AR 414BR* 1.82414CR 414DR 415AL 416AR423AL 423BL 423EL 423FL 424AR 424BR* 1.82424CR 424DR 425AL 426ARZL-410-0403-2 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 5 YE MRB Z SIL 54-0191 1.00 PRE 024344201 1.00GENERAL VISUAL INSPECTION OF ZONE STRUCTURE. MRB REFERENCE:ZL-410ACCESS: 413AL 413BL 413EL 413FL 414AR 414BR* 1.82414CR 414DR 415AL 416AR* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 24APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-410-0403-2 * * * * * C O N T I N U E * * * * *423AL 423BL 423EL 423FL 424AR 424BR* 1.82424CR 424DR 425AL 426ARZL-410-0403-3 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.50 POST 02434420 ZL-4101 1.50GENERAL VISUAL INSPECTION OF ZONES, INCLUDING:- FUEL CONTROLS,- ENGINE CONTROLS,- PNEUMATIC INSTALLATIONS,- HYDRAULIC INSTALLATIONS.ACCESS: 413AL 413BL 413FL 413GL 413HL 414AR* 2.10414BR 414CR 414DR 414ER 415AL 416AR423AL 423BL 423FL 423GL 423HL 424AR* 2.10424BR 424CR 424DR 424ER 425AL 426ARZL-410-0403-4 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 5 YE MRB Z SIL 54-0191 1.00 POST 024344201 1.00GENERAL VISUAL INSPECTION OF ZONES FOR CONDITION OF MRB REFERENCE:STRUCTURE ZL-410ACCESS: 413AL 413BL 413FL 413GL 413HL 414AR* 2.10414BR 414CR 414DR 414ER 415AL 416AR423AL 423BL 423FL 423GL 423HL 424AR* 2.10424BR 424CR 424DR 424ER 425AL 426ARZL-410-0403-5 410 PYLON LEADING EDGE AND LOWER AFT ZONE MEC GVI I: ENG. CHG MRB Z MRB REFERENCE: 1 0.25 PRE 02434420 ZL-4101 0.25470 GENERAL VISUAL INSPECTION OF:1 0.25480 - PYLON LEADING EDGE ZONE 411/412 AND 421/422,1 0.25- LOWER AFT PYLON ZONE 475/476 AND 485/486.ACCESS: 411AL* 0.29421AL* 0.29475AL 475BL 475CL 475DL 476AR 476BR* 1.01485AL 485BL 485CL 485DL 486AR 486BR* 1.00ZL-410-0403-6 410 PYLON LEADING EDGE AND LOWER AFT ZONE MEC GVI I: ENG. CHG MRB Z MRB REFERENCE: 1 0.25 POST 02434420 ZL-4101 0.25* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 25APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-410-0403-6 * * * * * C O N T I N U E * * * * *470 GENERAL VISUAL INSPECTION OF:1 0.25480 - PYLON LEADING EDGE ZONE 411/412 AND 421/422,1 0.25- LOWER AFT PYLON ZONE 475/476 AND 485/486.ACCESS: 411AL* 0.29421AL* 0.29475AL 475BL 475CL 476AR* 0.74485AL 485BL 485CL 486AR* 0.74ZL-430-0403-1 430 ENGINE MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 0.50 ALL440 ZL-4301 0.50450 GENERAL VISUAL INSPECTION OF COWLING STRUCTURE,1 0.50460 LOCKS AND LATCHES IN ZONES 435, 436, 451, 452, 453,1 0.50454, 455, 456, 445, 446, 461, 462, 463, 464, 465AND 466.ZL-430-0403-2 430 NOSE COWL ENG GVI I: ENGINE MRB Z MRB REFERENCE: 1 0.50 ALL440 BUILD UP ZL-4301 0.50GENERAL VISUAL INSPECTION OF AIR INTAKE RING(NOSE COWL).NOTE: RIVETED ACCESS PANELS (PW-ENGINES) NOT TO BEREMOVEDACCESS: 433AL 434AR 434BR* 0.81443AL 444AR 444BR* 0.98ZL-430-0403-3 430 ENGINE ENG GVI I: C MRB Z MRB REFERENCE: 1 1.50 ALL440 OR ZL-4301 1.50GENERAL VISUAL INSPECTION OF ENGINE ZONES INCLUDING: SHOP VIS- FUEL FEED,- ENGINE CONTROL AND INDICATING,- ENGINE VANE AND ENGINE BLEED AIR,- BLEED AIR AND PNEUMATIC (INCLUDING STARTERAIR SUPPLY),- OIL,- IGNITION,- HYDRAULIC POWER,- ELECTRICAL POWER,- THRUST REVERSER AIR SUPPLY,* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 26APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-430-0403-3 * * * * * C O N T I N U E * * * * *FOR GENERAL CONDITION AND PROPER INSTALLATION OFCOMPONENTS, PLUMBING, CLAMPS, BRACKETS, LINKAGES ANDELECTRICAL LEADS ETC.ZL-450-0403-1 450 FAN REVERSER/ENGINE CORE ENG GVI I: 1 C MRB Z MRB REFERENCE: 1 1.00 GE460 ZL-4501 1.00GENERAL VISUAL INSPECTION OF FAN REVERSER AND ENGINECORE INCLUDING FOLLOWING COMPONENTS:- REVERSER,- ENGINE CONTROL AND INDICATING SYSTEM COMPONENTS,- FUEL CONTROL AND INDICATING SYSTEM COMPONENTS.(ZONES 451, 452, 461 AND 462)ACCESS: 435AL 455AL 456AR* 0.04445AL 465AL 466AR* 0.04ZL-450-0403-2 450 FAN REVERSER/ENGINE CORE ENG GVI I: 1 C MRB Z MRB REFERENCE: 1 1.00 PW460 ZL-4501 1.00GENERAL VISUAL INSPECTION OF FAN REVERSER AND ENGINECORE INCLUDING FOLLOWING COMPONENTS:- REVERSER,- ENGINE CONTROL AND INDICATING SYSTEM COMPONENTS,- FUEL CONTROL AND INDICATING SYSTEM COMPONENTS.(ZONES 451, 452, 461 AND 462)ZL-470-0403-1 470 PYLON/WING LEADING EDGE MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 1.00 ALL480 ZL-4701 1.00GENERAL VISUAL INSPECTION OF ZONES, INCLUDING:- ENGINE CONTROLS,- FIRE EXTINGUISHER CONTAINER & MOUNTS,- INDICATING SYSTEM COMPONENTS.ACCESS: 471AL 471BL 472AR 472BR 473AL 473BL* 2.04473DL481AL 481BL 482AR 482BR 484AR 484BR* 2.05484DRZL-470-0403-2 470 PYLON/WING LEADING EDGE MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 0.50 ALL480 ZL-4701 0.50* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 27APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-470-0403-2 * * * * * C O N T I N U E * * * * *GENERAL VISUAL INSPECTION OF ZONES FOR:- CONDITION OF STRUCTURE,- PROPER INSTALLATION OF LOW PRESSURE FUEL FIRESHUT-OFF VALVES AND ASSOCIATED CONTROLS.ACCESS: 471AL 471BL 472AR 472BR 473AL 473BL* 2.04473DL481AL 481BL 482AR 482BR 484AR 484BR* 2.05484DRZL-500-0402-1 500 EXTERNAL SURFACE OF MAIN WING BOX UPPER MEC GVI I: 2 C CPCP MRB REFERENCE: 1 1.00 ALL600 AND LOWER SKIN OR MRB Z ZL-5001 1.0030 MO 573301-C602-1GENERAL VISUAL INSPECTION OF EXTERNAL SURFACE OF MAINWING BOX UPPER AND LOWER SKIN SURFACE FROM ROOT TOTIP (EXCLUDING SKIN PANEL N°2 BETWEEN RIB 1 TO RIB 9)ZL-500-0402-2 500 WING MEC GVI I: 1 C CPCP ISB 24-0731 4.00 ALL600 MRB Z SIL 27-0221 4.00EXTEND SLATS, FLAPS AND AIRBRAKES AND PERFORM AGENERAL VISUAL INSPECTION OF THE FOLLOWING AREAS: MRB REFERENCE:- AREA FORWARD OF FRONT SPAR,INCLUDING WING LEADING ZL-500EDGE, SLATS, SLAT TRACKS AND SEALS, KRUEGER FLAP 573301-C602-1AND MECHANISM, FLIGHT CONTROLS,ANTI-ICE AND FUEL 573330-C603-1SYSTEM INSTALLATIONS AND ANTI-ICE EXHAUST HOLES 573401-C602-1- WING TIP 578255-C603-1- BOTTOM SKIN BETWEEN FRONT AND REAR SPARS 578261-C603-1- AREA AFT OF REAR SPAR, INCLUDING INSTALLATIONS AS 578271-C603-1VISIBLE IN PARTICULAR AREA FWD OF ALL SPEED AILE- 578281-C603-1RON,REAR SPAR AND ATTACHMENTS OUTBOARD OF RIB 9,FLAP BEAM AND ATTACHMENTS AT REAR SPAR,FLAP CAR-RIAGES MECHANISM,FLAP ATTACHMENTS AND SCREWJACKS- LOW AND ALL SPEED AILERONS AND THEIR RESPECTIVEDRAIN HOLES- SPOILERS AND AIRBRAKES SKIN AND ATTACHMENT LUGSAND BEARINGS AND THEIR RESPECTIVE DRAIN HOLES- FLAPS, IN PARTICULAR BOTTOM SKIN AND THEIRRESPECTIVE DRAIN HOLES- EXTERNAL SURFACES OF WING LEADING EDGE UPPER ANDLOWER INCLUDING MOVABLE SURFACES.WING TRAILING EDGE SURFACES INCLUDING MOVABLE* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 28APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-500-0402-2 * * * * * C O N T I N U E * * * * *SURFACES.NOTE: SLATS 1 TO 3 - ALL TRACKS.PREP: FLAPS AND SLATS EXTENDEDZL-500-0402-3 500 EXTERNAL SURFACE OF MAIN WING BOX UPPER MEC GVI I: 2 YE CPCP MRB REFERENCE: 1 1.00 ALL600 AND LOWER SKIN MRB Z ZL-5001 1.00573302-C602-1GENERAL VISUAL INSPECTION OF EXTERNAL SURFACE OF MAINWING BOX UPPER AND LOWER SKIN PANEL N°2.(BETWEEN RIB 1 TO RIB 9)ZL-510-0403-2 512 INBOARD LEADING EDGE MEC GVI I: 1 C CPCP MRB REFERENCE: 1 1.00 ALL612 MRB Z ZL-5101 1.00GENERAL VISUAL INSPECTION OF ZONE, WITH PARTICULAR 578013-C603-1ATTENTION TO FLIGHT CONTROLS INCLUDING DRIVE SHAFTSAND UNIVERSAL JOINTS (GAITERS IN PLACE AND NOTDAMAGED), ENGINE CONTROL CABLES FOR WEAR ATFAIRLEADS (4 OFF), ANTI-ICE VALVES AND LOW PRESSUREFUEL FIRE SHUT-OFF VALVES AND ASSOCIATED CONTROLS.NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.ACCESS: 512AB 512BB 512CB 512DB 512EB 512FB* 1.59512GB 512HB 512JB 512KB 512LB 513AT612AB 612BB 612CB 612DB 612EB 612FB* 1.49612GB 612HB 612JB 612KB 612LB 613ATZL-510-0403-3 512 INBOARD LEADING EDGE MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 1.00 ALL612 MRB Z ZL-5101 1.00GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE OF 574120-C603-1WING LEADING EDGE UPPER AND LOWER SKIN FROM ROOT TOTIP.PREP.: EXTEND SLATS.ACCESS: 512AB 512BB 512CB 512DB 512EB 512FB* 1.59512GB 512HB 512JB 512KB 512LB 513AT612AB 612BB 612CB 612DB 612EB 612FB* 1.49612GB 612HB 612JB 612KB 612LB 613ATZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 29APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-520-0403-2 523 FIXED LEADING EDGE MEC GVI I: 1 C CPCP MRB REFERENCE: 1 1.50 ALL623 MRB Z ZL-5201 1.50GENERAL VISUAL INSPECTION OF ZONE, WITH PARTICULAR 578013-C603-1ATTENTION TO FLIGHT CONTROLS INCLUDING DRIVE SHAFTSAND UNIVERSAL JOINTS (GAITERS IN PLACE AND NOTDAMAGED), ENGINE CONTROLS, ANTI ICE, PNEUMATIC DUCTAND REFUEL/DEFUEL COUPLING.(INCLUDES ZONE 524 RESPECTIVELY 624)NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.PREP.: EXTEND SLATS.ACCESS: 523AB 523BB 523CB 523DB 523EB 523FB* 2.36523GB 523HB 523JB 523KB 523LB 523MB524AB 524BB 524CB 524DB 524EB 524FB524GB 524HB 524JB 524KB623AB 623BB 623CB 623DB 623EB 623FB* 2.36623GB 623HB 623JB 623KB 623LB 623MB624AB 624BB 624CB 624DB 624EB 624FB624GB 624HB 624JB 624KBZL-520-0403-3 523 FIXED LEADING EDGE MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 2.00 ALL623 MRB Z ZL-5201 2.00GENERAL VISUAL INSPECTION OF ZONE FOR CONDITION OF 578013-C603-1INTERNAL STRUCTURE(INCLUDES ZONE 524 RESPECTIVELY 624)NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.ACCESS: 523AB 523BB 523CB 523DB 523EB 523FB* 2.36523GB 523HB 523JB 523KB 523LB 523MB524AB 524BB 524CB 524DB 524EB 524FB524GB 524HB 524JB 524KB623AB 623BB 623CB 623DB 623EB 623FB* 2.36623GB 623HB 623JB 623KB 623LB 623MB624AB 624BB 624CB 624DB 624EB 624FB624GB 624HB 624JB 624KBZL-530-0403-1 530 FAIRINGS-FLAP TRACKS 2 TO 6 MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 10.00 ALL630 ZL-5301 10.00* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 30APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-530-0403-1 * * * * * C O N T I N U E * * * * *GENERAL VISUAL INSPECTION AT FLAP TRACK NO.2 TO 6INCLUDING:- SCREW JACKS, CARRIAGES AND OTHER INSTALLATIONS,- FLAP TRACK BEAM AND FAIRINGS.PREP.: EXTEND FLAPS.ACCESS: 532AF 532AM 533AF 533AM 534AF 534AM* 3.33535AF 535AM 536AF 536AM632AF 632AM 633AF 633AM 634AF 634AM* 3.33635AF 635AM 636AF 636AMZL-530-0403-2 531 WING TIP MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 0.10 ALL631 MRB Z ZL-5301 0.10GENERAL VISUAL INSPECTION OF ZONE. 572401-C603-1ACCESS: 531AB 531AT 531BB* 0.35631AB 631AT 631BB* 0.35ZL-540-0403-1 540 MAIN FUEL TANK-INBOARD MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 1.50 ALL550 MRB Z ZL-5401 1.50560 GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 571180-C603-11 1.50640 - FUEL FEED,REFUEL,DEFUEL,VENTILATION AND JETTISON 571185-C603-11 1.50650 SYSTEM PIPES (WHEN FITTED) AND COMPONENTS AND 571190-C603-11 1.50660 QUANTITY INDICATION SYSTEM, 573310-C603-11 1.50- STRUCTURE, 573320-C603-1- STRONTIUM CHROMATE CAPSULES (IF INSTALLED) FOR 573330-C603-1CORRECT CONTENT.- OUTBOARD WING LOWER SKIN AT FUEL TANK ACCESS DOORSAND ASSOCIATED DOORS BETWEEN RIB 01 AND RIB 27.- WING MAIN BOX INTERNAL STRUCTURE FROM FRONT TOREAR SPAR BETWWEN RIB 1 AN RIB 27 AND WING TIPACCESS: 541AB 541BB 541CB 542CB 542DB 542EB* 15.00543AB 543BB 543CB 543DB550BB 550DB 550EB 550GB 550LB 550QB* 9.00560AB* 1.50641AB 641BB 641CB 642CB 642DB 642EB* 15.00643AB 643BB 643CB 643DB650BB 650DB 650EB 650GB 650LB 650QB* 9.00660AB* 1.50ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 31APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-550-0403-1 550 FUEL TANK & SURGE TANK MEC GVI I: 5 YE CPCP MRB REFERENCE: 1 1.50 ALL650 MRB Z ZL-5501 1.50GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 571180-C603-1- FUEL FEED,REFUEL,DEFUEL,VENTILATION AND JETTISON 571185-C603-1SYSTEM (WHEN FITTED), PIPES AND COMPONENTS, 571190-C603-1QUANTITY INDICATING SYSTEM, 573310-C603-1- VENT HOLES IN RIB 15 (FOR OBSTRUCTION), 573320-C603-1- INTERNAL STRUCTURE, INCLUDES ZONE 560 RESPECTIVELY 573330-C603-1660,- WING MAIN BOX INTERNAL STRUCTURE FROM FRONT TOREAR SPAR, BETWEEN RIB 27 AND WING TIP.- OUTBOARD WING LOWER SKIN AT SURGE TANK ACCESS DOORSAND ASSOCIATED DOORS.- STRONTIUM CHROMATE CAPSULES (IF INSTALLED) FORCORRECT CONTENT.ACCESS: 550BB 550DB 550EB 550GB 550LB 550QB* 10.50560AB650BB 650DB 650EB 650GB 650LB 650QB* 10.50660ABZL-570-0402-1 571 MAIN LANDING GEAR BAY MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 0.50 ALL671 ZL-5701 0.50GENERAL VISUAL INSPECTION OF ZONE INCLUDING:- FLIGHT CONTROLS AND FUEL ISOLATION VALVE,- STRUCTURE.ZL-570-0403-1 572 T/E FLAP-ALLSPEED AIL. MEC GVI I: 1 C CPCP MRB REFERENCE: 1 2.00 ALL672 MRB Z ZL-5701 2.0001. GENERAL VISUAL INSPECTION OF: 572201-C603-1- WING FIXED TRAILING EDGE INCLUDING REAR SPARAFT FACE AND FALSE REAR SPAR RIB 1 TO RIB 9- WING FIXED TRAILING EDGE INCLUDING REAR SPARAFT FACE RIBS 9 TO RIB 25.- TRAILING EDGE AREA INCLUDING FLIGHT CONTROLSAND FUEL ISOLATION VALVE- AFT WING ROOT AREA INCLUDING FLIGHT CONTROLSINNER FLAP HINGES- ALL SPEED AILERON HINGE AND ACTUATORATTACHMENTS- FLAPS DRIVE SYSTEM UNIVERSAL JOINTS (GAITERS INPLACE AND NOT DAMAGED)02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 32APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-570-0403-1 * * * * * C O N T I N U E * * * * *G2 OR G3 AFTER INSPECTION WITH AN INTERVAL NOTEXCEEDING 9 YEARSPREP.: FLAPS FULLY EXTENDEDACCESS: 572AB 572CB 572GB 572LB 575AB 575AT* 3.75575BB 575CB 575DB 575EB 575FB 575GB576AB 576BB 576CB 576DB 576EB 576FB577AB 577BB 577ET 577FT 577GT672AB 672CB 672GB 672LB 675AB 675AT* 3.79675BB 675CB 675DB 675EB 675FB 675GB676AB 676BB 676CB 676DB 676EB 676FB677AB 677BB 677ET 677FT 677GTZL-570-0403-2 572 T/E FLAP-ALLSPEED AIL. MEC GVI I: 9 YE CPCP MRB REFERENCE: 1 2.00 ALL672 MRB Z ZL-5701 2.0001. GENERAL VISUAL INSPECTION OF STRUCTURE INCLUDING: 572201-C603-1-TRAILING EDGE AREA INTERNAL STRUCTURE, 572210-C603-1-INNER FLAP INTERNAL STRUCTURE AS FAR AS VISIBLE, 572220-C603-1-ALL SPEED AILERON INTERNAL STRUCTURE, 573301-C602-102. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.PREP.: FLAPS FULLY EXTENDEDACCESS: 572AB 572CB 572GB 572LB 575AB 575AT* 3.75575BB 575CB 575DB 575EB 575FB 575GB576AB 576BB 576CB 576DB 576EB 576FB577AB 577BB 577ET 577FT 577GT672AB 672CB 672GB 672LB 675AB 675AT* 3.79675BB 675CB 675DB 675EB 675FB 675GB676AB 676BB 676CB 676DB 676EB 676FB677AB 677BB 677ET 677FT 677GTZL-570-0403-3 577 AFT WING ROOT MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 0.17 ALL677 ZL-5701 0.17GENERAL VISUAL INSPECTION OF ZONE FOR CONDITION OFSTRUCTURE INCLUDING FLAP BEAM AND ATTACHMENTBEARINGS.PREP.: EXTEND FLAPS.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 33APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-570-0403-3 * * * * * C O N T I N U E * * * * *ACCESS: 577AB 577AT 577BB 577BT 577CT 577DT* 2.38677AB 677AT 677BB 677BT 677CT 677DT* 2.38ZL-580-0403-1 580 INTERM/OUTB.FLAP TRAIL.EDGE MEC GVI I: 2 C CPCP MRB REFERENCE: 1 1.00 ALL680 MRB Z ZL-5801 1.00GENERAL VISUAL INSPECTION OF ZONE INCLUDING FLIGHT 572210-C603-1CONTROL INSTALLATIONS AND FLAP TAB HINGES AND FLAPSDRIVE SYSTEM UNIVERSAL JOINTS(GAITERS IN PLACE AND NOT DAMAGED)NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.WITH AN INTERVAL NOT EXCEEDING 9 YEARSPREP.: EXTEND FLAPS.ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB* 0.35581JB 581KB681CB 681DB 681EB 681FB 681GB 681HB* 0.35681JB 681KBZL-580-0403-2 580 INTERM/OUTB.FLAP TRAIL.EDGE MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 0.50 ALL680 ZL-5801 0.50GENERAL VISUAL INSPECTION OF ZONE FOR CONDITION OFSTRUCTURE INCLUDING FLAP INTERNAL STRUCTURE.PREP.: EXTEND FLAPS.ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB* 0.35581JB 581KB681CB 681DB 681EB 681FB 681GB 681HB* 0.35681JB 681KBZL-590-0403-1 590 TRAIL.EDGE-LOWSPEED AIL. MEC GVI I: 2 C CPCP MRB REFERENCE: 1 0.50 ALL690 MRB Z ZL-5901 0.50GENERAL VISUAL INSPECTION OF ZONE INCLUDING FLIGHT 572210-C603-1CONTROL INSTALLATIONS AND LOW SPEED AILERON HINGES 572220-C603-1AND ACTUATOR ATTACHMENTS AND WING FIXED TRAILINGEDGE INCLUDING REAR SPAR AFT FACE RIBS 25 TO TOP.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 34APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-590-0403-1 * * * * * C O N T I N U E * * * * *NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,G2 OR G3 AFTER INSPECTION.WITH AN INTERVAL NOT EXCEEDING 9 YEARSACCESS: 591AB 591BB 591CB 591DB 592AB 592BB* 0.79592CB 592DB 592EB 592FB 592GB 592HB691AB 691BB 691CB 691DB 692AB 692BB* 0.88692CB 692DB 692EB 692FB 692GB 692HBZL-590-0403-2 590 TRAIL.EDGE-LOWSPEED AIL. MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 0.17 ALL690 ZL-5901 0.17GENERAL VISUAL INSPECTION OF ZONE STRUCTUREINCLUDING LOW SPEED AILERON STRUCTURE.ACCESS: 591AB 591BB 591CB 591DB 592AB 592BB* 0.79592CB 592DB 592EB 592FB 592GB 592HB691AB 691BB 691CB 691DB 692AB 692BB* 0.88692CB 692DB 692EB 692FB 692GB 692HBZL-710-0402-1 711 NOSE GEAR MEC GVI I: 1 C CPCP MRB REFERENCE: 1 2.00 ALLMRB Z C53-100-02-02GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: ZL-710NOSE LANDING GEAR BAY ZONE 123/124,NOSE GEAR ZONE 711,INCLUDING,- LANDING GEAR COMPONENTS- STEERING MECHANISM- TELESCOPIC STRUT VISUAL LOCK INDICATOR ASSY.ZL-710-0402-2 710 NOSE GEAR DOORS & AREA MEC GVI I: 1 C CPCP MRB REFERENCE: 1 1.00 ALLMRB Z C53-100-02-02GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: ZL-710LOWER HALF OF FUSELAGE ZONE 120- DOOR HINGE FITTINGSNOSE GEAR DOORS ZONES 712,713,714,715, AND 716- STRUCTURE- HINGES- ATTACHMENT FITTINGS ( RODS AND SPRINGS )ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 35APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-730-0402-1 731 MAIN GEAR MEC GVI I: 1 C MRB Z MRB REFERENCE: 1 2.00 ALL741 ZL-7301 2.00GENERAL VISUAL INSPECTION OF ZONE INCLUDINGLANDING GEAR COMPONENTS AND INSTALLATIONS.ZL-730-0402-2 730 MAIN GEAR DOORS & AREA MEC GVI I: 1 C CPCP MRB REFERENCE: 1 1.00 ALL740 MRB Z C53-100-02-071 1.00GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: ZL-730LOWER HALF OF FUSELAGE ZONE 147/148- SKIN SURROUNDING MAIN GEAR BAY CUT-OUT- DOOR HINGE FITTINGSMAIN LANDING GEAR DOORS- STRUCTURE -INCLUDING HINGES AND ATTACHMENTS (RODS AND SPRINGS)ZL-810-0402-1 811 FWD CARGO COMPARTMENT DOOR MEC GVI I: 1 C CPCP MRB REFERENCE: 1 0.50 ALLMRB Z ZL-810GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 523101-C602-1- HOOK FITTINGS,- SEALS,- STRUCTURE,- HYDRAULIC SYSTEM AS APPLICABLE.ACCESS: 811* 0.15ZL-810-0402-2 812 AFT CARGO COMPARTMENT DOOR MEC GVI I: 1 C CPCP MRB REFERENCE: 1 0.50 ALLMRB Z ZL-810GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 523201-C602-1- HOOK FITTINGS,- SEALS,- STRUCTURE,- HYDRAULIC SYSTEM AS APPLICABLE.ACCESS: 812* 0.01ZL-810-0402-3 813 BULK CARGO COMPARTMENT DOOR MEC GVI I: 1 C CPCP MRB REFERENCE: 1 0.20 ALLMRB Z ZL-810GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 523401-C602-1- SEALS,- OPERATING MECHANISM,- STRUCTURE.* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 36APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-810-0402-3 * * * * * C O N T I N U E * * * * *ACCESS: 813* 0.01ZL-830-0402-1 830 PAX/CREW DOORS & EMERG.EXIT MEC GVI I: 1 C CPCP MRB REFERENCE: 1 3.20 ALL840 MRB Z ZL-8301 3.20 EXCL. F4GENERAL VISUAL INSPECTION OF ALL PAX/CREW AND 521101-C602-1EMERGENCY EXIT DOORS INCLUDING: 521110-C602-1- SEALS, 521210-C602-1- DOOR STOPS, 521301-C602-1- HOOK ATTACHMENTS, 522201-C602-1- STRUCTURE.(INCLUDING ZONE 840)ZL-830-0402-2 835 UDC DOOR MEC GVI I: 1 C CPCP MRB REFERENCE: 1 0.50 C4MRB Z ZL-830F4GENERAL VISUAL INSPECTION OF UPPER (MAIN) DECK CARGO 523601-C602-1MSN 256DOOR INCLUDING:- HOOK FITTINGS,- SEALS,- STRUCTURE,- HYDRAULIC COMPONENTS AND INSTALLATION.ACCESS: 835* 0.05ZL-830-0402-3 830 FWD PAX/CREW DOOR MEC GVI I: 1 C CPCP MRB REFERENCE: 1 0.80 F4840 MRB Z ZL-8301 0.80GENERAL VISUAL INSPECTION OF FWD PAX/CREW AND 521101-C602-1EMERGENCY EXIT DOORS INCLUDING: 521110-C602-1- SEALS, 521210-C602-1- DOOR STOPS, 521301-C602-1- HOOK ATTACHMENTS, 522201-C602-1- STRUCTURE.(INCLUDING ZONE 840)ZL-830-0403-2 835 UPPER DECK CARGO DOOR MEC GVI I: 5 YE MRB Z MRB REFERENCE: 1 15.00 C4ZL-830F401. GENERAL VISUAL INSPECTION OF UDC DOOR FOR GENERALMSN 256CONDITION INCLUDING;- DOOR MECHANISM AND INSTALLATIONS- INTERNAL STRUCTURE* * * * * C O N T I N U E D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 37APPLICABILITYREFERENCESOURCEDESCRIPTIONTASK NUMBER ZONEMEN M/H



# A300MAINTENANCE PLANNING DOCUMENTSAMPLE THRESHOLD (ST)SAMPLE INTERVAL (SI)THRESHOLD (T)INTERVAL (I)ZL-830-0403-2 * * * * * C O N T I N U E * * * * *PREP.: DOOR LINING AND INSULATION REMOVED.ACCESS: 835AR 835BR 835CR 835DR 835ER 835FR* 0.88835GRZL-830-0403-3 830 PAX/CREW DOORS & EMERG.EXIT MEC GVI I: 5 YE CPCP MRB REFERENCE: 2 2.00 F4840 MRB Z ZL-8302 2.00GENERAL VISUAL INSPECTION OF MID AND AFT PAX/CREW 521101-C602-1DOORS AND EMERG. EXIT, INCLUDING: 521110-C602-1- SEALS 521210-C602-1- DOOR STOPS 521301-C602-1- STRUCTURE FOR CONDITION 522201-C602-1(INCLUDING ZONE 840)PREP.: DOORS REMOVED* * * * * E N D * * * * *ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION:4-ZL PAGE 38

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 1 

# APPENDIX 1 — LIST OF DELETED TASKS

LIST OF DELETED TASKS

TASK NUMBER DELETION DATE REVISION NBR

ZL-100-0402-4 1997/04/15 0021

ZL-120-0403-2 1997/04/15 0021

ZL-120-0403-5 1997/04/15 0021

ZL-120-0403-6 1997/04/15 0021

ZL-130-0403-A 2005/11/18 0027

ZL-130-0403-B 2005/11/18 0027

ZL-130-0403-9 2002/08/30 0026

ZL-170-0403-3 1997/04/15 0021

ZL-200-0402-5 1997/04/15 0021

ZL-200-0402-6 1997/04/15 0021

ZL-220-0403-4 1997/04/15 0021

ZL-220-0403-7 1997/04/15 0021

ZL-221-0403-2 1997/04/15 0021

ZL-221-0403-5 1997/04/15 0021

ZL-221-0403-8 2006/10/01 0028

ZL-330-0403-3 1997/04/15 0021

ZL-400-0402-2 1997/04/15 0021

ZL-410-0802-1 1999/04/23 0024

ZL-410-0812-1 1999/04/23 0024

ZL-430-0803-1 1999/04/23 0024

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 2 

# ZL-430-0803-2 1999/04/23 0024

ZL-430-0813-1 1999/04/23 0024

ZL-430-0813-2 1999/04/23 0024

ZL-510-0403-1 1997/04/15 0021

ZL-830-0403-4 2006/10/01 0028

251100-0504-1 2002/08/30 0026

256531-0504-1 1995/10/30 0019

261900-0502-1 2006/10/01 0028

262411-0504-4 2009/10/01 0029

273411-0503-2 2009/10/01 0029

274211-0503-5 2010/04/01 0030

275100-0504-1 1993/10/30 0017

275112-0504-1 1993/10/30 0017

281100-0503-4 2006/10/01 0028

281100-0505-2 2006/10/01 0028

291000-0802-1 1999/04/23 0024

291000-0812-1 1999/04/23 0024

291133-0503-2 1994/10/30 0018

323100-0502-1 1999/04/23 0024

323300-0503-3 2006/10/01 0028

342200-0503-1 2009/10/01 0029

342538-0504-2 1997/11/18 0022

352100-0502-1 2006/10/01 0028

352100-0502-2 2009/10/01 0029

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 3 

# 352100-0503-1 2009/10/01 0029

352100-0503-2 2009/10/01 0029

352100-0503-3 2006/10/01 0028

352100-0503-4 2006/10/01 0028

352100-0503-5 2006/10/01 0028

352100-0503-6 2006/10/01 0028

352100-0504-1 2006/10/01 0028

352100-0505-1 2006/10/01 0028

383124-0505-1 1998/12/14 0023

492000-0702-2 1994/10/30 0018

493116-0702-1 2009/10/01 0029

495000-0702-4 1989/10/30 0012

521031-0502-1 2009/10/01 0029

521114-0505-2 2006/10/01 0028

521121-0503-2 2006/10/01 0028

521121-0505-2 2006/10/01 0028

521301-0602-1 2009/10/01 0029

522231-0502-1 2009/10/01 0029

523305-0603-1 1997/04/15 0021

523307-0602-1 1997/04/15 0021

523311-0602-1 1993/10/30 0017

523311-0603-1 1995/10/30 0019

523313-0603-1 1993/10/30 0017

523313-0603-2 1993/10/30 0017

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 4 

# 523325-0603-1 2006/10/01 0028

523326-0603-1 2006/10/01 0028

523327-0602-1 2006/10/01 0028

523328-0603-1 2006/10/01 0028

523703-0603-1 1997/04/15 0021

523705-0603-1 1997/04/15 0021

523707-0602-1 1997/04/15 0021

523711-0603-1 1997/04/15 0021

528001-0607-1 1997/04/15 0021

528001-0608-1 1993/01/30 0016

528003-0607-1 1997/04/15 0021

528011-0608-1 1997/04/15 0021

528023-0607-1 1997/04/15 0021

528025-0608-1 1997/04/15 0021

529001-0603-1 2009/10/01 0029

529001-0603-2 2009/10/01 0029

529002-0603-1 2009/10/01 0029

529002-0603-2 2009/10/01 0029

530501-0602-1 1997/04/15 0021

530501-0604-1 1995/10/30 0019

530503-0604-1 1997/04/15 0021

530711-0604-1 1997/04/15 0021

530901-0602-1 1997/04/15 0021

530903-0604-1 1995/10/30 0019

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 5 

# 530907-0602-1 1997/04/15 0021

531000-0602-1 1999/04/23 0024

531000-0603-4 1997/04/15 0021

531001-0603-4 1997/04/15 0021

531101-0604-1 1995/10/30 0019

531105-0604-1 1995/10/30 0019

531107-0604-1 1997/04/15 0021

531115-0604-1 1995/10/30 0019

531133-0602-1 1997/04/15 0021

531135-0602-1 1997/04/15 0021

531214-0604-1 2009/10/01 0029

531239-0602-1 1997/04/15 0021

531241-0602-1 1997/04/15 0021

531245-0602-1 1997/04/15 0021

531247-0602-1 1997/04/15 0021

531252-0605-1 2010/04/01 0030

531252-0605-2 2010/04/01 0030

531307-0604-1 1997/04/15 0021

531313-0602-1 1997/04/15 0021

531313-0603-2 1997/11/18 0022

531315-0602-1 1997/04/15 0021

531315-0602-2 1997/04/15 0021

531317-0602-1 1997/04/15 0021

531407-0602-1 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 6 

# 531413-0604-1 1993/10/30 0017

531415-0603-1 1997/04/15 0021

531416-0603-1 2006/10/01 0028

531532-0604-1 1995/10/30 0019

531547-0602-1 1997/04/15 0021

531548-0602-1 1997/04/15 0021

531557-0604-1 1997/04/15 0021

531605-0604-2 2002/08/30 0026

531605-0604-3 2002/08/30 0026

531607-0602-1 1997/04/15 0021

531700-0603-1 1997/04/15 0021

531701-0602-1 1997/04/15 0021

531718-0603-1 2002/08/30 0026

531719-0602-1 1997/04/15 0021

531719-0603-1 1997/04/15 0021

531814-0603-1 1997/04/15 0021

531814-0603-2 1995/10/30 0019

531814-0603-3 1995/10/30 0019

531815-0602-1 1997/04/15 0021

531815-0602-3 1997/04/15 0021

531815-0604-1 1997/04/15 0021

531815-0604-2 1997/04/15 0021

531815-0604-3 1997/04/15 0021

531817-0604-2 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 7 

# 531821-0603-1 1997/04/15 0021

531822-0603-1 1997/04/15 0021

531901-0602-1 1997/04/15 0021

531903-0602-1 1997/04/15 0021

531905-0602-1 1997/04/15 0021

531907-0602-1 1997/04/15 0021

531909-0602-1 1997/04/15 0021

531911-0602-1 1997/04/15 0021

531913-0602-1 1997/04/15 0021

531914-0602-1 1997/04/15 0021

531914-0604-1 1997/04/15 0021

531915-0604-1 1995/10/30 0019

531926-0604-1 1993/10/30 0017

531927-0602-1 1993/10/30 0017

531929-0602-1 1997/04/15 0021

531940-0602-1 2009/10/01 0029

533113-0602-1 1997/04/15 0021

533115-0602-1 1997/04/15 0021

533213-0602-1 1997/04/15 0021

533215-0604-1 1995/10/30 0019

533216-0604-1 1995/10/30 0019

533220-0602-1 1989/10/30 0012

533220-0604-1 1997/04/15 0021

533313-0602-2 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 8 

# 533327-0602-1 1997/04/15 0021

533327-0602-2 1997/04/15 0021

533329-0602-2 1997/04/15 0021

533333-0602-1 1993/10/30 0017

533333-0602-2 1993/10/30 0017

533337-0602-1 1993/10/30 0017

533337-0603-1 1993/10/30 0017

533339-0603-2 1997/04/15 0021

533341-0603-2 1997/04/15 0021

533343-0603-2 1997/04/15 0021

533345-0602-2 1997/04/15 0021

533350-0602-1 2006/10/01 0028

533351-0602-1 2006/10/01 0028

533352-0602-1 2006/10/01 0028

533354-0602-1 2006/10/01 0028

533355-0602-1 2006/10/01 0028

533405-0602-1 1997/04/15 0021

533421-0602-1 1997/04/15 0021

533437-0602-2 2002/08/30 0026

533450-0602-1 2006/10/01 0028

533451-0602-1 2006/10/01 0028

533452-0602-1 2006/10/01 0028

533453-0602-1 2006/10/01 0028

533454-0602-1 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETED TASKS Page 9 

# 533455-0602-1 2006/10/01 0028

533456-0602-1 2006/10/01 0028

533457-0602-1 2006/10/01 0028

533503-0602-1 1997/04/15 0021

533505-0602-1 1997/04/15 0021

533517-0602-3 2009/10/01 0029

533522-0604-1 1995/10/30 0019

533523-0602-1 1997/04/15 0021

533723-0602-1 1997/04/15 0021

533727-0602-2 1997/04/15 0021

533729-0602-2 1997/04/15 0021

533731-0604-1 1990/10/30 0013

533733-0604-1 1990/10/30 0013

533801-0602-1 1997/04/15 0021

533805-0602-1 1997/04/15 0021

533815-0602-4 1999/04/23 0024

533815-0603-1 1995/10/30 0019

533815-0604-1 1990/10/30 0013

533824-0602-1 1993/10/30 0017

533824-0603-1 1993/10/30 0017

533824-0604-1 1997/04/15 0021

533903-0602-1 1997/04/15 0021

533905-0602-1 1997/04/15 0021

533907-0602-1 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 10 

# 533913-0603-1 1991/10/30 0014

533917-0602-1 1997/04/15 0021

533935-0603-4 2009/10/01 0029

534000-0603-1 1997/04/15 0021

534705-0604-1 2009/10/01 0029

534705-0604-2 1997/04/15 0021

534705-0604-3 2009/10/01 0029

534901-0604-1 1995/10/30 0019

536114-0606-3 2009/10/01 0029

536202-0606-A 2005/11/18 0027

536202-0606-B 2005/11/18 0027

536202-0606-C 2005/11/18 0027

536202-0606-D 2005/11/18 0027

536202-0606-E 2005/11/18 0027

536204-0607-1 2009/10/01 0029

536204-0607-3 2009/10/01 0029

536204-0608-1 2009/10/01 0029

536204-0608-3 2009/10/01 0029

536206-0606-1 1999/04/23 0024

536206-0606-2 1999/04/23 0024

536206-0606-3 1999/04/23 0024

536206-0606-4 1999/04/23 0024

536206-0606-5 1999/04/23 0024

536206-0606-6 1999/04/23 0024

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 11 

# 536214-0606-2 2009/10/01 0029

536214-0606-3 2009/10/01 0029

536505-0606-A 2005/11/18 0027

536505-0606-B 2005/11/18 0027

536505-0606-C 2005/11/18 0027

536505-0606-D 2005/11/18 0027

536505-0606-E 2009/10/01 0029

536505-0606-F 2005/11/18 0027

536505-0606-G 2005/11/18 0027

536505-0606-H 2005/11/18 0027

536505-0606-I 2005/11/18 0027

536505-0606-J 2005/11/18 0027

536505-0606-K 2005/11/18 0027

536505-0606-L 2005/11/18 0027

536505-0606-2 2006/10/01 0028

536505-0606-3 2006/10/01 0028

536505-0606-4 2006/10/01 0028

536505-0606-5 2006/10/01 0028

536505-0606-6 2006/10/01 0028

536505-0606-7 2006/10/01 0028

536505-0606-8 2006/10/01 0028

536505-0606-9 2006/10/01 0028

536505-0607-1 2006/10/01 0028

536505-0607-2 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 12 

# 536505-0607-3 2006/10/01 0028

536506-0606-1 1997/04/15 0021

536509-0606-2 2006/10/01 0028

536509-0606-3 2006/10/01 0028

536509-0606-4 2006/10/01 0028

536509-0606-5 2006/10/01 0028

536509-0606-6 2006/10/01 0028

536511-0606-A 2005/11/18 0027

536511-0606-B 2005/11/18 0027

536511-0606-C 2005/11/18 0027

536511-0606-D 2005/11/18 0027

536511-0606-E 2005/11/18 0027

536511-0606-F 2005/11/18 0027

536511-0606-G 2005/11/18 0027

536511-0606-H 2005/11/18 0027

536511-0606-I 2005/11/18 0027

536511-0606-J 2005/11/18 0027

536511-0606-2 2006/10/01 0028

536511-0606-3 2006/10/01 0028

536511-0606-4 2006/10/01 0028

536511-0606-5 2006/10/01 0028

536511-0606-6 2006/10/01 0028

536511-0606-7 2006/10/01 0028

536511-0606-8 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 13 

# 536511-0606-9 2006/10/01 0028

536511-0607-1 2006/10/01 0028

536512-0606-2 2006/10/01 0028

536512-0606-3 2006/10/01 0028

536512-0606-4 2006/10/01 0028

536512-0606-5 2006/10/01 0028

536512-0606-6 2006/10/01 0028

536512-0606-7 2006/10/01 0028

536512-0606-8 1994/10/30 0018

536513-0606-A 2005/11/18 0027

536513-0606-B 2005/11/18 0027

536513-0606-C 2005/11/18 0027

536513-0606-D 2005/11/18 0027

536513-0606-E 2005/11/18 0027

536513-0606-F 2005/11/18 0027

536513-0606-G 2005/11/18 0027

536513-0606-H 2005/11/18 0027

536513-0606-I 2005/11/18 0027

536513-0606-J 2005/11/18 0027

536513-0606-2 2006/10/01 0028

536513-0606-3 2006/10/01 0028

536513-0606-4 2006/10/01 0028

536513-0606-5 2006/10/01 0028

536513-0606-6 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 14 

# 536513-0606-7 2006/10/01 0028

536513-0606-8 2006/10/01 0028

536513-0606-9 2006/10/01 0028

536513-0607-1 2006/10/01 0028

536514-0606-1 2010/04/01 0030

536514-0606-2 2010/04/01 0030

536515-0606-A 2005/11/18 0027

536515-0606-B 2005/11/18 0027

536515-0606-C 2005/11/18 0027

536515-0606-D 2005/11/18 0027

536515-0606-E 2005/11/18 0027

536515-0606-F 2005/11/18 0027

536515-0606-G 2005/11/18 0027

536515-0606-H 2005/11/18 0027

536515-0606-J 2005/11/18 0027

536515-0606-K 2005/11/18 0027

536515-0606-L 2005/11/18 0027

536515-0606-M 2005/11/18 0027

536515-0606-N 2005/11/18 0027

536515-0606-O 2005/11/18 0027

536515-0606-P 2005/11/18 0027

536515-0606-Q 2005/11/18 0027

536515-0606-R 2005/11/18 0027

536515-0606-S 2005/11/18 0027

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 15 

# 536515-0606-T 2005/11/18 0027

536515-0606-U 2005/11/18 0027

536515-0606-V 2005/11/18 0027

536515-0606-W 2005/11/18 0027

536515-0606-X 2005/11/18 0027

536515-0606-2 2006/10/01 0028

536515-0606-3 2006/10/01 0028

536515-0606-4 2006/10/01 0028

536515-0606-5 2006/10/01 0028

536515-0606-6 2006/10/01 0028

536515-0606-7 2006/10/01 0028

536515-0606-8 2006/10/01 0028

536515-0606-9 2006/10/01 0028

536515-0607-1 2006/10/01 0028

536515-0607-2 2006/10/01 0028

536515-0607-3 2006/10/01 0028

536515-0607-4 2006/10/01 0028

536515-0607-5 2006/10/01 0028

536515-0607-6 2006/10/01 0028

536515-0607-7 2006/10/01 0028

536515-0607-8 2006/10/01 0028

536515-0607-9 2006/10/01 0028

536515-0608-1 2006/10/01 0028

536515-0608-2 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 16 

# 536515-0608-3 2006/10/01 0028

536515-0608-4 2006/10/01 0028

536515-0608-5 2006/10/01 0028

536515-0608-6 2006/10/01 0028

536516-0606-2 2005/11/18 0027

536516-0606-3 2005/11/18 0027

536516-0606-5 2005/11/18 0027

536516-0606-7 2005/11/18 0027

536521-0606-1 1997/04/15 0021

536523-0606-1 1997/04/15 0021

536529-0606-2 2006/10/01 0028

536529-0606-3 2006/10/01 0028

536529-0606-4 2006/10/01 0028

536529-0606-5 2006/10/01 0028

536529-0606-6 2006/10/01 0028

536529-0606-7 2006/10/01 0028

536529-0606-8 2006/10/01 0028

536529-0606-9 2006/10/01 0028

536530-0606-1 2006/10/01 0028

536535-0606-2 2006/10/01 0028

536535-0606-3 2006/10/01 0028

536535-0606-4 2006/10/01 0028

536535-0606-5 2006/10/01 0028

536535-0606-6 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 17 

# 536535-0606-7 2006/10/01 0028

536535-0606-8 2006/10/01 0028

536543-0606-2 2006/10/01 0028

536543-0606-3 2006/10/01 0028

536543-0606-4 2006/10/01 0028

536543-0606-5 2006/10/01 0028

536543-0606-6 2006/10/01 0028

536544-0606-2 2006/10/01 0028

536544-0606-3 2006/10/01 0028

536544-0606-4 2006/10/01 0028

536544-0606-5 2006/10/01 0028

536544-0606-6 2006/10/01 0028

536545-0606-2 2006/10/01 0028

536548-0606-2 2006/10/01 0028

536548-0606-3 2006/10/01 0028

536548-0606-4 1997/04/15 0021

536549-0606-2 2006/10/01 0028

536549-0606-3 2006/10/01 0028

536549-0606-4 2006/10/01 0028

536549-0606-5 1999/04/23 0024

536549-0606-6 1999/04/23 0024

536549-0606-7 1999/04/23 0024

536554-0606-2 2006/10/01 0028

536555-0606-2 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 18 

# 536555-0606-3 2006/10/01 0028

536576-0606-1 2005/11/18 0027

536576-0606-2 2005/11/18 0027

536577-0606-1 2005/11/18 0027

536580-0606-1 2006/10/01 0028

536580-0606-2 2006/10/01 0028

536581-0606-1 2006/10/01 0028

536581-0606-2 2006/10/01 0028

536596-0606-1 1997/04/15 0021

536597-0606-A 2005/11/18 0027

536597-0606-B 2005/11/18 0027

536597-0606-C 2005/11/18 0027

536597-0606-D 2005/11/18 0027

536597-0606-E 2005/11/18 0027

536597-0606-F 2005/11/18 0027

536597-0606-G 2005/11/18 0027

536597-0606-H 2005/11/18 0027

536597-0606-I 2005/11/18 0027

536597-0606-J 2005/11/18 0027

536597-0606-K 2005/11/18 0027

536597-0606-L 2005/11/18 0027

536597-0606-5 2006/10/01 0028

536597-0606-6 2006/10/01 0028

536597-0606-7 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 19 

# 536597-0606-8 2006/10/01 0028

536597-0606-9 2006/10/01 0028

536598-0606-4 1997/04/15 0021

536598-0606-7 2006/10/01 0028

536598-0606-8 2006/10/01 0028

536598-0606-9 2006/10/01 0028

536601-0606-2 2006/10/01 0028

536601-0606-3 2006/10/01 0028

536601-0606-4 2006/10/01 0028

536601-0606-5 2006/10/01 0028

536601-0606-6 2006/10/01 0028

536602-0606-2 2006/10/01 0028

536603-0606-2 1997/04/15 0021

536603-0606-3 2006/10/01 0028

536603-0606-4 1997/04/15 0021

536603-0606-5 2006/10/01 0028

536603-0606-6 1997/04/15 0021

536651-0606-1 1997/04/15 0021

536651-0606-8 2006/10/01 0028

536651-0606-9 2006/10/01 0028

536652-0606-1 1997/04/15 0021

536702-0606-A 2005/11/18 0027

536702-0606-B 1999/04/23 0024

536702-0606-C 2005/11/18 0027

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 20 

# 536702-0606-D 1999/04/23 0024

536702-0606-E 2005/11/18 0027

536702-0606-F 1999/04/23 0024

536702-0606-G 2005/11/18 0027

536702-0606-H 1999/04/23 0024

536702-0606-I 2005/11/18 0027

536702-0606-J 1999/04/23 0024

536702-0606-K 2005/11/18 0027

536702-0606-L 1999/04/23 0024

536702-0606-3 2006/10/01 0028

536702-0606-5 2006/10/01 0028

536702-0606-7 2006/10/01 0028

536702-0606-8 2006/10/01 0028

536702-0606-9 2006/10/01 0028

536703-0606-4 2006/10/01 0028

536801-0606-2 2006/10/01 0028

536801-0606-3 2006/10/01 0028

536801-0606-4 2006/10/01 0028

536801-0606-5 2006/10/01 0028

536801-0606-6 2006/10/01 0028

536901-0606-A 2005/11/18 0027

536901-0606-B 2005/11/18 0027

536901-0606-C 2005/11/18 0027

536901-0606-D 2005/11/18 0027

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 21 

# 536901-0606-E 2005/11/18 0027

536901-0606-F 2005/11/18 0027

536901-0606-G 2005/11/18 0027

536901-0606-H 2005/11/18 0027

536901-0606-I 2005/11/18 0027

536901-0606-J 2005/11/18 0027

536901-0606-4 2006/10/01 0028

536901-0606-6 2006/10/01 0028

536901-0606-7 2006/10/01 0028

536901-0606-8 2006/10/01 0028

536901-0606-9 2006/10/01 0028

538003-0607-1 1997/04/15 0021

538013-0608-1 1997/04/15 0021

538041-0607-1 1997/04/15 0021

538051-0607-1 1993/01/30 0016

538052-0607-1 1993/01/30 0016

538053-0607-1 1993/01/30 0016

538101-0608-1 1997/04/15 0021

538123-0608-1 1995/10/30 0019

538141-0607-1 1997/04/15 0021

538151-0607-1 1997/04/15 0021

538161-0607-2 1993/01/30 0016

538173-0607-1 1993/01/30 0016

538221-0607-1 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 22 

# 538223-0608-1 1997/04/15 0021

538227-0607-1 1997/04/15 0021

538241-0607-1 1993/01/30 0016

538255-0608-1 1997/04/15 0021

538285-0608-1 1997/04/15 0021

538285-0608-2 1997/04/15 0021

538305-0608-1 1997/04/15 0021

538315-0608-1 1993/01/30 0016

538375-0608-1 1997/04/15 0021

538425-0608-1 1997/04/15 0021

538427-0608-1 1997/04/15 0021

538477-0608-1 1997/04/15 0021

538527-0608-1 1997/04/15 0021

538547-0607-1 1993/01/30 0016

538549-0608-1 1997/04/15 0021

538559-0608-1 1997/04/15 0021

538561-0608-1 1997/04/15 0021

538563-0603-1 2005/11/18 0027

538585-0608-1 1997/04/15 0021

538591-0608-1 1997/04/15 0021

538595-0603-1 2002/08/30 0026

538597-0608-1 1997/04/15 0021

538667-0608-1 1997/04/15 0021

538671-0603-1 2002/08/30 0026

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 23 

# 538677-0608-1 1997/04/15 0021

538689-0608-1 1997/04/15 0021

538699-0608-1 1997/04/15 0021

538719-0608-1 1997/04/15 0021

538723-0608-1 1997/04/15 0021

538759-0608-1 1997/04/15 0021

538809-0608-1 1997/04/15 0021

539002-0603-1 2005/11/18 0027

539002-0603-2 2005/11/18 0027

539004-0603-1 2005/11/18 0027

539007-0603-1 2009/10/01 0029

540001-0604-1 1997/04/15 0021

540002-0602-1 1997/04/15 0021

540003-0604-1 1995/10/30 0019

540008-0602-1 1997/04/15 0021

540011-0604-1 1997/04/15 0021

541000-0502-2 2002/08/30 0026

541003-0603-1 1997/04/15 0021

541013-0604-1 1995/10/30 0019

543002-0602-1 2006/10/01 0028

543002-0602-2 2006/10/01 0028

543002-0602-3 2006/10/01 0028

544003-0604-1 1997/04/15 0021

544004-0604-1 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 24 

# 544011-0604-1 1997/04/15 0021

544012-0604-1 1997/04/15 0021

544200-0603-3 2009/10/01 0029

548011-0607-1 1993/01/30 0016

548011-0608-1 1997/04/15 0021

548022-0608-1 1993/01/30 0016

551005-0603-1 1997/04/15 0021

551007-0603-1 1997/04/15 0021

551031-0603-1 1997/04/15 0021

552003-0603-1 1997/04/15 0021

552005-0603-1 1997/04/15 0021

553001-0603-1 1997/04/15 0021

553003-0603-1 1997/04/15 0021

553009-0603-1 1997/04/15 0021

553011-0604-1 1995/10/30 0019

553013-0603-1 1997/04/15 0021

553015-0603-1 1997/04/15 0021

553017-0604-1 1995/10/30 0019

553019-0603-1 1997/04/15 0021

554001-0603-1 1997/04/15 0021

554003-0603-1 1997/04/15 0021

554009-0603-1 1997/04/15 0021

554011-0603-1 1997/04/15 0021

554013-0603-1 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 25 

# 554015-0604-1 1995/10/30 0019

555001-0603-1 1997/04/15 0021

555003-0603-1 1997/04/15 0021

555005-0603-1 1997/04/15 0021

555007-0603-1 1997/04/15 0021

555007-0604-1 1997/04/15 0021

555009-0603-1 1997/04/15 0021

555009-0604-1 1995/10/30 0019

555011-0603-1 1997/04/15 0021

555011-0604-1 1995/10/30 0019

555013-0603-1 1997/04/15 0021

555013-0604-1 1995/10/30 0019

555015-0603-1 1997/04/15 0021

555015-0604-1 1997/04/15 0021

555017-0603-1 1997/04/15 0021

555017-0604-1 1997/04/15 0021

555019-0603-1 1997/04/15 0021

555019-0604-1 1997/04/15 0021

555023-0603-1 2009/10/01 0029

556001-0606-2 2006/10/01 0028

556001-0606-3 2006/10/01 0028

556002-0606-1 2009/10/01 0029

556002-0606-2 2009/10/01 0029

556002-0606-3 2009/10/01 0029

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 26 

# 556002-0606-4 2009/10/01 0029

556002-0606-5 2009/10/01 0029

556002-0606-6 2009/10/01 0029

558001-0608-1 1997/04/15 0021

558131-0608-1 1997/04/15 0021

558151-0608-1 1997/04/15 0021

558171-0608-1 1997/04/15 0021

558173-0608-1 1997/04/15 0021

558177-0608-1 1997/04/15 0021

558197-0608-1 1997/04/15 0021

558213-0608-1 1997/04/15 0021

558265-0608-1 1997/04/15 0021

571004-0603-1 1993/10/30 0017

571004-0603-2 1993/10/30 0017

571014-0603-1 1997/04/15 0021

571020-0603-2 2005/11/18 0027

571040-0604-1 1995/10/30 0019

571046-0603-1 1993/10/30 0017

571046-0603-2 1993/10/30 0017

571047-0603-1 1993/01/30 0016

571047-0603-2 1993/01/30 0016

571052-0602-1 1997/04/15 0021

571052-0603-1 1997/04/15 0021

571069-0602-1 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 27 

# 571069-0603-2 1997/04/15 0021

571070-0603-2 1997/04/15 0021

571072-0602-1 1997/04/15 0021

571072-0603-2 1997/04/15 0021

571072-0604-1 1997/04/15 0021

571079-0602-1 1997/04/15 0021

571089-0602-1 1997/04/15 0021

571089-0604-1 1997/04/15 0021

571093-0604-1 1997/04/15 0021

571104-0604-1 1991/10/30 0014

571106-0604-2 2002/08/30 0026

571107-0604-1 1997/04/15 0021

571108-0604-1 1997/04/15 0021

571109-0604-1 1997/04/15 0021

571110-0604-1 1997/04/15 0021

571111-0604-1 1997/04/15 0021

571112-0604-1 1997/04/15 0021

571114-0603-1 1993/01/30 0016

571142-0604-1 1997/04/15 0021

571145-0604-1 1997/04/15 0021

571163-0604-1 1995/10/30 0019

571174-0604-1 1997/11/18 0022

572001-0604-1 1997/04/15 0021

572083-0602-1 1997/04/15 0021

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 28 

# 572500-0502-1 2002/08/30 0026

573600-0502-1 1999/04/23 0024

573600-0502-2 1999/04/23 0024

575021-0604-2 2006/10/01 0028

575021-0604-3 2006/10/01 0028

575061-0604-2 2006/10/01 0028

575061-0604-3 2006/10/01 0028

575087-0604-2 2006/10/01 0028

575087-0604-3 2006/10/01 0028

575291-0604-1 1995/10/30 0019

576001-0606-2 2006/10/01 0028

576001-0606-3 2006/10/01 0028

576001-0606-4 2006/10/01 0028

576001-0606-5 2006/10/01 0028

576001-0606-6 2006/10/01 0028

576002-0606-2 2006/10/01 0028

576002-0606-3 2006/10/01 0028

576002-0606-4 2006/10/01 0028

576002-0606-5 1997/11/18 0022

576002-0606-6 2006/10/01 0028

576003-0606-2 2006/10/01 0028

576003-0606-3 2006/10/01 0028

576003-0606-4 1999/04/23 0024

576003-0606-5 1999/04/23 0024

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 29 

# 576003-0606-6 1999/04/23 0024

576005-0606-2 2006/10/01 0028

576005-0606-3 2006/10/01 0028

576005-0606-4 2006/10/01 0028

576005-0606-5 2006/10/01 0028

576005-0606-6 2006/10/01 0028

576006-0606-1 1994/10/30 0018

576006-0606-3 1994/10/30 0018

576006-0606-4 2006/10/01 0028

576006-0606-5 1994/10/30 0018

576006-0606-6 2006/10/01 0028

576008-0606-2 2006/10/01 0028

576008-0606-3 2006/10/01 0028

576008-0606-4 2006/10/01 0028

576008-0606-5 2006/10/01 0028

576008-0606-6 2006/10/01 0028

576010-0606-A 2006/10/01 0028

576010-0606-B 2006/10/01 0028

576010-0606-C 2006/10/01 0028

576010-0606-2 2006/10/01 0028

576010-0606-3 2006/10/01 0028

576010-0606-4 2006/10/01 0028

576010-0606-5 2006/10/01 0028

576010-0606-6 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 30 

# 576010-0606-7 2006/10/01 0028

576010-0606-8 2006/10/01 0028

576010-0606-9 2006/10/01 0028

576012-0606-2 2006/10/01 0028

576012-0606-3 2006/10/01 0028

576012-0606-4 2006/10/01 0028

576012-0606-5 2006/10/01 0028

576012-0606-6 2006/10/01 0028

576012-0606-7 2006/10/01 0028

576012-0606-8 2006/10/01 0028

576012-0606-9 2006/10/01 0028

576014-0606-A 2006/10/01 0028

576014-0606-B 2006/10/01 0028

576014-0606-C 2006/10/01 0028

576014-0606-2 2006/10/01 0028

576014-0606-3 2006/10/01 0028

576014-0606-4 2006/10/01 0028

576014-0606-5 2006/10/01 0028

576014-0606-6 2006/10/01 0028

576014-0606-7 2006/10/01 0028

576014-0606-8 2006/10/01 0028

576014-0606-9 2006/10/01 0028

576016-0606-2 2006/10/01 0028

576016-0606-3 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 31 

# 576016-0606-4 2006/10/01 0028

576016-0606-5 2006/10/01 0028

576016-0606-6 2006/10/01 0028

576041-0606-7 2010/04/01 0030

576053-0605-2 2006/10/01 0028

576053-0605-3 2006/10/01 0028

576053-0605-4 1997/11/18 0022

576053-0605-5 2006/10/01 0028

576053-0605-6 2006/10/01 0028

576053-0605-7 2006/10/01 0028

576053-0605-8 1997/11/18 0022

576053-0605-9 2006/10/01 0028

576055-0606-2 2006/10/01 0028

576055-0606-3 2006/10/01 0028

576055-0606-4 2006/10/01 0028

576055-0606-5 2006/10/01 0028

576055-0606-6 2006/10/01 0028

576056-0606-2 2006/10/01 0028

576057-0606-2 2006/10/01 0028

576057-0606-3 2006/10/01 0028

576058-0606-2 2006/10/01 0028

576058-0606-3 2006/10/01 0028

576058-0606-4 2006/10/01 0028

576058-0606-5 2006/10/01 0028

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 32 

# 576059-0606-2 2006/10/01 0028

576060-0605-2 2006/10/01 0028

576066-0606-2 2006/10/01 0028

576066-0606-3 2006/10/01 0028

576066-0606-4 2006/10/01 0028

576066-0606-5 2006/10/01 0028

576066-0606-6 2006/10/01 0028

576069-0606-2 2006/10/01 0028

576069-0606-3 2006/10/01 0028

576069-0606-4 2006/10/01 0028

576071-0606-2 2006/10/01 0028

578001-0608-1 1997/04/15 0021

578003-0607-1 1997/04/15 0021

578011-0607-1 1997/04/15 0021

578041-0607-1 1997/04/15 0021

578043-0608-1 1997/04/15 0021

578051-0608-1 1997/04/15 0021

578061-0607-1 1997/04/15 0021

578121-0608-1 1997/04/15 0021

578171-0608-1 1997/04/15 0021

578191-0608-1 1997/04/15 0021

578241-0608-1 1997/04/15 0021

578251-0608-1 1997/04/15 0021

720000-0801-1 1989/10/30 0012

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 1 — LIST OF DELETE D TASKS Page 33 

# 723100-0802-1 1997/04/15 0021

723400-0802-1 1998/12/14 0023

725300-0802-2 1997/04/15 0021

725400-0802-1 2006/10/01 0028

725700-0801-2 1993/10/30 0017

726000-0802-3 1996/10/30 0020

781100-0802-3 2009/10/01 0029

783100-0805-4 1997/11/18 0022

783300-0802-2 1997/04/15 0021

783600-0801-1 1998/12/14 0023

783600-0805-2 1998/12/14 0023

790000-0805-1 1998/12/14 0023

792000-0802-1 1998/12/14 0023

792000-0802-2 1998/12/14 0023

792100-0802-1 1998/12/14 0023

792200-0802-1 1998/12/14 0023

801300-0801-1 1998/12/14 0023

801301-0801-1 1994/10/30 0018

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2 — CROSS REFERENCE LIST Page 1 

# APPENDIX 2 — CROSS REFERENCE LIST

1. Scope

The present section provides a cross-reference between the following documents

– Airworthiness Directives (French: CN; USA: AD)

– Modifications (MOD)

– Inspection Service Bulletins (ISB)

– Service Information Letters (SIL)

– All Operator Telexes (AOT)

and the respective Task Number(s) of their related repetitive maintenance repercussion(s).

NOTE: This section only reflects the latest revision of the above documents. Revisions, or new issues,

taking place after the present A300 MPD revision are not included. It is the operators

responsibility to adjust their program on receipt of the source document and not to wait until the

amended A300 MPD revision.

NOTE: In XLS and PDF format, the Cross Reference Lists are provided within the Appendix 2 (below

this introduction).

In AirN@v / Planning, the Cross Reference Lists are provided via interactive functions in the

menu “MPD”.

2. FORMAT

This section is divided into fife (5) sub–sections as follows:

SUB-SECTION 01:

CONSIGNES DE NAVIGABILITE - REPETITIVE MAINTENANCE REPERCUSSIONS

CN AD MOD TASK NUMBER SECTION



# The "MOD" information is quoted only if the AD/CN requirement results in a pre or post modification

configuration.

SUB-SECTION 02:

MODIFICATIONS - REPETITIVE MAINTENANCE REPERCUSSIONS

MOD MOD-SB ISB PRE MOD. POST MOD.

TASK NUMBER SECTION TASK NUMBER SECTION



# The "MOD SB" information is quoted only when applicable (i.e. retrofitable modifications).

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2 — CROSS REFERENCE LIST Page 2 

# The "ISB" information is quoted only, if applicable, for the pre or post modification related task(s)

covered by such a publication.

SUB-SECTION 03:

INSPECTION SERVICE BULLETINS - REPETITIVE MAITENANCE REPE RCUSSIONS

ISB MOD TASK NUMBER SECTION



# The "MOD" information is quoted only if the ISB instructions depend on a pre or post modification

configuration.

SUB-SECTION 04:

SERVICE INFORMATION LETTERS - REPETITIVE MAINTENANCE REPERCUSSIONS

SIL MOD TASK NUMBER SECTION



# The "MOD" information is quoted only if the SIL recommendations depend on a pre or post modification

configuration.

SUB-SECTION 05:

ALL OPERATOR TELEXES - REPETITIVE MAINTENANCE REPERCUSSIONS

AOT TASK NUMBER CN/AD ISB MOD

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 1 

# APPENDIX 2-1

AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

1977-163-IMP(B) FAA AD77-17-06 PRE 02011

(49-0029) 492000-0703-2 2-49

1979-125-018(B) PRE 01208 530503-0603-1 3-53

1980-151-027(B) FAA AD80-16-52 PRE 03101

(32-0267) 324247-0502-1 2-32

1980-218-028(B) FAA AD94-09-15 PRE 02476

(53-0121) 531912-0603-1 3-53

1980-218-028(B) FAA AD94-09-15 PRE 02476

(53-0121) 531912-0603-2 3-53

1980-222-030(B) FAA AD80-18-02 NON FWD-FACE

POST 01508

(22-0025) 222300-0503-1 2-22

1981-058-033(B) FAA AD80-26-07 MSN 003-116

PRE (24-0048) 242200-0502-1 2-24

1981-085-036(B) FAA AD85-09-05

POST 2684

(27-128)

P/N CHA723-20XX 274211-0503-3 2-27

1981-085-036(B) FAA AD85-09-05 PRE 2684

(27-128)

P/N CHA723-010

THRU

P/N CHA723-018 274211-0503-4 2-27

1981-085-036(B) FAA AD85-09-05 POST 02684

(27-0128)

PRE 02787

(27-0129)

P/N CHA723-010

THRU

P/N CHA723-018

P/N CHA723-20XX 274211-0504-2 2-27

1981-174-041(B) FAA AD84-02-04 PRE 01257

MHB 224 321100-0502-2 2-32

1982-022-044(B) FAA AD85-17-06 PRE 01878

(25-0149)

PRE 02506

(25-0248) 255120-0502-1 2-25

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 2 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

1982-022-044(B) FAA AD85-17-06 POST 01878

(25-0149)

POST 02506

(25-0248)

PRE 03361

(25-0332) 255120-0502-2 2-25

1982-160-049(B)

1983-051-050(B) FAA AD84-03-08 POST 01257

MHB 224

PRE 04544

(32-0348)

(32-0355)

MHB 542/ 585

P/N C65381-4

P/N C65381-6 321100-0503-1 2-32

1983-011-IMP(B) FAA AD82-25-08 GE 725300-0803-1 2-72

1983-052-051(B) FAA AD84-02-04 PRE 01257

MHB 485

P/N C65381-2

P/N C65381-4 321100-0503-2 2-32

1983-102-053(B) FAA AD98-20-36 PRE 02611 531400-0602-2 3-53

1983-102-053(B) FAA AD98-20-36 PRE 02643

(53-0132) 531700-0602-1 3-53

1983-102-053(B) FAA AD98-20-36 PRE 01358

(53-0027) 533437-0602-3 3-53

1983-102-053(B) FAA AD98-20-36 PRE 02147

(53-0110)

PRE 02348

PRE 02526

(53-0128) 533731-0602-2 3-53

1983-102-053(B) FAA AD98-20-36 MSN 003-052

PRE 03760

(53-0170) 533815-0602-3 3-53

1983-147-055(B) FAA AD84-06-01 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275124-0504-4 2-27

1983-147-055(B) FAA AD84-06-01 PRE 01789

(27-0084)

PRE 04494 275136-0504-4 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 3 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(27-0164)

1983-147-055(B) FAA AD84-06-01 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275137-0504-4 2-27

1983-148-056(B) FAA AD84-06-01 POST 01789

(27-0084)

PRE 04494

(27-0164) 278117-0504-2 2-27

1983-148-056(B) FAA AD84-06-01 POST 01789

(27-0084)

PRE 04494

(27-0164) 278118-0504-2 2-27

1983-148-056(B) FAA AD84-06-01 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278118-0504-4 2-27

1983-148-056(B) FAA AD84-06-01 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278119-0504-2 2-27

1983-148-056(B) FAA AD84-06-01 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278119-0504-4 2-27

1983-148-056(B) FAA AD84-06-01 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278153-0504-2 2-27

1983-148-056(B) FAA AD84-06-01 PRE 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278153-0504-4 2-27

1983-148-056(B) FAA AD84-06-01 PRE 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278153-0504-7 2-27

1983-148-056 FAA AD84-06-01 PRE 01789

(27-0084) 278120-0504-4 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 4 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

PRE 04494

(27-0164)

KRUG.FLAP

1984-066-061(B)

2001-184(B) FAA AD87-21-03

FAA AD91-05-14 PRE 05240

(27-0173) 275126-0502-3 2-27

1984-117-062(B)

1990-222-116(B) FAA AD2000-10-

01

FAA AD87-04-12

FAA AD96-08-08 B2

PRE 05760

(53-0198) 531540-0603-2 3-53

1984-140-064(B) FAA AD2000-16-

07 MSN 003-156

NOTE 531000-0602-4 3-53

1984-140-064(B) FAA AD2000-16-

07 MSN 003-156

NOTE 531000-0603-1 3-53

1984-140-064(B) FAA AD2000-16-

07 MSN 003-156

NOTE 531000-0603-2 3-53

1985-146-IMP(B) FAA AD90-23-11 PRE 01758

(29-0039)

PRE 02528

(29-0060) 292527-0503-3 2-29

1985-146-IMP(B) FAA AD90-23-11 POST 01758

(29-0039)

POST 02528

(29-0060)

PRE 06054

(29-0088) 292527-0503-4 2-29

1985-146-IMP(B) FAA AD90-23-11 POST 01758

(29-0039)

POST 02528

(29-0060)

PRE 06054

(29-0088) 292527-0503-5 2-29

1985-165-071(B) FAA AD85-16-06 GE

PRE 05912

(73-0007) 731000-0802-1 2-73

1986-003-IMP(B) FAA AD85-25-

56GEGE 754300-0802-2 2-75

1986-187-076(B) FAA AD95-21-09 ALL 572512-0603-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 5 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

1987-029-078(B) FAA AD88-03-04 B2 321100-0503-3 2-32

1987-100-080(B) PRE 01257

(32-0383)

MHB SB

470-32-605 322112-0504-2 2-32

1987-121-081(B) FAA AD88-22-08 PRE 06891

(57-0145) 572512-0502-1 2-57

1987-132-082(B) FAA AD88-11-

10R1 GE

PRE (71-0053) 711301-0802-1 2-71

1988-061-083(B) FAA AD89-03-09 PRE 06925

(53-0221) 531820-0603-1 3-53

1988-143-088(B) FAA AD69-23-11 PRE 01257

(32-0389) MHB SB

470-32-642 322112-0504-3 2-32

1988-181-089(B) FAA AD89-09-01 POST 01988

(54-0022) 262100-0503-3 2-26

1989-019-097(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 533727-0602-1 3-53

1989-019-097(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 533727-0602-3 3-53

1989-019-097(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533727-0602-4 3-53

1989-061-092(B) FAA AD90-01-10 MSN 003-156

PRE 02611

POST 01421

(53-0033)

RETROFIT

POST 07085

(53-0223)

OR

POST 01421

SERIAL 531000-0603-5 3-53

1989-061-092(B) FAA AD90-01-10 MSN 003-156

PRE 02611

PRE 02525

(53-0126) 531000-0603-6 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 6 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

POST 01421

(53-0033)

RETROFIT

POST 07085

(53-0223)

OR

POST 01421

SERIAL

1989-061-092(B) FAA AD90-01-10 MSN 003-156

PRE 2611 531000-0603-7 3-53

1989-061-092(B) FAA AD90-01-10 PRE 02727

MSN 003-103 531001-0603-1 3-53

1989-061-092(B) FAA AD90-01-10 PRE 02727

MSN 003-156 531001-0603-2 3-53

1989-061-092(B) FAA AD90-01-10 PRE 02727

MSN 003-156 531001-0603-3 3-53

1989-061-092(B) FAA AD90-01-10 PRE 02727

MSN 105 531001-0603-5 3-53

1989-061-092(B) FAA AD90-01-10 PRE 02727

MSN 107 531001-0603-6 3-53

1989-061-092(B) FAA AD90-01-10 PRE 02727

MSN 109 531001-0603-7 3-53

1989-092-095(B) FAA AD90-17-16 PRE 06240

(52-0132) 521014-0504-1 2-52

1989-157-099(B) FAA AD90-22-06 PRE 01692 551033-0603-1 3-55

1990-005-101(B) FAA AD90-26-03 PRE 01257

(32-0396)

MHB SB

470-32-672 321114-0502-1 2-32

1990-020-102(B) FAA AD91-05-12 PRE 07715

(53-0270) 551004-0603-1 3-55

1990-056-106(B) FAA AD92-23-05 PRE 03599

PRE 08430

(26-0055) 262100-0502-1 2-26

1990-222-116(B) FAA AD2000-10-

01 PRE 02109 532100-0603-1 3-53

1990-222-116(B) FAA AD96-0808 POST 00733

PRE 02434 540006-0603-1 3-54

1991-019-IMP(B) FAA AD90-23-15 GE 725400-0802-2 2-72

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 7 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

1991-053-IMP(B) FAA AD91-01-04 GE 722100-0802-1 2-72

1991-070-IMP(B) FAA AD91-04-10 PW 725000-0812-2 2-72

1991-124-122(B) FAA AD92-19-03 PRE 04803

PRE 08732

(29-0099) 292527-0503-6 2-29

1991-132-124(B) FAA AD97-11-03 ALL 531605-0603-1 3-53

1991-132-124(B) FAA AD97-11-03 ALL 531719-0603-2 3-53

1991-132-124(B) FAA AD97-11-03 ALL 533220-0603-2 3-53

1991-132-124(B) FAA AD97-11-03 PRE

(53-0192) 533220-0603-3 3-53

1991-132-124(B) FAA AD97-11-03 ALL 533439-0603-1 3-53

1991-132-124(B) FAA AD97-11-03 PRE

(53-0192) 533439-0603-2 3-53

1991-132-124(B) FAA AD97-11-03 PRE

(53-0192) 533727-0603-2 3-53

1991-132-124(B) FAA AD97-11-03 ALL 533727-0603-3 3-53

1991-135IMP(B) FAA AD91-10-

03R1 GE 723100-0804-1 2-72

1991-173-126(B) FAA AD97-07-09 PRE 04845

(28-0055)

PRE 08964

(28-0061) 282116-0503-3 2-28

1991-232-IMP(B) FAA AD91-15-

16GEGE

PRE

SB GE 72-0885 725300-0802-4 2-72

1992-253-138(B) FAA AD96-12-15 PRE 10414

(53-0294) 539008-0603-1 3-53

1993-159-IMP(B) FAA AD93-14-20 PW 725200-0812-1 2-72

1994-104-160(B) FAA AD94-10-51 ALL

NOTE 561100-0502-2 2-56

1994-187-163(B) FAA AD95-10-14 PRE 10929

(24-0086) 240000-0503-1 2-24

1994-187-163(B) FAA AD95-10-14 PRE 10929 532411-0502-1 2-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 8 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(24-0086)

1994-207-168(B) FAA AD95-24-04 B2

PRE 11130

(57-221) 571175-0603-1 3-57

1994-207-168(B) FAA AD95-24-04 B4-100

PRE 11130

(57-221) 571175-0603-2 3-57

1994-207-168(B) FAA AD95-24-04 B4-200

C4

F4

PRE 11130

(57-221) 571175-0603-3 3-57

1994-207-168(B) FAA AD95-24-04 B2

POST 11130

(57-221) 571175-0603-4 3-57

1994-213(B) FAA AD94-10-09 PW

PRE SB PW 5847

OR

PRE SB PW 6054 725000-0812-1 2-72

1994-213(B) FAA AD94-10-09 PW

PRE SB PW 6054 725000-0812-3 2-72

1995-011-174(B) FAA AD95-12-09 NLG DOOR

ASSY P/N

A52810648000

NLG DOOR FITTING

P/N

A52810629200/

201 528212-0503-1 2-52

1995-163-182(B) FAA AD98-21-32 PRE 11527

(29-0109) 292527-0504-1 2-29

1995-225-IMP(B) FAA AD95-17-15 GE NOTE 712003-0802-1 2-71

1996-135-199(B) FAA AD98-06-31 ALL 534805-0603-1 3-53

1997-113-221 FAA AD99-25-15 PRE 04443

(32-0425)

POST 02781

(32-0272)

PRE 03433 323300-0503-4 2-32

1997-124-223(B) FAA AD98-20-22 PRE 11286

(53-0334) 539010-0603-1 3-53

1997-124-223(B) FAA AD98-20-22 POST 11286 539010-0603-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 9 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(53-0334)

1997-357-231(B) FAA AD98-20-13 ALL 539009-0603-1 3-53

1997-358-232(B) AD

EASA AD2007-

0243

AD2009-01-08 ALL 574113-0603-1 3-57

1998-028-242(B) FAA AD2000-20-

15 B2 539001-0603-1 3-53

1998-028-242(B) FAA AD2000-20-

15 B4-100 539001-0603-2 3-53

1998-028-242(B) FAA AD2000-20-

15 B4-200 539001-0603-3 3-53

1998-150-246(B) FAA AD99-26-15 PRE 02611

PRE 10715

(53-0306) 533730-0603-1 3-53

1998-263-255(B) FAA AD2001-15-

10 POST 12012

(32-0429) 324314-0505-1 2-32

1998-449-265(B) FAA AD90-11-05 PRE 06661

(57-0143) 572090-0603-1 3-57

1999-292-IMP(B) FAA AD99-11-09 PW 724000-0812-1 2-72

1999-410-294(B) FAA AD2003-03-

04 B2

B4

C4

PRE 12024

(52-0173) 521000-0502-1 2-52

1999-410-294(B) FAA AD2003-03-

04 F4

PRE 12024

(52-0173) 521000-0502-2 2-52

1999-410-294(B) FAA AD2003-03-

04 PRE 12024

(52-0173) 529003-0603-2 3-52

1999-422-IMP(B) AD

AD2008-02-17

FAA AD99-18-20 GE 783100-0801-7 2-78

1999-511-297(B) FAA AD98-21-30 POST 03135 534100-0603-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 10 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(53-0188)

PRE 12167

(53-0358)

2000-259-315(B) FAA AD2001-01-

06 PRE 11206

(29-0106) 292527-0503-7 2-29

2000-434-321(B) ALL 571099-0603-1 3-57

2001-108-IMP(B) FAA AD2001-04-

16 GE

PRE

SB GE 72-A1201 725600-0802-1 2-72

2001-212(B) FAA AD2002-02-

05 ALL 292527-0503-8 2-29

2001-555(B) FAA AD2002-04-

05 PRE 11349

(54-0095) 242200-0503-2 2-24

2001-603(B) FAA AD2004-04-

10 POST 02529

(32-0228)

POST 03083

(32-0269) 323112-0503-4 2-32

2001-603(B) FAA AD2004-04-

10 PRE 02529

(32-0228) 323112-0503-5 2-32

2002-184(B) FAA AD2004-20-

14 B4

C4

F4 539015-0603-1 3-53

2002-620(B) FAA AD2000-05-

07 B2

PRE 11932

(57-0235) 579003-0603-1 3-57

2002-620(B) FAA AD2000-05-

07 B4

PRE 11932

(57-0235) 579003-0603-2 3-57

2002-639(B) FAA AD2000-02-

39 MSN 003 TO 156 539016-0603-1 3-53

2002-639(B) FAA AD2000-02-

39 MSN 157 TO 305 539016-0603-2 3-53

2002-639(B) FAA AD2004-08-

05 MSN 001 TO 156

B2

B4-100

B4-200 539017-0603-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 11 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

F4

2002-639(B) AD2004-08-05 MSN 001 TO 156

C4 539017-0603-2 3-53

2003-317(B) FAA AD2005-15-

09 PRE 08057

(21-0116)

OR

PRE 05946

(53-0201) 538295-0603-2 3-53

2005-111(B) AD2006-15-06 FWD-FACE 222000-0504-1 2-22

2006-0071(B) FAA AD96-13-11 PRE 02295

FROM 0 FC/FH

TO LOV 523301-0602-1 3-52

2006-0071(B) FAA AD96-13-11 POST 02295

FROM 0 FC/FH

TO LOV 523301-0602-2 3-52

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 523303-0603-1 3-52

2006-0071(B) FAA AD96-13-11 C4

F4

FROM 0 FC/FH

TO LOV 523315-0603-1 3-52

2006-0071(B) FAA AD96-13-11 C4

F4

FROM 0 FC/FH

TO LOV 523317-0603-1 3-52

2006-0071(B) FAA AD96-13-11 POST 06208

MSN 256

FROM 0 FC/FH

TO LOV 523317-0603-2 3-52

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO 40000 FC 523701-0602-1 3-52

2006-0071(B) FAA AD96-13-11 ALL

FROM 40000 FC

TO LOV 523701-0602-2 3-52

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO 40000 FC 523719-0602-1 3-52

2006-0071(B) FAA AD96-13-11 B2

PRE 05134 526101-0602-1 3-52

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 12 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 B4

C4

F4

PRE 05134

FROM 0 FC/FH

TO LOV 526101-0602-2 3-52

2006-0071(B) FAA AD96-13-11 B4-2C

POST 6208

C4

F4

FROM 0 FC/FH

TO 34000 FC 526305-0606-1 3-52

2006-0071(B) FAA AD96-13-11 B4-2C

POST 6208

C4

F4

FROM 34000 FC

TO LOV 526305-0606-2 3-52

2006-0071(B) FAA AD96-13-11 B4-2C

POST 6208

C4

F4

FROM 0 FC/FH

TO 34000 FC 526305-0606-3 3-52

2006-0071(B) FAA AD96-13-11 B4-2C

POST 6208

C4

F4

FROM 34000 FC

TO LOV 526305-0606-4 3-52

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 530407-0603-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 530407-0603-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 530407-0603-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH 530407-0603-4 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 13 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO 40000 FC

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 530407-0603-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 530407-0603-6 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 45000 FC

TO LOV 531107-0602-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 531107-0602-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 531107-0602-3 3-53

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 531121-0602-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 531125-0602-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 531137-0602-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 531215-0602-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 531531-0602-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 531531-0602-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4 531531-0602-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 14 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 531711-0602-1 3-53

2006-0071(B) FAA AD96-13-11 POST 02476

(53-0121)

FROM 0 FC/FH

TO LOV 531921-0603-1 3-53

2006-0071(B) FAA AD96-13-11 POST 02476

(53-0121)

FROM 0 FC/FH

TO LOV 531921-0603-2 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 531925-0603-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 531925-0603-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 531925-0603-3 3-53

2006-0071(B) FAA AD96-13-11 C4

F4

POST 06208

B4-2C

FROM 0 FC/FH

TO LOV 533331-0602-1 3-53

2006-0071(B) FAA AD96-13-11 POST 06208

MSN 256

FROM 0 FC/FH

TO LOV 533331-0603-1 3-53

2006-0071(B) FAA AD96-13-11 C4

F4

POST 06208

MSN 256

B4-2C

FROM 0 FC/F

TO LOV 533339-0603-1 3-53

2006-0071(B) FAA AD96-13-11 C4

F4 533343-0603-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 15 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

POST 06208

MSN 256

B4-2C

FROM 0 FC/F

TO LOV

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 533407-0602-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 533415-0602-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 533415-0602-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533415-0602-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 533614-0602-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 533614-0602-3 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533614-0602-4 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 533615-0603-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 533615-0603-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533615-0603-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH 533616-0603-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 16 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 533616-0603-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533616-0603-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 534901-0603-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 534901-0603-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 534901-0603-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536101-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536101-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536101-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536101-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536101-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536101-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4 536101-0606-7 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 17 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 34000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536101-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536101-0607-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536101-0607-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536101-0607-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536101-0607-5 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536110-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536110-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536110-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536110-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536110-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536110-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4 536110-0606-7 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 18 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

F4

FROM 34000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536110-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536110-0607-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536110-0607-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536110-0607-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536110-0607-5 3-53

2006-0071(B) FAA AD96-13-11 B4-100

PRE 01282

FROM 0 FC/FH

TO 40000 FC 536204-0606-3 3-53

2006-0071(B) FAA AD96-13-11 POST 00726

(53-0902)

SERIAL

PRE 00600

FROM 0 FC/FH

TO 48000 FC 536205-0606-1 3-53

2006-0071(B) FAA AD96-13-11 POST 00726

(53-0902)

RETROFIT

PRE 00600

FROM 0 FC/FH

TO 48000 FC 536205-0606-2 3-53

2006-0071(B) FAA AD96-13-11 POST 00726

(53-0902)

PRE 00600

FROM 48000 FC

TO LOV 536205-0606-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 19 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 POST 00600

FROM 0 FC/FH

TO 48000 FC 536205-0606-4 3-53

2006-0071(B) FAA AD96-13-11 POST 00600

FROM 48000 FC

TO LOV 536205-0606-5 3-53

2006-0071(B) FAA AD96-13-11 POST 00726

(53-0902)

SERIAL

PRE 00600

FROM 0 FC/FH

TO 48000 FC 536205-0606-6 3-53

2006-0071(B) FAA AD96-13-11 POST 00726

(53-0902)

RETROFIT

PRE 00600

FROM 0 FC/FH

TO 48000 FC 536205-0606-7 3-53

2006-0071(B) FAA AD96-13-11 POST 00726

(53-0902)

PRE 00600

FROM 48000 FC

TO LOV 536205-0606-8 3-53

2006-0071(B) FAA AD96-13-11 POST 00600

FROM 0 FC/FH

TO 48000 FC 536205-0606-9 3-53

2006-0071(B) FAA AD96-13-11 POST 00600

FROM 48000 FC

TO LOV 536205-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 00797

(53-0905)

RETROFIT

FROM 0 FC/FH

TO 48000 FC 536207-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 00797

(53-0905)

SERIAL

FROM 0 FC/FH

TO 48000 FC 536207-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 00797 536207-0606-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 20 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(53-0905)

FROM 0 FC/FH

TO 40000 FC

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 00797

(53-0905)

FROM 0 FC/FH

TO 34000 FC 536207-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 00797

FROM 48000 FC

TO LOV 536207-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 00797

(53-0905)

FROM 40000 FC

TO LOV 536207-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 00797

(53-0905)

FROM 34000 FC

TO LOV 536207-0606-7 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536210-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536210-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536210-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536210-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536210-0606-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 21 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536210-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC 536301-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC 536301-0607-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000 FC 536301-0607-3 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 48000 FC

TO LOV 536301-0607-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536301-0607-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV 536301-0607-6 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC 536301-0608-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC 536301-0608-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4 536301-0608-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 22 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

F4

POST 02611

FROM 0 FC/FH

TO 34000 FC

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 48000 FC

TO LOV 536301-0608-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536301-0608-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV 536301-0608-6 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536311-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536311-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536311-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536311-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536311-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536311-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536311-0606-7 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 23 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536311-0606-8 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536311-0606-9 3-53

2006-0071(B) FAA AD96-13-11 F4

OR

C4

OR

B4-2C

POST 06208

IN CARGO CONFIG

FROM 0 FC/FH

TO LOV 536355-0606-1 3-53

2006-0071(B) FAA AD96-13-11 C4

OR

B4-2C

POST 06208

IN PAX CONFIG

FROM 0 FC/FH

TO LOV 536355-0606-2 3-53

2006-0071(B) FAA AD96-13-11 F4

POST 06208

FROM 0 FC/FH

TO LOV 536359-0606-1 3-53

2006-0071(B) FAA AD96-13-11 C4

OR

B4-2C

POST 06208

FROM 0 FC/FH

TO LOV 536359-0606-2 3-53

2006-0071(B) FAA AD96-13-11 C4

POST 02611

FROM 0 FC/FH

TO 34000 FC 536365-0606-1 3-53

2006-0071(B) FAA AD96-13-11 C4

POST 02611

FROM 34000 FC

TO LOV 536365-0606-2 3-53

2006-0071(B) FAA AD96-13-11 C4 536367-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 24 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

F4

B4-2C

POST 6208

FROM 0 FC/FH

TO LOW

2006-0071(B) FAA AD96-13-11 C4

F4

B4-2C

POST 6208

FROM 0 FC/FH

TO LOW 536367-0606-2 3-53

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 536369-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536403-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536403-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536403-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536403-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536403-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536403-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536407-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536407-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2 536407-0606-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 25 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO 48000 FC

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536407-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536407-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536407-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536407-0606-7 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536407-0606-8 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536407-0606-9 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536415-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536415-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536415-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536415-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536415-0606-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 26 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536415-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 536421-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536421-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC 536502-0603-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC 536502-0603-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC 536502-0603-3 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 48000 FC

TO LOV 536502-0603-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536502-0603-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV 536502-0603-6 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611 536502-0604-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 27 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO 48000 FC

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC 536502-0604-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC 536502-0604-3 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 48000 FC

TO LOV 536502-0604-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536502-0604-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV 536502-0604-6 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC 536502-0605-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC 536502-0605-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC 536502-0605-3 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 48000 FC 536502-0605-4 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 28 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536502-0605-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV 536502-0605-6 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC 536502-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC 536502-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC 536502-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02611

FROM 48000 FC

TO LOV 536502-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536502-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV 536502-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 01669

RETROFIT

(53-0061) 536503-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 29 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO 48000 FC

2006-0071(B) FAA AD96-13-11 B2

POST 01669

SERIAL

FROM 0 FC/FH

TO 48000 FC 536503-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 01669

RETROFIT

(53-0061)

FROM 0 FC/FH

TO 40000 FC 536503-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 01669

SERIAL

PRE 02626

FROM 0 FC/FH

TO 40000 FC 536503-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01669

RETROFIT

(53-0061)

FROM 0 FC/FH

TO 34000 FC 536503-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01669

SERIAL

PRE 02626

FROM 0 FC/FH

TO 34000 FC 536503-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536503-0606-7 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02626

FROM 40000 FC

TO LOV 536503-0606-8 3-53

2006-0071(B) FAA AD96-13-11 B4-100 536503-0606-9 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 30 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

POST 01669

SERIAL

PRE 02626

FROM 40000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

POST 01669

RETROFIT

(53-0061)

FROM 40000 FC

TO LOV 536503-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01669

RETROFIT

(53-0061)

FROM 34000 FC

TO LOV 536503-0607-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01669

SERIAL

PRE 02626

FROM 34000 FC

TO LOV 536503-0607-3 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02626

FROM 0 FC/FH

TO LOV 536503-0607-4 3-53

2006-0071(B) FAA AD96-13-11-

01-1 ALL

SB 53-0243

FROM 0 FC/FH

TO LOV 536505-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 03476

FROM 0 FC/FH

TO 48000 FC 536506-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 03476

FROM 0 FC/FH 536506-0606-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 31 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO 40000 FC

44400 FH

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02626

FROM 0 FC/FH

TO 40000 FC 536506-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02626

FROM 0 FC/FH

TO 34000 FC 536506-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02626

FROM 0 FCFH

TO 40000 FC

82000 FH 536506-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 03476

FROM 48000 FC

TO 53600 FC

57900 FH 536506-0606-7 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 03476

FROM 53600 FC

57900 FH

TO LOV 536506-0606-8 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 03476

TO 40000 FC

44400 FH

TO LOV 536506-0606-9 3-53

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02626

FROM 40000 FC

TO LOV 536506-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02626

FROM 34000 FC 536506-0607-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 32 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO 40000 FC

82000-FH

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02626

FROM 40000 FC

82000 FH

TO LOV 536506-0607-3 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02626

FROM 40000 FC

82000 FH

TO LOV 536506-0607-4 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 536506-0607-5 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 536506-0607-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536506-0607-7 3-53

2006-0071(B) FAA AD96-13-11 PRE 02626

FROM 0 FC/FH

TO LOV 536509-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 536510-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536510-0606-6 3-53

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0265

FROM 0 FC/FH

TO LOV 536512-0606-1 3-53

2006-0071(B) FAA AD96-13-11 ALL 536513-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 33 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

SB 53-0299

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0259

FROM 0 FC/FH

TO LOV 536515-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 02974

FROM 0 FC/FH

TO 48000 FC 536521-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02974

FROM 0 FC/FH

TO 48000 FC 536521-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02974

FROM 0 FC/FH

TO 40000 FC 536521-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02974

FROM 0 FC/FH

TO 40000 FC 536521-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02974

FROM 0 FC/FH

TO 34000 FC 536521-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02974

FROM 0 FC/FH

TO 34000 FC 536521-0606-7 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 02974

FROM 48000 FC

TO LOV 536521-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02974

FROM 48000 FC

TO LOV 536521-0607-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 34 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02974

FROM 40000 FC

TO LOV 536521-0607-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02974

FROM 40000 FC

TO LOV 536521-0607-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02974

FROM 34000 FC

TO LOV 536521-0607-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02974

FROM 34000 FC

TO LOV 536521-0607-6 3-53

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0244

FROM 0 FC/FH

TO LOV 536535-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 00317

PRE 08486

(57-0179)

FROM 0 FC/FH

TO LOV 536541-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 00317

POST 08486

(57-0179)

FROM 0 FC/FH

TO LOV 536541-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 00317

PRE 08486

(57-0179)

FROM 0 FC/FH

TO LOV 536541-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B2 536541-0606-4 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 35 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

POST 00317

POST 08486

(57-0179)

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

PRE 10089

(57-0191)

FROM 0 FC/FH

TO LOV 536541-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 10752

(57-0191)

POST 11213

(57-0191)

POST 10089

(57-0191)

FROM 0 FC/FH

TO LOV 536541-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 10089

(57-0191)

FROM 0 FC/FH

TO LOV 536541-0606-7 3-53

2006-0071(B) FAA AD96-13-11 SB 53-0245

FROM 0 FC/FH

TO LOV 536545-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536546-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536546-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 536546-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536546-0606-4 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 36 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 536547-0606-1 3-53

2006-0071(B) FAA AD96-13-11 SB 53-0310

FROM 0 FC/FH

TO LOV 536548-0606-1 3-53

2006-0071(B) FAA AD96-13-11 SB 53-0304

FROM 0 FC/FH

TO LOV 536549-0606-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0254

FROM 0 FC/FH

TO LOV 536601-0606-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 536602-0606-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO 42500 FC 536603-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

PRE 02974

FROM 0 FC/FH

TO LOV

MSN 4 EXCLUDED 536651-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02974

FROM 0 FC/FH

TO LOV 536651-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02974

FROM 0 FC/FH

TO LOV 536651-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02974

FROM 0 FC/FH

TO LOV 536651-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02974

FROM 0 FC/FH

TO LOV 536651-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200 536651-0606-7 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 37 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

C4

F4

POST 02974

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 B2

PRE 02974

FROM 0 FC/FH

TO LOV 536651-0607-2 3-53

2006-0071(B) FAA AD96-13-11 B2

POST 02974

FROM 0 FC/FH

TO LOV 536651-0607-3 3-53

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02974

FROM 0 FC/FH

TO LOV 536651-0607-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

POST 02974

FROM 0 FC/FH

TO LOV 536651-0607-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02974

FROM 0 FC/FH

TO LOV 536651-0607-6 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02974

FROM 0 FC/FH

TO LOV 536651-0607-7 3-53

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0255

FROM 0 FC/FH

TO LOV 536701-0606-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0260

FROM 0 FC/FH

TO LOV

TO 42500 FC 536702-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2 536703-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 38 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

SB 53-0261

FROM 0 FC/FH

TO 42500 FC

2006-0071(B) FAA AD96-13-11 B4-100

SB 53-0261

FROM 0 FC/FH

TO 41700 FC 536703-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

SB 53-0261

FROM 0 FC/FH

TO 48000 FC 536703-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536704-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536704-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536704-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 536704-0606-4 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536704-0606-5 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 536704-0606-6 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536704-0607-1 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536704-0607-2 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4 536704-0607-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 39 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

F4

FROM 34000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536704-0607-4 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536704-0607-5 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536704-0607-6 3-53

2006-0071(B) FAA AD96-13-11 B2

B4-100

FROM 0 FC/FH

TO LOV 536705-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536705-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02643

(53-0132)

FROM 0 FC/FH

TO LOV 536706-0606-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0262

FROM 0 FC/FH

TO 40750 FC 536801-0606-1 3-53

2006-0071(B) FAA AD96-13-11 ALL

SB 53-0256

FROM 0 FC/FH

TO LOV 536901-0606-1 3-53

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 536901-0606-2 3-53

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 536901-0606-3 3-53

2006-0071(B) FAA AD96-13-11 B4-200 536901-0606-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 40 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

C4

F4

FROM 34000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B2

PRE 02434

FROM 0 FC/FH

TO 48000 FC 546001-0607-2 3-54

2006-0071(B) FAA AD96-13-11 B2

PRE 02434

FROM 48000 FC

TO LOV 546001-0607-3 3-54

2006-0071(B) FAA AD96-13-11 B2

POST 02434

FROM 0 FC/FH

TO 48000 FC 546001-0607-4 3-54

2006-0071(B) FAA AD96-13-11 B2

POST 02434

FROM 48000 FC

TO LOV 546001-0607-5 3-54

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02434

FROM 0 FC/FH

TO 40000 FC 546001-0607-6 3-54

2006-0071(B) FAA AD96-13-11 B4-100

PRE 02434

FROM 40000 FC

TO LOV 546001-0607-7 3-54

2006-0071(B) FAA AD96-13-11 B4-100

POST 02434

FROM 0 FC/FH

TO LOV 546001-0607-8 3-54

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02434

FROM 0 FC/FH

TO 34000 FC 546001-0607-9 3-54

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 02434

FROM 34000 FC 546001-0608-1 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 41 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO LOV

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 02434

FROM 0 FC/FH

TO LOV 546001-0608-2 3-54

2006-0071(B) FAA AD96-13-11 ALL

SB 55-0036

FROM 0 FC/FH

TO LOV 556001-0606-1 3-55

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 556003-0606-1 3-55

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 556003-0606-2 3-55

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 556003-0606-3 3-55

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 556003-0606-4 3-55

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 556003-0606-5 3-55

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 556003-0606-6 3-55

2006-0071(B) FAA AD96-13-11 B2

B4-100

FROM 0 FC/FH

TO LOV 571001-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571001-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B2 571002-0602-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 42 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

B4-100

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571002-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B2

B4-100

FROM 0 FC/FH

TO LOV 571003-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571003-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 571005-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 571005-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571005-0602-3 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 571006-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 571006-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571006-0602-3 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 571007-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100 571007-0602-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 43 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571007-0602-3 3-57

2006-0071(B) FAA AD96-13-11 B2

B4-100

FROM 0 FC/FH

TO LOV 571017-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571017-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 571018-0603-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 571018-0603-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571018-0603-3 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 571028-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 571028-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571028-0602-3 3-57

2006-0071(B) FAA AD96-13-11 B2

B4-100

FROM 0 FC/FH

TO LOV 571031-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-200 571031-0602-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 44 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

C4

F4

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 571033-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 571033-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571033-0602-3 3-57

2006-0071(B) FAA AD96-13-11 B2

B4-100

FROM 0 FC/FH

TO LOV 571035-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571035-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 571040-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 571040-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571040-0602-3 3-57

2006-0071(B) FAA AD96-13-11 B2

B4-100

POST 01868

POST 01869

OR

POST 02101

(57-0079)

FROM 0 FC/FH 571045-0602-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 45 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO LOV

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868

POST 01869

OR

POST 02101

(57-0079)

FROM 0 FC/FH

TO LOV 571045-0602-2 3-57

2006-0071(B) FAA AD96-13-11 B2

B4-100

FROM 0 FC/FH

TO LOV 571055-0602-1 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571055-0602-2 3-57

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 572063-0603-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0152

FROM 0 FC/FH

TO LOV 576003-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 576004-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576004-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576004-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576004-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH 576004-0606-5 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 46 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO 34000 FC

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 576004-0606-6 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0155

FROM 0 FC/FH

TO LOV 576005-0606-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0148

FROM 0 FC/FH

TO LOV 576006-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 576007-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576007-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576007-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576007-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 576007-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 576007-0606-6 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0146

FROM 0 FC/FH

TO LOV 576008-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 576009-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 47 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576009-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 576009-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576009-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576009-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 576009-0606-6 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0147

FROM 0 FC/FH

TO LOV 576010-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 576011-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576011-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 576011-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576011-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576011-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4 576011-0606-6 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 48 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 34000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0148

FROM 0 FC/FH

TO LOV 576012-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 48000 FC 576013-0604-1 3-57

2006-0071(B) FAA AD96-13-11 B2

PRE 08253

(57-0175)

FROM 48000 FC

TO LOV 576013-0604-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 40000 FC 576013-0604-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 08253

(57-0175)

FROM 40000

TO LOV 576013-0604-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 34000 FC 576013-0604-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 08253

(57-0175)

FROM 34000 FC

TO LOV 576013-0604-6 3-57

2006-0071(B) FAA AD96-13-11 B2

PRE 08253

(57-0175) 576013-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 49 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO 48000 FC

2006-0071(B) FAA AD96-13-11 B2

PRE 08253

(57-0175)

FROM 48000 FC

TO LOV 576013-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 40000 FC 576013-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 08253

(57-0175)

FROM 40000

TO LOV 576013-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 34000 FC 576013-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 08253

(57-0175)

FROM 34000 FC

TO LOV 576013-0606-6 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0153

FROM 0 FC/FH

TO LOV 576014-0606-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

FROM 0 FC/FH

TO LOV 576016-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 576017-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH 576021-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 50 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO 48000 FC

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576021-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 576021-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576021-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576021-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 576021-0606-6 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01868

FROM 0 FC/FH

TO 48000 FC 576029-0605-1 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01868

FROM 48000 FC

TO LOV 576029-0605-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868

FROM 0 FC/FH

TO 40000 FC 576029-0605-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868

FROM 40000 FC

TO LOV 576029-0605-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868

FROM 0 FC/FH

TO 34000 FC 576029-0605-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200 576029-0605-6 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 51 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

C4

F4

POST 01868

FROM 34000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B2

POST 01868

FROM 0 FC/FH

TO 48000 FC 576029-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01868

FROM 48000 FC

TO LOV 576029-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868

FROM 0 FC/FH

TO 40000 FC 576029-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868

FROM 40000 FC

TO LOV 576029-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868

FROM 0 FC/FH

TO 34000 FC 576029-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868

FROM 34000 FC

TO LOV 576029-0606-6 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 0 FC/FH

TO 48000 FC 576031-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01868 OR

POST 02101 576031-0606-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 52 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(57-0079) AND

PRE 02338

FROM 48000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 0 FC/FH

TO 40000 FC 576031-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 40000 FC

TO LOV 576031-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 0 FC/FH

TO 34000 FC 576031-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 34000 FC

TO LOV 576031-0606-6 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 48000 FC 576041-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2 576041-0606-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 53 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

POST 01869

OR

POST 02099

(57-0077)

FROM 48000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 40000 FC 576041-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 40000 FC

TO LOV 576041-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 34000 FC 576041-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 34000 FC

TO LOV 576041-0606-6 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01868

FROM 0 FC/FH

TO 48000 FC 576047-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01868 576047-0606-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 54 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 48000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868

FROM 0 FC/FH

TO 40000 FC 576047-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01868

FROM 40000 FC

TO LOV 576047-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868

FROM 0 FC/FH

TO 34000 FC 576047-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01868

FROM 34000 FC

TO LOV 576047-0606-6 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576051-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576051-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 576051-0606-6 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0158

FROM 0 FC/FH

TO LOV 576053-0605-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0162

FROM 0 FC/FH

TO LOV 576055-0606-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0164 576056-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 55 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO LOV

2006-0071(B) FAA AD96-13-11 B2

SB 57-0151

FROM 0 FC/FH

TO LOV 576057-0606-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0193

FROM 0 FC/FH

TO LOV 576058-0606-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0119

FROM 0 FC/FH

TO LOV 576059-0606-1 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0187

FROM 0 FC/FH

TO LOV 576060-0605-1 3-57

2006-0071(B) FAA AD96-13-11 B2

PRE 01868

PRE 02100

(57-0078)

FROM 0 FC/FH

TO LOV 576062-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 01868

PRE 02100

(57-0078)

FROM 0 FC/FH

TO 40000 FC 576062-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 01868

PRE 02100

(57-0078)

FROM 40000 FC

TO LOV 576062-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 01868

PRE 02100

(57-0078)

FROM 0 FC/FH 576062-0606-4 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 56 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO 34000 FC

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 01868

PRE 02100

(57-0078)

FROM 34000 FC

TO LOV 576062-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 10470

(57-0207)

FROM 0 FC/FH

TO 40000 FC 576063-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 10470

(57-0207)

FROM 40000 FC

TO LOV 576063-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 10470

(57-0207)

FROM 0 FC/FH

TO 34000 FC 576063-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 10470

(57-0207)

FROM 34000 FC

TO LOV 576063-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B2

PRE 10326

(57-0203)

FROM 0 FC/FH

TO 48000 FC 576064-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

PRE 10326

(57-0203)

FROM 48000 FC

TO LOV 576064-0606-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 57 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

2006-0071(B) FAA AD96-13-11 B4-100

PRE 10326

(57-0203)

FROM 0 FC/FH

TO 40000 FC 576064-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

PRE 10326

(57-0203)

FROM 40000 FC

TO LOV 576064-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 10326

(57-0203)

FROM 0 FC/FH

TO 34000 FC 576064-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

PRE 10326

(57-0203)

FROM 34000 FC

TO LOV 576064-0606-6 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 576065-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576065-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576065-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576065-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 576065-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4 576065-0606-6 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 58 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

F4

FROM 34000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 576065-0607-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576065-0607-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576065-0607-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576065-0607-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 576065-0607-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 576065-0607-6 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0208

FROM 0 FC/FH

TO LOV 576066-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO 48000 FC 576067-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576067-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B2

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 48000 FC 576068-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2 576068-0606-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 59 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

POST 01869

OR

POST 02099

(57-0077)

FROM 48000 FC

TO LOV

2006-0071(B) FAA AD96-13-11 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 40000 FC 576068-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 40000 FC

TO LOV 576068-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 34000 FC 576068-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 34000 FC

TO LOV 576068-0606-6 3-57

2006-0071(B) FAA AD96-13-11 ALL

SB 57-0211

FROM 0 FC/FH

TO LOV 576069-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH 576070-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 60 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO 48000 FC

2006-0071(B) FAA AD96-13-11 B2

FROM 48000 FC

TO LOV 576070-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO 40000 FC 576070-0606-3 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 40000 FC

TO LOV 576070-0606-4 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 576070-0606-5 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 34000 FC

TO LOV 576070-0606-6 3-57

2006-0071(B) FAA AD96-13-11 B2

SB 57-0225

FROM 0 FC/FH

TO LOV 576071-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B2

FROM 0 FC/FH

TO LOV 576074-0606-1 3-57

2006-0071(B) FAA AD96-13-11 B4-100

FROM 0 FC/FH

TO LOV 576074-0606-2 3-57

2006-0071(B) FAA AD96-13-11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 576074-0606-3 3-57

2009-0081 AD2006-12-13

ADF-2003-318

FAA AD2000-05-

07 POST 11932

(57-0235) 574212-0602-1 3-57

2009-0081 AD2006-12-13

ADF-2003-318

FAA AD2000-05- POST 11932

(57-0235) 574212-0602-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 61 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

07

83-102-53(B) FAA AD86-19-02 PRE 03172

(55-0024) 553017-0603-1 3-55

83-102-53(B) FAA AD86-19-02 B2

PRE 1307 571200-0603-1 3-57

90-222-116(B) AD2000-10-01 POST 00793

(53-0906)

NOTE

PRE 01446 536208-0605-1 3-53

90-222-116(B) AD2000-10-01 POST 00793

(53-0906)

PRE 01446 536208-0605-2 3-53

90-222-116(B) AD2000-10-01 POST 00793

(53-0906)

POST 01446 536208-0605-3 3-53

90-222-116(B) FAA AD2000-10-

01 GE

PRE 2434

PRE 6770

(54-065) 544011-0603-1 3-54

90-222-116(B) FAA AD2000-10-

01 PW

POST 2434

PRE 6442

(54-064) 544012-0603-1 3-54

94-185-165(B) FWD-FACE

POST 11150

(22-0112) 221000-0503-1 2-22

97-080-211(B) FAA AD98-04-10 PRE 11602

(57-0231) 575412-0602-1 3-57

:TBD B2

POST

(53-0282) 539006-0603-1 3-53

F-2005-107(B) AD2007-04-05

FAA AD2007-04-5 POST 12790

(22-0117) 221000-0503-2 2-22

F-2005-109(B) AD2006-26-10 POST 13043

(22-0119) 222300-0504-1 2-22

F-2005-157(B) AD2006-25-03 NON FWD-FACE 222300-0503-3 2-22

FAA AD2000-10- GE 541101-0603-1 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 62 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

01 PRE 07175

(54-0067)

PRE 02434

F-1989-068-093 AD2005-26-16

ADF-2004-193

FAA AD90-03-08 POST 06788

(53-0226) 531933-0603-3 3-53

F-1989-068-093 AD2005-26-16

ADF-2004-193

FAA AD90-03-08 POST 06788

(53-0226) 531933-0603-4 3-53

F-1991-148 ABEX EDP

P/N 65066-06

S/N 242001 THRU

242082 291136-0502-1 2-29

F-1998-481-270 FAA AD2002-07-

05 ALL 539007-0603-2 3-53

F-2002-639 FAA AD2004-08-

05 MSN 003-156

PRE 06653

(53-0209) 531820-0603-2 3-53

F-2002-639 FAA AD2004-08-

05 MSN 157-305

OR

MSN 003-156

POST 06653

(53-0209) 531820-0603-3 3-53

F-2002-639 FAA AD2004-08-

05 PRE 02611 533439-0603-3 3-53

F-2002-639 FAA AD2004-08-

05 PRE 02611 533616-0603-4 3-53

F-2003-457(B) FAA AD2006-01-

03OITSE999.0029/

03/VHR B2

PRE 03686

(34-0092)

B4

PRE 03686

(34-0092) 222339-0504-1 2-22

F-2004-092 FAA AD2005-17-

14 ALL 272400-0503-1 2-27

F-2004-185 FAA AD96-17-14 ALL 533430-0602-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 63 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

F-2005-084 FAA AD2005-25-

19 B2

B4-100

B4-200

PRE 12662

(53-0364) 531208-0603-1 3-53

F-2005-084 FAA AD2005-25-

19 C4-203

F4-203

PRE 12662

(53-0364) 531208-0603-2 3-53

F-2005-198

2006-0179 FAA AD2006-13-

04 PRE 13031

OR

PRE 13241

(57-0245) 575126-0602-1 3-57

F-2005-199 FAA AD2006-12-

05 B4

C4

F4

PRE 13041

(28-0085) 282100-0503-1 2-28

F-2005-208 GE 783100-0801-9 2-78

F-2006-016 AD2007-26-14

FAA AD2003-06-

04 B2 536516-0606-1 3-53

F-2006-016 AD2007-26-14

FAA AD2003-06-

04 B4-100 536516-0606-4 3-53

F-2006-016 AD2007-26-14

FAA AD2003-06-

04 B4-200

C4

F4 536516-0606-6 3-53

FAA AD74-08-09 ALL 254000-0502-1 2-25

AD2009-0111 ALL 274211-0502-2 2-27

EASA AD2010-

0019 ALL 274211-0505-5 2-27

AD2007-0094 B4 C4 F4 281800-0502-1 2-28

AD2007-0094 B4 C4 F4 281800-0503-1 2-28

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 64 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

AD2007-0094 ALL 281800-0503-2 2-28

EASA AD2008-

0052 PRE 13212

(32-0453) 322114-0505-3 2-32

AD2006-0370

FAA AD2005-20-

06 POST 12513

(31-0077) 331300-0503-1 2-33

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 531214-0602-1 3-53

EASA AD2009-

0165 ALL 531253-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO 42500 FC 531321-0602-3 3-53

AD2007-04-11

AD2006-0071 ALL 531411-0603-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 531411-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 531548-0603-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 531548-0603-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 531548-0603-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 65 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 531548-0603-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 531548-0603-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 531548-0603-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 IF VHF 3

ANTENNA

INSTALLED

FROM 0 FC/FH

TO LOV 531572-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 531573-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 531605-0604-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 531605-0604-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 531605-0604-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 531815-0604-4 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 66 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 531816-0603-1 3-53

ADF-2004-193 PRE 06788

(53-0226) 531933-0603-1 3-53

ADF-2004-193 PRE 06788

(53-0226) 531933-0603-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 533209-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 533435-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 533435-0602-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533435-0602-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 533437-0602-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01288

FROM 0 FC/FH

TO LOV 533517-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01288

FROM 0 FC/FH

TO LOV 533517-0602-4 3-53

EASA AD2006- B4-200 533517-0602-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 67 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 C4

F4

POST 01288

FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 533605-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 533605-0602-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533605-0602-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 533729-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 533729-0602-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533729-0602-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 533821-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 533821-0602-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 68 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 533821-0602-3 3-53

EASA ADF-2005-

093

FAA AD2006-25-

04 ALL 533935-0603-1 3-53

EASA ADF-2005-

093

FAA AD2006-25-

04 ALL 533935-0603-2 3-53

EASA ADF-2005-

093

FAA AD2006-25-

04 ALL 533935-0603-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 PRE 03632

FROM 0 FC/FH

TO LOV 536111-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 MSN 003 TO 156 536112-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 MSN 157 TO 305 536112-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536113-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536114-0606-1 3-53

EASA AD2006- ALL 536114-0606-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 69 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01115

FROM 0 FC/FH

T0 48000 FC 536202-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01115

PRE 01282

FROM 0 FC/FH

TO 48000 FC 536202-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01282

FROM 0 FC/FH

TO 48000 FC 536202-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 01115

FROM 0 FC/FH

TO 40000 FC 536202-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01115

PRE 01282

FROM 0 FC/FH

TO 40000 FC 536202-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01282

FROM 0 FC/FH

TO 40000 FC 536202-0606-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01115

FROM 0 FC/FH

TO 34000 FC 536202-0606-7 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01115

FROM 0 FC/FH

T0 48000 FC 536202-0606-8 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 70 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01115

PRE 01282

FROM 0 FC/FH

TO 48000 FC 536202-0606-9 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01115

FROM 48000 FC

TO LOV 536202-0607-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01115

PRE 01282

FROM 0 FC/FH

TO 34000 FC 536202-0607-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01115

PRE 01282

FROM 48000 FC

TO LOV 536202-0607-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01282

FROM 48000 FC

TO LOV 536202-0607-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01282

FROM 40000 FC

TO LOV 536202-0607-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV 536202-0607-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 01115

FROM 40000 FC

TO LOV 536202-0607-7 3-53

EASA AD2006-

0071 B4-200 536202-0607-8 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 71 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FAA AD2007-04-

11 C4

F4

PRE 01115

FROM 34000 FC

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01115

PRE 01282

FROM 40000 FC

TO LOV 536202-0607-9 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01115

PRE 01282

FROM 34000 FC

TO LOV 536202-0608-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01115

FROM 48000 FC

TO LOV 536202-0608-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01115

PRE 01282

FROM 0 FC/FH

TO 34000 FC 536202-0608-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01115

PRE 01282

FROM 48000 FC

TO LOV 536202-0608-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01282

FROM 48000 FC

TO LOV 536202-0608-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01282

FROM 40000 FC

TO LOV 536202-0608-6 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 72 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV 536202-0608-7 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 01115

FROM 40000 FC

TO LOV 536202-0608-8 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01115

FROM 34000 FC

TO LOV 536202-0608-9 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01115

PRE 01282

FROM 40000 FC

TO LOV 536202-0609-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01115

PRE 01282

FROM 34000 FC

TO LOV 536202-0609-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01282

FROM 0 FC/FH

TO 48000 FC 536203-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 01115

FROM 0 FC/FH

TO 40000 FC 536203-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01115

PRE 01282

FROM 0 FC/FH

TO 40000 FC 536203-0606-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 73 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01282

FROM 0 FC/FH

TO 40000 FC 536203-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01115

FROM 0 FC/FH

TO 34000 FC 536203-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01282

FROM 0 FC/FH

TO LOV 536204-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01282

FROM 0 FC/FH

TO 48000 FC 536204-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01282

FROM 0 FC/FH

TO LOV 536204-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01282

FROM 0 FC/FH

TO 34000 FC 536204-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01282

FROM 0 FC/FH

TO 48000 FC 536204-0606-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01282

FROM 0 FC/FH

TO LOV 536204-0606-7 3-53

EASA AD2006-

0071

FAA AD2007-04- B4-100

PRE 01282

FROM 0 FC/FH 536204-0606-8 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 74 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11 TO 40000 FC

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01282

FROM 0 FC/FH

TO 40000 FC 536204-0606-9 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV 536204-0607-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01282

FROM 48000 FC

TO LOV 536204-0607-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 01282

FROM 40000 FC

TO LOV 536204-0607-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01282

FROM 34000 FC

TO LOV 536204-0607-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01282

FROM 48000 FC

TO LOV 536204-0607-7 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV 536204-0607-8 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01282

FROM 40000 FC

TO LOV 536204-0607-9 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 75 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 01282

FROM 40000 FC

TO LOV 536204-0608-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01282

FROM 0 FC/FH

TO LOV 536204-0608-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01282

FROM 0 FC/FH

TO 34000 FC 536214-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO 40000 FC 536225-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 PRE 01282

FROM 40000 FC

TO LOV 536225-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 POST 01282

FROM 40000 FC

TO LOV 536225-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 40000 FC 536225-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 536225-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04- B4-200

C4

F4 536225-0606-6 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 76 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11 FROM 0 FC/FH

TO 40000 FC

EASA AD2006-

0071

FAA AD2007-04-

11 PRE 01282

FROM 40000 FC

TO LOV 536225-0606-7 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

B4-100

POST 01282

FROM 40000 FC

TO LOV 536225-0606-8 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01282

FROM 40000 FC

TO LOV 536225-0606-9 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536230-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536231-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536232-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536233-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 PRE 03632

FROM 0 FC/FH

TO LOV 536234-0606-1 3-53

EASA AD2006-

0071 POST 03632

FROM 0 FC/FH 536234-0606-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 77 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FAA AD2007-04-

11 TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536235-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536235-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536235-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC 536301-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC 536301-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000 FC 536301-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 02611

FROM 48000 FC

TO LOV 536301-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536301-0606-5 3-53

EASA AD2006- B4-200 536301-0606-6 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 78 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 C4

F4

POST 02611

FROM 34000 FC

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536405-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 536405-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536405-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536405-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 536405-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536405-0606-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 00751

(53-0247)

FROM 48000 FC

TO LOV 536405-0606-7 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 00751

(53-0247)

FROM 40000 FC

TO LOV 536405-0606-8 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 79 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 00751

(53-0247)

FROM 34000 FC

TO LOV 536405-0606-9 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 536510-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 40000 FC

TO LOV 536510-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536510-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 34000 FC

TO LOV 536510-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 PRE SB

(53-0282)

FROM 0 FC/FH

TO LOV 536511-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536523-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 536523-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04- B4-100

FROM 0 FC/FH

TO 40000 FC 536523-0606-4 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 80 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 40000 FC

TO LOV 536523-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536523-0606-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536523-0606-7 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 536523-0606-8 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 536523-0606-9 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 40000 FC

TO LOV 536523-0607-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536523-0607-2 3-53

EASA AD2006-

0071(B)

FAA AD96-13-11 ALL

ISB 53-0242

FROM 0 FC/FH

TO LOV 536529-0606-1 3-53

FAA AD96-13-11 B4-200

C4

F4

POST 10089 536541-0606-8 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 81 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(57-0191)

POST 11213

(57-0191)

FROM 0 FC/F

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 PRE 10453

(53-0297)

FROM 0 FC/FH

TO LOV 536543-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

SB 53-0252

FROM 0 FC/FH

TO LOV 536544-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536551-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536551-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536551-0604-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536553-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536553-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536553-0604-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 82 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

SB 53-0238

FROM 0 FC/FH

TO LOV 536554-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

SB 53-0345

FROM 0 FC/FH

TO LOV 536555-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536556-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536556-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536556-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536557-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536557-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536557-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536560-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 83 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

AD

FAA AD2008-14-

09 B2

POST

(53-0282) 536561-0606-1 3-53

AD

FAA AD2008-14-

09 B4, C4, F4

POST

(53-0291) 536561-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 POST 07301

(53-0239)

FROM 0 FC/FH

TO LOV 536578-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 536590-0606-1 3-53

EASA AD2006-177

FAA AD2004-18-

13 ALL 536596-0603-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 02611

FROM 48000FC

TO LOV 536597-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 02611

FROM 48000 FC

TO LOV 536597-0602-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 02611

FROM 40000 FC

TO LOV 536597-0602-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 02611

FROM 40000 FC

TO LOV 536597-0602-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4 536597-0602-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 84 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

PRE 02611

FROM 34000 FC

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV 536597-0602-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536597-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 536597-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536597-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 07757

(53-0272)

FROM 0 FC/FH

TO LOV 536598-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 07757

(53-0272)

PRE 03474

FROM 0 FC/FH

TO LOV 536598-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 07757

(53-0272)

PRE 03474

FROM 0 FC/FH

TO LOV 536598-0606-3 3-53

EASA AD2006- B4-200 536598-0606-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 85 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 C4

F4

PRE 07757

(53-0272)

POST 03474

FROM 0 FC/FH

TO 34000 FC

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 07757

(53-0272)

POST 03474

FROM 34000 FC

TO LOV 536598-0606-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 07757

(53-0272)

FROM 0 FC/FH

TO LOV 536598-0607-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 07757

(53-0272)

PRE 03474

FROM 0 FC/FH

TO 40000 FC 536598-0607-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 07757

(53-0272)

PRE 03474

FROM 40000 FC

TO LOV 536598-0607-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 07757

(53-0272)

PRE 03474

FROM 0 FC/FH

TO LOV 536598-0607-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 07757 536598-0607-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 86 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

(53-0272)

POST 03474

FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536599-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 536599-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536599-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536599-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536599-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536599-0606-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 536599-0607-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 40000 FC

TO LOV 536599-0607-2 3-53

EASA AD2006- B4-200 536599-0607-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 87 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 C4

F4

FROM 34000 FC

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 536599-0607-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536652-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 536652-0606-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536652-0606-4 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536652-0606-5 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 536652-0606-6 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 536652-0606-7 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536652-0606-8 3-53

EASA AD2006-

0071 B4-200 536652-0606-9 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 88 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FAA AD2007-04-

11 C4

F4

FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536653-0602-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536654-0604-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536707-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536707-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536707-0604-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536708-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536708-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536708-0604-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 89 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536709-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536709-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536709-0604-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536710-0602-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536710-0602-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536710-0602-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536711-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536711-0606-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536711-0606-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 90 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

SB 53-0258

FROM 0 FC/FH

TO LOV 536902-0606-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536903-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 536903-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 536903-0604-3 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 536905-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 57000 FC 536905-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO 57000 FC 536905-0604-3 3-53

AD200-262-313(B) B1

B2-1C

B2K-3C

B2-203

B4-2C

B4-103

B4-203

POST 02140

(53-0109) 538592-0603-1 3-53

EASA AD2006- ALL 538789-0604-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 91 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 538839-0604-1 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 538839-0604-2 3-53

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 538839-0604-3 3-53

EASA AD1990-

116(B)

FAA AD96-08-08 GE

PRE 10598

(54-0085)

PRE 02434 541010-0603-1 3-54

EASA AD1992-

049-130(B)

FAA AD95-10-03 GE

POST 02434

PRE 10328

(54-0079) 541105-0603-1 3-54

EASA AD1992-

049-130(B)

FAA AD95-10-03 PW

PRE 10328

(54-0079) 541105-0603-2 3-54

EASA AD1993-

228-154(B)

FAA AD2000-10-

18 GE

PRE 10335

(54-0080)

POST 02434 541107-0603-1 3-54

EASA AD1993-

228-154(B)

FAA AD2000-10-

18 PW

PRE 10335

(54-0080)

POST 02434 541107-0603-2 3-54

EASA AD1993-

228-154(B)

FAA AD2000-10-

18 GE

PRE 10335

(54-0080)

PRE 02434 541107-0603-3 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 92 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD1993-

228-154(B)

FAA AD2000-10-

18 GE

POST 10335

(54-0080)

POST 02434 541107-0603-4 3-54

EASA AD1993-

228-154(B)

FAA AD2000-10-

18 PW

POST 10335

(54-0080) 541107-0603-5 3-54

EASA AD1993-

228-154(B)

FAA AD2000-10-

18 GE

POST 10335

(54-0080)

PRE 02434 541107-0603-6 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 543001-0602-1 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 543001-0602-2 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 543001-0602-3 3-54

AD

FAA AD93-05-04 GE

PRE 02434

PRE (54-0046) 543001-0602-4 3-54

AD PRE 10431

(54-0081) 543002-0602-4 3-54

AD POST 10431

(54-0081) 543002-0602-5 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 02434

FROM 0 FC/FH

TO 48000 FC 546001-0606-1 3-54

EASA AD2006-

0071 B2

POST 02434 546001-0606-2 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 93 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

FAA AD2007-04-

11 FROM 0 FC/FH

TO 48000 FC

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 02434

FROM 0 FC/FH

TO 40000 FC 546001-0606-3 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 02434

FROM 0 FC/FH

TO LOV 546001-0606-4 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 02434

FROM 0 FC/FH

TO 34000 FC 546001-0606-5 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 02434

FROM 0 FC/FH

TO LOV 546001-0606-6 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 02434

FROM 48000 FC

TO LOV 546001-0606-7 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 02434

FROM 48000 FC

TO LOV 546001-0606-8 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 02434

FROM 40000 FC

TO LOV 546001-0606-9 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 02434

FROM 34000 FC 546001-0607-1 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 94 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 546014-0606-1 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 546014-0606-2 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 546014-0606-3 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 40000 FC

TO LOV 546014-0606-4 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 546014-0606-5 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 546014-0607-1 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 546014-0607-2 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 546014-0607-3 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 40000 FC

TO LOV 546014-0607-4 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 95 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 546014-0607-5 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO 48000 FC 546014-0608-1 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 48000 FC

TO LOV 546014-0608-2 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 546014-0608-3 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 40000 FC

TO LOV 546014-0608-4 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 546014-0608-5 3-54

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 556002-0602-1 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 556002-0602-2 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 556002-0602-3 3-55

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 96 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B2

PRE 01236

FROM 0 FC/FH

TO LOV 556004-0606-1 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01236

FROM 0 FC/FH

TO LOV 556004-0606-2 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

PRE 01236

FROM 0 FC/FH

TO LOV 556004-0606-3 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01236

FROM 0 FC/FH

TO LOV 556004-0606-4 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

PRE 01236

FROM 0 FC/FH

TO LOV 556004-0606-5 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01236

FROM 0 FC/FH

TO LOV 556004-0606-6 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 556005-0604-1 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 556005-0604-2 3-55

EASA AD2006-

0071

FAA AD2007-04- B4-200

C4

F4 556005-0604-3 3-55

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 97 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11 FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 556006-0604-1 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 556006-0604-2 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 556006-0604-3 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 556007-0604-1 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 556007-0604-2 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 556007-0604-3 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 556008-0604-1 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 556008-0604-2 3-55

EASA AD2006-

0071

FAA AD2007-04- B4-200

C4

F4 556008-0604-3 3-55

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 98 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11 FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 556009-0604-1 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 556009-0604-2 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 556009-0604-3 3-55

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 571047-0602-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 571047-0602-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571047-0602-3 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 571057-0602-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 571057-0602-2 3-57

EASA AD2006-

0071

FAA AD2007-04- B4-200

C4

F4 571057-0602-3 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-1 Page 99 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11 FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 571058-0602-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 571058-0602-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 571058-0602-3 3-57

AD2008-06-18 ALL

SB 57-0177 572090-0604-1 3-57

AD2008-06-18 ALL 572090-0604-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 572093-0604-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 572094-0604-1 3-57

ADF-2005-113

FAA AD2006-12-

13 PRE 11932

(57-0235) 574212-0602-3 3-57

ADF-2005-113

FAA AD2006-12-

13 PRE 11932

(57-0235) 574212-0602-4 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 575021-0604-1 3-57

EASA AD2006- ALL 575061-0604-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2- 1 Page 100 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 FROM 0 FC/FH

TO LOV

AD2006-0071 ALL 575082-0604-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 575087-0604-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 575088-0604-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 575104-0604-1 3-57

AD PRE 13400

(57-0252)

PRE 04770

(57-0205) 575127-0602-2 3-57

AD PRE 13400

(57-0252)

POST 04770

(57-0205) 575127-0602-3 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 575171-0603-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 575223-0603-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 575293-0602-1 3-57

EASA AD2006- ALL 576001-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2- 1 Page 101 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

0071

FAA AD2007-04-

11 SB 57-0184

FROM 0 FC/FH

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

SB 57-0147

FROM 0 FC/FH

TO LOV 576002-0606-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01868

PRE (53-0282)

FROM 0 FC/FH

TO 48000 FC 576035-0606-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01868

PRE (53-0282)

FROM 48000 FC

TO LOV 576035-0606-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01868

POST (53-0282)

FROM 0 FC/FH

TO 48000 FC 576035-0606-3 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01868

POST (53-0282)

FROM 48000 FC

TO LOV 576035-0606-4 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01868

PRE (53-0291)

FROM 0 FC/FH

TO 40000 FC 576035-0606-5 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01868

PRE (53-0291)

FROM 40000 FC

TO LOV 576035-0606-6 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01868

POST (53-0291)

FROM 0 FC/FH

TO 40000 FC 576035-0606-7 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2- 1 Page 102 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01868

POST (53-0291)

FROM 40000 FC

TO LOV 576035-0606-8 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01868

PRE (53-0291)

FROM 0 FC/FH

TO 34000 FC 576035-0606-9 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01868

PRE (53-0291)

FROM 34000 FC

TO LOV 576035-0607-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01868

POST (53-0291)

FROM 0 FC/FH

TO 34000 FC 576035-0607-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01868

POST (53-0291)

FROM 34000 FC

TO LOV 576035-0607-3 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 0 FC/FH

TO 48000 FC 576037-0606-1 3-57

EASA AD2006-

0071

FAA AD2007-04- B2

POST 01868

OR 576037-0606-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2- 1 Page 103 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11 POST 02100

(57-0078)

PRE 02338

FROM 48000 FC

TO LOV

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 0 FC/FH

TO 40000 FC 576037-0606-3 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 40000 FC

TO LOV 576037-0606-4 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 0 FC/FH

TO 34000 FC 576037-0606-5 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 34000 FC

TO LOV 576037-0606-6 3-57

EASA AD2006-

0071

FAA AD2007-04- B2

FROM 0 FC/FH

TO 48000 FC 576051-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2- 1 Page 104 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO 40000 FC 576051-0606-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC

TO 34000 FC 576051-0606-3 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 576072-0606-1 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B2

FROM 0 FC/FH

TO LOV 576072-0606-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 576072-0606-3 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 576072-0606-4 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 576072-0606-5 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 576072-0606-6 3-57

EASA AD2006-

0071

FAA AD2007-04- B2

FROM 0 FC/FH

TO LOV 576073-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2- 1 Page 105 AIRWORTHINESS DIRECTIVES - CROSS REFERENCE LIST

CN LTA AD MPD APPLICABILITY TASK NUMBER SECTION

11

EASA AD2006-

0071

FAA AD2007-04-

11 B4-100

FROM 0 FC/FH

TO LOV 576073-0606-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 B4-200

C4

F4

FROM 0 FC/FH

TO LOV 576073-0606-3 3-57

AD

EASA ADF-2008-

0208

FAA AD98-21-34 ALL 578021-0602-2 3-57

EASA AD2006-

0071

FAA AD2007-04-

11 ALL

FROM 0 FC/FH

TO LOV 578261-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 1 

# APPENDIX 2-2

MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

00317 536541-0606-1 3-53

00317 536541-0606-2 3-53

00317 536541-0606-3 3-53

00317 536541-0606-4 3-53

00600 536205-0606-1 3-53

00600 536205-0606-2 3-53

00600 536205-0606-3 3-53

00600 536205-0606-4 3-53

00600 536205-0606-5 3-53

00600 536205-0606-6 3-53

00600 536205-0606-7 3-53

00600 536205-0606-8 3-53

00600 536205-0606-9 3-53

00600 536205-0607-1 3-53

00726 (53-0902) 536205-0606-1 3-53

00726 (53-0902) 536205-0606-2 3-53

00726 (53-0902) 536205-0606-3 3-53

00726 (53-0902) 536205-0606-6 3-53

00726 (53-0902) 536205-0606-7 3-53

00726 (53-0902) 536205-0606-8 3-53

00733 54-0045 540006-0603-1 3-54

00751 (53-0247) 536405-0606-7 3-53

00751 (53-0247) 536405-0606-8 3-53

00751 (53-0247) 536405-0606-9 3-53

00793 (53-0906) 53-0278 536208-0605-1 3-53

00793 (53-0906) 53-0278 536208-0605-2 3-53

00793 (53-0906) 53-0278 536208-0605-3 3-53

00797 (53-0905) 536207-0606-1 3-53

00797 (53-0905) 536207-0606-2 3-53

00797 (53-0905) 536207-0606-3 3-53

00797 (53-0905) 536207-0606-4 3-53

00797 536207-0606-5 3-53

00797 (53-0905) 536207-0606-6 3-53

00797 (53-0905) 536207-0606-7 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 2 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

00854 (26-0011) 212200-0505-4 2-21

00854 (26-0011) 261700-0503-1 2-26

01024 (28-0010) 282611-0502-1 2-28

01033 (32-0040) 32-0233 321100-0502-1 2-32

01033 32-0373 324200-0503-1 2-32

01055 53-0075 533218-0602-2 3-53

01094 (53-0051) 52-0014 521031-0502-2 2-52

01094 (53-0051) 52-0014 521031-0502-3 2-52

01094 (53-0051) 52-0014 522231-0502-2 2-52

01094 (53-0051) 52-0014 522231-0502-3 2-52

01115 53-0076 533220-0603-1 3-53

01115 536202-0606-1 3-53

01115 536202-0606-2 3-53

01115 536202-0606-4 3-53

01115 536202-0606-5 3-53

01115 536202-0606-7 3-53

01115 536202-0606-8 3-53

01115 536202-0606-9 3-53

01115 536202-0607-1 3-53

01115 536202-0607-2 3-53

01115 536202-0607-3 3-53

01115 536202-0607-7 3-53

01115 536202-0607-8 3-53

01115 536202-0607-9 3-53

01115 536202-0608-1 3-53

01115 536202-0608-2 3-53

01115 536202-0608-3 3-53

01115 536202-0608-4 3-53

01115 536202-0608-8 3-53

01115 536202-0608-9 3-53

01115 536202-0609-1 3-53

01115 536202-0609-2 3-53

01115 536203-0606-2 3-53

01115 536203-0606-3 3-53

01115 536203-0606-5 3-53

01201 (78-0006) 783300-0802-1 2-78

01202 (52-0078) 52-0136 523307-0603-1 3-52

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 3 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

01202 (52-0078) 52-136 523707-0603-1 3-52

01208 53-0096 530503-0603-1 3-53

01232 (32-0072) 323200-0503-5 2-32

01236 556004-0606-1 3-55

01236 556004-0606-2 3-55

01236 556004-0606-3 3-55

01236 556004-0606-4 3-55

01236 556004-0606-5 3-55

01236 556004-0606-6 3-55

01257 32-0328 321100-0502-2 2-32

01257 32-0356 321100-0503-1 2-32

01257 32-0365

470-32-442 321100-0503-2 2-32

01257 (32-0396) 32-0394 321114-0502-1 2-32

01257 (32-0383) 32-0382 322112-0504-2 2-32

01257 (32-0389) 32-0388 322112-0504-3 2-32

01257 32-0298 323200-0503-4 2-32

01282 536202-0606-2 3-53

01282 536202-0606-3 3-53

01282 536202-0606-5 3-53

01282 536202-0606-6 3-53

01282 536202-0606-9 3-53

01282 536202-0607-2 3-53

01282 536202-0607-3 3-53

01282 536202-0607-4 3-53

01282 536202-0607-5 3-53

01282 536202-0607-6 3-53

01282 536202-0607-9 3-53

01282 536202-0608-1 3-53

01282 536202-0608-3 3-53

01282 536202-0608-4 3-53

01282 536202-0608-5 3-53

01282 536202-0608-6 3-53

01282 536202-0608-7 3-53

01282 536202-0609-1 3-53

01282 536202-0609-2 3-53

01282 536203-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 4 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

01282 536203-0606-3 3-53

01282 536203-0606-4 3-53

01282 536204-0606-1 3-53

01282 536204-0606-2 3-53

01282 536204-0606-3 3-53

01282 536204-0606-4 3-53

01282 536204-0606-5 3-53

01282 536204-0606-6 3-53

01282 536204-0606-7 3-53

01282 536204-0606-8 3-53

01282 536204-0606-9 3-53

01282 536204-0607-2 3-53

01282 536204-0607-4 3-53

01282 536204-0607-5 3-53

01282 536204-0607-6 3-53

01282 536204-0607-7 3-53

01282 536204-0607-8 3-53

01282 536204-0607-9 3-53

01282 536204-0608-2 3-53

01282 536204-0608-4 3-53

01282 536214-0606-1 3-53

01282 536225-0606-2 3-53

01282 536225-0606-3 3-53

01282 536225-0606-7 3-53

01282 536225-0606-8 3-53

01282 536225-0606-9 3-53

01288 533517-0602-1 3-53

01288 533517-0602-2 3-53

01288 533517-0602-4 3-53

01288 533517-0602-5 3-53

01351 (73-0001) 282611-0502-1 2-28

01358 (53-0027) 53-0112 533437-0602-3 3-53

01421 (53-0033) 53-0211 531000-0603-5 3-53

01421 53-0211 531000-0603-5 3-53

01421 (53-0033) 53-211 531000-0603-6 3-53

01421 53-211 531000-0603-6 3-53

01421 (53-0033) 53-0225 533824-0602-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 5 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

01430 (32-0143) 324200-0503-2 2-32

01444 (53-0078) 531563-0602-1 3-53

01444 (53-0078) 53-0129 531563-0602-2 3-53

01446 53-0278 536208-0605-1 3-53

01446 53-0278 536208-0605-2 3-53

01446 53-0278 536208-0605-3 3-53

01501 (57-0035) 27-0044 275138-0502-1 2-27

01501 (57-0035) 27-0044 275138-0502-2 2-27

01508 (22-0025) 222300-0503-1 2-22

01508 (22-0025) 222700-0503-1 2-22

01510 (22-0017) 342400-0503-1 2-34

01510 (22-0017) 342400-0503-2 2-34

01545 (53-0050) 252331-0503-1 2-25

01572 (29-0031)

(ABEX

MODELPMP 09

V01 29-0015 292000-0502-1 2-29

01646 (49-0019) 495000-0703-4 2-49

01646 (49-0019) 49-0017 495000-0703-5 2-49

01654 (77-0007) 793500-0801-1 2-79

01654 (77-0007) 793500-0801-2 2-79

01661 56-0002 562100-0502-1 2-56

01661 56-0007 562100-0502-2 2-56

01669 536503-0606-1 3-53

01669 536503-0606-2 3-53

01669 536503-0606-3 3-53

01669 536503-0606-4 3-53

01669 536503-0606-5 3-53

01669 536503-0606-6 3-53

01669 536503-0606-9 3-53

01669 536503-0607-1 3-53

01669 536503-0607-2 3-53

01669 536503-0607-3 3-53

01673 (57-0007) 27-0044 275138-0502-1 2-27

01673 (57-0007) 27-0044 275138-0502-2 2-27

01692 55-0035 551033-0603-1 3-55

01698 (57-0053) 57-0052 574414-0502-1 2-57

01721 (49-0026) 494000-0702-4 2-49

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 6 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

01758 (29-0039) 292527-0503-1 2-29

01758 (29-0039) 292527-0503-3 2-29

01758 (29-0039) 29-0087 292527-0503-4 2-29

01758 (29-0039) 29-0087 292527-0503-5 2-29

01782 (49-0025) 49-0031 495000-0703-2 2-49

01786 (29-0042) 291400-0505-1 2-29

01789 (27-0084) 275123-0504-1 2-27

01789 (27-0084) 275123-0504-2 2-27

01789 (27-0084) 275124-0504-1 2-27

01789 (27-0084) 275124-0504-2 2-27

01789 (27-0084) 275124-0504-3 2-27

01789 (27-0084) 275124-0504-4 2-27

01789 (27-0084) 275136-0504-1 2-27

01789 (27-0084) 275136-0504-2 2-27

01789 (27-0084) 275136-0504-3 2-27

01789 (27-0084) 275136-0504-4 2-27

01789 (27-0084) 275136-0504-5 2-27

01789 (27-0084) 275136-0504-6 2-27

01789 (27-0084) 275137-0504-1 2-27

01789 (27-0084) 275137-0504-2 2-27

01789 (27-0084) 275137-0504-3 2-27

01789 (27-0084) 275137-0504-4 2-27

01789 (27-0084) 278117-0504-1 2-27

01789 (27-0084) 278117-0504-2 2-27

01789 (27-0084) 278117-0504-3 2-27

01789 (27-0084) 278117-0504-4 2-27

01789 (27-0084) 278118-0504-1 2-27

01789 (27-0084) 278118-0504-2 2-27

01789 (27-0084) 278118-0504-3 2-27

01789 (27-0084) 278118-0504-4 2-27

01789 (27-0084) 278119-0504-1 2-27

01789 (27-0084) 278119-0504-2 2-27

01789 (27-0084) 278119-0504-3 2-27

01789 (27-0084) 278119-0504-4 2-27

01789 (27-0084) 278119-0504-5 2-27

01789 (27-0084) 278119-0504-6 2-27

01789 (27-0084) 278119-0504-7 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 7 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

01789 (27-0084) 278119-0504-8 2-27

01789 (27-0084) 278120-0504-1 2-27

01789 (27-0084) 278120-0504-2 2-27

01789 (27-0084) 278120-0504-3 2-27

01789 (27-0084) 278120-0504-4 2-27

01789 (27-0084) 278121-0504-1 2-27

01789 (27-0084) 278121-0504-2 2-27

01789 (27-0084) 278121-0504-3 2-27

01789 (27-0084) 278121-0504-4 2-27

01789 (27-0084) 278153-0504-1 2-27

01789 (27-0084) 278153-0504-2 2-27

01789 (27-0084) 278153-0504-3 2-27

01789 (27-0084) 278153-0504-4 2-27

01789 (27-0084) 278153-0504-5 2-27

01789 (27-0084) 278153-0504-6 2-27

01789 (27-0084) 278153-0504-7 2-27

01796 (26-0017) 262500-0502-2 2-26

01796 (26-0017) 262500-0504-1 2-26

01798 (27-0087) 27-0044 275138-0502-1 2-27

01798 (27-0087) 27-0044 275138-0502-2 2-27

01819 (21-0047) 212400-0503-1 2-21

01820 (21-0048) 216200-0503-1 2-21

01820 (21-0048) 216200-0505-1 2-21

01824 (57-0060) 571070-0604-2 3-57

01824 (57-0060) 571070-0604-3 3-57

01839 314213-0503-1 2-31

01868 571045-0602-1 3-57

01868 571045-0602-2 3-57

01868 576029-0605-1 3-57

01868 576029-0605-2 3-57

01868 576029-0605-3 3-57

01868 576029-0605-4 3-57

01868 576029-0605-5 3-57

01868 576029-0605-6 3-57

01868 576029-0606-1 3-57

01868 576029-0606-2 3-57

01868 576029-0606-3 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 8 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

01868 576029-0606-4 3-57

01868 576029-0606-5 3-57

01868 576029-0606-6 3-57

01868 576031-0606-1 3-57

01868 576031-0606-2 3-57

01868 576031-0606-3 3-57

01868 576031-0606-4 3-57

01868 576031-0606-5 3-57

01868 576031-0606-6 3-57

01868 576035-0606-1 3-57

01868 576035-0606-2 3-57

01868 576035-0606-3 3-57

01868 576035-0606-4 3-57

01868 576035-0606-5 3-57

01868 576035-0606-6 3-57

01868 576035-0606-7 3-57

01868 576035-0606-8 3-57

01868 576035-0606-9 3-57

01868 576035-0607-1 3-57

01868 576035-0607-2 3-57

01868 576035-0607-3 3-57

01868 576037-0606-1 3-57

01868 576037-0606-2 3-57

01868 576037-0606-3 3-57

01868 576037-0606-4 3-57

01868 576037-0606-5 3-57

01868 576037-0606-6 3-57

01868 576047-0606-1 3-57

01868 576047-0606-2 3-57

01868 576047-0606-3 3-57

01868 576047-0606-4 3-57

01868 576047-0606-5 3-57

01868 576047-0606-6 3-57

01868 576062-0606-1 3-57

01868 576062-0606-2 3-57

01868 576062-0606-3 3-57

01868 576062-0606-4 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 9 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

01868 576062-0606-5 3-57

01869 571045-0602-1 3-57

01869 571045-0602-2 3-57

01869 576041-0606-1 3-57

01869 576041-0606-2 3-57

01869 576041-0606-3 3-57

01869 576041-0606-4 3-57

01869 576041-0606-5 3-57

01869 576041-0606-6 3-57

01869 576068-0606-1 3-57

01869 576068-0606-2 3-57

01869 576068-0606-3 3-57

01869 576068-0606-4 3-57

01869 576068-0606-5 3-57

01869 576068-0606-6 3-57

01871 (24-0022) 275512-0502-1 2-27

01872 (57-0064) 57-0052 574414-0502-1 2-57

01878 (25-0149) 25-0138 255120-0502-1 2-25

01878 (25-0149) 25-0138 255120-0502-2 2-25

01928 (26-0028) 261700-0503-1 2-26

01988 (54-0022) 262100-0503-3 2-26

01988 (54-0022) 262111-0503-1 2-26

01988 (54-0022) 262111-0504-1 2-26

01988 (54-0022) 26-025 262111-0504-3 2-26

02009 (27-0097) 27-0093 272312-0503-2 2-27

02011 (49-0029) 492000-0703-2 2-49

02021 (53-0089) 53-0068 535300-0502-2 2-53

02022 (21-0055) 212100-0505-3 2-21

02022 (21-0055) 212100-0505-4 2-21

02022 (21-0055) 212100-0505-5 2-21

02022 (21-0055) 212200-0505-1 2-21

02022 (21-0055) 212200-0505-2 2-21

02022 (21-0055) 212300-0505-1 2-21

02066 (34-0049) 344243-0503-1 2-34

02099 (57-0077) 576041-0606-1 3-57

02099 (57-0077) 576041-0606-2 3-57

02099 (57-0077) 576041-0606-3 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 10 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02099 (57-0077) 576041-0606-4 3-57

02099 (57-0077) 576041-0606-5 3-57

02099 (57-0077) 576041-0606-6 3-57

02099 (57-0077) 576068-0606-1 3-57

02099 (57-0077) 576068-0606-2 3-57

02099 (57-0077) 576068-0606-3 3-57

02099 (57-0077) 576068-0606-4 3-57

02099 (57-0077) 576068-0606-5 3-57

02099 (57-0077) 576068-0606-6 3-57

02100 (57-0078) 576037-0606-1 3-57

02100 (57-0078) 576037-0606-2 3-57

02100 (57-0078) 576037-0606-3 3-57

02100 (57-0078) 576037-0606-4 3-57

02100 (57-0078) 576037-0606-5 3-57

02100 (57-0078) 576037-0606-6 3-57

02100 (57-0078) 576062-0606-1 3-57

02100 (57-0078) 576062-0606-2 3-57

02100 (57-0078) 576062-0606-3 3-57

02100 (57-0078) 576062-0606-4 3-57

02100 (57-0078) 576062-0606-5 3-57

02101 (57-0079) 571045-0602-1 3-57

02101 (57-0079) 571045-0602-2 3-57

02101 (57-0079) 576031-0606-1 3-57

02101 (57-0079) 576031-0606-2 3-57

02101 (57-0079) 576031-0606-3 3-57

02101 (57-0079) 576031-0606-4 3-57

02101 (57-0079) 576031-0606-5 3-57

02101 (57-0079) 576031-0606-6 3-57

02109 53-0103 532100-0603-1 3-53

02109 (53-0107) 53-0179 532100-0603-3 3-53

02139 345600-0503-1 2-34

02140 (53-0109) 53-0339 538592-0603-1 3-53

02147 (53-0110) 533617-0603-1 3-53

02147 (53-0110) 53-0127 533731-0602-2 3-53

02187 (26-0031) 262500-0502-2 2-26

02187 (26-0031) 262500-0504-1 2-26

02295 523301-0602-1 3-52

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 11 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02295 523301-0602-2 3-52

02295 52-0101 523307-0502-1 2-52

02295 531303-0604-1 3-53

02295 531303-0604-2 3-53

02295 531303-0604-3 3-53

02295 531303-0604-4 3-53

02295 531303-0604-5 3-53

02295 531303-0604-6 3-53

02295 531315-0604-1 3-53

02295 531315-0604-2 3-53

02295 531315-0604-3 3-53

02295 531315-0604-4 3-53

02295 531315-0604-5 3-53

02295 531315-0604-6 3-53

02295 531319-0602-1 3-53

02295 531319-0602-2 3-53

02295 531319-0604-1 3-53

02295 531319-0604-2 3-53

02295 531319-0604-3 3-53

02295 531319-0604-4 3-53

02295 531319-0604-5 3-53

02295 531319-0604-6 3-53

02295 534303-0604-1 3-53

02295 534303-0604-2 3-53

02295 534303-0604-3 3-53

02295 534303-0604-4 3-53

02295 534303-0604-5 3-53

02295 534303-0604-6 3-53

02298 (54-0030) 54-0029 540000-0502-1 2-54

02300 (57-0083) 57-0089 573111-0503-1 2-57

02300 (57-0083) 57-0089 573111-0503-2 2-57

02328 (32-0207) 322200-0502-1 2-32

02328 (32-0207) 322200-0505-1 2-32

02338 576031-0606-1 3-57

02338 576031-0606-2 3-57

02338 576031-0606-3 3-57

02338 576031-0606-4 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 12 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02338 576031-0606-5 3-57

02338 576031-0606-6 3-57

02338 576037-0606-1 3-57

02338 576037-0606-2 3-57

02338 576037-0606-3 3-57

02338 576037-0606-4 3-57

02338 576037-0606-5 3-57

02338 576037-0606-6 3-57

02340 (32-0415) 324200-0503-2 2-32

02348 53-0127 533731-0602-2 3-53

02352 (32-0203) 291000-0505-2 2-29

02372 301100-0503-3 2-30

02372 301100-0503-4 2-30

02372 301100-0503-6 2-30

02372 301112-0503-1 2-30

02372 301113-0503-1 2-30

02373 53-0195 531540-0603-1 3-53

02378 (53-0003) 56-0002 562100-0502-1 2-56

02378 (53-0003) 56-0007 562100-0502-2 2-56

02380 (53-0119) 53-0187 531716-0602-1 3-53

02424 (26-0029) 261200-0503-1 2-26

02434 540003-0602-1 3-54

02434 540003-0602-2 3-54

02434 540003-0602-3 3-54

02434 540004-0602-1 3-54

02434 540004-0602-2 3-54

02434 540004-0602-3 3-54

02434 540004-0603-1 3-54

02434 540004-0603-2 3-54

02434 540004-0603-3 3-54

02434 540005-0604-1 3-54

02434 540005-0604-2 3-54

02434 540005-0604-3 3-54

02434 54-0045 540006-0603-1 3-54

02434 540006-0604-1 3-54

02434 540006-0604-2 3-54

02434 540006-0604-3 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 13 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02434 540009-0604-1 3-54

02434 540009-0604-2 3-54

02434 540009-0604-3 3-54

02434 540010-0604-1 3-54

02434 540010-0604-2 3-54

02434 540010-0604-3 3-54

02434 54-0076 540011-0603-2 3-54

02434 540011-0603-3 3-54

02434 54-0076 540011-0603-4 3-54

02434 54-0089 540012-0603-1 3-54

02434 541001-0604-1 3-54

02434 541001-0604-2 3-54

02434 541001-0604-3 3-54

02434 541002-0604-1 3-54

02434 541002-0604-2 3-54

02434 541002-0604-3 3-54

02434 541007-0604-1 3-54

02434 541007-0604-2 3-54

02434 541007-0604-3 3-54

02434 541008-0603-1 3-54

02434 541008-0603-2 3-54

02434 541008-0603-3 3-54

02434 541009-0604-1 3-54

02434 541009-0604-2 3-54

02434 541009-0604-3 3-54

02434 54-0084 541010-0603-1 3-54

02434 541011-0604-1 3-54

02434 541011-0604-2 3-54

02434 541011-0604-3 3-54

02434 541012-0604-1 3-54

02434 541012-0604-2 3-54

02434 541012-0604-3 3-54

02434 54-0066 541101-0603-1 3-54

02434 54-0071 541105-0603-1 3-54

02434 54-0073 541107-0603-1 3-54

02434 54-0073 541107-0603-2 3-54

02434 54-0073 541107-0603-3 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 14 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02434 54-0073 541107-0603-4 3-54

02434 54-0073 541107-0603-6 3-54

02434 54-0070 543001-0602-4 3-54

02434 546001-0606-1 3-54

02434 546001-0606-2 3-54

02434 546001-0606-3 3-54

02434 546001-0606-4 3-54

02434 546001-0606-5 3-54

02434 546001-0606-6 3-54

02434 546001-0606-7 3-54

02434 546001-0606-8 3-54

02434 546001-0606-9 3-54

02434 546001-0607-1 3-54

02434 546001-0607-2 3-54

02434 546001-0607-3 3-54

02434 546001-0607-4 3-54

02434 546001-0607-5 3-54

02434 546001-0607-6 3-54

02434 546001-0607-7 3-54

02434 546001-0607-8 3-54

02434 546001-0607-9 3-54

02434 546001-0608-1 3-54

02434 546001-0608-2 3-54

02434 548051-0603-1 3-54

02434 548051-0603-2 3-54

02434 548051-0603-3 3-54

02434 54-096 549002-0603-1 3-54

02434 ZL-410-0403-1 4-ZL

02434 ZL-410-0403-2 4-ZL

02434 ZL-410-0403-3 4-ZL

02434 ZL-410-0403-4 4-ZL

02434 ZL-410-0403-5 4-ZL

02434 ZL-410-0403-6 4-ZL

02437 (57-0088) 57-085 574211-0602-1 3-57

02475 256531-0503-1 2-25

02476 (53-0121) 53-0152 531912-0603-1 3-53

02476 (53-0121) 53-0152 531912-0603-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 15 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02476 (53-0121) 531921-0603-1 3-53

02476 (53-0121) 531921-0603-2 3-53

02503 (26-0030) 212200-0505-4 2-21

02503 (26-0030) 261700-0503-1 2-26

02506 (25-0248) 25-0138 255120-0502-1 2-25

02506 (25-0248) 25-0138 255120-0502-2 2-25

02525 (53-0126) 53-211 531000-0603-6 3-53

02526 (53-0128) 53-0127 533731-0602-2 3-53

02528 (29-0060) 292527-0503-1 2-29

02528 (29-0060) 292527-0503-3 2-29

02528 (29-0060) 29-0087 292527-0503-4 2-29

02528 (29-0060) 29-0087 292527-0503-5 2-29

02529 (32-0228) 32-0055 323112-0503-1 2-32

02529 (32-0228) 32-0055 323112-0503-2 2-32

02529 (32-0228) 32-0055 323112-0503-3 2-32

02529 (32-0228) 323112-0503-4 2-32

02529 (32-0228) 323112-0503-5 2-32

02538 (29-0061) 291000-0505-2 2-29

02574 221512-0503-1 2-22

02574 221521-0503-1 2-22

02574 222000-0503-2 2-22

02574 222634-0504-1 2-22

02574 223000-0503-1 2-22

02574 223512-0503-1 2-22

02574 223512-0503-2 2-22

02574 223634-0503-1 2-22

02574 223634-0503-2 2-22

02599 212100-0505-3 2-21

02599 212100-0505-4 2-21

02599 212100-0505-5 2-21

02599 212200-0505-1 2-21

02599 212200-0505-2 2-21

02599 212300-0505-1 2-21

02611 53-0211 531000-0603-5 3-53

02611 53-211 531000-0603-6 3-53

02611 53-0182 531400-0602-2 3-53

02611 53-0356 533439-0603-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 16 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02611 53-0356 533616-0603-4 3-53

02611 53-0305 533730-0603-1 3-53

02611 536301-0606-1 3-53

02611 536301-0606-2 3-53

02611 536301-0606-3 3-53

02611 536301-0606-4 3-53

02611 536301-0606-5 3-53

02611 536301-0606-6 3-53

02611 536301-0607-1 3-53

02611 536301-0607-2 3-53

02611 536301-0607-3 3-53

02611 536301-0607-4 3-53

02611 536301-0607-5 3-53

02611 536301-0607-6 3-53

02611 536301-0608-1 3-53

02611 536301-0608-2 3-53

02611 536301-0608-3 3-53

02611 536301-0608-4 3-53

02611 536301-0608-5 3-53

02611 536301-0608-6 3-53

02611 536365-0606-1 3-53

02611 536365-0606-2 3-53

02611 536502-0603-1 3-53

02611 536502-0603-2 3-53

02611 536502-0603-3 3-53

02611 536502-0603-4 3-53

02611 536502-0603-5 3-53

02611 536502-0603-6 3-53

02611 536502-0604-1 3-53

02611 536502-0604-2 3-53

02611 536502-0604-3 3-53

02611 536502-0604-4 3-53

02611 536502-0604-5 3-53

02611 536502-0604-6 3-53

02611 536502-0605-1 3-53

02611 536502-0605-2 3-53

02611 536502-0605-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 17 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02611 536502-0605-4 3-53

02611 536502-0605-5 3-53

02611 536502-0605-6 3-53

02611 536502-0606-1 3-53

02611 536502-0606-2 3-53

02611 536502-0606-3 3-53

02611 536502-0606-4 3-53

02611 536502-0606-5 3-53

02611 536502-0606-6 3-53

02611 536597-0602-1 3-53

02611 536597-0602-2 3-53

02611 536597-0602-3 3-53

02611 536597-0602-4 3-53

02611 536597-0602-5 3-53

02611 536597-0602-6 3-53

02624 (52-0098) 52-0048 523011-0502-1 2-52

02624 (52-0098) 52-0048 523011-0504-1 2-52

02626 536503-0606-4 3-53

02626 536503-0606-6 3-53

02626 536503-0606-8 3-53

02626 536503-0606-9 3-53

02626 536503-0607-3 3-53

02626 536503-0607-4 3-53

02626 536506-0606-4 3-53

02626 536506-0606-5 3-53

02626 536506-0606-6 3-53

02626 536506-0607-1 3-53

02626 536506-0607-2 3-53

02626 536506-0607-3 3-53

02626 536506-0607-4 3-53

02626 53-0275 536509-0606-1 3-53

02628 (27-0136) 278124-0505-1 2-27

02628 (27-0136) 278124-0505-3 2-27

02643 (53-0132) 53-0143 531700-0602-1 3-53

02643 (53-0132) 536706-0606-1 3-53

02672 (26-0036) 261112-0505-1 2-26

02672 (26-0036) 261112-0505-2 2-26

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 18 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02684 (27-0128) 274211-0504-1 2-27

02684 (27-0128) 274211-0504-2 2-27

02688 341134-0503-1 2-34

02688 342500-0503-1 2-34

02688 342723-0503-1 2-34

02688 343600-0503-2 2-34

02688 345100-0503-1 2-34

02688 345300-0503-2 2-34

02688 345500-0503-2 2-34

02689 223634-0503-1 2-22

02689 223634-0503-2 2-22

02695 (28-0043) 281300-0503-1 2-28

02695 (28-0043) 281300-0503-2 2-28

02695 (28-0043) 281300-0503-3 2-28

02701 (27-0126) 278149-0505-1 2-27

02709 52-0151 524215-0502-1 2-52

02727 53-0154 531000-0602-3 3-53

02727 53-0229 531001-0603-1 3-53

02727 53-0229 531001-0603-2 3-53

02727 53-0229 531001-0603-3 3-53

02727 53-0229 531001-0603-5 3-53

02727 53-0229 531001-0603-6 3-53

02727 53-0229 531001-0603-7 3-53

02727 ZL-100-0402-2 4-ZL

02727 ZL-100-0402-3 4-ZL

02727 ZL-200-0402-2 4-ZL

02727 ZL-200-0402-3 4-ZL

02738 540004-0602-1 3-54

02738 540004-0602-2 3-54

02738 540004-0602-3 3-54

02738 540004-0603-1 3-54

02738 540004-0603-2 3-54

02738 540004-0603-3 3-54

02781 (32-0272) 32-0335 323300-0503-1 2-32

02781 (32-0272) 323300-0503-4 2-32

02787 (27-0129) 274211-0502-1 2-27

02787 (27-0129) 274211-0504-1 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 19 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

02787 (27-0129) 274211-0504-2 2-27

02787 (27-0129) 274211-0505-3 2-27

02787 (27-0129) 274211-0505-4 2-27

02862 (32-0336) 325000-0503-1 2-32

02862 (32-0336) 325000-0503-2 2-32

02862 (32-0336) 325000-0503-3 2-32

02899 53-0155 531300-0502-1 2-53

02949 (32-0258) 321115-0505-1 2-32

02949 (32-0258) 321115-0505-2 2-32

02949 (32-0258) 321115-0505-3 2-32

02949 (32-0258) 321115-0505-4 2-32

02974 536521-0606-2 3-53

02974 536521-0606-3 3-53

02974 536521-0606-4 3-53

02974 536521-0606-5 3-53

02974 536521-0606-6 3-53

02974 536521-0606-7 3-53

02974 536521-0607-1 3-53

02974 536521-0607-2 3-53

02974 536521-0607-3 3-53

02974 536521-0607-4 3-53

02974 536521-0607-5 3-53

02974 536521-0607-6 3-53

02974 536651-0606-2 3-53

02974 536651-0606-3 3-53

02974 536651-0606-4 3-53

02974 536651-0606-5 3-53

02974 536651-0606-6 3-53

02974 536651-0606-7 3-53

02974 536651-0607-2 3-53

02974 536651-0607-3 3-53

02974 536651-0607-4 3-53

02974 536651-0607-5 3-53

02974 536651-0607-6 3-53

02974 536651-0607-7 3-53

03054 (52-0104) 52-0101 523307-0502-1 2-52

03054 (52-0104) 52-0136 523307-0603-1 3-52

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 20 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

03070 (32-0265) 325000-0503-1 2-32

03070 (32-0265) 325000-0503-2 2-32

03070 (32-0265) 325000-0503-3 2-32

03072 533617-0603-1 3-53

03080 (32-0268) 321115-0505-1 2-32

03080 (32-0268) 321115-0505-2 2-32

03080 (32-0268) 321115-0505-3 2-32

03080 (32-0268) 321115-0505-4 2-32

03083 (32-0269) 32-0055 323112-0503-1 2-32

03083 (32-0269) 32-0055 323112-0503-2 2-32

03083 (32-0269) 32-0055 323112-0503-3 2-32

03083 (32-0269) 323112-0503-4 2-32

03101 (32-0267) 32-0264 324247-0502-1 2-32

03135 (53-0188) 53-0179 532100-0603-3 3-53

03135 (53-0188) 53-0329 534100-0603-1 3-53

03172 (55-0024) 55-026 553017-0603-1 3-55

03185 53-0274 531409-0603-1 3-53

03226 (D2396) 555021-0603-1 3-55

03245 ZL-100-0402-2 4-ZL

03245 ZL-200-0402-2 4-ZL

03245 ZL-200-0402-3 4-ZL

03255 (26-0043) 262300-0503-3 2-26

03275 53-0162 531400-0602-1 3-53

03275 53-0162 531400-0602-3 3-53

03275 53-0162 531400-0602-4 3-53

03275 53-0162 531400-0602-5 3-53

03275 53-0162 531400-0602-6 3-53

03275 53-0162 531400-0602-7 3-53

03324 (27-0146) 275125-0502-1 2-27

03324 (27-0146) 275125-0504-1 2-27

03347 215500-0503-1 2-21

03361 (25-0332) 25-0138 255120-0502-2 2-25

03373 (57-0099) 574600-0505-3 2-57

03378 (29-0077) 531557-0602-1 3-53

03378 (29-0077) 531557-0602-2 3-53

03378 (29-0077) ZL-140-0403-8 4-ZL

03378 (29-0077) ZL-140-0413-1 4-ZL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 21 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

03433 32-0335 323300-0503-1 2-32

03433 323300-0503-4 2-32

03474 536598-0606-2 3-53

03474 536598-0606-3 3-53

03474 536598-0606-5 3-53

03474 536598-0606-6 3-53

03474 536598-0607-2 3-53

03474 536598-0607-3 3-53

03474 536598-0607-4 3-53

03474 536598-0607-5 3-53

03476 536506-0606-2 3-53

03476 536506-0606-3 3-53

03476 536506-0606-7 3-53

03476 536506-0606-8 3-53

03476 536506-0606-9 3-53

03500 345600-0503-1 2-34

03521 (54-0059) 548041-0603-1 3-54

03521 (54-0059) 548041-0603-2 3-54

03554 57-0101 571020-0603-1 3-57

03556 (53-0168) 53-0165 534212-0502-1 2-53

03599 262100-0502-1 2-26

03632 53-0348 536111-0606-1 3-53

03632 536234-0606-1 3-53

03632 536234-0606-2 3-53

03686 (34-0092) 222339-0504-1 2-22

03760 (53-0170) 533815-0602-1 3-53

03760 (53-0170) 53-0101 533815-0602-3 3-53

04125 (54-0057) 54-0042 541000-0502-1 2-54

04242 553645-0505-1 2-55

04307 (36-0014) 361415-0505-1 2-36

04400 (57-0123) 57-0122 572500-0502-2 2-57

04439 (52-0121) 523316-0503-1 2-52

04443 (32-0425) 323300-0503-4 2-32

04494 (27-0164) 275123-0504-1 2-27

04494 (27-0164) 275123-0504-2 2-27

04494 (27-0164) 275124-0504-1 2-27

04494 (27-0164) 275124-0504-2 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 22 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

04494 (27-0164) 275124-0504-3 2-27

04494 (27-0164) 275124-0504-4 2-27

04494 (27-0164) 275136-0504-1 2-27

04494 (27-0164) 275136-0504-2 2-27

04494 (27-0164) 275136-0504-3 2-27

04494 (27-0164) 275136-0504-4 2-27

04494 (27-0164) 275136-0504-5 2-27

04494 (27-0164) 275136-0504-6 2-27

04494 (27-0164) 275137-0504-1 2-27

04494 (27-0164) 275137-0504-2 2-27

04494 (27-0164) 275137-0504-3 2-27

04494 (27-0164) 275137-0504-4 2-27

04494 (27-0164) 278117-0504-1 2-27

04494 (27-0164) 278117-0504-2 2-27

04494 (27-0164) 278117-0504-3 2-27

04494 (27-0164) 278117-0504-4 2-27

04494 (27-0164) 278118-0504-1 2-27

04494 (27-0164) 278118-0504-2 2-27

04494 (27-0164) 278118-0504-3 2-27

04494 (27-0164) 278118-0504-4 2-27

04494 (27-0164) 278119-0504-1 2-27

04494 (27-0164) 278119-0504-2 2-27

04494 (27-0164) 278119-0504-3 2-27

04494 (27-0164) 278119-0504-4 2-27

04494 (27-0164) 278119-0504-5 2-27

04494 (27-0164) 278119-0504-6 2-27

04494 (27-0164) 278119-0504-7 2-27

04494 (27-0164) 278119-0504-8 2-27

04494 (27-0164) 278120-0504-1 2-27

04494 (27-0164) 278120-0504-2 2-27

04494 (27-0164) 278120-0504-3 2-27

04494 (27-0164) 278120-0504-4 2-27

04494 (27-0164) 278121-0504-1 2-27

04494 (27-0164) 278121-0504-2 2-27

04494 (27-0164) 278121-0504-3 2-27

04494 (27-0164) 278121-0504-4 2-27

04494 (27-0164) 278153-0504-1 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 23 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

04494 (27-0164) 278153-0504-2 2-27

04494 (27-0164) 278153-0504-3 2-27

04494 (27-0164) 278153-0504-4 2-27

04494 (27-0164) 278153-0504-5 2-27

04494 (27-0164) 278153-0504-6 2-27

04494 (27-0164) 278153-0504-7 2-27

04530 (54-0058) 548041-0603-1 3-54

04530 (54-0058) 548041-0603-2 3-54

04544 (32-0348)

(32-0355) 32-0356 321100-0503-1 2-32

04580 56-0002 562100-0502-1 2-56

04580 56-0007 562100-0502-2 2-56

04770 (21-0112) 212100-0505-1 2-21

04770 (21-0112) 212100-0505-2 2-21

04770 (36-0024) 361119-0502-1 2-36

04770 (49-0046) 49-0031 495000-0703-2 2-49

04770 (57-0201) 57-0215 575125-0602-1 3-57

04770 (57-0205) 57-0214 575127-0602-1 3-57

04770 (57-0205) 57-0250 575127-0602-2 3-57

04770 (57-0205) 57-0250 575127-0602-3 3-57

04803 29-0097 292527-0503-6 2-29

04845 (28-0055) 282116-0503-3 2-28

04868 (53-0191) 53-0190 534213-0603-1 3-53

04959 (57-0132) 57-130 571037-0603-1 3-57

04959 (57-0132) 57-130 571037-0603-2 3-57

04959 (57-0132) 57-130 571037-0603-3 3-57

05119 212100-0505-1 2-21

05119 212100-0505-2 2-21

05132 (57-0134) 57-133 574300-0603-1 3-57

05134 526101-0602-1 3-52

05134 526101-0602-2 3-52

05240 (27-0173) 27-0172 275126-0502-3 2-27

05240 (27-0173) 275126-0502-4 2-27

05262 521131-0505-1 2-52

05569 552007-0602-1 3-55

05724 (53-0161) 53-0162 531400-0602-1 3-53

05724 (53-0161) 53-0162 531400-0602-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 24 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

05724 (53-0161) 53-0162 531400-0602-4 3-53

05724 (53-0161) 53-0162 531400-0602-5 3-53

05724 (53-0161) 53-0162 531400-0602-6 3-53

05724 (53-0161) 53-0162 531400-0602-7 3-53

05760 (53-0198) 53-0194

53-0196 531540-0603-2 3-53

05912 (73-0007) 73-0007 731000-0802-1 2-73

05946 (53-0201) 538295-0603-1 3-53

05946 (53-0201) 53-0286 538295-0603-2 3-53

06054 (29-0088) 292527-0503-1 2-29

06054 (29-0088) 29-0087 292527-0503-4 2-29

06054 (29-0088) 29-0087 292527-0503-5 2-29

06208 523316-0603-1 3-52

06208 523317-0603-2 3-52

06208 531549-0602-2 3-53

06208 531549-0604-2 3-53

06208 531568-0604-2 3-53

06208 531569-0604-2 3-53

06208 533329-0602-1 3-53

06208 533331-0602-1 3-53

06208 533331-0603-1 3-53

06208 533335-0603-2 3-53

06208 533339-0603-1 3-53

06208 533343-0603-1 3-53

06208 533345-0602-1 3-53

06208 536355-0606-1 3-53

06208 536355-0606-2 3-53

06208 536359-0606-1 3-53

06208 536359-0606-2 3-53

06240 (52-0132) 52-0130 521014-0504-1 2-52

06329 (32-0377) 321124-0504-1 2-32

06335 (26-0049) 212200-0505-4 2-21

06335 (26-0049) 261700-0503-1 2-26

06653 (53-0209) 53-0357 531820-0603-2 3-53

06653 (53-0209) 53-0357 531820-0603-3 3-53

06661 (57-0143) 57-0142 572090-0603-1 3-57

06675 (29-0091) 271414-0504-1 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 25 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

06676 (29-0092) 271414-0504-2 2-27

06788 (53-0226) 53-0363 531933-0603-1 3-53

06788 (53-0226) 53-0363 531933-0603-2 3-53

06788 (53-0226) 53-0363 531933-0603-3 3-53

06788 (53-0226) 53-0363 531933-0603-4 3-53

06857 (21-0113) 213400-0503-1 2-21

06883 (38-0037) 307200-0503-1 2-30

06891 (57-0145) 57-0150 572512-0502-1 2-57

06925 (53-0221) 53-0220 531820-0603-1 3-53

07085 (53-0223) 53-0211 531000-0603-5 3-53

07085 (53-0223) 53-211 531000-0603-6 3-53

07085 (53-0223) 53-0225 533824-0602-2 3-53

07175 (54-0067) 54-0066 541101-0603-1 3-54

07191 53-0248 531249-0603-1 3-53

07191 53-0248 531249-0603-2 3-53

07191 53-0248 531249-0603-3 3-53

07191 53-0248 531249-0603-4 3-53

07301 (53-0239) 536578-0604-1 3-53

07587 53-0248 531249-0603-1 3-53

07587 53-0248 531249-0603-2 3-53

07587 53-0248 531249-0603-3 3-53

07587 53-0248 531249-0603-4 3-53

07602 (57-0160) 278141-0502-1 2-27

07715 (53-0270) 53-0269 551004-0603-1 3-55

07757 (53-0272) 536598-0606-1 3-53

07757 (53-0272) 536598-0606-2 3-53

07757 (53-0272) 536598-0606-3 3-53

07757 (53-0272) 536598-0606-5 3-53

07757 (53-0272) 536598-0606-6 3-53

07757 (53-0272) 536598-0607-1 3-53

07757 (53-0272) 536598-0607-2 3-53

07757 (53-0272) 536598-0607-3 3-53

07757 (53-0272) 536598-0607-4 3-53

07757 (53-0272) 536598-0607-5 3-53

07864 561100-0502-1 2-56

08057 (21-0116) 538295-0603-1 3-53

08057 (21-0116) 53-0286 538295-0603-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 26 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

08238 (57-0174) 275421-0505-1 2-27

08253 (57-0175) 576013-0604-1 3-57

08253 (57-0175) 576013-0604-2 3-57

08253 (57-0175) 576013-0604-3 3-57

08253 (57-0175) 576013-0604-4 3-57

08253 (57-0175) 576013-0604-5 3-57

08253 (57-0175) 576013-0604-6 3-57

08253 (57-0175) 576013-0606-1 3-57

08253 (57-0175) 576013-0606-2 3-57

08253 (57-0175) 576013-0606-3 3-57

08253 (57-0175) 576013-0606-4 3-57

08253 (57-0175) 576013-0606-5 3-57

08253 (57-0175) 576013-0606-6 3-57

08344 (53-0279) 53-0277 539005-0603-1 3-53

08357 (52-0148) 527300-0503-2 2-52

08357 (52-0148) 527300-0503-3 2-52

08430 (26-0055) 262100-0502-1 2-26

08486 (57-0179) 536541-0606-1 3-53

08486 (57-0179) 536541-0606-2 3-53

08486 (57-0179) 536541-0606-3 3-53

08486 (57-0179) 536541-0606-4 3-53

08492 (53-0263) 53-0248 531249-0603-1 3-53

08492 (53-0263) 53-0248 531249-0603-2 3-53

08492 (53-0263) 53-0248 531249-0603-3 3-53

08492 (53-0263) 53-0248 531249-0603-4 3-53

08729 (26-0058) 26-057 262500-0502-1 2-26

08732 (29-0099) 29-0097 292527-0503-6 2-29

08762 (35-0010) 35-0009 351241-0502-2 2-35

08854 (52-0152) 52-0151 524215-0502-1 2-52

08964 (28-0061) 282116-0503-3 2-28

10086 (57-0188) 57-130 571037-0603-1 3-57

10086 (57-0188) 57-130 571037-0603-2 3-57

10086 (57-0188) 57-130 571037-0603-3 3-57

10089 (57-0191) 536541-0606-5 3-53

10089 (57-0191) 536541-0606-6 3-53

10089 (57-0191) 536541-0606-7 3-53

10089 (57-0191) 536541-0606-8 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 27 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

10261 (54-0076) 54-0076 540011-0603-2 3-54

10261 (54-0076) 54-0076 540011-0603-4 3-54

10262 548051-0603-1 3-54

10262 548051-0603-2 3-54

10262 548051-0603-3 3-54

10263 (54-0078) 548051-0603-1 3-54

10263 (54-0078) 548051-0603-2 3-54

10293 (34-0121) 344800-0503-1 2-34

10326 (57-0203) 576064-0606-1 3-57

10326 (57-0203) 576064-0606-2 3-57

10326 (57-0203) 576064-0606-3 3-57

10326 (57-0203) 576064-0606-4 3-57

10326 (57-0203) 576064-0606-5 3-57

10326 (57-0203) 576064-0606-6 3-57

10328 (54-0079) 54-0071 541105-0603-1 3-54

10328 (54-0079) 54-0071 541105-0603-2 3-54

10335 (54-0080) 54-0073 541107-0603-1 3-54

10335 (54-0080) 54-0073 541107-0603-2 3-54

10335 (54-0080) 54-0073 541107-0603-3 3-54

10335 (54-0080) 54-0073 541107-0603-4 3-54

10335 (54-0080) 54-0073 541107-0603-5 3-54

10335 (54-0080) 54-0073 541107-0603-6 3-54

10414 (53-0294) 53-0300 539008-0603-1 3-53

10431 (54-0081) 54-0075 543002-0602-4 3-54

10431 (54-0081) 54-0075 543002-0602-5 3-54

10453 (53-0297) 53-0268 536543-0606-1 3-53

10459 (54-0077) 54-0076 540011-0603-2 3-54

10459 (54-0077) 540011-0603-3 3-54

10459 (54-0077) 54-0076 540011-0603-4 3-54

10470 (57-0207) 576063-0606-1 3-57

10470 (57-0207) 576063-0606-2 3-57

10470 (57-0207) 576063-0606-3 3-57

10470 (57-0207) 576063-0606-4 3-57

10598 (54-0085) 54-0084 541010-0603-1 3-54

10617 (34-0126) 344800-0503-1 2-34

10715 (53-0306) 53-0305 533730-0603-1 3-53

10720 (29-0105) 291133-0503-4 2-29

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 28 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

10752 (57-0191) 536541-0606-6 3-53

10756 (36-0032) 36-0031 361115-0502-1 2-36

10796 275126-0505-2 2-27

10796 (27-0186) 275126-0505-3 2-27

10822 (54-0090) 54-0089 540012-0603-1 3-54

10929 (24-0086) 24-0087 240000-0503-1 2-24

10929 (24-0086) 24-0087 532411-0502-1 2-53

11045 (53-0315) 53-0162 531400-0602-1 3-53

11045 (53-0315) 53-0162 531400-0602-3 3-53

11045 (53-0315) 53-0162 531400-0602-4 3-53

11045 (53-0315) 53-0162 531400-0602-5 3-53

11045 (53-0315) 53-0162 531400-0602-6 3-53

11045 (53-0315) 53-0162 531400-0602-7 3-53

11058 (57-220) 57-219 572512-0603-3 3-57

11058 (57-220) 57-219 572512-0603-4 3-57

11109 (54-0094) 54-096 549002-0603-1 3-54

11130 (57-221) 57-0213 571175-0603-1 3-57

11130 (57-221) 57-0213 571175-0603-2 3-57

11130 (57-221) 57-0213 571175-0603-3 3-57

11130 (57-221) 57-0213 571175-0603-4 3-57

11150 (22-0112) 221000-0503-1 2-22

11206 (29-0106) 29-0101 292527-0503-7 2-29

11206 (29-0106) 292527-0505-1 2-29

11206 (29-0106) 292527-0505-2 2-29

11213 (57-0191) 536541-0606-6 3-53

11213 (57-0191) 536541-0606-8 3-53

11220 (32-0416) 322200-0502-1 2-32

11220 (32-0416) 322200-0505-1 2-32

11286 (53-0334) 53-0309 539010-0603-1 3-53

11286 (53-0334) 53-0309 539010-0603-2 3-53

11349 (54-0095) 24-0053

24-0083 242200-0503-2 2-24

11361 (52-0165) 523600-0502-1 2-52

11421 (53-0326) 53-0248 531249-0603-4 3-53

11480 (30-0044) 304100-0502-2 2-30

11527 (29-0109) 29-0108 292527-0504-1 2-29

11602 (57-0231) 57-0229 575412-0602-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 29 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

11639 (35-0143) 345600-0503-1 2-34

11767 (29-0112) 291133-0503-4 2-29

11768 (09-0113) 291133-0503-4 2-29

11862 (34-0150) 342500-0503-1 2-34

11862 (34-0150) 342500-0503-2 2-34

11932 (57-0235) 57A0246 574212-0602-1 3-57

11932 (57-0235) 57A0246 574212-0602-2 3-57

11932 (57-0235) 57A0234 574212-0602-3 3-57

11932 (57-0235) 57A0234 574212-0602-4 3-57

11932 (57-0235) 57A0234 579003-0603-1 3-57

11932 (57-0235) 57A0234 579003-0603-2 3-57

12009 (34-0159) 342538-0504-1 2-34

12012 (32-0429) 324314-0505-1 2-32

12024 (52-0173) 52-0168 521000-0502-1 2-52

12024 (52-0173) 52-0168 521000-0502-2 2-52

12024 (52-0173) 52-168 529003-0603-2 3-52

12026 (27-0192) 271412-0502-1 2-27

12026 (27-0192) 272411-0502-1 2-27

12026 (27-0192) 273411-0502-1 2-27

12167 (53-0358) 53-0329 534100-0603-1 3-53

12167 (53-0358) 534100-0603-2 3-53

12513 (31-0077) 331300-0503-1 2-33

12662 531208-0602-1 3-53

12662 531208-0602-2 3-53

12662 (53-0364) 53-0365 531208-0603-1 3-53

12662 (53-0364) 53-0365 531208-0603-2 3-53

12790 (22-0117) 22-0118 221000-0503-2 2-22

12938 (25-0479) 25-0477 257200-0502-1 2-25

13031 57-0240 575126-0602-1 3-57

13041 (28-0085) 28-0084 282100-0503-1 2-28

13043 (22-0119) 22-0120 222300-0504-1 2-22

1307 57-0109 571200-0603-1 3-57

13212 (32-0453) 32-0447 322114-0505-3 2-32

13241 (57-0245) 57-0240 575126-0602-1 3-57

13297 29-0122 290000-0502-1 2-29

13348 (57-0249) 57-0251 579004-0603-1 3-57

13348 (57-0249) 57-0251 579004-0603-2 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 30 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

13400 (57-0252) 57-0250 575127-0602-2 3-57

13400 (57-0252) 57-0250 575127-0602-3 3-57

13424 (29-0121) 29-0122 290000-0502-1 2-29

1644 57-0076 575000-0502-1 2-57

1654 793500-0811-1 2-79

1824 571069-0604-1 3-57

1824 571072-0604-2 3-57

2300 571072-0604-2 3-57

2434 204130-0505-1 2-20

2434 204130-0505-2 2-20

2434 54-060 544011-0603-1 3-54

2434 54-063 544012-0603-1 3-54

2574 201210-0505-1 2-20

2574 201210-0505-2 2-20

2574 201210-0505-3 2-20

2574 201210-0505-4 2-20

2574 201210-0505-5 2-20

2574 201210-0505-6 2-20

2611 53-0211 531000-0603-7 3-53

2684 (27-128) 27-0132 274211-0503-3 2-27

2684 (27-128) 27-0132 274211-0503-4 2-27

2973 57-091 572512-0603-1 3-57

2973 57-219 572512-0603-3 3-57

2973 57-219 572512-0603-4 3-57

3039 531513-0602-1 3-53

3079 291400-0502-1 2-29

4152 (29-0080) 291400-0502-1 2-29

5132 578265-0603-1 3-57

6208 526305-0606-1 3-52

6208 526305-0606-2 3-52

6208 526305-0606-3 3-52

6208 526305-0606-4 3-52

6208 536367-0606-1 3-53

6208 536367-0606-2 3-53

6442 (54-064) 54-063 544012-0603-1 3-54

6770 (54-065) 54-060 544011-0603-1 3-54

8758 (57-182) 57-181 571213-0603-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 31 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

(24-0048) 24-0048 242200-0502-1 2-24

(33-0113) 335100-0503-3 2-33

53-0274 531409-0603-1 3-53

(53-0192) 53-0227 533220-0603-3 3-53

(53-0192) 53-0227 533439-0603-2 3-53

(53-0192) 53-0227 533727-0603-2 3-53

SB

(53-0282) 536511-0606-1 3-53

(53-0336) 53-0341 539014-0603-1 3-53

(54-0046) 54-0070 543001-0602-4 3-54

(53-0282) 576035-0606-1 3-57

(53-0282) 576035-0606-2 3-57

(53-0282) 576035-0606-3 3-57

(53-0282) 576035-0606-4 3-57

(53-0291) 576035-0606-5 3-57

(53-0291) 576035-0606-6 3-57

(53-0291) 576035-0606-7 3-57

(53-0291) 576035-0606-8 3-57

(53-0291) 576035-0606-9 3-57

(53-0291) 576035-0607-1 3-57

(53-0291) 576035-0607-2 3-57

(53-0291) 576035-0607-3 3-57

(71-0053) 71-0054 711301-0802-1 2-71

SBGE 72-548 723200-0802-1 2-72

SBGE 72-548 723200-0802-3 2-72

SBGE 72-861 723300-0802-2 2-72

SBGE 72-099 723300-0802-3 2-72

SB PW 5189 724400-0812-1 2-72

SB PW 5195 724400-0812-1 2-72

SB PW 5189 724400-0812-2 2-72

SB PW 5195 724400-0812-2 2-72

SB PW 5847 725000-0812-1 2-72

SB PW 6054 725000-0812-1 2-72

SB PW 6054 725000-0812-3 2-72

SB PW 5416 725000-0814-1 2-72

SB PW 5416 725000-0814-2 2-72

SB PW 5195 731301-0811-1 2-73

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-2 Page 32 MODIFICATIONS (MOD) - CROSS REFERENCE LIST

PRE-MOD POST-MOD

MOD MOD-SB ISB TASK NUMBER SECTION TASK NUMBER SECTION

SB 6035 752400-0813-1 2-75

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 1 

# APPENDIX 2-3

INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

-A300-27-0201 ALL 274211-0502-2 2-27

05-0004 ALL 271122-0504-1 2-27

05-0004 ALL 272100-0504-1 2-27

05-0004 ALL 272311-0504-1 2-27

05-0004 ALL 272312-0504-1 2-27

05-0004 ALL 273100-0504-1 2-27

05-0004 ALL 273311-0504-1 2-27

20-0007 ALL 510000-0603-1 3-51

21-0120 ALL 212200-0505-5 2-21

22-0118 POST 12790

(22-0117) 221000-0503-2 2-22

22-0120 POST 13043

(22-0119) 222300-0504-1 2-22

22-0121 NON FWD-FACE 222300-0503-3 2-22

22A0115 FWD-FACE 222000-0504-1 2-22

24-0048 MSN 003-116

PRE (24-0048) 242200-0502-1 2-24

24-0053 PRE 11349

(54-0095) 242200-0503-2 2-24

24-0083 PRE 11349

(54-0095) 242200-0503-2 2-24

24-0087 PRE 10929

(24-0086) 240000-0503-1 2-24

24-0087 PRE 10929

(24-0086) 532411-0502-1 2-53

24-073 ALL ZL-500-0402-2 4-ZL

25-0138 PRE 01878

(25-0149)

PRE 02506

(25-0248) 255120-0502-1 2-25

25-0138 POST 01878

(25-0149)

POST 02506

(25-0248)

PRE 03361

(25-0332) 255120-0502-2 2-25

25-0477 PRE 12938 257200-0502-1 2-25

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 2 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

(25-0479)

26-025 PRE 01988

(54-0022) 262111-0504-3 2-26

26-057 PRE 08729

(26-0058) 262500-0502-1 2-26

27-0044 PRE 01501

(57-0035)

PRE 01673

(57-0007)

PRE 01798

(27-0087) 275138-0502-1 2-27

27-0044 POST 01501

(57-0035)

POST 01673

(57-0007)

PRE 01798

(27-0087) 275138-0502-2 2-27

27-0093 PRE 02009

(27-0097) 272312-0503-2 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 275123-0504-1 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275123-0504-2 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164) 275124-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 275124-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164) 275124-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275124-0504-4 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 3 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164) 275136-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 275136-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164) 275136-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275136-0504-4 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 275136-0504-5 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275136-0504-6 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164) 275137-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 275137-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164) 275137-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275137-0504-4 2-27

27-0101 POST 01789

(27-0084)

POST 04494 278117-0504-1 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 4 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

(27-0164)

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 278117-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164) 278117-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278117-0504-4 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164) 278118-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 278118-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164) 278118-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278118-0504-4 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278119-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278119-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164) 278119-0504-3 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 5 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

KRUG.FLAP

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278119-0504-4 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164)

NON-KRUG.FLAP 278119-0504-5 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164)

NON-KRUG.FLAP 278119-0504-6 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164)

NON-KRUG.FLAP 278119-0504-7 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278119-0504-8 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278120-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278120-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278120-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278120-0504-4 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 6 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

KRUG.FLAP

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164) 278121-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164) 278121-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164) 278121-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164) 278121-0504-4 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278153-0504-1 2-27

27-0101 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278153-0504-2 2-27

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278153-0504-3 2-27

27-0101 PRE 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278153-0504-4 2-27

27-0101 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278153-0504-5 2-27

27-0101 POST 01789 278153-0504-6 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 7 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP

27-0101 PRE 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278153-0504-7 2-27

27-0107 MACHINED PULLEYS 271216-0502-1 2-27

27-0107 MACHINED PULLEYS 271216-0502-2 2-27

27-0107 MACHINED PULLEYS 325100-0502-1 2-32

27-0109 ALL 271400-0504-1 2-27

27-0132

POST 2684

(27-128)

P/N CHA723-20XX 274211-0503-3 2-27

27-0132 PRE 2684

(27-128)

P/N CHA723-010

THRU

P/N CHA723-018 274211-0503-4 2-27

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164) 278117-0504-1 2-27

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164) 278117-0504-2 2-27

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164) 278118-0504-1 2-27

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164) 278118-0504-2 2-27

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278119-0504-1 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 8 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278119-0504-2 2-27

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164)

NON-KRUG.FLAP 278119-0504-5 2-27

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164)

NON-KRUG.FLAP 278119-0504-6 2-27

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278120-0504-1 2-27

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278120-0504-2 2-27

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164) 278121-0504-1 2-27

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164) 278121-0504-2 2-27

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278153-0504-1 2-27

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278153-0504-2 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 9 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

27-0158 POST 01789

(27-0084)

POST 04494

(27-0164)

KRUG.FLAP 278153-0504-5 2-27

27-0158 POST 01789

(27-0084)

PRE 04494

(27-0164)

KRUG.FLAP 278153-0504-6 2-27

27-0159 PRE 01789

(27-0084)

POST 04494

(27-0164) 275124-0504-3 2-27

27-0159 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275124-0504-4 2-27

27-0159 PRE 01789

(27-0084)

POST 04494

(27-0164) 275136-0504-3 2-27

27-0159 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275136-0504-4 2-27

27-0159 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275136-0504-6 2-27

27-0159 PRE 01789

(27-0084)

POST 04494

(27-0164) 275137-0504-3 2-27

27-0159 PRE 01789

(27-0084)

PRE 04494

(27-0164) 275137-0504-4 2-27

27-0172 PRE 05240

(27-0173) 275126-0502-3 2-27

27-0188 ALL 272400-0503-1 2-27

27-0189 ALL 271412-0503-2 2-27

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 10 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

27-0203 ALL 274211-0505-5 2-27

28-0084 B4

C4

F4

PRE 13041

(28-0085) 282100-0503-1 2-28

29-0015 PRE 01572

(29-0031)

(ABEX MODEL

PMP 09 V01

P/N 4007) 292000-0502-1 2-29

29-0087 POST 01758

(29-0039)

POST 02528

(29-0060)

PRE 06054

(29-0088) 292527-0503-4 2-29

29-0087 POST 01758

(29-0039)

POST 02528

(29-0060)

PRE 06054

(29-0088) 292527-0503-5 2-29

29-0097 PRE 04803

PRE 08732

(29-0099) 292527-0503-6 2-29

29-0101 PRE 11206

(29-0106) 292527-0503-7 2-29

29-0108 PRE 11527

(29-0109) 292527-0504-1 2-29

29-0118 ALL 292527-0503-8 2-29

29-0122 PRE 13297

PRE 13424

(29-0121) 290000-0502-1 2-29

30-0047 ALL 304200-0502-1 2-30

32-0055 POST 02529

(32-0228)

POST 03083

(32-0269) 323112-0503-1 2-32

32-0055 POST 02529

(32-0228)

PRE 03083 323112-0503-2 2-32

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 11 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

(32-0269)

32-0055 PRE 02529

(32-0228)

PRE 03083

(32-0269) 323112-0503-3 2-32

32-0233 PRE 01033

(32-0040)

MHB 322 321100-0502-1 2-32

32-0264 PRE 03101

(32-0267) 324247-0502-1 2-32

32-0298 PRE 01257

MHB 384 323200-0503-4 2-32

32-0328 PRE 01257

MHB 224 321100-0502-2 2-32

32-0335 POST 02781

(32-0272)

PRE 03433 323300-0503-1 2-32

32-0353 ALL

NOTE 323200-0503-3 2-32

32-0356 POST 01257

MHB 224

PRE 04544

(32-0348)

(32-0355)

MHB 542/ 585

P/N C65381-4

P/N C65381-6 321100-0503-1 2-32

32-0365 PRE 01257

MHB 485

P/N C65381-2

P/N C65381-4 321100-0503-2 2-32

32-0369 B2 321100-0503-3 2-32

32-0373 POST 01033

MHB 423 324200-0503-1 2-32

32-0382 PRE 01257

(32-0383)

MHB SB

470-32-605 322112-0504-2 2-32

32-0388 PRE 01257

(32-0389) MHB SB 322112-0504-3 2-32

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 12 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

470-32-642

32-0394 PRE 01257

(32-0396)

MHB SB

470-32-672 321114-0502-1 2-32

32-0447 PRE 13212

(32-0453) 322114-0505-3 2-32

35-0009 PRE 08762

(35-0010) 351241-0502-2 2-35

36-0031 PRE 10756

(36-0032) 361115-0502-1 2-36

470-32-420 B2 321100-0503-3 2-32

470-32-442 PRE 01257

MHB 485

P/N C65381-2

P/N C65381-4 321100-0503-2 2-32

49-0017 PRE 01646

(49-0019) 495000-0703-5 2-49

49-0031 POST 01782

(49-0025)

PRE 04770

(49-0046) 495000-0703-2 2-49

52-0014 PRE 01094

(53-0051) 521031-0502-2 2-52

52-0014 POST 01094

(53-0051) 521031-0502-3 2-52

52-0014 PRE 01094

(53-0051) 522231-0502-2 2-52

52-0014 POST 01094

(53-0051) 522231-0502-3 2-52

52-0048 PRE 02624

(52-0098) 523011-0502-1 2-52

52-0048 PRE 02624

(52-0098) 523011-0504-1 2-52

52-0101 PRE 02295

PRE 03054

(52-0104) 523307-0502-1 2-52

52-0130 PRE 06240

(52-0132) 521014-0504-1 2-52

52-0136 POST 01202

(52-0078) 523307-0603-1 3-52

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 13 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

OR

POST 03054

(52-0104)

52-0151 POST 02709

PRE 08854

(52-0152) 524215-0502-1 2-52

52-0161 NLG DOOR

ASSY P/N

A52810648000

NLG DOOR FITTING

P/N

A52810629200/

201 528212-0503-1 2-52

52-0168 B2

B4

C4

PRE 12024

(52-0173) 521000-0502-1 2-52

52-0168 F4

PRE 12024

(52-0173) 521000-0502-2 2-52

52-136 POST 01202

(52-0078) 523707-0603-1 3-52

52-168 PRE 12024

(52-0173) 529003-0603-2 3-52

53-0068 PRE 02021

(53-0089) 535300-0502-2 2-53

53-0075 PRE 01055 533218-0602-2 3-53

53-0076 PRE 01115 533220-0603-1 3-53

53-0096 PRE 01208 530503-0603-1 3-53

53-0101 MSN 003-052

PRE 03760

(53-0170) 533815-0602-3 3-53

53-0103 PRE 02109 532100-0603-1 3-53

53-0104 MSN 033 539003-0603-1 3-53

53-0112 PRE 01358

(53-0027) 533437-0602-3 3-53

53-0127 PRE 02147

(53-0110)

PRE 02348

PRE 02526

(53-0128) 533731-0602-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 14 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

53-0129 PRE 01444

(53-0078) 531563-0602-2 3-53

53-0143 PRE 02643

(53-0132) 531700-0602-1 3-53

53-0148 MSN 003-156

NOTE 531000-0603-1 3-53

53-0149 MSN 003-156

NOTE 531000-0603-2 3-53

53-0152 PRE 02476

(53-0121) 531912-0603-1 3-53

53-0152 PRE 02476

(53-0121) 531912-0603-2 3-53

53-0154 MSN 003-156

PRE 02727 531000-0602-3 3-53

53-0155 PRE 02899 531300-0502-1 2-53

53-0162 B2

PRE 03275

PRE 05724

(53-0161)

PRE 11045

(53-0315) 531400-0602-1 3-53

53-0162 B4-100

PRE 03275

PRE 05724

(53-0161)

PRE 11045

(53-0315) 531400-0602-3 3-53

53-0162 B4-200

C4

F4

PRE 03275

PRE 05724

(53-0161)

PRE 11045

(53-0315) 531400-0602-4 3-53

53-0162 B2

POST 03275

OR

POST 05724

(53-0161)

PRE 11045

(53-0315) 531400-0602-5 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 15 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

53-0162 B4-100

POST 03275

OR

POST 05724

(53-0161)

PRE 11045

(53-0315) 531400-0602-6 3-53

53-0162 B4-200

C4

F4

POST 03275

OR

POST 05724

(53-0161)

PRE 11045

(53-0315) 531400-0602-7 3-53

53-0165 PRE 03556

(53-0168) 534212-0502-1 2-53

53-0178 MSN 003-156

NOTE 531000-0602-4 3-53

53-0179 POST 02109

(53-0107)

PRE 03135

(53-0188) 532100-0603-3 3-53

53-0182 PRE 02611 531400-0602-2 3-53

53-0187 PRE 02380

(53-0119) 531716-0602-1 3-53

53-0190 PRE 04868

(53-0191) 534213-0603-1 3-53

53-0194 B2

PRE 05760

(53-0198) 531540-0603-2 3-53

53-0195 B2

PRE 02373 531540-0603-1 3-53

53-0196 B2

PRE 05760

(53-0198) 531540-0603-2 3-53

53-0204 ALL 531605-0603-1 3-53

53-0204 ALL 531719-0603-2 3-53

53-0204 ALL 533220-0603-2 3-53

53-0204 ALL 533439-0603-1 3-53

53-0204 ALL 533727-0603-3 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 16 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

53-0211 MSN 003-156

PRE 02611

POST 01421

(53-0033)

RETROFIT

POST 07085

(53-0223)

OR

POST 01421

SERIAL 531000-0603-5 3-53

53-0211 MSN 003-156

PRE 2611 531000-0603-7 3-53

53-0218 ALL 533935-0603-1 3-53

53-0218 ALL 533935-0603-2 3-53

53-0218 ALL 533935-0603-3 3-53

53-0220 PRE 06925

(53-0221) 531820-0603-1 3-53

53-0225 MSN 003-036

PRE 01421

(53-0033)

PRE 07085

(53-0223) 533824-0602-2 3-53

53-0227 PRE

(53-0192) 533220-0603-3 3-53

53-0227 PRE

(53-0192) 533439-0603-2 3-53

53-0227 PRE

(53-0192) 533727-0603-2 3-53

53-0229 PRE 02727

MSN 003-103 531001-0603-1 3-53

53-0229 PRE 02727

MSN 003-156 531001-0603-2 3-53

53-0229 PRE 02727

MSN 003-156 531001-0603-3 3-53

53-0229 PRE 02727

MSN 105 531001-0603-5 3-53

53-0229 PRE 02727

MSN 107 531001-0603-6 3-53

53-0229 PRE 02727

MSN 109 531001-0603-7 3-53

53-0233 ALL 531605-0603-1 3-53

53-0233 ALL 531719-0603-2 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 17 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

53-0233 ALL 533220-0603-2 3-53

53-0233 ALL 533439-0603-1 3-53

53-0233 ALL 533727-0603-3 3-53

53-0237 B2

FROM 0 FC/FH

TO 48000 FC 536597-0606-1 3-53

53-0237 B4-100

FROM 0 FC/FH

TO 40000 FC 536597-0606-2 3-53

53-0237 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC 536597-0606-3 3-53

53-0238 ALL

SB 53-0238

FROM 0 FC/FH

TO LOV 536554-0606-1 3-53

53-0242 ALL

ISB 53-0242

FROM 0 FC/FH

TO LOV 536529-0606-1 3-53

53-0243 ALL

SB 53-0243

FROM 0 FC/FH

TO LOV 536505-0606-1 3-53

53-0244 ALL

SB 53-0244

FROM 0 FC/FH

TO LOV 536535-0606-1 3-53

53-0245 SB 53-0245

FROM 0 FC/FH

TO LOV 536545-0606-1 3-53

53-0246536516 B2 536516-0606-1 3-53

53-0246536516 B4-100 536516-0606-4 3-53

53-0246 B4-200

C4

F4 536516-0606-6 3-53

53-0248 PRE 07191

PRE 07587

PRE 08492

(53-0263) 531249-0603-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 18 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

53-0248 PRE 07191

PRE 07587

PRE 08492

(53-0263) 531249-0603-2 3-53

53-0248 POST 07191

POST 07587

POST 08492

(53-0263) 531249-0603-3 3-53

53-0248 PRE 07191

PRE 07587

PRE 08492

(53-0263)

POST 11421

(53-0326) 531249-0603-4 3-53

53-0252 ALL

SB 53-0252

FROM 0 FC/FH

TO LOV 536544-0606-1 3-53

53-0254 ALL

SB 53-0254

FROM 0 FC/FH

TO LOV 536601-0606-1 3-53

53-0255 ALL

SB 53-0255

FROM 0 FC/FH

TO LOV 536701-0606-1 3-53

53-0256 ALL

SB 53-0256

FROM 0 FC/FH

TO LOV 536901-0606-1 3-53

53-0256 B2

FROM 48000 FC

TO LOV 536901-0606-2 3-53

53-0256 B4-100

FROM 40000 FC

TO LOV 536901-0606-3 3-53

53-0256 B4-200

C4

F4

FROM 34000 FC

TO LOV 536901-0606-5 3-53

53-0257 ALL

FROM 0 FC/FH 536602-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 19 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

TO LOV

53-0257 ALL

FROM 0 FC/FH

TO 42500 FC 536603-0606-1 3-53

53-0258 ALL

SB 53-0258

FROM 0 FC/FH

TO LOV 536902-0606-1 3-53

53-0259 ALL

SB 53-0259

FROM 0 FC/FH

TO LOV 536515-0606-1 3-53

53-0260 ALL

SB 53-0260

FROM 0 FC/FH

TO LOV

TO 42500 FC 536702-0606-1 3-53

53-0261 B2

SB 53-0261

FROM 0 FC/FH

TO 42500 FC 536703-0606-1 3-53

53-0261 B4-100

SB 53-0261

FROM 0 FC/FH

TO 41700 FC 536703-0606-2 3-53

53-0261 B4-200

C4

F4

SB 53-0261

FROM 0 FC/FH

TO 48000 FC 536703-0606-3 3-53

53-0262 ALL

SB 53-0262

FROM 0 FC/FH

TO 40750 FC 536801-0606-1 3-53

53-0265 ALL

SB 53-0265

FROM 0 FC/FH

TO LOV 536512-0606-1 3-53

53-0268 PRE 10453

(53-0297)

FROM 0 FC/FH

TO LOV 536543-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 20 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

53-0269 PRE 07715

(53-0270) 551004-0603-1 3-55

53-0274 PRE 03185

PRE SRM 531400 531409-0603-1 3-53

53-0275 PRE 02626

FROM 0 FC/FH

TO LOV 536509-0606-1 3-53

53-0277 PRE 08344

(53-0279) 539005-0603-1 3-53

53-0278 POST 00793

(53-0906)

NOTE

PRE 01446 536208-0605-1 3-53

53-0278 POST 00793

(53-0906)

PRE 01446 536208-0605-2 3-53

53-0278 POST 00793

(53-0906)

POST 01446 536208-0605-3 3-53

53-0283 ALL 533430-0602-1 3-53

53-0286 PRE 08057

(21-0116)

OR

PRE 05946

(53-0201) 538295-0603-2 3-53

53-0287 B2

POST

(53-0282) 539006-0603-1 3-53

53-0296 ALL 539007-0603-2 3-53

53-0299 ALL

SB 53-0299

FROM 0 FC/FH

TO LOV 536513-0606-1 3-53

53-0300 PRE 10414

(53-0294) 539008-0603-1 3-53

53-0301 ALL 539009-0603-1 3-53

53-0303 ALL 534805-0603-1 3-53

53-0304 SB 53-0304

FROM 0 FC/FH

TO LOV 536549-0606-1 3-53

53-0305 PRE 02611

PRE 10715 533730-0603-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 21 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

(53-0306)

53-0309 PRE 11286

(53-0334) 539010-0603-1 3-53

53-0309 POST 11286

(53-0334) 539010-0603-2 3-53

53-0310 SB 53-0310

FROM 0 FC/FH

TO LOV 536548-0606-1 3-53

53-0311 ALL 539011-0603-1 3-53

53-0314 B2 539012-0603-1 3-53

53-0327 ALL 531253-0604-1 3-53

53-0327 ALL 539013-0603-1 3-53

53-0328 B2 538015-0603-1 3-53

53-0328 B2K

B4

C4

F4 538015-0603-2 3-53

53-0329 POST 03135

(53-0188)

PRE 12167

(53-0358) 534100-0603-1 3-53

53-0332 B2 539001-0603-1 3-53

53-0332 B4-100 539001-0603-2 3-53

53-0332 B4-200 539001-0603-3 3-53

53-0337 B2 531570-0603-1 3-53

53-0337 B4-100 531570-0603-2 3-53

53-0337 B4-200 531570-0603-3 3-53

53-0339 B1

B2-1C

B2K-3C

B2-203

B4-2C

B4-103

B4-203

POST 02140

(53-0109) 538592-0603-1 3-53

53-0341 B4-100

B4-200

PRE (53-0336) 539014-0603-1 3-53

53-0345 ALL

SB 53-0345 536555-0606-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 22 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

FROM 0 FC/FH

TO LOV

53-0348 PRE 03632

FROM 0 FC/FH

TO LOV 536111-0606-1 3-53

53-0350 B4

C4

F4 539015-0603-1 3-53

53-0354 MSN 003 TO 156 539016-0603-1 3-53

53-0354 MSN 157 TO 305 539016-0603-2 3-53

53-0356 PRE 02611 533439-0603-3 3-53

53-0356 PRE 02611 533616-0603-4 3-53

53-0356 MSN 001 TO 156

B2

B4-100

B4-200

F4 539017-0603-1 3-53

53-0356 MSN 001 TO 156

C4 539017-0603-2 3-53

53-0357 MSN 003-156

PRE 06653

(53-0209) 531820-0603-2 3-53

53-0357 MSN 157-305

OR

MSN 003-156

POST 06653

(53-0209) 531820-0603-3 3-53

53-0359 MSN 003 TO 156 536112-0606-1 3-53

53-0359 MSN 157 TO 305 536112-0606-2 3-53

53-0363 PRE 06788

(53-0226) 531933-0603-1 3-53

53-0363 PRE 06788

(53-0226) 531933-0603-2 3-53

53-0363 POST 06788

(53-0226) 531933-0603-3 3-53

53-0363 POST 06788

(53-0226) 531933-0603-4 3-53

53-0365 B2

B4-100

B4-200

PRE 12662

(53-0364) 531208-0603-1 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 23 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

53-0365 C4-203

F4-203

PRE 12662

(53-0364) 531208-0603-2 3-53

53-0378 B2K-3C

B4-103F

B4-120

B4-203

B4-203F

B4-2C 531314-0604-1 3-53

53-0378 B2K-3C

B4-103F

B4-120

B4-203

B4-203F

B4-2C 531314-0604-2 3-53

53-0378 B2K-3C

B4-103F

B4-120

B4-203

B4-203F

B4-2C 531314-0604-3 3-53

53-0378 B2K-3C

B4-103F

B4-120

B4-203

B4-203F

B4-2C 531314-0604-4 3-53

53-0379 ALL 536596-0603-1 3-53

53-0381 B2

POST

(53-0282) 536561-0606-1 3-53

53-0383 B4, C4, F4

POST

(53-0291) 536561-0606-2 3-53

53-0388 ALL 536215-0603-1 3-53

53-211 MSN 003-156

PRE 02611

PRE 02525

(53-0126)

POST 01421

(53-0033)

RETROFIT 531000-0603-6 3-53

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 24 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

POST 07085

(53-0223)

OR

POST 01421

SERIAL

53-258 ALL 531926-0603-1 3-53

54-0029 PRE 02298

(54-0030) 540000-0502-1 2-54

54-0042 PRE 04125

(54-0057) 541000-0502-1 2-54

54-0045 POST 00733

PRE 02434 540006-0603-1 3-54

54-0066 GE

PRE 07175

(54-0067)

PRE 02434 541101-0603-1 3-54

54-0070 GE

PRE 02434

PRE (54-0046) 543001-0602-4 3-54

54-0071 GE

POST 02434

PRE 10328

(54-0079) 541105-0603-1 3-54

54-0071 PW

PRE 10328

(54-0079) 541105-0603-2 3-54

54-0072 ALL 549001-0603-1 3-54

54-0073 GE

PRE 10335

(54-0080)

POST 02434 541107-0603-1 3-54

54-0073 PW

PRE 10335

(54-0080)

POST 02434 541107-0603-2 3-54

54-0073 GE

PRE 10335

(54-0080)

PRE 02434 541107-0603-3 3-54

54-0073 GE

POST 10335

(54-0080) 541107-0603-4 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 25 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

POST 02434

54-0073 PW

POST 10335

(54-0080) 541107-0603-5 3-54

54-0073 GE

POST 10335

(54-0080)

PRE 02434 541107-0603-6 3-54

54-0075 PRE 10431

(54-0081) 543002-0602-4 3-54

54-0075 POST 10431

(54-0081) 543002-0602-5 3-54

54-0076 POST 02434

PRE 10459

(54-0077)

PRE 10261

(54-0076) 540011-0603-2 3-54

54-0076 POST 02434

PRE 10459

(54-0077)

POST 10261

(54-0076) 540011-0603-4 3-54

54-0084 GE

PRE 10598

(54-0085)

PRE 02434 541010-0603-1 3-54

54-0089 PRE 02434

PRE 10822

(54-0090) 540012-0603-1 3-54

54-060 GE

PRE 2434

PRE 6770

(54-065) 544011-0603-1 3-54

54-063 PW

POST 2434

PRE 6442

(54-064) 544012-0603-1 3-54

54-068 GE

MSN 003 TO 161

PW 541102-0603-1 3-54

54-096 POST 02434

PRE 11109

(54-0094) 549002-0603-1 3-54

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 26 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

55-0032 ALL 552111-0504-1 2-55

55-0035 PRE 01692 551033-0603-1 3-55

55-0036 ALL

SB 55-0036

FROM 0 FC/FH

TO LOV 556001-0606-1 3-55

55-026 PRE 03172

(55-0024) 553017-0603-1 3-55

56-0002 PRE 01661

PRE 02378

(53-0003)

POST 04580 562100-0502-1 2-56

56-0007 POST 01661

POST 02378

(53-0003)

PRE 04580 562100-0502-2 2-56

56-0008 ALL

NOTE 561100-0502-2 2-56

5668 PW

PRE SB PW 5416 725000-0814-1 2-72

57-0052 PRE 01698

(57-0053)

PRE 01872

(57-0064) 574414-0502-1 2-57

57-0072 MSN 003-012 575612-0603-1 3-57

57-0076 PRE 1644 575000-0502-1 2-57

57-0089 B4

C4

F4

POST 02300

(57-0083) 573111-0503-1 2-57

57-0089 B4

C4

F4

PRE 02300

(57-0083) 573111-0503-2 2-57

57-0101 PRE 03554 571020-0603-1 3-57

57-0109 B2

PRE 1307 571200-0603-1 3-57

57-0119 ALL

SB 57-0119

FROM 0 FC/FH 576059-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 27 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

TO LOV

57-0122 PRE 04400

(57-0123) 572500-0502-2 2-57

57-0142 PRE 06661

(57-0143) 572090-0603-1 3-57

57-0146 ALL

SB 57-0146

FROM 0 FC/FH

TO LOV 576008-0606-1 3-57

57-0147 ALL

SB 57-0147

FROM 0 FC/FH

TO LOV 576010-0606-1 3-57

57-0148 ALL

SB 57-0148

FROM 0 FC/FH

TO LOV 576012-0606-1 3-57

57-0149 ALL

SB 57-0147

FROM 0 FC/FH

TO LOV 576002-0606-1 3-57

57-0150 PRE 06891

(57-0145) 572512-0502-1 2-57

57-0151 B2

SB 57-0151

FROM 0 FC/FH

TO LOV 576057-0606-1 3-57

57-0152 ALL

SB 57-0152

FROM 0 FC/FH

TO LOV 576003-0606-1 3-57

57-0153 ALL

SB 57-0153

FROM 0 FC/FH

TO LOV 576014-0606-1 3-57

57-0155 ALL

SB 57-0155

FROM 0 FC/FH

TO LOV 576005-0606-1 3-57

57-0157 ALL

FROM 0 FC/FH

TO LOV 576016-0606-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 28 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

57-0158 ALL

SB 57-0158

FROM 0 FC/FH

TO LOV 576053-0605-1 3-57

57-0162 ALL

SB 57-0162

FROM 0 FC/FH

TO LOV 576055-0606-1 3-57

57-0164 ALL

SB 57-0164

FROM 0 FC/FH

TO LOV 576056-0606-1 3-57

57-0176 ALL

SB 57-0148

FROM 0 FC/FH

TO LOV 576006-0606-2 3-57

57-0177 ALL

SB 57-0177 572090-0604-1 3-57

57-0177 ALL 572090-0604-2 3-57

57-0184 ALL

SB 57-0184

FROM 0 FC/FH

TO LOV 576001-0606-1 3-57

57-0187 ALL

SB 57-0187

FROM 0 FC/FH

TO LOV 576060-0605-1 3-57

57-0193 ALL

SB 57-0193

FROM 0 FC/FH

TO LOV 576058-0606-1 3-57

57-0204 ALL 578021-0602-2 3-57

57-0212 ALL 572030-0502-1 2-57

57-0212 ALL 579001-0603-1 3-57

57-0213 B2

PRE 11130

(57-221) 571175-0603-1 3-57

57-0213 B4-100

PRE 11130

(57-221) 571175-0603-2 3-57

57-0213 B4-200

C4 571175-0603-3 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 29 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

F4

PRE 11130

(57-221)

57-0213 B2

POST 11130

(57-221) 571175-0603-4 3-57

57-0214 PRE 04770

(57-0205) 575127-0602-1 3-57

57-0215 PRE 04770

(57-0201) 575125-0602-1 3-57

57-0229 PRE 11602

(57-0231) 575412-0602-1 3-57

57-0230 B2

FROM 0 FC/FH

TO LOV 576017-0606-1 3-57

57-0232 ALL 574113-0603-1 3-57

57-0237 ALL 579002-0603-1 3-57

57-0240 PRE 13031

OR

PRE 13241

(57-0245) 575126-0602-1 3-57

57-0250 PRE 13400

(57-0252)

PRE 04770

(57-0205) 575127-0602-2 3-57

57-0250 PRE 13400

(57-0252)

POST 04770

(57-0205) 575127-0602-3 3-57

57-0251 PRE 13348

(57-0249) 579004-0603-1 3-57

57-0251 PRE 13348

(57-0249) 579004-0603-2 3-57

57-085 PRE 02437

(57-0088) 574211-0602-1 3-57

57-091 PRE 2973 572512-0603-1 3-57

57-115 ALL 574111-0603-1 3-57

57-115 ALL 574112-0603-1 3-57

57-116 ALL 572512-0603-2 3-57

57-130 PRE 04959

(57-0132)

PRE 10086 571037-0603-1 3-57

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 30 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

(57-0188)

57-130 POST 04959

(57-0132)

PRE 10086

(57-0188)

NOTE 571037-0603-2 3-57

57-130 POST 04959

(57-0132)

PRE 10086

(57-0188)

NOTE 571037-0603-3 3-57

57-133 PRE 05132

(57-0134) 574300-0603-1 3-57

57-181 PRE 8758

(57-182) 571213-0603-1 3-57

57-206 ALL 571099-0603-1 3-57

57-210 ALL 571009-0602-1 3-57

57-219 PRE 2973

PRE 11058

(57-220) 572512-0603-3 3-57

57-219 PRE 2973

POST 11058

(57-220) 572512-0603-4 3-57

5786 PW

POST SB PW 5416 725000-0814-2 2-72

57A0234 PRE 11932

(57-0235) 574212-0602-3 3-57

57A0234 PRE 11932

(57-0235) 574212-0602-4 3-57

57A0234 B2

PRE 11932

(57-0235) 579003-0603-1 3-57

57A0234 B4

PRE 11932

(57-0235) 579003-0603-2 3-57

57A0246OIT9991.001709 POST 11932

(57-0235) 574212-0602-1 3-57

57A0246OIT9991.001709 POST 11932

(57-0235) 574212-0602-2 3-57

71-0054 GE

PRE (71-0053) 711301-0802-1 2-71

73-0007 GE 731000-0802-1 2-73

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 31 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

PRE 05912

(73-0007)

78-0025 GE 783100-0801-9 2-78

A78-3001 GE 783100-0801-7 2-78

GARRETT123894-36-1215 GARRETT

P/N 123894-1

123894-2

123940-1 361113-0504-1 2-36

GARRETT123894-36-1215 GARRETT

P/N 123894-1

123894-2

123940-1

(UP TO S/N1380) 361113-0504-2 2-36

GE72-099 GE

PRE SB

GE 72-099 723300-0802-3 2-72

GE72-1092 GE NOTE 712003-0802-1 2-71

GE72-1251 GE

PRE

SB GE 72-1239 725700-0802-4 2-72

GE72-227 GE

PRE

SB GE 72-0675 725700-0802-2 2-72

GE72-658 GE 725400-0802-3 2-72

GE72-675 GE

POST

SB GE 72-0675 725700-0802-3 2-72

GE72-688 GE

PRE

SB GE 72-717

PRE

SB GE 72-688 724100-0802-2 2-72

GE72-748 GE 725300-0803-1 2-72

GE72-750 GE

PRE

04685(71-0050)

SB GE 72-750 723400-0802-4 2-72

GE72-758 GE 723400-0802-5 2-72

GE72-758 GE 723400-0802-6 2-72

GE72-780 GE 723400-0802-3 2-72

GE72-837 GE 723400-0802-3 2-72

GE72-839 GE 723400-0802-2 2-72

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 32 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

GE72-861 GE

PRE SB

GE 72-861 723300-0802-2 2-72

GE72-879 GE

PRE

SB GE 72-0885 725300-0802-4 2-72

GE72-898 GE 723300-0802-1 2-72

GE72-957 GE 725400-0802-2 2-72

GE72-999 GE 722100-0802-1 2-72

GE72-A1197 GE

PRE

SB GE 72-A1201 725600-0802-1 2-72

GE75-0058 GE 754300-0802-2 2-75

GE75-0063 GE 754300-0802-2 2-75

GE75-064 GE

PRE

SB GE 75-0077

OR

PRE

SB GE 75-0078 750000-0802-1 2-75

GE75-070 GE

PRE

SB GE 75-0077

OR

PRE

SB GE 75-0078 750000-0802-1 2-75

GE78-228 GE 783605-0802-1 2-78

GE GE 783100-0801-7 2-78

GTSCP700-49-A3912 PRE 02011

(49-0029) 492000-0703-2 2-49

MHB470-32-001 ALL 324111-0504-1 2-32

MHB470-32-001 ALL 324111-0504-2 2-32

MHB470-32-001 ALL 324112-0504-1 2-32

MHB470-32-001 ALL 324112-0504-2 2-32

MHB470-32-206 ALL 323114-0503-1 2-32

MHB470-32-206 ALL 323133-0503-1 2-32

MHB470-32-349 PRE 01257

MHB 384 323200-0503-4 2-32

MHB470-32-409 ALL

NOTE 323200-0503-3 2-32

MHB470-32-604 PRE 01257 322112-0504-2 2-32

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-3 Page 33 INSPECTION SERVICE BULLETIN (ISB) - CROSS REFERENCE LIST

I.S.B. MPD APPLICABILITY TASK NUMBER SECTION

(32-0383)

MHB SB

470-32-605

MHB470-32-641 PRE 01257

(32-0389) MHB SB

470-32-642 322112-0504-3 2-32

MHB470-32-659 PRE 01257

(32-0396)

MHB SB

470-32-672 321114-0502-1 2-32

PW5551 PW 725300-0812-2 2-72

PW5667 PW 725200-0812-1 2-72

PW5749 PW 724000-0812-1 2-72

PW5890 PW 792203-0812-1 2-79

PW5978 PW

PRE SB PW 6054 725000-0812-3 2-72

PW5979 PW

PRE SB PW 5847

OR

PRE SB PW 6054 725000-0812-1 2-72

PWA5806 PW

P/N -789914

-790114

-791214 723100-0813-1 2-72

PW PW

PRE SB PW 5416 725000-0814-1 2-72

PW PW

POST SB PW 5416 725000-0814-2 2-72

SUN24-1341 ALL 241111-0505-2 2-24

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-4 Page 1 

# APPENDIX 2-4

SERVICE INFORMATION LETTER (SIL) - CROSS REFERENCE LIST

S.I.L MPD APPLICABILITY TASK NUMBER SECTION

20-0017 ALL 240000-0503-2 2-24

20-032 PRE 2574 201210-0505-1 2-20

20-032 POST 2574 201210-0505-2 2-20

20-032 PRE 2574 201210-0505-3 2-20

20-032 POST 2574 201210-0505-4 2-20

20-032 PRE 2574 201210-0505-5 2-20

20-032 POST 2574 201210-0505-6 2-20

20-032 ALL 201210-0505-7 2-20

20-032 ALL 201230-0505-1 2-20

20-032 ALL 201310-0505-1 2-20

20-032 ALL 201310-0505-2 2-20

20-032 ALL 201310-0505-3 2-20

20-032 ALL 201330-0505-1 2-20

20-032 ALL 201330-0505-2 2-20

20-032 ALL 201370-0505-1 2-20

20-032 ALL 201370-0505-2 2-20

20-032 ALL 201370-0505-3 2-20

20-032 ALL 201410-0505-1 2-20

20-032 ALL 201410-0505-2 2-20

20-032 ALL 201430-0505-1 2-20

20-032 ALL 201450-0505-1 2-20

20-032 ALL 201450-0505-2 2-20

20-032 ALL 201470-0505-1 2-20

20-032 ALL 201510-0505-1 2-20

20-032 ALL 201510-0505-2 2-20

20-032 ALL 201530-0505-1 2-20

20-032 ALL 201530-0505-2 2-20

20-032 ALL 201610-0505-1 2-20

20-032 ALL 201630-0505-1 2-20

20-032 ALL 201710-0505-1 2-20

20-032 ALL 202110-0505-1 2-20

20-032 ALL 202110-0505-2 2-20

20-032 ALL 202110-0505-3 2-20

20-032 ALL 202210-0505-1 2-20

20-032 ALL 202230-0505-1 2-20

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-4 Page 2 SERVICE INFORMATION LETTER (SIL) - CROSS REFERENCE LIST

S.I.L MPD APPLICABILITY TASK NUMBER SECTION

20-032 ALL 202230-0505-2 2-20

20-032 ALL 202230-0505-3 2-20

20-032 ALL 202310-0505-1 2-20

20-032 ALL 202310-0505-2 2-20

20-032 ALL 202310-0505-3 2-20

20-032 ALL 202330-0505-1 2-20

20-032 ALL 202330-0505-2 2-20

20-032 ALL

(SEE NOTE) 202410-0505-1 2-20

20-032 ALL 202410-0505-2 2-20

20-032 ALL 202410-0505-3 2-20

20-032 ALL 202430-0505-1 2-20

20-032 ALL 202430-0505-2 2-20

20-032 ALL

(SEE NOTE) 202510-0505-1 2-20

20-032 ALL 202510-0505-2 2-20

20-032 ALL 202510-0505-3 2-20

20-032 ALL 202530-0505-1 2-20

20-032 ALL 202530-0505-2 2-20

20-032 ALL 202610-0505-1 2-20

20-032 ALL 202610-0505-2 2-20

20-032 ALL 202610-0505-3 2-20

20-032 ALL 202630-0505-1 2-20

20-032 ALL 202630-0505-2 2-20

20-032 ALL 202630-0505-3 2-20

20-032 ALL 202630-0505-4 2-20

20-032 ALL 203110-0505-1 2-20

20-032 ALL 203130-0505-1 2-20

20-032 ALL 203150-0505-1 2-20

20-032 ALL 203150-0505-2 2-20

20-032 ALL 203150-0505-3 2-20

20-032 ALL 203340-0505-1 2-20

20-032 ALL 204110-0505-1 2-20

20-032 PRE 2434 204130-0505-1 2-20

20-032 POST 2434 204130-0505-2 2-20

20-032 ALL 204150-0505-1 2-20

20-032 GE 204330-0505-1 2-20

20-032 PW 204330-0505-2 2-20

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-4 Page 3 SERVICE INFORMATION LETTER (SIL) - CROSS REFERENCE LIST

S.I.L MPD APPLICABILITY TASK NUMBER SECTION

20-032 ALL 204350-0505-1 2-20

20-032 ALL 204510-0505-1 2-20

20-032 ALL 204530-0505-1 2-20

20-032 ALL 204710-0505-1 2-20

20-032 ALL 204730-0505-1 2-20

20-032 ALL 205120-0505-1 2-20

20-032 ALL 205120-0505-2 2-20

20-032 B2 205130-0505-1 2-20

20-032 B4 205130-0505-2 2-20

20-032 ALL 205230-0505-1 2-20

20-032 ALL 205230-0505-2 2-20

20-032 ALL 205240-0505-1 2-20

20-032 ALL 205240-0505-2 2-20

20-032 ALL 205300-0505-1 2-20

20-032 ALL 205410-0505-1 2-20

20-032 ALL 205410-0505-2 2-20

20-032 ALL 205420-0505-1 2-20

20-032 ALL 205420-0505-2 2-20

20-032 ALL 205430-0505-1 2-20

20-032 ALL 205430-0505-2 2-20

20-032 ALL 205500-0505-1 2-20

20-032 ALL 205500-0505-2 2-20

20-032 ALL 205710-0505-1 2-20

20-032 ALL 205710-0505-2 2-20

20-032 ALL 205720-0505-1 2-20

20-032 ALL 205720-0505-2 2-20

20-032 ALL 205750-0505-1 2-20

20-032 ALL 205770-0505-1 2-20

20-032 ALL 205810-0505-1 2-20

20-032 ALL 205810-0505-2 2-20

20-032 ALL 205910-0505-1 2-20

20-032 ALL 207110-0505-1 2-20

20-032 ALL 207310-0505-1 2-20

21-0148 ALL 212200-0505-5 2-21

21-017 FWD-FACE

PRE 05119

PRE 04770

(21-0112) 212100-0505-1 2-21

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-4 Page 4 SERVICE INFORMATION LETTER (SIL) - CROSS REFERENCE LIST

S.I.L MPD APPLICABILITY TASK NUMBER SECTION

24-025 ALL 243211-0503-1 2-24

25-085 ALL 252331-0502-1 2-25

26-015 POST 02672

(26-0036) 261112-0505-1 2-26

26-015 PRE 02672

(26-0036) 261112-0505-2 2-26

26-015 C4

IN CARGO CONFIG

F4 261911-0505-1 2-26

26-018 POST 00854

(26-0011)

OR

POST 02503

(26-0030)

OR

POST 06335

(26-0049) 212200-0505-4 2-21

27-020 PRE 02701

(27-0126)

KRUG.FLAP 278149-0505-1 2-27

27-022 ALL ZL-500-0402-2 4-ZL

27-063 ALL 275126-0505-1 2-27

27-076 ALL 275126-0502-2 2-27

27-077 PRE 07602

(57-0160) 278141-0502-1 2-27

27-081 POST 10796 275126-0505-2 2-27

27-081 PRE 10796

(27-0186) 275126-0505-3 2-27

27-081 POST 02628

(27-0136) 278124-0505-1 2-27

27-081 PRE 02628

(27-0136) 278124-0505-3 2-27

27-087 PRE 12026

(27-0192) 271412-0502-1 2-27

27-087 PRE 12026

(27-0192) 272411-0502-1 2-27

27-087 PRE 12026

(27-0192) 273411-0502-1 2-27

27-102 ALL ZL-310-0403-1 4-ZL

27-112 KRUEGER FLAP 278149-0504-1 2-27

28-079 B4 281100-0503-1 2-28

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-4 Page 5 SERVICE INFORMATION LETTER (SIL) - CROSS REFERENCE LIST

S.I.L MPD APPLICABILITY TASK NUMBER SECTION

C4

F4

28-079 B2 281100-0503-2 2-28

28-079 B4

C4

F4

CENTER TANK

NON-USAGE 281100-0503-3 2-28

28-079 ALL 281100-0505-1 2-28

29-034 ALL 291000-0503-5 2-29

29-052 POST 10720

(29-0105)

PRE 11767

(29-0112)

OR

POST 10720

(29-0105)

PRE 11768

(09-0113) 291133-0503-4 2-29

29-081 ALL 291000-0503-5 2-29

32-038 PRE 06329

(32-0377) 321124-0504-1 2-32

32-055 POST 02328

(32-0207)

PRE 11220

(32-0416) 322200-0502-1 2-32

32-055 POST 02328

(32-0207)

POST 11220

(32-0416) 322200-0505-1 2-32

32-111 ALL 321112-0505-3 2-32

34-005 PRE 12009

(34-0159) 342538-0504-1 2-34

34-055 DELCO UNIT 342500-0504-1 2-34

34-084 ALL 341100-0505-1 2-34

34-099 ALL 344200-0503-2 2-34

35-003 ALL 352000-0504-1 2-35

36-023 GE 361116-0502-1 2-36

36-026 GARRETT

P/N 123894-1

123894-2

123940-1 361113-0504-1 2-36

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-4 Page 6 SERVICE INFORMATION LETTER (SIL) - CROSS REFERENCE LIST

S.I.L MPD APPLICABILITY TASK NUMBER SECTION

36-026 GARRETT

P/N 123894-1

123894-2

123940-1

(UP TO S/N1380) 361113-0504-2 2-36

38-013 RECIRC

TOILETS 383100-0502-1 2-38

38-013 ALL 520000-0502-2 2-52

49-056 ALL 493000-0703-3 2-49

52-029 ALL 521022-0505-1 2-52

52-030 PRE 05262 521131-0505-1 2-52

52-043 POST 08357

(52-0148) 527300-0503-2 2-52

52-043 POST 08357

(52-0148) 527300-0503-3 2-52

53-030 ALL 531200-0603-1 3-53

53-030 ALL 538589-0603-1 3-53

53-030 ALL 538709-0603-1 3-53

53-041 ALL 538031-0603-1 3-53

53-043 ALL 534700-0502-1 2-53

53-060 ALL 513000-0502-1 2-51

53-060 ALL 513000-0502-4 2-51

53-061 ALL 538121-0603-1 3-53

54-019 PRE 02434 ZL-410-0403-2 4-ZL

54-019 POST 02434 ZL-410-0403-4 4-ZL

55-013 ALL 558085-0603-1 3-55

55-019 POST 04242 553645-0505-1 2-55

55-023 ALL 555100-0503-1 2-55

55-023 ALL 555200-0503-1 2-55

55-023 ALL 555300-0503-1 2-55

55-023 ALL 555400-0503-1 2-55

55-033 ALL 558041-0603-1 3-55

56-009 ALL 561200-0505-1 2-56

56-011 PRE 07864 561100-0502-1 2-56

56-011 ALL

NOTE 561100-0502-2 2-56

56-017 ALL 561000-0502-1 2-56

56-017 ALL 561100-0502-3 2-56

56-017 ALL 561200-0502-1 2-56

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-4 Page 7 SERVICE INFORMATION LETTER (SIL) - CROSS REFERENCE LIST

S.I.L MPD APPLICABILITY TASK NUMBER SECTION

73-007 PW 731200-0811-1 2-73

73-011 GE 731200-0801-1 2-73

76-015 GE 761131-0802-1 2-76

SUN 192 GE 241111-0504-1 2-24

SUN 192 PW 241111-0504-2 2-24

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 1 

# APPENDIX 2-5

MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

521101-C602-1 521101-0602-1 ALL

EXCL. F4

521101-C602-1 ZL-830-0402-1 ALL

EXCL. F4

521101-C602-1 ZL-830-0402-3 F4

521101-C602-1 ZL-830-0403-3 F4

521110-C602-1 521110-0602-1 F4

521110-C602-1 ZL-830-0402-1 ALL

EXCL. F4

521110-C602-1 ZL-830-0402-3 F4

521110-C602-1 ZL-830-0403-3 F4

521202-C603-1 521202-0603-1 ALL

521210-C602-1 521210-0602-1 ALL

EXCL. F4

521210-C602-1 ZL-830-0402-1 ALL

EXCL. F4

521210-C602-1 ZL-830-0402-3 F4

521210-C602-1 ZL-830-0403-3 F4

521301-C602-1 521801-0602-1 ALL

EXCL. F4

521301-C602-1 ZL-830-0402-1 ALL

EXCL. F4

521301-C602-1 ZL-830-0402-3 F4

521301-C602-1 ZL-830-0403-3 F4

521403-C603-1 521403-0603-1 ALL

521803-C603-1 521803-0603-1 ALL

522201-C602-1 522201-0602-1 ALL

522201-C602-1 ZL-830-0402-1 ALL

EXCL. F4

522201-C602-1 ZL-830-0402-3 F4

522201-C602-1 ZL-830-0403-3 F4

522601-C603-1 522601-0603-1 ALL

523101-C602-1 523309-0602-1 ALL

523101-C602-1 ZL-810-0402-1 ALL

523201-C602-1 523715-0602-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 2 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

523201-C602-1 ZL-810-0402-2 ALL

523401-C602-1 523717-0602-1 ALL

523401-C602-1 ZL-810-0402-3 ALL

523601-C602-1 523601-0602-1 C4

F4

MSN 256

523601-C602-1 ZL-830-0402-2 C4

F4

MSN 256

523715 523715-0602-1 ALL

528021-C603-1 528021-0603-1 ALL

528023-C603-1 528023-0603-1 C4

F4

MSN 256

530905 491200-0703-1 ALL

530907 491200-0703-1 ALL

531140-C603-1 ZL-210-0403-3 ALL

531150-C603-1 531150-0603-1 ALL

531150-C603-1 ZL-120-0403-4 ALL

531220-C603-A 531220-0603-1 ALL

531220-C603-B 531220-0603-1 ALL

531313-C603-1 531313-0603-1 ALL

531330-C603-1 ZL-130-0413-1 TOILET K

531330-C603-1 ZL-130-0413-2 TOILETS H,K,L,M

531411-C603-A 531411-0603-1 ALL

531411-C603-B 531411-0603-1 ALL

531420-C603-1 ZL-130-0403-3 ALL

EXCEPT

F4,C4

531420-C603-1 ZL-130-0403-4 C4

F4

NOTE

531430-C603-1 ZL-130-0403-4 C4

F4

NOTE

531440-C603-1 ZL-130-0403-5 ALL

531580-C603-1 ZL-140-0403-2 B2

531580-C603-1 ZL-140-0403-3 B4

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 3 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

531583-C603-1 ZL-140-0403-5 ALL

531586-C603-1 ZL-140-0403-6 B4

C4

F4

531590-C603-1 ZL-140-0403-8 PRE 03378

(29-0077)

531590-C603-1 ZL-140-0413-1 POST 03378

(29-0077)

531593-C603-1 ZL-140-0403-9 ALL

531605-C604-A 531605-0604-1 ALL

531605-C604-B 531605-0604-1 ALL

531610-C603-1 ZL-150-0403-3 ALL

EXCL. F4

531620-C603-1 ZL-150-0403-4 C4

F4

NOTE

531630-C603-1 ZL-150-0403-5 ALL

531701-C603-1 531701-0603-1 ALL

531720-C603-1 531720-0603-1 ALL

531730-C603-1 ZL-160-0403-3 ALL

EXCL. F4

531730-C603-1 ZL-160-0403-4 C4

F4

NOTE

531750-C603-1 ZL-160-0403-5 ALL

531815-C602-2 531815-0602-2 ALL

531815-C603-A 531815-0603-1 ALL

531815-C603-B 531815-0603-1 ALL

531830-C603-1 ZL-170-0403-2 ALL

531931-C603-1 531931-0603-1 ALL

531940-C602-1 ZL-300-0402-1 ALL

531940-C602-1 ZL-300-0402-2 ALL

531940-C602-1 ZL-300-0402-3 ALL

531940-C602-1 ZL-300-0402-4 ALL

531940-C603-1 ZL-310-0403-2 ALL

532110-C603-1 ZL-130-0403-8 B2

B4

532120-C603-1 ZL-220-0403-5 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 4 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

EXCL. F4

532130-C603-1 ZL-221-0403-3 F4

533120-C602-1 ZL-100-0402-1 ALL

533130-C602-1 ZL-100-0402-2 POST 02727

OR

POST 03245

533130-C602-1 ZL-100-0402-3 PRE 02727

533140-C602-1 ZL-200-0402-2 POST 02727

OR

POST 03245

533140-C602-1 ZL-200-0402-3 PRE 02727

PRE 03245

533218-C602-1 533218-0602-1 ALL

533230-C603-1 ZL-220-0403-6 ALL

EXCL. F4

533240-C603-1 ZL-220-0403-6 ALL

EXCL. F4

533250-C603-1 ZL-221-0403-4 F4

533260-C603-1 ZL-221-0403-4 F4

533437-C602-1 533437-0602-1 ALL

FROM 0 FC/FH

TO LOV

533614-C602-2 533614-0602-2 ALL

534101-C603-1 ZL-220-0403-9 ALL

EXCL. F4

534110-C603-1 ZL-220-0403-9 ALL

EXCL. F4

534110-C603-1 ZL-230-0403-1 ALL

EXCL. F4

534120-C603-1 ZL-220-0403-9 ALL

EXCL. F4

534120-C603-1 ZL-240-0403-1 ALL

EXCL. F4

534130-C603-1 ZL-220-0403-9 ALL

EXCL. F4

534130-C603-1 ZL-250-0403-1 ALL

EXCL. F4

534140-C603-1 ZL-220-0403-9 ALL

EXCL. F4

534140-C603-1 ZL-260-0403-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 5 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

EXCL. F4

538001-C603-1 538001-0603-1 ALL

538011-C602-1 538011-0602-1 ALL

538013-C602-1 538013-0602-1 B2K,

B2 MSN 049 051

059 AND ON,

B4 C4 F4

538014-C603-1 538014-0603-1 B2K

B4

C4

F4

538015-C603-1 538015-0603-1 B2

538015-C603-2 538015-0603-2 B2K

B4

C4

F4

538021-C602-1 538021-0602-1 ALL

538031-C603-1 538031-0603-1 ALL

538050-C602-1 538050-0603-1 ALL

538051-C602-1 538051-0602-1 ALL

538052-C603-1 538052-0603-1 ALL

538053-C603-1 538053-0603-1 ALL

538071-C602-1 538071-0602-1 ALL

538081-C602-1 538081-0602-1 ALL

538091-C602-1 538091-0602-1 ALL

538102-C603-1 538102-0603-1 MSN 005 AND UP

538111-C603-1 538111-0603-1 ALL

538121-C603-1 538121-0603-1 ALL

538153-C602-1 538153-0602-1 C4

F4

MSN 256

538161-C602-1 538161-0602-1 ALL

538171-C602-1 538171-0602-1 ALL

538173-C603-1 538173-0603-1 ALL

538233-C603-1 538233-0603-1 ALL

538235-C603-1 538235-0603-1 C4

F4

538245-C603-1 538245-0603-1 ALL

538265-C603-1 538265-0603-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 6 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

538295-C603-1 538295-0603-1 POST 08057

(21-0116)

POST 05946

(53-0201)

538325-C603-1 538325-0603-1 ALL

538435-C603-1 538435-0603-1 ALL

538537-C603-1 538537-0603-1 ALL

538547-C603-1 538547-0603-1 ALL

538553-C603-1 538553-0603-1 ALL

538555-C603-1 538555-0603-1 ALL

538557-C603-1 538557-0603-1 ALL

538587-C603-1 538587-0603-1 ALL

538589-C603-1 538589-0603-1 ALL

538593-C603-1 538593-0603-1 ALL

538617-C603-1 538617-0603-1 ALL

538679-C603-1 538679-0603-1 C4

F4

MSN 256

538691-C603-1 538691-0603-1 C4

F4

MSN 256

538693-C603-1 538693-0603-1 C4

F4

538709-C603-1 538709-0603-1 ALL

538769-C603-1 538769-0603-1 ALL

538779-C603-1 538779-0603-1 ALL

538789-C603-1 538789-0603-1 ALL

538791-C603-1 538791-0603-1 ALL

538829-C603-1 538829-0603-1 ALL

538829-C603-1 ZL-310-0403-3 ALL

538839-C603-1 538839-0603-1 ALL

543101-C602-1 548031-0603-1 ALL

543101-C602-1 ZL-400-0402-1 ALL

544200-C603-1 544200-0603-1 ALL

544200-C603-2 544200-0603-2 ALL

548021-C603-1 548021-0603-1 ALL

548023-C603-1 548023-0603-1 ALL

548031-C603-1 548031-0603-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 7 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

548041-C603-1 548041-0603-1 PRE 03521

(54-0059)

PRE 04530

(54-0058)

548041-C603-2 548041-0603-2 POST 03521

(54-0059)

OR

POST 04530

(54-0058)

548051-C603-1 548051-0603-1 POST 02434

PRE 10262

PRE 10263

(54-0078)

548051-C603-2 548051-0603-2 POST 02434

PRE 10262

POST 10263

(54-0078)

548051-C603-3 548051-0603-3 POST 02434

POST 10262

551001-C602-1 551001-0602-1 B2

551001-C602-1 551001-0602-2 B4-100

551001-C602-1 551001-0602-3 B4-200

C4

F4

551029-C603-1 551029-0603-1 B2

551029-C603-1 551029-0603-2 B4-100

551029-C603-1 551029-0603-3 B4-200

C4

F4

551101-C603-1 ZL-310-0403-2 ALL

551101-C603-1 ZL-310-0403-3 ALL

551110-C603-1 ZL-310-0403-3 ALL

551120-C603-1 ZL-330-0403-1 ALL

551130-C603-1 ZL-330-0403-1 ALL

551301-C603-1 ZL-330-0403-1 ALL

552004-C603-1 552004-0603-1 ALL

553101-C603-1 ZL-320-0403-2 ALL

558011-C603-1 558011-0603-1 ALL

558021-C603-1 558021-0603-1 ALL

558041-C603-1 558041-0603-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 8 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

558061-C603-1 558061-0603-1 ALL

558065-C603-1 558065-0603-1 ALL

558081-C603-1 558081-0603-1 ALL

558085-C603-A 558085-0603-1 ALL

558085-C603-B 558085-0603-1 ALL

558089-C603-1 558089-0603-1 ALL

558193-C603-1 558193-0603-1 ALL

558215-C603-1 558215-0603-1 ALL

571100-C603-1 571100-0603-1 ALL

571103-C604-1 571103-0604-1 B2

571103-C604-1 571103-0604-2 B4-100

571103-C604-1 571103-0604-3 B4-200

C4

F4

571103-C604-1 571105-0604-1 B2

571103-C604-1 571105-0604-2 B4-100

571103-C604-1 571105-0604-3 B4-200

C4

F4

571105-C604-1 571105-0604-1 B2

571105-C604-1 571105-0604-2 B4-100

571105-C604-1 571105-0604-3 B4-200

C4

F4

571173-C603-1 571173-0603-1 ALL

571174-C603-1 571174-0603-1 ALL

571180-C603-1 ZL-540-0403-1 ALL

571180-C603-1 ZL-550-0403-1 ALL

571185-C603-1 ZL-540-0403-1 ALL

571185-C603-1 ZL-550-0403-1 ALL

571190-C603-1 ZL-540-0403-1 ALL

571190-C603-1 ZL-550-0403-1 ALL

572091-C604-1 572091-0604-1 ALL

572091 572091-0604-1 ALL

572095-C604-1 572095-0604-1 ALL

572095 572095-0604-1 ALL

572099-C604-1 572099-0604-1 ALL

572099 572099-0604-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 9 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

572103-C604-1 572103-0604-1 ALL

572103 572103-0604-1 ALL

572105-C604-1 572105-0604-1 ALL

572105 572105-0604-1 ALL

572109-C604-1 572109-0604-1 ALL

572109 572109-0604-1 ALL

572111-C604-1 572111-0604-1 ALL

572111 572111-0604-1 ALL

572113-C604-1 572113-0604-1 ALL

572113 572113-0604-1 ALL

572115-C604-1 572115-0604-1 ALL

572115 572115-0604-1 ALL

572117-C604-1 572117-0604-1 ALL

572117 572117-0604-1 ALL

572119-C604-1 572119-0604-1 ALL

572119 572119-0604-1 ALL

572121-C604-1 572121-0604-1 ALL

572121 572121-0604-1 ALL

572127-C604-1 572127-0604-1 ALL

572127 572127-0604-1 ALL

572129-C604-1 572129-0604-1 ALL

572129 572129-0604-1 ALL

572131-C604-1 572131-0604-1 ALL

572131 572131-0604-1 ALL

572199-C603-1 572199-0603-1 ALL

572201-C603-1 ZL-570-0403-1 ALL

572201-C603-1 ZL-570-0403-2 ALL

572210-C603-1 ZL-570-0403-2 ALL

572210-C603-1 ZL-580-0403-1 ALL

572210-C603-1 ZL-590-0403-1 ALL

572220-C603-1 ZL-570-0403-2 ALL

572220-C603-1 ZL-590-0403-1 ALL

572401-C603-1 ZL-530-0403-2 ALL

573301-C602-1 ZL-500-0402-1 ALL

573301-C602-1 ZL-500-0402-2 ALL

573301-C602-1 ZL-570-0403-2 ALL

573302-C602-1 ZL-500-0402-3 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-5 Page 10 MRB REPORT / MPD - CROSS REFERENCE LIST

MRB

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

573310-C603-1 ZL-540-0403-1 ALL

573310-C603-1 ZL-550-0403-1 ALL

573320-C603-1 ZL-540-0403-1 ALL

573320-C603-1 ZL-550-0403-1 ALL

573330-C603-1 ZL-500-0402-2 ALL

573330-C603-1 ZL-540-0403-1 ALL

573330-C603-1 ZL-550-0403-1 ALL

573401-C602-1 ZL-500-0402-2 ALL

574120-C603-1 ZL-510-0403-3 ALL

575010-C603-1 575010-0603-1 ALL

575082-C604-1 575082-0604-1 ALL

578011-C602-1 578011-0602-1 ALL

578013-C603-1 578013-0603-1 ALL

578013-C603-1 ZL-510-0403-2 ALL

578013-C603-1 ZL-520-0403-2 ALL

578013-C603-1 ZL-520-0403-3 ALL

578021-C602-1 578021-0602-1 ALL

578023-C603-1 578023-0603-1 ALL

578031-C603-1 578031-0603-1 KRUEGER FLAP

578101-C603-1 578101-0603-1 ALL

578255-C603-1 578255-0603-1 ALL

578255-C603-1 ZL-500-0402-2 ALL

578261-C603-1 578261-0603-1 ALL

578261-C603-1 ZL-500-0402-2 ALL

578265-C603-1 578265-0603-1 POST 5132

578271-C603-1 578271-0603-1 ALL

578271-C603-1 ZL-500-0402-2 ALL

578281-C603-1 578281-0603-1 ALL

578281-C603-1 ZL-500-0402-2 ALL

578301-C603-1 578301-0603-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 1 

# APPENDIX 2-6

ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

523301-01-1 523301-0602-1 PRE 02295

FROM 0 FC/FH

TO LOV

523301-01-1 523301-0602-2 POST 02295

FROM 0 FC/FH

TO LOV

523303-01-1 523303-0603-1 ALL

FROM 0 FC/FH

TO LOV

523315-01-1 523315-0603-1 C4

F4

FROM 0 FC/FH

TO LOV

523317-01-1 523317-0603-1 C4

F4

FROM 0 FC/FH

TO LOV

523317-01-1 523317-0603-2 POST 06208

MSN 256

FROM 0 FC/FH

TO LOV

523701-01-1 523701-0602-1 ALL

FROM 0 FC/FH

TO 40000 FC

523701-01-2 523701-0602-2 ALL

FROM 40000 FC

TO LOV

523719-01-1 523719-0602-1 ALL

FROM 0 FC/FH

TO 40000 FC

523719-01-1 523719-0602-2 ALL

FROM 40000 FC

TO LOV

526101-01-1 526101-0602-1 B2

PRE 05134

FROM 0 FC/FH

TO LOV

526101-01-1 526101-0602-2 B4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 2 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

PRE 05134

FROM 0 FC/FH

TO LOV

526305-01-1 526305-0606-1 B4-2C

POST 6208

C4

F4

FROM 0 FC/FH

TO 34000 FC

526305-01-2 526305-0606-2 B4-2C

POST 6208

C4

F4

FROM 34000 FC

TO LOV

526305-02-1 526305-0606-3 B4-2C

POST 6208

C4

F4

FROM 0 FC/FH

TO 34000 FC

526305-02-2 526305-0606-4 B4-2C

POST 6208

C4

F4

FROM 34000 FC

TO LOV

530407-01-1 530407-0603-1 B2

FROM 0 FC/FH

TO 48000 FC

530407-01-2 530407-0603-2 B2

FROM 48000 FC

TO LOV

530407-01-3 530407-0603-3 B4-100

FROM 40000 FC

TO LOV

530407-01-4 530407-0603-5 B4-200

C4

F4

FROM 34000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 3 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

530407-01-5 530407-0603-4 B4-100

FROM 0 FC/FH

TO 40000 FC

530407-01-6 530407-0603-6 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

531107-01-1 531107-0602-1 B2

FROM 45000 FC

TO LOV

531107-01-2 531107-0602-2 B4-100

FROM 40000 FC

TO LOV

531107-01-3 531107-0602-3 B4-200

C4

F4

FROM 34000 FC

TO LOV

531121-01-1 531121-0602-1 ALL

FROM 0 FC/FH

TO LOV

531125-01-1 531125-0602-1 ALL

FROM 0 FC/FH

TO LOV

531137-01-1 531137-0602-1 ALL

FROM 0 FC/FH

TO LOV

531208-01-1 531208-0602-1 B2

POST 12662

OR

B4-100

POST 12662

OR

B4-200

POST 12662

FROM 0 FC/FH

TO LOV

531208-01-2 531208-0602-2 C4

POST 12662

OR

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 4 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4-100

POST 12662

FROM 0 FC/FH

TO LOV

531214-01-1 531214-0602-1 ALL

FROM 0 FC/FH

TO LOV

531215-01-1 531215-0602-1 ALL

FROM 0 FC/FH

TO LOV

531321-01-1 531321-0602-1 B2

FROM 0 FC/FH

TO 42500 FC

531321-01-2 531321-0602-2 B4-100

FROM 0 FC/FH

TO 42500 FC

531321-01-3 531321-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO 42500 FC

531411-01-1 531411-0603-1 ALL

531411-01-1 531411-0604-1 ALL

FROM 0 FC/FH

TO LOV

531411-02-1 531411-0604-1 ALL

FROM 0 FC/FH

TO LOV

531531-01-1 531531-0602-1 B2

FROM 0 FC/FH

TO LOV

531531-01-2 531531-0602-2 B4-100

FROM 0 FC/FH

TO LOV

531531-01-3 531531-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

531548-01-1 531548-0603-1 B2

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 5 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

531548-01-2 531548-0603-2 B4-100

FROM 0 FC/FH

TO LOV

531548-01-3 531548-0603-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

531548-02-1 531548-0603-4 B2

FROM 0 FC/FH

TO LOV

531548-02-2 531548-0603-5 B4-100

FROM 0 FC/FH

TO LOV

531548-02-3 531548-0603-6 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

531572-01-1 531572-0602-1 IF VHF 3

ANTENNA

INSTALLED

FROM 0 FC/FH

TO LOV

531573-01-4 531573-0602-1 ALL

FROM 0 FC/FH

TO LOV

531605-01-1 531605-0604-4 B2

FROM 0 FC/FH

TO LOV

531605-01-2 531605-0604-5 B4-100

FROM 0 FC/FH

TO LOV

531605-01-3 531605-0604-6 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

531711-01-1 531711-0602-1 ALL

FROM 0 FC/FH

TO LOV

531815-01-1 531815-0604-4 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 6 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

531816-01-1 531816-0603-1 ALL

FROM 0 FC/FH

TO LOV

531921-01-1 531921-0603-1 POST 02476

(53-0121)

FROM 0 FC/FH

TO LOV

531921-02-1 531921-0603-2 POST 02476

(53-0121)

FROM 0 FC/FH

TO LOV

531925-01-1 531925-0603-1 B2

FROM 0 FC/FH

TO LOV

531925-01-2 531925-0603-2 B4-100

FROM 0 FC/FH

TO LOV

531925-01-3 531925-0603-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533209-01-1 533209-0602-1 ALL

FROM 0 FC/FH

TO LOV

533331-01-1 533331-0602-1 C4

F4

POST 06208

B4-2C

FROM 0 FC/FH

TO LOV

533331-01-1 533331-0603-1 POST 06208

MSN 256

FROM 0 FC/FH

TO LOV

533339-01-1 533339-0603-1 C4

F4

POST 06208

MSN 256

B4-2C

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 7 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/F

TO LOV

533343-01-1 533343-0603-1 C4

F4

POST 06208

MSN 256

B4-2C

FROM 0 FC/F

TO LOV

533407-01-1 533407-0602-1 ALL

FROM 0 FC/FH

TO LOV

533415-01-1 533415-0602-1 B2

FROM 0 FC/FH

TO LOV

533415-01-2 533415-0602-2 B4-100

FROM 0 FC/FH

TO LOV

533415-01-3 533415-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533435-01-1 533435-0602-1 B2

FROM 0 FC/FH

TO LOV

533435-01-2 533435-0602-2 B4-100

FROM 0 FC/FH

TO LOV

533435-01-3 533435-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533437-01-1 533437-0602-4 ALL

FROM 0 FC/FH

TO LOV

533517-01-1 533517-0602-1 B2

POST 01288

FROM 0 FC/FH

TO LOV

533517-01-2 533517-0602-4 B4-100

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 8 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

POST 01288

FROM 0 FC/FH

TO LOV

533517-01-3 533517-0602-5 B4-200

C4

F4

POST 01288

FROM 0 FC/FH

TO LOV

533605-01-1 533605-0602-1 B2

FROM 0 FC/FH

TO LOV

533605-01-2 533605-0602-2 B4-100

FROM 0 FC/FH

TO LOV

533605-01-3 533605-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533614-01-1 533614-0602-1 B2

FROM 0 FC/FH

TO LOV

533614-01-2 533614-0602-3 B4-100

FROM 0 FC/FH

TO LOV

533614-01-3 533614-0602-4 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533615-01-1 533615-0603-1 B2

FROM 0 FC/FH

TO LOV

533615-01-2 533615-0603-2 B4-100

FROM 0 FC/FH

TO LOV

533615-01-3 533615-0603-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 9 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

533616-01-1 533616-0603-1 B2

FROM 0 FC/FH

TO LOV

533616-01-2 533616-0603-2 B4-100

FROM 0 FC/FH

TO LOV

533616-01-3 533616-0603-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533727-01-1 533727-0602-1 B2

FROM 0 FC/FH

TO LOV

533727-01-1 533727-0602-4 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533727-01-2 533727-0602-3 B4-100

FROM 0 FC/FH

TO LOV

533729-01-1 533729-0602-1 B2

FROM 0 FC/FH

TO LOV

533729-01-2 533729-0602-3 B4-100

FROM 0 FC/FH

TO LOV

533729-01-3 533729-0602-4 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

533821-01-1 533821-0602-1 B2

FROM 0 FC/FH

TO LOV

533821-01-2 533821-0602-2 B4-100

FROM 0 FC/FH

TO LOV

533821-01-3 533821-0602-3 B4-200

C4

F4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 10 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

534705-01-1 534705-0604-4 ALL

FROM 0 FC/FH

TO LOV

534901-01-1 534901-0603-1 B2

FROM 0 FC/FH

TO LOV

534901-01-2 534901-0603-2 B4-100

FROM 0 FC/FH

TO LOV

534901-01-3 534901-0603-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536101-01-1 536101-0606-2 B2

FROM 0 FC/FH

TO 48000 FC

536101-01-2 536101-0606-3 B2

FROM 48000 FC

TO LOV

536101-01-3 536101-0606-4 B4-100

FROM 0 FC/FH

TO 40000 FC

536101-01-4 536101-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536101-01-5 536101-0606-6 B4-100

FROM 40000 FC

TO LOV

536101-01-6 536101-0606-7 B4-200

C4

F4

FROM 34000 FC

TO LOV

536101-02-1 536101-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536101-02-2 536101-0607-1 B2

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 11 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 48000 FC

TO LOV

536101-02-3 536101-0607-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536101-02-4 536101-0607-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536101-02-5 536101-0607-4 B4-100

FROM 40000 FC

TO LOV

536101-02-6 536101-0607-5 B4-200

C4

F4

FROM 34000 FC

TO LOV

536110-01-1 536110-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536110-01-2 536110-0606-3 B2

FROM 48000 FC

TO LOV

536110-01-3 536110-0606-4 B4-100

FROM 0 FC/FH

TO 40000 FC

536110-01-4 536110-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536110-01-5 536110-0606-6 B4-100

FROM 40000 FC

TO LOV

536110-01-6 536110-0606-7 B4-200

C4

F4

FROM 34000 FC

TO LOV

536110-02-1 536110-0606-2 B2

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 12 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 48000 FC

536110-02-2 536110-0607-1 B2

FROM 48000 FC

TO LOV

536110-02-3 536110-0607-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536110-02-4 536110-0607-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536110-02-5 536110-0607-4 B4-100

FROM 40000 FC

TO LOV

536110-02-6 536110-0607-5 B4-200

C4

F4

FROM 34000 FC

TO LOV

536111-01-1 536111-0606-1 PRE 03632

FROM 0 FC/FH

TO LOV

536112-01-1 536112-0606-1 MSN 003 TO 156

536112-01-1 536112-0606-2 MSN 157 TO 305

536112-01-1 536113-0606-1 ALL

FROM 0 FC/FH

TO LOV

536114-01-1 536114-0606-1 ALL

FROM 0 FC/FH

TO LOV

536114-01-2 536114-0606-2 ALL

FROM 0 FC/FH

TO LOV

536202-01-10 536202-0607-4 B2

POST 01282

FROM 48000 FC

TO LOV

536202-01-11 536202-0606-6 B4-100

POST 01282

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 13 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 40000 FC

536202-01-12 536202-0607-5 B4-100

POST 01282

FROM 40000 FC

TO LOV

536202-01-13 536202-0607-6 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV

536202-01-14 536202-0607-7 B4-100

PRE 01115

FROM 40000 FC

TO LOV

536202-01-15 536202-0607-8 B4-200

C4

F4

PRE 01115

FROM 34000 FC

TO LOV

536202-01-16 536202-0607-9 B4-100

POST 01115

PRE 01282

FROM 40000 FC

TO LOV

536202-01-17 536202-0608-1 B4-200

C4

F4

POST 01115

PRE 01282

FROM 34000 FC

TO LOV

536202-01-1 536202-0606-1 B2

PRE 01115

FROM 0 FC/FH

T0 48000 FC

536202-01-2 536202-0606-4 B4-100

PRE 01115

FROM 0 FC/FH

TO 40000 FC

536202-01-3 536202-0606-7 B4-200

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 14 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

PRE 01115

FROM 0 FC/FH

TO 34000 FC

536202-01-4 536202-0607-1 B2

PRE 01115

FROM 48000 FC

TO LOV

536202-01-5 536202-0606-2 B2

POST 01115

PRE 01282

FROM 0 FC/FH

TO 48000 FC

536202-01-6 536202-0606-5 B4-100

POST 01115

PRE 01282

FROM 0 FC/FH

TO 40000 FC

536202-01-7 536202-0607-2 B4-200

C4

F4

POST 01115

PRE 01282

FROM 0 FC/FH

TO 34000 FC

536202-01-8 536202-0607-3 B2

POST 01115

PRE 01282

FROM 48000 FC

TO LOV

536202-01-9 536202-0606-3 B2

POST 01282

FROM 0 FC/FH

TO 48000 FC

536202-02-10 536202-0608-5 B2

POST 01282

FROM 48000 FC

TO LOV

536202-02-11 536203-0606-4 B4-100

POST 01282

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 15 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 40000 FC

536202-02-12 536202-0608-6 B4-100

POST 01282

FROM 40000 FC

TO LOV

536202-02-13 536202-0608-7 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV

536202-02-14 536202-0608-8 B4-100

PRE 01115

FROM 40000 FC

TO LOV

536202-02-15 536202-0608-9 B4-200

C4

F4

PRE 01115

FROM 34000 FC

TO LOV

536202-02-16 536202-0609-1 B4-100

POST 01115

PRE 01282

FROM 40000 FC

TO LOV

536202-02-17 536202-0609-2 B4-200

C4

F4

POST 01115

PRE 01282

FROM 34000 FC

TO LOV

536202-02-1 536202-0606-8 B2

PRE 01115

FROM 0 FC/FH

T0 48000 FC

536202-02-2 536203-0606-2 B4-100

PRE 01115

FROM 0 FC/FH

TO 40000 FC

536202-02-3 536203-0606-5 B4-200

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 16 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

PRE 01115

FROM 0 FC/FH

TO 34000 FC

536202-02-4 536202-0608-2 B2

PRE 01115

FROM 48000 FC

TO LOV

536202-02-5 536202-0606-9 B2

POST 01115

PRE 01282

FROM 0 FC/FH

TO 48000 FC

536202-02-6 536203-0606-3 B4-100

POST 01115

PRE 01282

FROM 0 FC/FH

TO 40000 FC

536202-02-7 536202-0608-3 B4-200

C4

F4

POST 01115

PRE 01282

FROM 0 FC/FH

TO 34000 FC

536202-02-8 536202-0608-4 B2

POST 01115

PRE 01282

FROM 48000 FC

TO LOV

536202-02-9 536203-0606-1 B2

POST 01282

FROM 0 FC/FH

TO 48000 FC

536204-01-10 536204-0607-5 B4-100

PRE 01282

FROM 40000 FC

TO LOV

536204-01-11 536204-0607-6 B4-200

C4

F4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 17 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

PRE 01282

FROM 34000 FC

TO LOV

536204-01-1 536204-0606-1 B2

PRE 01282

FROM 0 FC/FH

TO LOV

536204-01-2 536204-0606-3 B4-100

PRE 01282

FROM 0 FC/FH

TO 40000 FC

536204-01-3 536204-0606-5 B4-200

C4

F4

PRE 01282

FROM 0 FC/FH

TO 34000 FC

536204-01-5 536204-0606-2 B2

POST 01282

FROM 0 FC/FH

TO 48000 FC

536204-01-6 536204-0606-4 B4-100

POST 01282

FROM 0 FC/FH

TO LOV

536204-01-7 536204-0607-2 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV

536204-01-9 536204-0607-4 B2

POST 01282

FROM 48000 FC

TO LOV

536204-02-10 536204-0608-2 B4-100

PRE 01282

FROM 40000 FC

TO LOV

536204-02-1 536204-0606-6 B2

PRE 01282

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 18 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 48000 FC

536204-02-2 536204-0606-8 B4-100

PRE 01282

FROM 0 FC/FH

TO 40000 FC

536204-02-3 536204-0608-4 B4-200

C4

F4

PRE 01282

FROM 0 FC/FH

TO LOV

536204-02-3 536214-0606-1 B4-200

C4

F4

PRE 01282

FROM 0 FC/FH

TO 34000 FC

536204-02-4 536204-0607-7 B2

PRE 01282

FROM 48000 FC

TO LOV

536204-02-5 536204-0606-7 B2

POST 01282

FROM 0 FC/FH

TO LOV

536204-02-6 536204-0606-9 B4-100

POST 01282

FROM 0 FC/FH

TO 40000 FC

536204-02-7 536204-0607-8 B4-200

C4

F4

POST 01282

FROM 0 FC/FH

TO LOV

536204-02-8 536204-0607-9 B4-100

POST 01282

FROM 40000 FC

TO LOV

536205-01-1 536205-0606-1 POST 00726

(53-0902)

SERIAL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 19 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

PRE 00600

FROM 0 FC/FH

TO 48000 FC

536205-01-2 536205-0606-2 POST 00726

(53-0902)

RETROFIT

PRE 00600

FROM 0 FC/FH

TO 48000 FC

536205-01-3 536205-0606-3 POST 00726

(53-0902)

PRE 00600

FROM 48000 FC

TO LOV

536205-01-4 536205-0606-4 POST 00600

FROM 0 FC/FH

TO 48000 FC

536205-01-5 536205-0606-5 POST 00600

FROM 48000 FC

TO LOV

536205-02-1 536205-0606-6 POST 00726

(53-0902)

SERIAL

PRE 00600

FROM 0 FC/FH

TO 48000 FC

536205-02-2 536205-0606-7 POST 00726

(53-0902)

RETROFIT

PRE 00600

FROM 0 FC/FH

TO 48000 FC

536205-02-3 536205-0606-8 POST 00726

(53-0902)

PRE 00600

FROM 48000 FC

TO LOV

536205-02-4 536205-0606-9 POST 00600

FROM 0 FC/FH

TO 48000 FC

536205-02-5 536205-0607-1 POST 00600

FROM 48000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 20 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536207-01-1 536207-0606-1 B2

POST 00797

(53-0905)

RETROFIT

FROM 0 FC/FH

TO 48000 FC

536207-01-2 536207-0606-2 B2

POST 00797

(53-0905)

SERIAL

FROM 0 FC/FH

TO 48000 FC

536207-01-3 536207-0606-3 B4-100

POST 00797

(53-0905)

FROM 0 FC/FH

TO 40000 FC

536207-01-4 536207-0606-4 B4-200

C4

F4

POST 00797

(53-0905)

FROM 0 FC/FH

TO 34000 FC

536207-01-5 536207-0606-5 B2

POST 00797

FROM 48000 FC

TO LOV

536207-01-6 536207-0606-6 B4-100

POST 00797

(53-0905)

FROM 40000 FC

TO LOV

536207-01-7 536207-0606-7 B4-200

C4

F4

POST 00797

(53-0905)

FROM 34000 FC

TO LOV

536210-01-1 536210-0606-1 B2

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 21 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO 48000 FC

536210-01-2 536210-0606-2 B2

FROM 48000 FC

TO LOV

536210-01-3 536210-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

536210-01-4 536210-0606-4 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536210-01-5 536210-0606-5 B4-100

FROM 40000 FC

TO LOV

536210-01-6 536210-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

536225-01-1 536225-0606-1 ALL

FROM 0 FC/FH

TO 40000 FC

536225-01-2 536225-0606-2 PRE 01282

FROM 40000 FC

TO LOV

536225-01-3 536225-0606-3 POST 01282

FROM 40000 FC

TO LOV

536225-02-1 536225-0606-4 B2

FROM 0 FC/FH

TO 40000 FC

536225-02-2 536225-0606-5 B4-100

FROM 0 FC/FH

TO 40000 FC

536225-02-3 536225-0606-6 B4-200

C4

F4

FROM 0 FC/FH

TO 40000 FC

536225-02-4 536225-0606-7 PRE 01282

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 22 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 40000 FC

TO LOV

536225-02-5 536225-0606-8 B2

B4-100

POST 01282

FROM 40000 FC

TO LOV

536225-02-8 536225-0606-9 B4-200

C4

F4

POST 01282

FROM 40000 FC

TO LOV

536230-01-1 536230-0606-1 ALL

FROM 0 FC/FH

TO LOV

536231-01-1 536231-0606-1 ALL

FROM 0 FC/FH

TO LOV

536231-02-1 536231-0606-1 ALL

FROM 0 FC/FH

TO LOV

536232-01-1 536232-0606-1 ALL

FROM 0 FC/FH

TO LOV

536233-01-1 536233-0606-1 ALL

FROM 0 FC/FH

TO LOV

536234-01-1 536234-0606-1 PRE 03632

FROM 0 FC/FH

TO LOV

536234-01-2 536234-0606-2 POST 03632

FROM 0 FC/FH

TO LOV

536235-01-1 536235-0606-1 B2

FROM 0 FC/FH

TO LOV

536235-01-2 536235-0606-2 B4-100

FROM 0 FC/FH

TO LOV

536235-01-3 536235-0606-3 B4-200

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 23 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

FROM 0 FC/FH

TO LOV

536301-01-2 536301-0606-2 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC

536301-01-3 536301-0606-3 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000 FC

536301-01-4 536301-0606-4 B2

POST 02611

FROM 48000 FC

TO LOV

536301-01-5 536301-0606-5 B4-100

POST 02611

FROM 40000 FC

TO LOV

536301-01-6 536301-0606-6 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV

536301-02-1 536301-0606-1 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC

536301-02-1 536301-0607-1 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC

536301-02-2 536301-0607-2 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC

536301-02-3 536301-0607-3 B4-200

C4

F4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 24 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

POST 02611

FROM 0 FC/FH

TO 34000 FC

536301-02-4 536301-0607-4 B2

POST 02611

FROM 48000 FC

TO LOV

536301-02-5 536301-0607-5 B4-100

POST 02611

FROM 40000 FC

TO LOV

536301-02-6 536301-0607-6 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV

536301-03-1 536301-0608-1 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC

536301-03-2 536301-0608-2 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC

536301-03-3 536301-0608-3 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000 FC

536301-03-4 536301-0608-4 B2

POST 02611

FROM 48000 FC

TO LOV

536301-03-5 536301-0608-5 B4-100

POST 02611

FROM 40000 FC

TO LOV

536301-03-6 536301-0608-6 B4-200

C4

F4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 25 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

POST 02611

FROM 34000 FC

TO LOV

536311-01-1 536311-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536311-01-2 536311-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536311-01-3 536311-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536311-02-1 536311-0606-4 B2

FROM 0 FC/FH

TO 48000 FC

536311-02-2 536311-0606-5 B4-100

FROM 0 FC/FH

TO 40000 FC

536311-02-3 536311-0606-6 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536311-02-4 536311-0606-7 B2

FROM 48000 FC

TO LOV

536311-02-5 536311-0606-8 B4-100

FROM 40000 FC

TO LOV

536311-02-6 536311-0606-9 B4-200

C4

F4

FROM 34000 FC

TO LOV

536355-01-1 536355-0606-1 F4

OR

C4

OR

B4-2C

POST 06208

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 26 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

IN CARGO CONFIG

FROM 0 FC/FH

TO LOV

536355-01-1 536355-0606-2 C4

OR

B4-2C

POST 06208

IN PAX CONFIG

FROM 0 FC/FH

TO LOV

536355-02-1 536355-0606-1 F4

OR

C4

OR

B4-2C

POST 06208

IN CARGO CONFIG

FROM 0 FC/FH

TO LOV

536355-02-1 536355-0606-2 C4

OR

B4-2C

POST 06208

IN PAX CONFIG

FROM 0 FC/FH

TO LOV

536359-01-1 536359-0606-1 F4

POST 06208

FROM 0 FC/FH

TO LOV

536359-01-1 536359-0606-2 C4

OR

B4-2C

POST 06208

FROM 0 FC/FH

TO LOV

536365-01-1 536365-0606-1 C4

POST 02611

FROM 0 FC/FH

TO 34000 FC

536365-01-2 536365-0606-2 C4

POST 02611

FROM 34000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 27 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536367-01-1 536367-0606-1 C4

F4

B4-2C

POST 6208

FROM 0 FC/FH

TO LOW

536367-02-1 536367-0606-2 C4

F4

B4-2C

POST 6208

FROM 0 FC/FH

TO LOW

536369-01-1 536369-0606-1 ALL

FROM 0 FC/FH

TO LOV

536403-01-1 536403-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536403-01-2 536403-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536403-01-3 536403-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536403-01-4 536403-0606-4 B2

FROM 48000 FC

TO LOV

536403-01-5 536403-0606-5 B4-100

FROM 40000 FC

TO LOV

536403-01-6 536403-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

536405-01-1 536405-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536405-01-2 536405-0606-2 B4-100

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 28 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO 40000 FC

536405-01-2 536405-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536405-02-1 536405-0606-4 B2

FROM 0 FC/FH

TO 48000 FC

536405-02-2 536405-0606-6 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536405-02-3 536405-0606-7 B2

POST 00751

(53-0247)

FROM 48000 FC

TO LOV

536405-02-4 536405-0606-8 B4-100

POST 00751

(53-0247)

FROM 40000 FC

TO LOV

536405-02-5 536405-0606-9 B4-200

C4

F4

POST 00751

(53-0247)

FROM 34000 FC

TO LOV

536405-02-6 536405-0606-5 B4-100

FROM 0 FC/FH

TO 40000 FC

536407-01-1 536407-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536407-01-2 536407-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536407-01-3 536407-0606-5 B4-200

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 29 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

FROM 0 FC/FH

TO 34000 FC

536407-02-1 536407-0606-3 B2

FROM 0 FC/FH

TO 48000 FC

536407-02-2 536407-0606-4 B4-100

FROM 0 FC/FH

TO 40000 FC

536407-02-3 536407-0606-6 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536407-02-4 536407-0606-7 B2

FROM 48000 FC

TO LOV

536407-02-5 536407-0606-8 B4-100

FROM 40000 FC

TO LOV

536407-02-6 536407-0606-9 B4-200

C4

F4

FROM 34000 FC

TO LOV

536415-01-1 536415-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536415-01-2 536415-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536415-01-3 536415-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536415-01-4 536415-0606-4 B2

FROM 48000 FC

TO LOV

536415-01-5 536415-0606-5 B4-100

FROM 40000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 30 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536415-01-6 536415-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

536421-01-1 536421-0606-1 B4-100

FROM 0 FC/FH

TO LOV

536421-01-2 536421-0606-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536502-01-1 536502-0603-1 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC

536502-01-2 536502-0603-2 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC

536502-01-3 536502-0603-3 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC

536502-01-4 536502-0603-4 B2

POST 02611

FROM 48000 FC

TO LOV

536502-01-5 536502-0603-5 B4-100

POST 02611

FROM 40000 FC

TO LOV

536502-01-6 536502-0603-6 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 31 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536502-02-1 536502-0604-1 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC

536502-02-2 536502-0604-2 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC

536502-02-3 536502-0604-3 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC

536502-02-4 536502-0604-4 B2

POST 02611

FROM 48000 FC

TO LOV

536502-02-5 536502-0604-5 B4-100

POST 02611

FROM 40000 FC

TO LOV

536502-02-6 536502-0604-6 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV

536502-03-1 536502-0605-1 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC

536502-03-2 536502-0605-2 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC

536502-03-3 536502-0605-3 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 32 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536502-03-4 536502-0605-4 B2

POST 02611

FROM 48000 FC

TO LOV

536502-03-5 536502-0605-5 B4-100

POST 02611

FROM 40000 FC

TO LOV

536502-03-6 536502-0605-6 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV

536502-04-1 536502-0606-1 B2

POST 02611

FROM 0 FC/FH

TO 48000 FC

536502-04-2 536502-0606-2 B4-100

POST 02611

FROM 0 FC/FH

TO 40000 FC

536502-04-3 536502-0606-3 B4-200

C4

F4

POST 02611

FROM 0 FC/FH

TO 34000FC

536502-04-4 536502-0606-4 B2

POST 02611

FROM 48000 FC

TO LOV

536502-04-5 536502-0606-5 B4-100

POST 02611

FROM 40000 FC

TO LOV

536502-04-6 536502-0606-6 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 33 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536503-01-10 536503-0606-6 B4-200

C4

F4

POST 01669

SERIAL

PRE 02626

FROM 0 FC/FH

TO 34000 FC

536503-01-11 536503-0607-2 B4-200

C4

F4

POST 01669

RETROFIT

(53-0061)

FROM 34000 FC

TO LOV

536503-01-12 536503-0607-3 B4-200

C4

F4

POST 01669

SERIAL

PRE 02626

FROM 34000 FC

TO LOV

536503-01-13 536503-0607-4 B4-200

C4

F4

POST 02626

FROM 0 FC/FH

TO LOV

536503-01-1 536503-0606-1 B2

POST 01669

RETROFIT

(53-0061)

FROM 0 FC/FH

TO 48000 FC

536503-01-2 536503-0606-2 B2

POST 01669

SERIAL

FROM 0 FC/FH

TO 48000 FC

536503-01-3 536503-0606-7 B2

FROM 48000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 34 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536503-01-4 536503-0606-3 B4-100

POST 01669

RETROFIT

(53-0061)

FROM 0 FC/FH

TO 40000 FC

536503-01-5 536503-0606-4 B4-100

POST 01669

SERIAL

PRE 02626

FROM 0 FC/FH

TO 40000 FC

536503-01-6 536503-0606-8 B4-100

POST 02626

FROM 40000 FC

TO LOV

536503-01-7 536503-0606-9 B4-100

POST 01669

SERIAL

PRE 02626

FROM 40000 FC

TO LOV

536503-01-8 536503-0607-1 B4-100

POST 01669

RETROFIT

(53-0061)

FROM 40000 FC

TO LOV

536503-01-9 536503-0606-5 B4-200

C4

F4

POST 01669

RETROFIT

(53-0061)

FROM 0 FC/FH

TO 34000 FC

536505-01-1 536505-0606-1 ALL

SB 53-0243

FROM 0 FC/FH

TO LOV

536506-01-10 536506-0607-3 B4-200

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 35 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

PRE 02626

FROM 40000 FC

82000 FH

TO LOV

536506-01-11 536506-0606-6 B4-200

C4

F4

POST 02626

FROM 0 FCFH

TO 40000 FC

82000 FH

536506-01-12 536506-0607-4 B4-200

C4

F4

POST 02626

FROM 40000 FC

82000 FH

TO LOV

536506-01-1 536506-0606-2 B2

PRE 03476

FROM 0 FC/FH

TO 48000 FC

536506-01-2 536506-0606-7 B2

PRE 03476

FROM 48000 FC

TO 53600 FC

57900 FH

536506-01-3 536506-0606-8 B2

PRE 03476

FROM 53600 FC

57900 FH

TO LOV

536506-01-4 536506-0606-3 B2

POST 03476

FROM 0 FC/FH

TO 40000 FC

44400 FH

536506-01-5 536506-0606-9 B2

POST 03476

TO 40000 FC

44400 FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 36 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536506-01-6 536506-0606-4 B4-100

PRE 02626

FROM 0 FC/FH

TO 40000 FC

536506-01-7 536506-0607-1 B4-100

PRE 02626

FROM 40000 FC

TO LOV

536506-01-8 536506-0606-5 B4-200

C4

F4

PRE 02626

FROM 0 FC/FH

TO 34000 FC

536506-01-9 536506-0607-2 B4-200

C4

F4

PRE 02626

FROM 34000 FC

TO 40000 FC

82000-FH

536506-02-1 536506-0607-5 B2

FROM 0 FC/FH

TO LOV

536506-02-2 536506-0607-6 B4-100

FROM 0 FC/FH

TO LOV

536506-02-3 536506-0607-7 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536509-01-1 536509-0606-1 PRE 02626

FROM 0 FC/FH

TO LOV

536510-01-1 536510-0606-1 B4-100

FROM 0 FC/FH

TO 40000 FC

536510-01-2 536510-0606-2 B4-100

FROM 40000 FC

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 37 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536510-01-3 536510-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536510-01-4 536510-0606-4 B4-200

C4

F4

FROM 34000 FC

TO LOV

536510-02-1 536510-0606-5 B4-100

FROM 0 FC/FH

TO LOV

536510-02-2 536510-0606-6 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536511-01-1 536511-0606-1 PRE SB

(53-0282)

FROM 0 FC/FH

TO LOV

536512-01-1 536512-0606-1 ALL

SB 53-0265

FROM 0 FC/FH

TO LOV

536513-01-1 536513-0606-1 ALL

SB 53-0299

FROM 0 FC/FH

TO LOV

536515-01-1 536515-0606-1 ALL

SB 53-0259

FROM 0 FC/FH

TO LOV

536521-01-10 536521-0607-5 B4-200

C4

F4

PRE 02974

FROM 34000 FC

TO LOV

536521-01-11 536521-0606-7 B4-200

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 38 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

POST 02974

FROM 0 FC/FH

TO 34000 FC

536521-01-12 536521-0607-6 B4-200

C4

F4

POST 02974

FROM 34000 FC

TO LOV

536521-01-1 536521-0606-2 B2

PRE 02974

FROM 0 FC/FH

TO 48000 FC

536521-01-2 536521-0607-1 B2

PRE 02974

FROM 48000 FC

TO LOV

536521-01-3 536521-0606-3 B2

POST 02974

FROM 0 FC/FH

TO 48000 FC

536521-01-4 536521-0607-2 B2

POST 02974

FROM 48000 FC

TO LOV

536521-01-5 536521-0606-4 B4-100

PRE 02974

FROM 0 FC/FH

TO 40000 FC

536521-01-6 536521-0607-3 B4-100

PRE 02974

FROM 40000 FC

TO LOV

536521-01-7 536521-0606-5 B4-100

POST 02974

FROM 0 FC/FH

TO 40000 FC

536521-01-8 536521-0607-4 B4-100

POST 02974

FROM 40000 FC

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 39 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536521-01-9 536521-0606-6 B4-200

C4

F4

PRE 02974

FROM 0 FC/FH

TO 34000 FC

536523-01-1 536523-0606-2 B2

FROM 0 FC/FH

TO 48000 FC

536523-01-2 536523-0606-3 B2

FROM 48000 FC

TO LOV

536523-01-3 536523-0606-4 B4-100

FROM 0 FC/FH

TO 40000 FC

536523-01-4 536523-0606-5 B4-100

FROM 40000 FC

TO LOV

536523-01-5 536523-0606-6 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536523-02-1 536523-0606-7 B2

FROM 0 FC/FH

TO 48000 FC

536523-02-2 536523-0606-8 B2

FROM 48000 FC

TO LOV

536523-02-3 536523-0606-9 B4-100

FROM 0 FC/FH

TO 40000 FC

536523-02-4 536523-0607-1 B4-100

FROM 40000 FC

TO LOV

536523-02-5 536523-0607-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536529-01-1 536529-0606-1 ALL

ISB 53-0242

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 40 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

536535-01-1 536535-0606-1 ALL

SB 53-0244

FROM 0 FC/FH

TO LOV

536541-01-1 536541-0606-1 B2

PRE 00317

PRE 08486

(57-0179)

FROM 0 FC/FH

TO LOV

536541-01-2 536541-0606-3 B2

POST 00317

PRE 08486

(57-0179)

FROM 0 FC/FH

TO LOV

536541-01-3 536541-0606-5 B4-100

PRE 10089

(57-0191)

FROM 0 FC/FH

TO LOV

536541-01-4 536541-0606-7 B4-200

C4

F4

PRE 10089

(57-0191)

FROM 0 FC/FH

TO LOV

536541-02-1 536541-0606-2 B2

PRE 00317

POST 08486

(57-0179)

FROM 0 FC/FH

TO LOV

536541-02-3 536541-0606-4 B2

POST 00317

POST 08486

(57-0179)

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 41 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536541-02-5 536541-0606-6 B4-100

POST 10752

(57-0191)

POST 11213

(57-0191)

POST 10089

(57-0191)

FROM 0 FC/FH

TO LOV

536541-02-7 536541-0606-8 B4-200

C4

F4

POST 10089

(57-0191)

POST 11213

(57-0191)

FROM 0 FC/F

TO LOV

536543-01-1 536543-0606-1 PRE 10453

(53-0297)

FROM 0 FC/FH

TO LOV

536544-01-2 536544-0606-1 ALL

SB 53-0252

FROM 0 FC/FH

TO LOV

536545-01-1 536545-0606-1 SB 53-0245

FROM 0 FC/FH

TO LOV

536546-01-1 536546-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536546-01-2 536546-0606-2 B2

FROM 48000 FC

TO LOV

536546-01-3 536546-0606-3 B4-100

FROM 0 FC/FH

TO LOV

536546-01-4 536546-0606-4 B4-200

C4

F4

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 42 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536547-01-1 536547-0606-1 B2

FROM 0 FC/FH

TO LOV

536548-01-1 536548-0606-1 SB 53-0310

FROM 0 FC/FH

TO LOV

536549-01-1 536549-0606-1 SB 53-0304

FROM 0 FC/FH

TO LOV

536551-01-1 536551-0604-1 B2

FROM 0 FC/FH

TO LOV

536551-01-1 536551-0604-2 B4-100

FROM 0 FC/FH

TO LOV

536551-01-1 536551-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536553-01-1 536553-0604-1 B2

FROM 0 FC/FH

TO LOV

536553-01-2 536553-0604-2 B4-100

FROM 0 FC/FH

TO LOV

536553-01-3 536553-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536554-01-1 536554-0606-1 ALL

SB 53-0238

FROM 0 FC/FH

TO LOV

536555-01-1 536555-0606-1 ALL

SB 53-0345

FROM 0 FC/FH

TO LOV

536556-01-1 536556-0606-1 B2

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 43 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536556-01-2 536556-0606-2 B4-100

FROM 0 FC/FH

TO LOV

536556-01-3 536556-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536557-01-1 536557-0606-1 B2

FROM 0 FC/FH

TO LOV

536557-01-2 536557-0606-2 B4-100

FROM 0 FC/FH

TO LOV

536557-01-3 536557-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536560-01-1 536560-0606-1 ALL

FROM 0 FC/FH

TO LOV

536578-01-1 536578-0604-1 POST 07301

(53-0239)

FROM 0 FC/FH

TO LOV

536590-01-1 536590-0606-1 ALL

FROM 0 FC/FH

TO LOV

536597-01-1 536597-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536597-01-1 536597-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536597-01-1 536597-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536597-02-10 536597-0602-4 B4-100

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 44 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

POST 02611

FROM 40000 FC

TO LOV

536597-02-11 536597-0602-5 B4-200

C4

F4

PRE 02611

FROM 34000 FC

TO LOV

536597-02-12 536597-0602-6 B4-200

C4

F4

POST 02611

FROM 34000 FC

TO LOV

536597-02-7 536597-0602-1 B2

PRE 02611

FROM 48000FC

TO LOV

536597-02-8 536597-0602-2 B2

POST 02611

FROM 48000 FC

TO LOV

536597-02-9 536597-0602-3 B4-100

PRE 02611

FROM 40000 FC

TO LOV

536598-01-1 536598-0606-1 B2

PRE 07757

(53-0272)

FROM 0 FC/FH

TO LOV

536598-01-2 536598-0606-2 B4-100

PRE 07757

(53-0272)

PRE 03474

FROM 0 FC/FH

TO LOV

536598-01-3 536598-0606-3 B4-200

C4

F4

PRE 07757

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 45 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

(53-0272)

PRE 03474

FROM 0 FC/FH

TO LOV

536598-01-4 536598-0606-5 B4-200

C4

F4

PRE 07757

(53-0272)

POST 03474

FROM 0 FC/FH

TO 34000 FC

536598-01-5 536598-0606-6 B4-200

C4

F4

PRE 07757

(53-0272)

POST 03474

FROM 34000 FC

TO LOV

536598-02-1 536598-0607-1 B2

PRE 07757

(53-0272)

FROM 0 FC/FH

TO LOV

536598-02-2 536598-0607-2 B4-100

PRE 07757

(53-0272)

PRE 03474

FROM 0 FC/FH

TO 40000 FC

536598-02-3 536598-0607-3 B4-100

PRE 07757

(53-0272)

PRE 03474

FROM 40000 FC

TO LOV

536598-02-4 536598-0607-4 B4-200

C4

F4

PRE 07757

(53-0272)

PRE 03474

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 46 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

536598-02-5 536598-0607-5 B4-200

C4

F4

PRE 07757

(53-0272)

POST 03474

FROM 0 FC/FH

TO LOV

536599-01-1 536599-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536599-01-2 536599-0607-1 B2

FROM 48000 FC

TO LOV

536599-01-3 536599-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

536599-01-4 536599-0607-2 B4-100

FROM 40000 FC

TO LOV

536599-01-5 536599-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536599-01-6 536599-0607-3 B4-200

C4

F4

FROM 34000 FC

TO LOV

536599-02-1 536599-0606-4 B2

FROM 0 FC/FH

TO 48000 FC

536599-02-2 536599-0607-4 B2

FROM 48000 FC

TO LOV

536599-02-3 536599-0606-5 B4-100

FROM 0 FC/FH

TO LOV

536599-02-4 536599-0606-6 B4-200

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 47 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

FROM 0 FC/FH

TO LOV

536601-01-1 536601-0606-1 ALL

SB 53-0254

FROM 0 FC/FH

TO LOV

536602-01-1 536602-0606-1 ALL

FROM 0 FC/FH

TO LOV

536603-01-1 536603-0606-1 ALL

FROM 0 FC/FH

TO 42500 FC

536651-01-1 536651-0606-2 B2

PRE 02974

FROM 0 FC/FH

TO LOV

MSN 4 EXCLUDED

536651-01-2 536651-0606-3 B2

POST 02974

FROM 0 FC/FH

TO LOV

536651-01-3 536651-0606-4 B4-100

PRE 02974

FROM 0 FC/FH

TO LOV

536651-01-4 536651-0606-5 B4-100

POST 02974

FROM 0 FC/FH

TO LOV

536651-01-5 536651-0606-6 B4-200

C4

F4

PRE 02974

FROM 0 FC/FH

TO LOV

536651-01-6 536651-0606-7 B4-200

C4

F4

POST 02974

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 48 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536651-02-1 536651-0607-2 B2

PRE 02974

FROM 0 FC/FH

TO LOV

536651-02-2 536651-0607-3 B2

POST 02974

FROM 0 FC/FH

TO LOV

536651-02-3 536651-0607-4 B4-100

PRE 02974

FROM 0 FC/FH

TO LOV

536651-02-4 536651-0607-5 B4-100

POST 02974

FROM 0 FC/FH

TO LOV

536651-02-5 536651-0607-6 B4-200

C4

F4

PRE 02974

FROM 0 FC/FH

TO LOV

536651-02-6 536651-0607-7 B4-200

C4

F4

POST 02974

FROM 0 FC/FH

TO LOV

536652-01-1 536652-0606-2 B2

FROM 0 FC/FH

TO 48000 FC

536652-01-2 536652-0606-3 B2

FROM 48000 FC

TO LOV

536652-01-3 536652-0606-4 B4-100

FROM 0 FC/FH

TO LOV

536652-01-4 536652-0606-5 B4-200

C4

F4

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 49 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

536652-02-1 536652-0606-6 B2

FROM 0 FC/FH

TO 48000 FC

536652-02-2 536652-0606-7 B2

FROM 48000 FC

TO LOV

536652-02-3 536652-0606-8 B4-100

FROM 0 FC/FH

TO LOV

536652-02-4 536652-0606-9 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536653-01-1 536653-0602-1 B2

FROM 0 FC/FH

TO LOV

536653-01-2 536653-0602-2 B4-100

FROM 0 FC/FH

TO LOV

536653-01-3 536653-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536654-01-1 536654-0604-1 B2

FROM 0 FC/FH

TO LOV

536654-01-2 536654-0604-2 B4-100

FROM 0 FC/FH

TO LOV

536654-01-3 536654-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536701-01-1 536701-0606-1 ALL

SB 53-0255

FROM 0 FC/FH

TO LOV

536702-01-1 536702-0606-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 50 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

SB 53-0260

FROM 0 FC/FH

TO LOV

TO 42500 FC

536703-01-1 536703-0606-1 B2

SB 53-0261

FROM 0 FC/FH

TO 42500 FC

536703-01-2 536703-0606-2 B4-100

SB 53-0261

FROM 0 FC/FH

TO 41700 FC

536703-01-3 536703-0606-3 B4-200

C4

F4

SB 53-0261

FROM 0 FC/FH

TO 48000 FC

536704-01-1 536704-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

536704-01-2 536704-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

536704-01-3 536704-0606-2 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536704-01-4 536704-0607-1 B2

FROM 48000 FC

TO LOV

536704-01-5 536704-0607-2 B4-100

FROM 40000 FC

TO LOV

536704-01-6 536704-0607-3 B4-200

C4

F4

FROM 34000 FC

TO LOV

536704-02-1 536704-0606-4 B2

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 51 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 48000 FC

536704-02-2 536704-0606-6 B4-100

FROM 0 FC/FH

TO 40000 FC

536704-02-3 536704-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

536704-02-4 536704-0607-4 B2

FROM 48000 FC

TO LOV

536704-02-5 536704-0607-5 B4-100

FROM 40000 FC

TO LOV

536704-02-6 536704-0607-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

536705-01-1 536705-0606-1 B2

B4-100

FROM 0 FC/FH

TO LOV

536705-01-2 536705-0606-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536706-01-1 536706-0606-1 B4-100

PRE 02643

(53-0132)

FROM 0 FC/FH

TO LOV

536707-01-1 536707-0604-1 B2

FROM 0 FC/FH

TO LOV

536707-01-2 536707-0604-2 B4-100

FROM 0 FC/FH

TO LOV

536707-01-3 536707-0604-3 B4-200

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 52 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

FROM 0 FC/FH

TO LOV

536708-01-1 536708-0604-1 B2

FROM 0 FC/FH

TO LOV

536708-01-2 536708-0604-2 B4-100

FROM 0 FC/FH

TO LOV

536708-01-3 536708-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536709-01-1 536709-0604-1 B2

FROM 0 FC/FH

TO LOV

536709-01-2 536709-0604-2 B4-100

FROM 0 FC/FH

TO LOV

536709-01-3 536709-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536710-01-1 536710-0602-1 B2

FROM 0 FC/FH

TO LOV

536710-01-2 536710-0602-2 B4-100

FROM 0 FC/FH

TO LOV

536710-01-3 536710-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536711-01-1 536711-0606-1 B2

FROM 0 FC/FH

TO LOV

536711-01-2 536711-0606-2 B4-100

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 53 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536711-01-3 536711-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536801-01-1 536801-0606-1 ALL

SB 53-0262

FROM 0 FC/FH

TO 40750 FC

536901-01-1 536901-0606-1 ALL

SB 53-0256

FROM 0 FC/FH

TO LOV

536901-02-1 536901-0606-2 B2

FROM 48000 FC

TO LOV

536901-02-2 536901-0606-3 B4-100

FROM 40000 FC

TO LOV

536901-02-3 536901-0606-5 B4-200

C4

F4

FROM 34000 FC

TO LOV

536902-01-1 536902-0606-1 ALL

SB 53-0258

FROM 0 FC/FH

TO LOV

536903-01-1 536903-0604-1 B2

FROM 0 FC/FH

TO LOV

536903-01-2 536903-0604-2 B4-100

FROM 0 FC/FH

TO LOV

536903-01-3 536903-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

536905-01-1 536905-0604-1 B2

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 54 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

536905-01-2 536905-0604-2 B4-100

FROM 0 FC/FH

TO 57000 FC

536905-01-3 536905-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO 57000 FC

538789-01-1 538789-0604-1 ALL

FROM 0 FC/FH

TO LOV

538839-01-1 538839-0604-1 B2

FROM 0 FC/FH

TO LOV

538839-01-2 538839-0604-2 B4-100

FROM 0 FC/FH

TO LOV

538839-01-3 538839-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

543001-01-1 543001-0602-1 B2

FROM 0 FC/FH

TO LOV

543001-01-2 543001-0602-2 B4-100

FROM 0 FC/FH

TO LOV

543001-01-3 543001-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

546001-01-10 546001-0606-6 B4-200

C4

F4

POST 02434

FROM 0 FC/FH

TO LOV

546001-01-1 546001-0606-1 B2

PRE 02434

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 55 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 48000 FC

546001-01-2 546001-0606-7 B2

PRE 02434

FROM 48000 FC

TO LOV

546001-01-3 546001-0606-2 B2

POST 02434

FROM 0 FC/FH

TO 48000 FC

546001-01-4 546001-0606-8 B2

POST 02434

FROM 48000 FC

TO LOV

546001-01-5 546001-0606-3 B4-100

PRE 02434

FROM 0 FC/FH

TO 40000 FC

546001-01-6 546001-0606-9 B4-100

PRE 02434

FROM 40000 FC

TO LOV

546001-01-7 546001-0606-4 B4-100

POST 02434

FROM 0 FC/FH

TO LOV

546001-01-8 546001-0606-5 B4-200

C4

F4

PRE 02434

FROM 0 FC/FH

TO 34000 FC

546001-01-9 546001-0607-1 B4-200

C4

F4

PRE 02434

FROM 34000 FC

TO LOV

546001-02-10 546001-0608-2 B4-200

C4

F4

POST 02434

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 56 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

546001-02-1 546001-0607-2 B2

PRE 02434

FROM 0 FC/FH

TO 48000 FC

546001-02-2 546001-0607-3 B2

PRE 02434

FROM 48000 FC

TO LOV

546001-02-3 546001-0607-4 B2

POST 02434

FROM 0 FC/FH

TO 48000 FC

546001-02-4 546001-0607-5 B2

POST 02434

FROM 48000 FC

TO LOV

546001-02-5 546001-0607-6 B4-100

PRE 02434

FROM 0 FC/FH

TO 40000 FC

546001-02-6 546001-0607-7 B4-100

PRE 02434

FROM 40000 FC

TO LOV

546001-02-7 546001-0607-8 B4-100

POST 02434

FROM 0 FC/FH

TO LOV

546001-02-8 546001-0607-9 B4-200

C4

F4

PRE 02434

FROM 0 FC/FH

TO 34000 FC

546001-02-9 546001-0608-1 B4-200

C4

F4

PRE 02434

FROM 34000 FC

TO LOV

546014-01-1 546014-0606-1 B2

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 57 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO 48000 FC

546014-01-2 546014-0606-2 B2

FROM 48000 FC

TO LOV

546014-01-3 546014-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

546014-01-4 546014-0606-4 B4-100

FROM 40000 FC

TO LOV

546014-01-5 546014-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

546014-02-1 546014-0607-1 B2

FROM 0 FC/FH

TO 48000 FC

546014-02-2 546014-0607-2 B2

FROM 48000 FC

TO LOV

546014-02-3 546014-0607-3 B4-100

FROM 0 FC/FH

TO 40000 FC

546014-02-4 546014-0607-4 B4-100

FROM 40000 FC

TO LOV

546014-02-5 546014-0607-5 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

546014-03-1 546014-0608-1 B2

FROM 0 FC/FH

TO 48000 FC

546014-03-2 546014-0608-2 B2

FROM 48000 FC

TO LOV

546014-03-3 546014-0608-3 B4-100

FROM 0 FC/FH

TO 40000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 58 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

546014-03-4 546014-0608-4 B4-100

FROM 40000 FC

TO LOV

546014-03-5 546014-0608-5 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

556001-01-1 556001-0606-1 ALL

SB 55-0036

FROM 0 FC/FH

TO LOV

556002-01-1 556002-0602-1 B2

FROM 0 FC/FH

TO LOV

556002-01-2 556002-0602-2 B4-100

FROM 0 FC/FH

TO LOV

556002-01-3 556002-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

556003-01-1 556003-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

556003-01-2 556003-0606-2 B2

FROM 48000 FC

TO LOV

556003-01-3 556003-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

556003-01-4 556003-0606-4 B4-100

FROM 40000 FC

TO LOV

556003-01-5 556003-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

556003-01-6 556003-0606-6 B4-200

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 59 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

FROM 34000 FC

TO LOV

556004-01-1 556004-0606-1 B2

PRE 01236

FROM 0 FC/FH

TO LOV

556004-01-2 556004-0606-3 B4-100

PRE 01236

FROM 0 FC/FH

TO LOV

556004-01-3 556004-0606-5 B4-200

C4

F4

PRE 01236

FROM 0 FC/FH

TO LOV

556004-01-4 556004-0606-2 B2

POST 01236

FROM 0 FC/FH

TO LOV

556004-01-5 556004-0606-4 B4-100

POST 01236

FROM 0 FC/FH

TO LOV

556004-01-6 556004-0606-6 B4-200

C4

F4

POST 01236

FROM 0 FC/FH

TO LOV

556005-01-1 556005-0604-1 B2

FROM 0 FC/FH

TO LOV

556005-01-2 556005-0604-2 B4-100

FROM 0 FC/FH

TO LOV

556005-01-3 556005-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 60 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

556006-01-1 556006-0604-1 B2

FROM 0 FC/FH

TO LOV

556006-01-2 556006-0604-2 B4-100

FROM 0 FC/FH

TO LOV

556006-01-3 556006-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

556007-01-1 556007-0604-1 B2

FROM 0 FC/FH

TO LOV

556007-01-2 556007-0604-2 B4-100

FROM 0 FC/FH

TO LOV

556007-01-3 556007-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

556008-01-1 556008-0604-1 B2

FROM 0 FC/FH

TO LOV

556008-01-2 556008-0604-2 B4-100

FROM 0 FC/FH

TO LOV

556008-01-3 556008-0604-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

556009-01-1 556009-0604-1 B2

FROM 0 FC/FH

TO LOV

556009-01-2 556009-0604-2 B4-100

FROM 0 FC/FH

TO LOV

556009-01-3 556009-0604-3 B4-200

C4

F4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 61 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

571001-01-1 571001-0602-1 B2

B4-100

FROM 0 FC/FH

TO LOV

571001-01-2 571001-0602-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571002-01-1 571002-0602-1 B2

B4-100

FROM 0 FC/FH

TO LOV

571002-01-2 571002-0602-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571003-01-1 571003-0602-1 B2

B4-100

FROM 0 FC/FH

TO LOV

571003-01-2 571003-0602-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571005-01-1 571005-0602-1 B2

FROM 0 FC/FH

TO LOV

571005-01-2 571005-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571005-01-3 571005-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571006-01-1 571006-0602-1 B2

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 62 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

571006-01-2 571006-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571006-01-3 571006-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571007-01-1 571007-0602-1 B2

FROM 0 FC/FH

TO LOV

571007-01-2 571007-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571007-01-3 571007-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571017-01-1 571017-0602-1 B2

B4-100

FROM 0 FC/FH

TO LOV

571017-01-2 571017-0602-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571018-01-1 571018-0603-1 B2

FROM 0 FC/FH

TO LOV

571018-01-2 571018-0603-2 B4-100

FROM 0 FC/FH

TO LOV

571018-01-3 571018-0603-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571028-01-1 571028-0602-1 B2

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 63 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

571028-01-2 571028-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571028-01-3 571028-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571031-01-1 571031-0602-1 B2

B4-100

FROM 0 FC/FH

TO LOV

571031-01-2 571031-0602-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571033-01-1 571033-0602-1 B2

FROM 0 FC/FH

TO LOV

571033-01-2 571033-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571033-01-3 571033-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571035-01-1 571035-0602-1 B2

B4-100

FROM 0 FC/FH

TO LOV

571035-01-2 571035-0602-2 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571040-01-1 571040-0602-1 B2

FROM 0 FC/FH

TO LOV

571040-01-2 571040-0602-2 B4-100

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 64 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

571040-01-3 571040-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571045-01-1 571045-0602-1 B2

B4-100

POST 01868

POST 01869

OR

POST 02101

(57-0079)

FROM 0 FC/FH

TO LOV

571045-01-2 571045-0602-2 B4-200

C4

F4

POST 01868

POST 01869

OR

POST 02101

(57-0079)

FROM 0 FC/FH

TO LOV

571047-01-1 571047-0602-1 B2

FROM 0 FC/FH

TO LOV

571047-01-2 571047-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571047-01-3 571047-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571055-01-1 571055-0602-1 B2

B4-100

FROM 0 FC/FH

TO LOV

571055-01-2 571055-0602-2 B4-200

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 65 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

FROM 0 FC/FH

TO LOV

571057-01-1 571057-0602-1 B2

FROM 0 FC/FH

TO LOV

571057-01-2 571057-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571057-01-3 571057-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

571058-01-1 571058-0602-1 B2

FROM 0 FC/FH

TO LOV

571058-01-2 571058-0602-2 B4-100

FROM 0 FC/FH

TO LOV

571058-01-3 571058-0602-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

572063-01-1 572063-0603-1 ALL

FROM 0 FC/FH

TO LOV

572093-01-1 572093-0604-1 ALL

FROM 0 FC/FH

TO LOV

572094-01-1 572094-0604-1 ALL

FROM 0 FC/FH

TO LOV

575021-01-1 575021-0604-1 ALL

FROM 0 FC/FH

TO LOV

575061-01-1 575061-0604-1 ALL

FROM 0 FC/FH

TO LOV

575087-01-1 575087-0604-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 66 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

575088-01-1 575088-0604-1 ALL

FROM 0 FC/FH

TO LOV

575104-01-1 575104-0604-1 ALL

FROM 0 FC/FH

TO LOV

575171-01-1 575171-0603-1 ALL

FROM 0 FC/FH

TO LOV

575223-01-1 575223-0603-1 ALL

FROM 0 FC/FH

TO LOV

575293-01-1 575293-0602-1 ALL

FROM 0 FC/FH

TO LOV

576001-01-1 576001-0606-1 ALL

SB 57-0184

FROM 0 FC/FH

TO LOV

576002-01-1 576002-0606-1 ALL

SB 57-0147

FROM 0 FC/FH

TO LOV

576003-01-1 576003-0606-1 ALL

SB 57-0152

FROM 0 FC/FH

TO LOV

576004-01-1 576004-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576004-01-2 576004-0606-2 B2

FROM 48000 FC

TO LOV

576004-01-3 576004-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

576004-01-4 576004-0606-4 B4-100

FROM 40000 FC

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 67 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

576004-01-5 576004-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

576004-01-6 576004-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576005-01-1 576005-0606-1 ALL

SB 57-0155

FROM 0 FC/FH

TO LOV

576006-01-1 576006-0606-2 ALL

SB 57-0148

FROM 0 FC/FH

TO LOV

576007-01-1 576007-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576007-01-2 576007-0606-2 B2

FROM 48000 FC

TO LOV

576007-01-3 576007-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

576007-01-4 576007-0606-4 B4-100

FROM 40000 FC

TO LOV

576007-01-5 576007-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

576007-01-6 576007-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576008-01-1 576008-0606-1 ALL

SB 57-0146

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 68 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 0 FC/FH

TO LOV

576009-01-1 576009-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576009-01-2 576009-0606-4 B2

FROM 48000 FC

TO LOV

576009-01-3 576009-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

576009-01-4 576009-0606-5 B4-100

FROM 40000 FC

TO LOV

576009-01-5 576009-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

576009-01-6 576009-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576010-01-1 576010-0606-1 ALL

SB 57-0147

FROM 0 FC/FH

TO LOV

576011-01-1 576011-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576011-01-2 576011-0606-4 B2

FROM 48000 FC

TO LOV

576011-01-3 576011-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

576011-01-4 576011-0606-5 B4-100

FROM 40000 FC

TO LOV

576011-01-5 576011-0606-3 B4-200

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 69 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

FROM 0 FC/FH

TO 34000 FC

576011-01-6 576011-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576012-01-1 576012-0606-1 ALL

SB 57-0148

FROM 0 FC/FH

TO LOV

576013-01-1 576013-0604-1 B2

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 48000 FC

576013-01-2 576013-0604-2 B2

PRE 08253

(57-0175)

FROM 48000 FC

TO LOV

576013-01-3 576013-0604-3 B4-100

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 40000 FC

576013-01-4 576013-0604-4 B4-100

PRE 08253

(57-0175)

FROM 40000

TO LOV

576013-01-5 576013-0604-5 B4-200

C4

F4

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 34000 FC

576013-01-6 576013-0604-6 B4-200

C4

F4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 70 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

PRE 08253

(57-0175)

FROM 34000 FC

TO LOV

576013-02-1 576013-0606-1 B2

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 48000 FC

576013-02-2 576013-0606-2 B2

PRE 08253

(57-0175)

FROM 48000 FC

TO LOV

576013-02-3 576013-0606-3 B4-100

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 40000 FC

576013-02-4 576013-0606-4 B4-100

PRE 08253

(57-0175)

FROM 40000

TO LOV

576013-02-5 576013-0606-5 B4-200

C4

F4

PRE 08253

(57-0175)

FROM 0 FC/FH

TO 34000 FC

576013-02-6 576013-0606-6 B4-200

C4

F4

PRE 08253

(57-0175)

FROM 34000 FC

TO LOV

576014-01-1 576014-0606-1 ALL

SB 57-0153

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 71 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

576016-01-1 576016-0606-1 ALL

FROM 0 FC/FH

TO LOV

576017-01-1 576017-0606-1 B2

FROM 0 FC/FH

TO LOV

576021-01-1 576021-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576021-01-2 576021-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

576021-01-3 576021-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

576021-01-4 576021-0606-4 B2

FROM 48000 FC

TO LOV

576021-01-5 576021-0606-5 B4-100

FROM 40000 FC

TO LOV

576021-01-6 576021-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576029-01-1 576029-0605-1 B2

POST 01868

FROM 0 FC/FH

TO 48000 FC

576029-01-2 576029-0605-2 B2

POST 01868

FROM 48000 FC

TO LOV

576029-01-3 576029-0605-3 B4-100

POST 01868

FROM 0 FC/FH

TO 40000 FC

576029-01-4 576029-0605-4 B4-100

POST 01868

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 72 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 40000 FC

TO LOV

576029-01-5 576029-0605-5 B4-200

C4

F4

POST 01868

FROM 0 FC/FH

TO 34000 FC

576029-01-6 576029-0605-6 B4-200

C4

F4

POST 01868

FROM 34000 FC

TO LOV

576029-02-1 576029-0606-1 B2

POST 01868

FROM 0 FC/FH

TO 48000 FC

576029-02-2 576029-0606-2 B2

POST 01868

FROM 48000 FC

TO LOV

576029-02-3 576029-0606-3 B4-100

POST 01868

FROM 0 FC/FH

TO 40000 FC

576029-02-4 576029-0606-4 B4-100

POST 01868

FROM 40000 FC

TO LOV

576029-02-5 576029-0606-5 B4-200

C4

F4

POST 01868

FROM 0 FC/FH

TO 34000 FC

576029-02-6 576029-0606-6 B4-200

C4

F4

POST 01868

FROM 34000 FC

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 73 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

576031-01-1 576031-0606-1 B2

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 0 FC/FH

TO 48000 FC

576031-01-2 576031-0606-2 B2

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 48000 FC

TO LOV

576031-01-3 576031-0606-3 B4-100

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 0 FC/FH

TO 40000 FC

576031-01-4 576031-0606-4 B4-100

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 40000 FC

TO LOV

576031-01-5 576031-0606-5 B4-200

C4

F4

POST 01868 OR

POST 02101

(57-0079) AND

PRE 02338

FROM 0 FC/FH

TO 34000 FC

576031-01-6 576031-0606-6 B4-200

C4

F4

POST 01868 OR

POST 02101

(57-0079) AND

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 74 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

PRE 02338

FROM 34000 FC

TO LOV

576035-01-10 576035-0607-1 B4-200

C4

F4

POST 01868

PRE (53-0291)

FROM 34000 FC

TO LOV

576035-01-11 576035-0607-2 B4-200

C4

F4

POST 01868

POST (53-0291)

FROM 0 FC/FH

TO 34000 FC

576035-01-12 576035-0607-3 B4-200

C4

F4

POST 01868

POST (53-0291)

FROM 34000 FC

TO LOV

576035-01-1 576035-0606-1 B2

POST 01868

PRE (53-0282)

FROM 0 FC/FH

TO 48000 FC

576035-01-2 576035-0606-2 B2

POST 01868

PRE (53-0282)

FROM 48000 FC

TO LOV

576035-01-3 576035-0606-3 B2

POST 01868

POST (53-0282)

FROM 0 FC/FH

TO 48000 FC

576035-01-4 576035-0606-4 B2

POST 01868

POST (53-0282)

FROM 48000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 75 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

576035-01-5 576035-0606-5 B4-100

POST 01868

PRE (53-0291)

FROM 0 FC/FH

TO 40000 FC

576035-01-6 576035-0606-6 B4-100

POST 01868

PRE (53-0291)

FROM 40000 FC

TO LOV

576035-01-7 576035-0606-7 B4-100

POST 01868

POST (53-0291)

FROM 0 FC/FH

TO 40000 FC

576035-01-8 576035-0606-8 B4-100

POST 01868

POST (53-0291)

FROM 40000 FC

TO LOV

576035-01-9 576035-0606-9 B4-200

C4

F4

POST 01868

PRE (53-0291)

FROM 0 FC/FH

TO 34000 FC

576037-01-1 576037-0606-1 B2

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 0 FC/FH

TO 48000 FC

576037-01-2 576037-0606-2 B2

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 48000 FC

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 76 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO LOV

576037-01-3 576037-0606-3 B4-100

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 0 FC/FH

TO 40000 FC

576037-01-4 576037-0606-4 B4-100

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 40000 FC

TO LOV

576037-01-5 576037-0606-5 B4-200

C4

F4

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 0 FC/FH

TO 34000 FC

576037-01-6 576037-0606-6 B4-200

C4

F4

POST 01868

OR

POST 02100

(57-0078)

PRE 02338

FROM 34000 FC

TO LOV

576041-01-1 576041-0606-1 B2

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 77 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 48000 FC

576041-01-2 576041-0606-2 B2

POST 01869

OR

POST 02099

(57-0077)

FROM 48000 FC

TO LOV

576041-01-3 576041-0606-3 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 40000 FC

576041-01-4 576041-0606-5 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 34000 FC

576041-01-5 576041-0606-6 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 34000 FC

TO LOV

576041-01-6 576041-0606-4 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 40000 FC

TO LOV

576047-01-1 576047-0606-1 B2

POST 01868

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 78 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 48000 FC

576047-01-2 576047-0606-2 B2

POST 01868

FROM 48000 FC

TO LOV

576047-01-3 576047-0606-3 B4-100

POST 01868

FROM 0 FC/FH

TO 40000 FC

576047-01-4 576047-0606-4 B4-100

POST 01868

FROM 40000 FC

TO LOV

576047-01-5 576047-0606-5 B4-200

C4

F4

POST 01868

FROM 0 FC/FH

TO 34000 FC

576047-01-6 576047-0606-6 B4-200

C4

F4

POST 01868

FROM 34000 FC

TO LOV

576047-02-1 576047-0606-1 B2

POST 01868

FROM 0 FC/FH

TO 48000 FC

576047-02-2 576047-0606-2 B2

POST 01868

FROM 48000 FC

TO LOV

576047-02-3 576047-0606-3 B4-100

POST 01868

FROM 0 FC/FH

TO 40000 FC

576047-02-4 576047-0606-4 B4-100

POST 01868

FROM 40000 FC

TO LOV

576047-02-5 576047-0606-5 B4-200

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 79 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

C4

F4

POST 01868

FROM 0 FC/FH

TO 34000 FC

576047-02-6 576047-0606-6 B4-200

C4

F4

POST 01868

FROM 34000 FC

TO LOV

576051-01-1 576051-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576051-01-2 576051-0606-4 B2

FROM 48000 FC

TO LOV

576051-01-3 576051-0606-2 B4-100

FROM 0 FC/FH

TO 40000 FC

576051-01-4 576051-0606-5 B4-100

FROM 40000 FC

TO LOV

576051-01-5 576051-0606-3 B4-200

C4

F4

FROM 0 FC

TO 34000 FC

576051-01-6 576051-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576053-01-1 576053-0605-1 ALL

SB 57-0158

FROM 0 FC/FH

TO LOV

576055-01-1 576055-0606-1 ALL

SB 57-0162

FROM 0 FC/FH

TO LOV

576056-01-1 576056-0606-1 ALL

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 80 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

SB 57-0164

FROM 0 FC/FH

TO LOV

576057-01-1 576057-0606-1 B2

SB 57-0151

FROM 0 FC/FH

TO LOV

576058-01-1 576058-0606-1 ALL

SB 57-0193

FROM 0 FC/FH

TO LOV

576059-01-1 576059-0606-1 ALL

SB 57-0119

FROM 0 FC/FH

TO LOV

576060-01-1 576060-0605-1 ALL

SB 57-0187

FROM 0 FC/FH

TO LOV

576062-01-1 576062-0606-1 B2

PRE 01868

PRE 02100

(57-0078)

FROM 0 FC/FH

TO LOV

576062-01-2 576062-0606-2 B4-100

PRE 01868

PRE 02100

(57-0078)

FROM 0 FC/FH

TO 40000 FC

576062-01-3 576062-0606-3 B4-100

PRE 01868

PRE 02100

(57-0078)

FROM 40000 FC

TO LOV

576062-01-4 576062-0606-4 B4-200

C4

F4

PRE 01868

PRE 02100

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 81 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

(57-0078)

FROM 0 FC/FH

TO 34000 FC

576062-01-5 576062-0606-5 B4-200

C4

F4

PRE 01868

PRE 02100

(57-0078)

FROM 34000 FC

TO LOV

576063-01-1 576063-0606-1 B4-100

PRE 10470

(57-0207)

FROM 0 FC/FH

TO 40000 FC

576063-01-2 576063-0606-2 B4-100

PRE 10470

(57-0207)

FROM 40000 FC

TO LOV

576063-01-3 576063-0606-3 B4-200

C4

F4

PRE 10470

(57-0207)

FROM 0 FC/FH

TO 34000 FC

576063-01-4 576063-0606-4 B4-200

C4

F4

PRE 10470

(57-0207)

FROM 34000 FC

TO LOV

576064-01-1 576064-0606-1 B2

PRE 10326

(57-0203)

FROM 0 FC/FH

TO 48000 FC

576064-01-2 576064-0606-2 B2

PRE 10326

(57-0203)

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 82 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 48000 FC

TO LOV

576064-01-3 576064-0606-3 B4-100

PRE 10326

(57-0203)

FROM 0 FC/FH

TO 40000 FC

576064-01-4 576064-0606-4 B4-100

PRE 10326

(57-0203)

FROM 40000 FC

TO LOV

576064-01-5 576064-0606-5 B4-200

C4

F4

PRE 10326

(57-0203)

FROM 0 FC/FH

TO 34000 FC

576064-01-6 576064-0606-6 B4-200

C4

F4

PRE 10326

(57-0203)

FROM 34000 FC

TO LOV

576065-01-1 576065-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576065-01-2 576065-0606-2 B2

FROM 48000 FC

TO LOV

576065-01-3 576065-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

576065-01-4 576065-0606-4 B4-100

FROM 40000 FC

TO LOV

576065-01-5 576065-0606-5 B4-200

C4

F4

FROM 0 FC/FH

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 83 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

TO 34000 FC

576065-01-6 576065-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576065-02-1 576065-0607-1 B2

FROM 0 FC/FH

TO 48000 FC

576065-02-2 576065-0607-2 B2

FROM 48000 FC

TO LOV

576065-02-3 576065-0607-3 B4-100

FROM 0 FC/FH

TO 40000 FC

576065-02-4 576065-0607-4 B4-100

FROM 40000 FC

TO LOV

576065-02-5 576065-0607-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

576065-02-6 576065-0607-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576066-01-1 576066-0606-1 ALL

SB 57-0208

FROM 0 FC/FH

TO LOV

576067-01-1 576067-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576067-01-2 576067-0606-2 B2

FROM 48000 FC

TO LOV

576068-01-1 576068-0606-1 B2

POST 01869

OR

POST 02099

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 84 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

(57-0077)

FROM 0 FC/FH

TO 48000 FC

576068-01-2 576068-0606-3 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 40000 FC

576068-01-3 576068-0606-5 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 34000 FC

576068-01-4 576068-0606-2 B2

POST 01869

OR

POST 02099

(57-0077)

FROM 48000 FC

TO LOV

576068-01-5 576068-0606-4 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 40000 FC

TO LOV

576068-01-6 576068-0606-6 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 34000 FC

TO LOV

576068-02-1 576068-0606-1 B2

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 85 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 48000 FC

576068-02-2 576068-0606-3 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 40000 FC

576068-02-3 576068-0606-5 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

FROM 0 FC/FH

TO 34000 FC

576068-02-4 576068-0606-2 B2

POST 01869

OR

POST 02099

(57-0077)

FROM 48000 FC

TO LOV

576068-02-5 576068-0606-4 B4-100

POST 01869

OR

POST 02099

(57-0077)

FROM 40000 FC

TO LOV

576068-02-6 576068-0606-6 B4-200

C4

F4

POST 01869

OR

POST 02099

(57-0077)

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 86 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

FROM 34000 FC

TO LOV

576069-01-1 576069-0606-1 ALL

SB 57-0211

FROM 0 FC/FH

TO LOV

576070-01-1 576070-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576070-01-2 576070-0606-2 B2

FROM 48000 FC

TO LOV

576070-01-3 576070-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

576070-01-4 576070-0606-4 B4-100

FROM 40000 FC

TO LOV

576070-01-5 576070-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO 34000 FC

576070-01-6 576070-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576070-02-1 576070-0606-1 B2

FROM 0 FC/FH

TO 48000 FC

576070-02-2 576070-0606-2 B2

FROM 48000 FC

TO LOV

576070-02-3 576070-0606-3 B4-100

FROM 0 FC/FH

TO 40000 FC

576070-02-4 576070-0606-4 B4-100

FROM 40000 FC

TO LOV

576070-02-5 576070-0606-5 B4-200

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 87 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

FROM 0 FC/FH

TO 34000 FC

576070-02-6 576070-0606-6 B4-200

C4

F4

FROM 34000 FC

TO LOV

576071-01-1 576071-0606-1 B2

SB 57-0225

FROM 0 FC/FH

TO LOV

576072-01-1 576072-0606-1 B2

FROM 0 FC/FH

TO LOV

576072-01-2 576072-0606-3 B4-100

FROM 0 FC/FH

TO LOV

576072-01-3 576072-0606-5 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

576072-02-1 576072-0606-2 B2

FROM 0 FC/FH

TO LOV

576072-02-2 576072-0606-4 B4-100

FROM 0 FC/FH

TO LOV

576072-02-3 576072-0606-6 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

576073-01-1 576073-0606-1 B2

FROM 0 FC/FH

TO LOV

576073-01-2 576073-0606-2 B4-100

FROM 0 FC/FH

TO LOV

576073-01-3 576073-0606-3 B4-200

C4

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-6 Page 88 ALI / MPD - CROSS REFERENCE LIST

ALI

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

F4

FROM 0 FC/FH

TO LOV

576074-01-1 576074-0606-1 B2

FROM 0 FC/FH

TO LOV

576074-01-2 576074-0606-2 B4-100

FROM 0 FC/FH

TO LOV

576074-01-3 576074-0606-3 B4-200

C4

F4

FROM 0 FC/FH

TO LOV

578261-01-1 578261-0606-1 ALL

FROM 0 FC/FH

TO LOV

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 2-7 Page 1 

# APPENDIX 2-7

CMR / MPD - CROSS REFERENCE LIST

CMR

TASK REFERENCE MPD

TASK NUMBER AMTOSS

REFERENCE MPD

APPLICABILITY

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 1 

# APPENDIX 3 — VENDOR RECOMMENDATIONS

1. GENERAL

This appendix contains, as far as available, all current vendor scheduled maintenance

recommendations which are linked to scheduled maintenance tasks in the A300 MPD.

2. PRESENTATION FORM LAYOUT

The following informations are provided for each component:

1. MPD Reference

This column provides reference to A300 MPD tasks in the “Systems, APU and Power Plant”, where

the task interval is expressed in the “Interval/Threshold” column as a program note, “Note 5-1",

Vendor Recommendation. Movement Code (N = New; R = Revised)

2. Designation

Component functional designation.

3. Manufacturer/Vendor

This column provides reference to the component manufacturer’s/vendor’s name and FSCM code.

The FSCM code in line with AIRBUS Vendor Information Manual.

4. Partnumber

Component Partnumber in line with the A300 IPC.

5. CMM Reference

The information quoted in this column provides reference to the specific component

manufacturer’s/vendor’s Component Maintenance Manual (CMM).).

6. Vendor Recommendation/Vendor Interval

This column reflects the component scheduled vendor recommendation for the designated item and

its recommended interval.

The scheduled maintenance requirements described in the MPD task have been developed via the

MSG 3; the interval and any specialities have been defined by the appropriate vendor.

Additional other scheduled maintenance requirements might exist in vendor documentation (CMM)

for various reasons (warranty) which have not been selected and reflected in the A300 MPD.

RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

N 237100-0504-1

237100-L504-1 COCKPIT

VOICE

RECORDE

R 06141 93A100-

()-

SERIES 23-70-

01 EVERY 2 YEARS: BEACON CLEANING AND

TESTING EVERY 6 YEARS: ULB BATTERY

REPLACEMENT.

N 237100-0504-1

237100-L504-1 COCKPIT

VOICE

RECORDE 4V792 522-

4057-

001...- 23-70-

01 NO VENDOR INTERVALS REFLECTED IN CMM

FOR INTERVALS CONCERNING THE ULB

BATTERY REFER TO ITS MANUFACTURER

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 2 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

R 012

N 237100-0504-1

237100-L504-1 COCKPIT

VOICE

RECORDE

R 97896 980-

6001-010

(103600)

980-

6001-001

(103600-

0001)

980-

6001-002

(103600-

0002)

980-

6001-004

(103600-

4) 23-70-

14 NO VENDOR INTERVALS REFLECTED IN CMM

FOR INTERVALS CONCERNING THE ULB

BATTERY REFER TO ITS MANUFACTURER

N 237100-0504-1

237100-L504-1 COCKPIT

VOICE

RECORDE

R 97896 980-

6005-010

(BASIC

1/2 HR)

980-

6005-011

(FLAME

RETARD

ANT

COVER)

980-

6005-012

(ULD)

980-

6005-013

(FLAME

RETARD

ANT

COVER

AND

ULD)

980-

6005-020

(BASIC 1

HR) 980-

6005-021

(FLAME

RETARD

ANT

COVER)

980-

6005-022

(ULD)

980-

6005-023

(FLAME

RETARD

ANT 23-70-

30 NO VENDOR INTERVALS REFLECTED IN CMM

FOR INTERVALS CONCERNING THE ULB

BATTERY REFER TO ITS MANUFACTURER

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

COVER

AND

ULD)

N 237100-0504-1

237100-L504-1 COCKPIT

VOICE

RECORDE

R 97896 980-

6005-

060...-

063 23-70-

38 EVERY 6000 ±500 OPERATING HOURS:

PERFORM PREVENTIVE ACTIONS IAW CMM

(CLEANING; CHECK/TEST, REPLACEMENTS)

EVERY 12000 ±500 OPERATING HOURS:

PERFORM PREVENTIVE ACTIONS IAW CMM

(INSPECTION, REPLACEMENTS) EVERY 48000

±500 OPERATING HOURS: PERFORM

PREVENTIVE ACTIONS IAW CMM

(REPLACEMENTS) 6 YEARS WARRANTY FOR

ULD-BATTERY (DK 100) RETURN ULD TO

MANUFACTURER FOR SERVICE / REPLACEMENT

N 237100-0504-1

237100-L504-1 COCKPIT

VOICE

RECORDE

R 97896 980-

6005-

054...-

058 23-70-

39 NO VENDOR INTERVALS REFLECTED IN CMM

FOR MORE INFORMATION REFER TO

SUNDSTRAND DATA CONTROL INC. DOCUMENT

NO. 060-1646-001 (RECOMMENDED PREVENTIVE

MAINTENACNE SCHEDULE FOR CVR AV557 A / B

/C. FOR INTERVALS CONCERNING THE ULB

BATTERY REFER TO ITS MANUFACTURER

N 237100-0504-1

237100-L504-1 COCKPIT

VOICE

RECORDE

R 97896 980-

6005-

074...-

079 23-70-

40 NO VENDOR INTERVALS REFLECTED IN CMM

FOR SERVICE LIFE AND CLEAINING/TESTING

INTERVALS OF ULD/UAB BATTERY REFER TO

RELATED CMM EVERY 6 YEARS: ULB BATTERY

REPLACEMENT / RETURN TO MANUFACTURER

IAW CMM

R 243111-0504-1

243111-L504-1 AIRCRAFT

BATTERY F6177 2520 24-31-

11 EVERY 1000FH: CHARGE BATTERY, ADJUST

ELECTROLYTE LEVEL. CLEANING. EVERY

2000FH LATEST AFTER 6 MONTHS: BATTERY

TEST IAW CMM, CAPACITY CHECK, ADJUST

ELECTROLYTE LEVEL. EVERY YEAR OR AT

EVERY MAJOR SERVICE OF A/C: BATTERY

OVERHAUL

N 342538-0504-1

342538-L504-1 AIRCRAFT

BATTERY F6177 605 A

605 B 24-31-

19 EVERY 1000FH: CHARGE BATTERY, ADJUST

ELECTROLYTE LEVEL. CLEANING. EVERY

2000FH LATEST AFTER 6 MONTHS: BATTERY

TEST IAW CMM, CAPACITY CHECK, ADJUST

ELECTROLYTE LEVEL. EVERY YEAR OR AT

EVERY MAJOR SERVICE OF A/C: BATTERY

OVERHAUL

N 255820-0504-1

255820-L504-1 BARRIER

NET K2429 AE30-

0228010 25-52-

44 EVERY 12 MONTHS VISUAL INSPECTION TEST

STRAP REMOVAL AND TEST 1ST AT START OF

3RD YEAR IN SERVICE 2ND AT START OF 5TH

YEAR IN SERVICE 3RD AT START OF 7TH YEAR

IN SERVICE 4TH AT START OF 11TH YEAR IN

SERVICE 5TH AT START OF 15TH YEAR IN

SERVICE 6TH AT START OF 19TH YEAR IN

SERVICE IF ALL THE TEST STRAPS HAVE BEEN

REMOVED, A SECTION OF WEBBING CAN BE

REMOVED FOR TESTING. THE REMOVED

SECTION IS TO BE REPLACED WITH A NEW

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 4 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

SECTION OF WEBBING (REPAIRING IAW CMM).

R 255820-0504-1

255820-L504-1 BARRIER

NET K2429 229996-

31

229996-

32 25-58-

51 PERIODICAL INTERVALS SHALL BE DEFINED BY

THE LEGAL HOLDER IN ACCORDANCE WITH

AVIATION ADMINISTRATION REQUIREMENTS

EVERY YEAR: EXTENSION OF THE NET SERVICE

LIFE: 3 YEARS

R 255820-0504-1

255820-L504-1 BARRIER

NET

ASSEMBL

Y K2429 AE30-

0228001

(ASSEM

BLY)

CONSIS

TS OF:

AE30-

0228021

(BARRIE

R NET)

AE40-

0228041

(SMOKE

CURTAI

N) AE30-

0228061

(CONTAI

NER) 25-58-

53 RE-CERTIFICATION INSPECTIONS FOR

CONTINUING AIRWORTHINESS ARE TO BE

DETERMINED BETWEEN PUBLIC AUTHORITY

AND EACH CARRIER (BARRIER NET) AFTER 3

YEARS: TENSILE TEST HAVE TO BE PERFORMED

IAW DOC. REF. 294-6112-00 (SMOKE CURTAIN)

SERVICE LIFE: SPECIFIED MINIMUM 5 YEARS.

THIS AND SUBSEQUENT LIFE IS ASSESSED ON

AN ON-CONDITION BASIS. SEE DOC. REF. 294-

6112-00

255820-0504-1

255820-L504-1 EMERGEN

CY

LOCATOR

TRANSMIT

TER (ELT) 649E2 9260013

93N6069 25-60-

01 EVERY 3 YEARS: REPLACE BATTERY

R 256531-0503-1

256531-L503-1 EMERGEN

CY

LOCATOR

TRANSMIT

TER 07217 607690-1

607690-2 25-60-

05 EVERY 5 YEARS: REPLACE BATTERY

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 70167 D21343-

XXX

21344-

XXX

D21348-

XXX

D21349-

XXX

21351-

XXX

21352-

XXX

24D2123

2-XXX

24D2125

1-1

D21280-

1 25-60-

05 LIFE PRESERVERS SHOULD BE RE-CERTIFIED

AT REGULAR INTERVALS DURING ITS SERVICE

LIFE: THE INTERVALS BETWEEN RECERTIFICATION, PER ATA 100 IS TO BE

DETERMINED BETWEEN THE LOCAL AUTHORITY

AND EACH CARRIER. EVERY 5 YEARS: PERFORM

A PERIODIC INSPECTION IAW CMM

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 5 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

24D2123

7-1

24D2126

0-XXX

24D2124

0-1

25D2126

2-1

25D2126

8-XXX

25D2126

9-1

25D2126

5-1

D21282-

XXX

D21312-

XXX

25D2125

4-1

24D2125

5-1

25D2126

1-XXX

25D2127

0-1

25D2127

1-1

D21290-

1

24D2125

2-1

D21291-

101

N 256531-0503-1

256531-L503-1 EMERGEN

CY

LOCATOR

TRANSMIT

TER 55827 P3-03-

0017- xxx

P3-03-

0018-xxx 25-60-

06 EVERY 3,5 YEARS: REPLACE 436MG BATTERY

PACK EVERY 4 YEARS: REPLACE 437AM

BATTERY PACK

N 256111-0503-2

256111-0503-3

256111-L503-2

256111-L503-3 EVACUATI

ON

SYSTEM 70167 22D2290

0-

SERIES

22D2290

1-

SERIES 25-60-

06 CHECK IF RESERVOIR GAGE SHOWES 3000PSI.

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 57399 P0723-

XXX 25-60-

07 EVERY 60 MONTHS: AFTER ENTRY INTO

SERVICE, BUT NOT LATER THAN 63 MONTH

AFTER DATE OF MANUFACTURE PERFORM AN

INSPECTION IAW CMM

N 256200-0504-1

256200-L504-1 35-42

PERSON

LIFERAFT

ASSEMBL 70167 D23835-

xxx

SERIES 25-60-

07 EVERY 3 YEARS FOR EVACUATION SYSTEMS UP

TO AND INCLUDING 15 YEARS OF AGE OR IF

INFLATABLE, RESERVOIR, HOSE AND

APPLICABLE LIFE-LIMITED ITEMS ARE

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 6 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

Y WITH

INFLATIO

N

ASSEMBL

Y REPLACED AT 15 YEARS FOR THE NEXT 15

YEARS: CHECK/TEST INCL. HYDROSTATIC TEST

EVERY YEAR FOR EVACUATION SYSTEMS

AFTER 15 YEARS OF IN-SERVICE LIFE:

CHECK/TEST INCL. HYDROSTATIC TEST EVERY 3

YEARS: PERFORM A SYSTEM CHECK OF

INFLATION SYSTEM CONCERNING THE

REQUALIFICATION AND SERVICE LIFE OF

RESERVOIR CMM REFERS TO DOT

SPECIFICATIONS AND EXEMPTIONS. VENDOR

RECOMMENDATIONS SERVE AS GENERAL

GUIDELINE. NOTE: VERIFY INCORPORATION OF

ALL OUTSTANDING SERVICE BULLETINS AND

SERVICE INFORMATION LETTERS. FOR

INFLATION SYSTEMS SEE CMM 25-65-07.

SERVICE LIFE OF ELT BATTERY: 3.5 YEARS

N 256531-0503-1

256531-L503-1 EMERGEN

CY

LOCATOR

TRANSMIT

TER 07217 607690-5

SERIES

1 25-60-

09 EVERY 2 YEARS: REPLACE THE WATER

SOLUBLE ANTENNA TAPE EVERY 5 YEARS:

REPLACE BATTERY.

N 256531-0503-1

256531-L503-1 EMERGEN

CY

LOCATOR

TRANSMIT

TER 55827 P3-03-

0002-101

(WITH

4EP5A

BATTER

Y) P3-

03-0002-

102

(WITH

4FP5B

BATTER

Y) P3-

03-0002-

103

(WITH

4EP5C

BATTER

Y) P3-

03-0002-

104

8WITH

4FP5D

BATTER

Y) 25-60-

09 EVERY 3,5 YEARS: REPLACE 4FP5A/B BATTERY

PACK EVERY 4 YEARS: REPLACE 4FP5C/D

BATTERY PACK

N 256200-0504-1

256200-L504-1 46

PERSON

LIFERAFT

ASSEMBL

Y WITH

INFLATIO

N

ASSEMBL 70167 D23940-

xxx

SERIES 25-60-

10 EVERY 3 YEARS: FOR EVACUATION SYSTEMS

UP TO AND INCLUDING 15 YEARS OF AGE OR IF

INFLATABLE, RESERVOIR, HOSE AND

APPLICABLE LIFE-LIMITED ITEMS ARE

REPLACED AT 15 YEARS FOR THE NEXT 15

YEARS CHECK/TEST INCL. HYDROSTATIC TEST

EVERY YEAR FOR EVACUATION SYSTEMS

AFTER 15 YEARS OF IN-SERVICE LIFE:

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 7 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

Y CHECK/TEST INCL. HYDROSTATIC TEST EVERY 3

YEARS: PERFORM A SYSTEM CHECK OF

INFLATION SYSTEM CONCERNING THE

REQUALIFICATION AND SERVICE LIFE OF

RESERVOIR CMM REFERS TO DOT

SPECIFICATIONS AND EXEMPTIONS. VENDOR

RECOMMENDATIONS SERVE AS GENERAL

GUIDELINE. NOTE: VERIFY INCORPORATION OF

ALL OUTSTANDING SERVICE BULLETINS AND

SERVICE INFORMATION LETTERS. FOR

INFLATION SYSTEMS SEE CMM 25-65-10.

SERVICE LIFE OF ELT BATTERY: 3.5 YEARS

N 256200-0504-1

256200-L504-1 REVERSIB

LE

LIFERAFT K6287 TYPE V,

SERIES

3 25-60-

11 FOR REGULARY REQUIREMENTS REGARDING

MAINTENANCE PERIODICITY CONSULT

NATIONAL OR LOCAL AVIATION AUTHORITY

EVERY 18 MONTHs: PERFORM LIFERAFT

OVERHAUL EVERY 48 MONTHS: PERFORM CO2

CYLINDERS OVERHAUL INCLUDING WEIGHT

CHECK

256200-0504-1

256200-L504-1 FLOTATIO

N VEST 16576 FV-35

SERIES

3500-

XXXXXX

(MODEL

129-D) 25-60-

20 CMM 25-60-20 (VENDOR: 16576) NO LONGER

AVAILABLE (Rev. 31)

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-1200 25-60-

24 EVERY 2 YEARS: PERFORM AN INSPECTION IAW

CMM INCLUDING WEIGHT CHECK OF CO2

CYLINDER

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-2500 25-60-

27 THE INTERVALS BETWEEN INSPECTIONS AND

TESTS, PER ATA 100, IS TO BE DETERMINED

BETWEEN PUBLIC AUTHORITY AND EACH

CARRIER, AND SHOULD TAKE INTO

CONSIDERATION SUCH THINGS AS

OPERATIONAL AND SERVICE HISTORY,

FREQUENCY OF HANDLING, ENVIRONMENTAL

CONDITION, ETC. FOR LIFE VEST UP AND

INCLUDING 10 YEARS EVERY 5 YEARS

PERFORM PROOF TEST IAW CMM LIFE VEST

OLDER THAN 10 YEARS AT EVERY REGULAR

SERVICE: PERFORM PROOF TEST IAW CMM

EVERY 5 YEARS: PERFORM ORAL TUBE

ATTACHMENT STRENGHT TEST IAW CMM

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-1500 25-60-

28 EVERY 2 YEARS: PERFORM AN INSPECTION IAW

CMM INCLUDING WEIGHT CHECK OF CO2

CYLINDER

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-1800 25-60-

34 THE INTERVALS BETWEEN INSPECTIONS AND

TESTS, PER ATA 100, IS TO BE DETERMINED

BETWEEN PUBLIC AUTHORITY AND EACH

CARRIER, AND SHOULD TAKE INTO

CONSIDERATION SUCH THINGS AS

OPERATIONAL AND SERVICE HISTORY,

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 8 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

FREQUENCY OF HANDLING, ENVIRONMENTAL

CONDITION, ETC. FOR LIFE VEST UP AND

INCLUDING 10 YEARS EVERY 5 YEARS

PERFORM PROOF TEST IAW CMM LIFE VEST

OLDER THAN 10 YEARS AT EVERY REGULAR

SERVICE: PERFORM PROOF TEST IAW CMM

EVERY 5 YEARS: PERFORM ORAL TUBE

ATTACHMENT STRENGHT TEST IAW CMM

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 INFLATAB

LE

EVACUATI

ON SLIDE 70167 D31020-

101

D31023-

101 25-60-

40 EVERY 3 YEARS FOR EVACUATION SYSTEMS UP

TO AND INCLUDING 15 YEARS OF AGE

CHECK/TEST INCL. HYDROSTATIC TEST EVERY

YEAR FOR EVACUATION SYSTEMS AFTER 15

YEARS OF IN-SERVICE LIFE: CHECK/TEST INCL.

HYDROSTATIC TEST EVERY 3 YEARS: PERFORM

A SYSTEM CHECK OF INFLATION SYSTEM

CONCERNING THE REQUALIFICATION AND

SERVICE LIFE OF RESERVOIR CMM REFERS TO

DOT SPECIFICATIONS AND EXEMPTIONS.

VENDOR RECOMMENDATIONS SERVE AS

GENERAL GUIDELINE. NOTE: VERIFY

INCORPORATION OF ALL OUTSTANDING

SERVICE BULLETINS AND SERVICE

INFORMATION LETTERS. FOR INFLATION

SYSTEMS SEE CMM 25-65-04. POWER UNIT HAS

A USABLE LIFE OF 4 YEARS FROM DATE OF

MANUFACTURE

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-2000(-

1) 25-60-

41 THE INTERVALS BETWEEN INSPECTIONS AND

TESTS, PER ATA 100, IS TO BE DETERMINED

BETWEEN PUBLIC AUTHORITY AND EACH

CARRIER, AND SHOULD TAKE INTO

CONSIDERATION SUCH THINGS AS

OPERATIONAL AND SERVICE HISTORY,

FREQUENCY OF HANDLING, ENVIRONMENTAL

CONDITION, ETC. FOR LIFE VEST UP AND

INCLUDING 10 YEARS EVERY 5 YEARS:

PERFORM PROOF TEST IAW CMM LIFE VEST

OLDER THAN 10 YEARS AT EVERY REGULAR

SERVICE: PERFORM PROOF TEST IAW CMM

EVERY 5 YEARS: PERFORM ORAL TUBE

ATTACHMENT STRENGHT TEST IAW CMM

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 A300

INFLATAB

LE

EVACUATI

ON

SLIDES

WITH

DECORATI

VE COVER 70167 D31021-

xxx

SERIES 25-60-

42 EVERY 3 YEARS FOR EVACUATION SYSTEMS UP

TO AND INCLUDING 15 YEARS OF AGE

CHECK/TEST INCL. HYDROSTATIC TEST IAW

CMM EVERY YEAR FOR EVACUATION SYSTEMS

AFTER 15 YEARS OF IN-SERVICE LIFE:

CHECK/TEST INCL. HYDROSTATIC TEST IAW

CMM EVERY 3 YEARS: PERFORM A SYSTEM

CHECK OF INFLATION SYSTEM CONCERNING

THE REQUALIFICATION AND SERVICE LIFE OF

RESERVOIR CMM REFERS TO DOT

SPECIFICATIONS AND EXEMPTIONS. VENDOR

RECOMMENDATIONS SERVE AS GENERAL

GUIDELINE. NOTE: VERIFY INCORPORATION OF

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 9 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

ALL OUTSTANDING SERVICE BULLETINS AND

SERVICE INFORMATION LETTERS. FOR

INFLATION SYSTEMS SEE CMM 25-65-03. POWER

UNIT HAS A USABLE LIFE OF 5 YEARS FROM

DATE OF MANUFACTURE

R 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-3200(-

1) 25-60-

42 EVERY 2 YEARS: PERFORM AN INSPECTION IAW

CMM INCLUDING WEIGHT CHECK OF CO2

CYLINDER

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-3100(-

1) 25-60-

43 THE INTERVALS BETWEEN INSPECTIONS AND

TESTS, PER ATA 100, IS TO BE DETERMINED

BETWEEN PUBLIC AUTHORITY AND EACH

CARRIER, AND SHOULD TAKE INTO

CONSIDERATION SUCH THINGS AS

OPERATIONAL AND SERVICE HISTORY,

FREQUENCY OF HANDLING, ENVIRONMENTAL

CONDITION, ETC. FOR LIFE VEST UP AND

INCLUDING 10 YEARS EVERY 5 YEARS

PERFORM PROOF TEST IAW CMM LIFE VEST

OLDER THAN 10 YEARS AT EVERY REGULAR

SERVICE: PERFORM PROOF TEST IAW CMM

EVERY 5 YEARS: PERFORM ORAL TUBE

ATTACHMENT STRENGHT TEST IAW CMM

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-3000 25-60-

45 EVERY 2 YEARS: PERFORM AN INSPECTION IAW

CMM INCLUDING WEIGHT CHECK OF CO2

CYLINDER

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 SLIDE/RAF

T 70167 A30466-

xxx

SERIES

A30476-

xxx

SERIES 25-60-

49 EVERY 3 YEARS: FOR EVACUATION SYSTEMS

UP TO AND INCLUDING 15 YEARS OF AGE OR IF

INFLATABLE, RESERVOIR, HOSE AND

APPLICABLE LIFE-LIMITED ITEMS ARE

REPLACED AT 15 YEARS FOR THE NEXT 15

YEARS CHECK/TEST INCL. HYDROSTATIC TEST

EVERY YEAR FOR EVACUATION SYSTEMS

AFTER 15 YEARS OF IN-SERVICE LIFE:

CHECK/TEST INCL. HYDROSTATIC TEST EVERY 3

YEARS: PERFORM A SYSTEM CHECK OF

INFLATION SYSTEM CONCERNING THE

REQUALIFICATION AND SERVICE LIFE OF

RESERVOIR CMM REFERS TO DOT

SPECIFICATIONS AND EXEMPTIONS. VENDOR

RECOMMENDATIONS SERVE AS GENERAL

GUIDELINE. NOTE: VERIFY INCORPORATION OF

ALL OUTSTANDING SERVICE BULLETINS AND

SERVICE INFORMATION LETTERS. FOR

INFLATION SYSTEMS SEE CMM 25-65-42.

SERVICE LIFE OF ELT BATTERY: 3.5 YEARS

N 256531-0503-1

256531-L503-1 EMERGEN

CY

LOCATOR

TRANSMIT

TER 59364 607690-4

SERIES

1 / 2 25-60-

60 EVERY 2 YEARs: REPLACE WATER-SOLUBLE

TAPE EVERY 5 YEARS: REPLACE BATTERY.

N 256200-0504-1

256200-L504-1 LIFE

PRESERV 78673 S-8600(-

1) 25-60-

65 EVERY 2 YEARS: PERFORM AN INSPECTION IAW

CMM INCLUDING WEIGHT CHECK OF CO2

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 10 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

ER CYLINDER

N 256200-0504-1

256200-L504-1 INFLATAB

LE LIFE

JACKET K0068 0000214

X,

0000215

0,

0000216

3,

0000217

3,

0000220

X,

0000221

0,

0000222

X,

0000223

X,

0000224

9,

0000226

20,

0000228

X,

0000229

3,

0000260

X 25-60-

68 EVERY 10 YEARS: - LIFEJACKET ARE LESS THAN

20 YEARS OLD - AND PN IS: 00002260, 00002285,

00002289, 00002293, 00002602, 00002603 OR

00002606 DO A MAINTENANCE CHECK. EVERY 5

YEARS: - LIFEJACKET ARE LESS THAN 20 YEARS

OLD - AND PN IS: NOT 0002260, 00002285,

00002289, 00002293, 00002602, 00002603 OR

00002606. DO A MAINTE NANCE CHECK. EVERY

12 MONTHS: -LIVE JACKED IS OLDER THAN 20

YEARS DO A MAINTENANCE CHECK. IN

ADDITION PERFORM A SAMPLE PROGRAM IAW

CMM

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-11000-

( ) 25-60-

90 LIFE PRESERVER SHOULD BE INSPECTED AND

LEAK TESTED AT REGULAR INTERVALS

BETWEEN INSPECTIONS AND TESTS. THE

INTERVALS BETWEEN INSPECTION AND LEAK

TEST, PER ATA 100, IS TO BE DETERMINED

BETWEEN THE AUTHORITY AND EACH CARRIER,

AND SHOULD TAKE INTO CONSIDERATION SUCH

THINGS AS OPERATIONAL AND SERVICE

HISTORY, FREQUENCY OF HANDLING,

ENVIRONMENTAL CONDITIONS, ETC. EVERY 5

YEARS FOR THE FIRST 10 YEARS FROM THE

DATE OF MANUFACTURE: PERFORM A PROOF

TEST IAW CMM AFTER 10 YEARS AT EACH

REGULAR SERVICE CHECK THEREAFTER:

PERFORM A PROOF TEST IAW CMM EVERY 5

YEARS: PERFORM ORAL TUBE ATTACHMENT

STRENGTH TEST IAW CMM

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 SLIDE

EVACUATI

ON

SYSTEMS 70167 A29784-

xxx-xx

SERIES

A29785-

xxx-xx

SERIES

A29786-

xxx-xx

SERIES 25-61-

11 EVERY 3 YEARS: FOR EVACUATION SYSTEMS

UP TO AND INCLUDING 15 YEARS OF AGE OR IF

INFLATABLE, RESERVOIR, HOSE AND

APPLICABLE LIFE-LIMITED ITEMS ARE

REPLACED AT 15 YEARS FOR THE NEXT 15

YEARS CHECK/TEST INCL. HYDROSTATIC TEST

EVERY YEAR FOR EVACUATION SYSTEMS

AFTER 15 YEARS OF IN-SERVICE LIFE:

CHECK/TEST INCL. HYDROSTATIC TEST EVERY 3

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 11 RE

V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

YEARS: PERFORM A SYSTEM CHECK OF

INFLATION SYSTEM CONCERNING THE

REQUALIFICATION AND SERVICE LIFE OF

RESERVOIR CMM REFERS TO DOT

SPECIFICATIONS AND EXEMPTIONS. VENDOR

RECOMMENDATIONS SERVE AS GENERAL

GUIDELINE. NOTE: VERIFY INCORPORATION OF

ALL OUTSTANDING SERVICE BULLETINS AND

SERVICE INFORMATION LETTERS. FOR

INFLATION SYSTEMS SEE CMM 25-61-11.

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 INFLATAB

LE

EVACUATI

ON SLIDE

RAFT 70167 D30546-

XXX

PER S.B.

003-25-

21,

REFER

TO CMM

25-61-39

FOR

NEW

CONFIG

URATIO

NS

D30545-

XXX 25-61-

17 EVERY 3 YEARS: FOR EVACUATION SYSTEMS

UP TO AND INCLUDING 15 YEARS OF AGE

CHECK/TEST INCL. HYDROSTATIC TEST EVERY

YEAR FOR EVACUATION SYSTEMS AFTER 15

YEARS OF IN-SERVICE LIFE: CHECK/TEST INCL.

HYDROSTATIC TEST EVERY 3 YEARS: PERFORM

A SYSTEM CHECK OF INFLATION SYSTEM

CONCERNING THE REQUALIFICATION AND

SERVICE LIFE OF RESERVOIR CMM REFERS TO

DOT SPECIFICATIONS AND EXEMPTIONS.

VENDOR RECOMMENDATIONS SERVE AS

GENERAL GUIDELINE. NOTE: VERIFY

INCORPORATION OF ALL OUTSTANDING

SERVICE BULLETINS AND SERVICE

INFORMATION LETTERS. FOR INFLATION

SYSTEMS SEE CMM 25-65-02. POWER UNIT

BATTERY 5 YEARS USABLE LIFE ELT-BATTERY

(D30545-101, -201, D30546-101, -105, -201, -205

only) SERVICE LIFE: 3 YEARS (3 1/2 YEARS)

R 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 78673 S-10002-

( ) 25-61-

17 LIFE PRESERVER SHOULD BE INSPECTED AND

LEAK TESTED AT REGULAR INTERVALS

BETWEEN INSPECTIONS AND TESTS. THE

INTERVALS BETWEEN INSPECTION AND LEAK

TEST, PER ATA 100, IS TO BE DETERMINED

BETWEEN THE AUTHORITY AND EACH CARRIER,

AND SHOULD TAKE INTO CONSIDERATION SUCH

THINGS AS OPERATIONAL AND SERVICE

HISTORY, FREQUENCY OF HANDLING,

ENVIRONMENTAL CONDITIONS, ETC. EVERY 5

YEARS FOR THE FIRST 10 YEARS FROM THE

DATE OF MANUFACTURE: PERFORM A PROOF

TEST IAW CMM AFTER 10 YEARS AT EACH

REGULAR SERVICE CHECK THEREAFTER:

PERFORM A PROOF TEST IAW CMM EVERY 5

YEARS: PERFORM ORAL TUBE ATTACHMENT

STRENGTH TEST IAW CMM

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 FORWARD

AFT DOOR

SLIDE

ASSEMBL

Y 0ACH4 7A1298-

XXX 25-62-

01 EVERY 3 YEARS: PERFORM AN OVERHAUL IAW

CMM. INCLUDING REGULATOR VALVE AND

HYDROSTATIC TEST OF CYLINDER. OPERATORS

SHOULD NOTE THAT THESE INTERVALS MAY BE

SHORTENED DUE TO LOCAL REGULATORY

REQUIREMENTS OR IN RESPONSE TO INSERVICE ENVIRONMENTAL FACTORS, RESULTS

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

OF PERIODIC TESTING AND MAINTENANCE OR

AGE. REFER TO VENDOR NEWSLETTER 25-163

FOR ADDITIONAL INFORMATION REGARDING

INSPECTION OF AGING EVACUATION SYSTEMS.

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 MID-DOOR

SLIDE

ASSEMBL

Y 0ACH4 7A1296-

XXX 25-62-

03 EVERY 3 YEARS: PERFORM AN OVERHAUL IAW

CMM. INCLUDING REGULATOR VALVE AND

HYDROSTATIC TEST OF CYLINDER. OPERATORS

SHOULD NOTE THAT THESE INTERVALS MAY BE

SHORTENED DUE TO LOCAL REGULATORY

REQUIREMENTS OR IN RESPONSE TO INSERVICE ENVIRONMENTAL FACTORS, RESULTS

OF PERIODIC TESTING AND MAINTENANCE OR

AGE. REFER TO VENDOR NEWSLETTER 25-163

FOR ADDITIONAL INFORMATION REGARDING

INSPECTION OF AGING EVACUATION SYSTEMS.

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 EMERGEN

CY EXIT

SLIDE

ASSEMBL

Y 0ACH4 7A1299-

XXX

SERIES 25-62-

04 EVERY 3 YEARS: PERFORM AN OVERHAUL OF

SLIDE AND INFLATION SYSTEM IAW CMM

INCLUDING REGULATOR VALVE AND

HYDROSTATIC TEST OF CYLINDER

ADDITIONALLY FOR EVACUATION SYSTEMS

WITH AN AGE OF 15 YEARS OR GREATER:

EVERY YEAR (ANNUALLY): PERFORM A

MAINTENANCE INSPECTION/CHECK OF SLIDE

IAW CMM USEFUL LIFE FOR DME POWER UNITS:

4 YEARS USEFUL LIFE FOR BASEWEST POWER

UNITS: 5 YEARS

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 FORWARD

/AFT

DOOR

SLIDE/RAF

T

ASSEMBL

Y 0ACH4 7A1300-

XXX 25-62-

05 EVERY 3 YEARS: PERFORM AN OVERHAUL OF

SLIDE AND INFLATION SYSTEM IAW CMM.

USEFUL LIFE FOR POWER UNITS: 4 YEARS.

R 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 MID-DOOR

SLIDE/RAF

T

ASSEMBL

Y 0ACH4 7A1359-

XXX 25-62-

06 EVERY 3 YEARS: PERFORM AN OVERHAUL OF

SLIDE AND INFLATION SYSTEM IAW CMM

INCLUDING REGULATOR VALVE AND

HYDROSTATIC TEST OF CYLINDER

ADDITIONALLY FOR EVACUATION SYSTEMS

WITH AN AGE OF 15 YEARS OR GREATER:

EVERY YEAR (ANNUALLY): PERFORM A

MAINTENANCE INSPECTION/CHECK OF SLIDE

IAW CMM OPERATORS SHOULD NOTE THAT

THESE INTERVALS MAY BE SHORTENED DUE TO

LOCAL REGULATORY REQUIREMENTS OR IN

RESPONSE TO IN-SERVICE ENVIRONMENTAL

FACTORS, RESULTS OF PERIODIC TESTING AND

MAINTENANCE OR AGE. USEFUL LIFE FOR

POWER UNIT: 4 YEARS

N 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2 FORWARD

/AFT

DOOR

SLIDE/RAF 0ACH4 7A1300-

XXX 25-62-

09 EVERY 3 YEARS: PERFORM AN OVERHAUL OF

SLIDE AND INFLATION SYSTEM IAW CMM

INCLUDING REGULATOR VALVE AND

HYDROSTATIC TEST OF CYLINDER

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

256111-L503-3

256111-L504-3 T

ASSEMBL

Y ADDITIONALLY FOR EVACUATION SYSTEMS

WITH AN AGE OF 15 YEARS OR GREATER:

EVERY YEAR (ANNUALLY): PERFORM A

MAINTENANCE INSPECTION/CHECK OF SLIDE

IAW CMM OPERATORS SHOULD NOTE THAT

THESE INTERVALS MAY BE SHORTENED DUE TO

LOCAL REGULATORY REQUIREMENTS OR IN

RESPONSE TO IN-SERVICE ENVIRONMENTAL

FACTORS, RESULTS OF PERIODIC TESTING AND

MAINTENANCE OR AGE. USEFUL LIFE FOR

POWER UNIT: 4 YEARS USEFUL LIFE FOR

BASEWEST POWER UNITS: 5 YEARS

N 256111-0504-3

256111-L504-3 RESERVOI

R

ASSEMBL

Y 0ACH4 4A3206

SERIES 25-62-

11 CONCERNING THE REQUALIFICATION AND

SERVICE LIFE OF RESERVOIR CMM REFERS TO

DOT SPECIFICATIONS AND EXEMPTIONS.

VENDOR RECOMMENDATIONS SERVE AS

GENERAL GUIDELINE. EVERY 3 YEARS:

PERFORM AN OVERHAUL INCL. HYDROSTATIC

TEST CYLINDERS RETESTED PRIOR TO JULY 1 ,

2001 MUST BE RETESTED WITHIN 3 YEARS OF

THE RETEST DATE MARKED ON THE CYLINDER.

CYLINDERS MANUFACTURED OR RETESTED

AFTER JULY 1 , 2001 MUST BE REINSPECTED

AND HYDROSTATICALLY RETESTED AT LEAST

EVERY 5 YEARS. SERVICE LIFE OF CYLINDER: 15

YEARS

N 256111-0503-2

256111-0503-3

256111-0504-3

256111-L503-2

256111-L503-3

256111-L504-3 DOOR 3

SLIDE/

RAFT 0ACH4 7A1510-

XXX 25-62-

13 OPERATORS SHOULD NOTE THAT INTERVAL

MAY NEED TO BE SHORTENED DUE TO LOCAL

REGULATORY MAINTENANCE OR IN RESPONSE

TO IN-SERVICE ENVIRONMENTAL FACTORS,

RESULTS OF PERIODIC TESTING AND

MAINTENANCE OR AGE. EVERY 3 YEARS:

PERFORM A FUNCTIONAL CHECK, AN

INSPECTION AND AN OVERHAUL IAW. CMM INCL.

OVERHAUL OF REGULATOR VALVE AND

HYDROSTATIC TESTING OF CYLINDER (IAW CMM

25-62-19 AND CMM 25-62-31) INCL. OVERHAUL OF

ASPIRATORS (IAW CMM 25-62-18 AND CMM 25-

62-30) REFER TO VENDOR NEWSLETTER 25-163

FOR ADDITIONAL INFORMATION REGARDING

INSPECTION OF AGING EVACUATION SYSTEMS.

N 256200-0504-1

256200-L504-1 LIFE

JACKET

ASSY F6101 153 445

153 697 25-62-

30 EVERY 2 YEARS: PERFORM A PERIODIC

INSPECTION IAW CMM

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 70167 D21343-

XXX

D21344-

XXX 25-64-

03 THE INTERVALS FOR RECERTIFICATION, PER

ATA 100, IS TO BE DETERMINED BETWEEN

PUBLIC AUTHORITY AND EACH CARRIER EVERY

5 YEARS: PERFORM CHECK AND TEST OF LIFE

PRESERVER IAW CMM

N 256111-0504-3

256111-L504-3 RESERVOI

R AND

VALVE 70167 D17925-

xxx

SERIES 25-65-

02 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. INSTRUCTIONS PROVIDED BY

VENDOR SERVE ONLY AS GENERAL GUIDELINE.

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

ASSEMBL

Y MID

DOOR

P/N

D17925-

101

FORWA

RD AND

AFT

DOOR

P/N

D17925-

103, -113

EMERG

ENCY

EXIT P/N

D17925-

107, -111 ALL INSPECTIONS AND TESTING SHALL BE

PERFORMED IAW. CMM AND APPLICABLE

REGULATIONS (E.G. RE-QUALIFICATIONS AND

SERVICE LIFE OF RESERVOIR) EVERY 3 YEARS:

PERFORM THE CHECKS AND TESTS OF

INFLATION SYSTEM IAW CMM

N 256111-0504-3

256111-L504-3 RESERVOI

R AND

VALVE

ASSEMBL

Y 70167 D17925-

xxx

SERIES

MID

DOOR

P/N

D17925-

105

FORWA

RD AND

AFT

DOOR

P/N

D17925-

109

EMERG

ENCY

EXIT P/N

D17925-

107, -111 25-65-

03 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. INSTRUCTIONS PROVIDED BY

VENDOR SERVE ONLY AS GENERAL GUIDELINE.

ALL INSPECTIONS AND TESTING SHALL BE

PERFORMED IAW. CMM AND APPLICABLE

REGULATIONS (E.G. RE-QUALIFICATIONS AND

SERVICE LIFE OF RESERVOIR) EVERY 3 YEARS:

PERFORM THE CHECKS AND TESTS OF

INFLATION SYSTEM IAW CMM

N 256532-0504-1

256532-L504-1 ELECTRO

NIC

MEGAPHO

NE 98905 A12S

A12SA 25-65-

04 EVERY YEAR: REPLACE BATTERIES NO VENDOR

INTERVALS RELATED TO OPERATIONAL CHECK

OF MEGAPHONE REFLECTED IN CMM

N 256111-0504-3

256111-L504-3 10

PERSON

LIFERAFT

RESERVOI

R AND

VALVE

ASSEMBL

Y 70167 D17924-

101 25-65-

06 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. INSTRUCTIONS PROVIDED BY

VENDOR SERVE ONLY AS GENERAL GUIDELINE.

ALL INSPECTIONS AND TESTING SHALL BE

PERFORMED IAW. CMM AND APPLICABLE

REGULATIONS (E.G. RE-QUALIFICATIONS AND

SERVICE LIFE OF RESERVOIR) EVERY 3 YEARS

(UP TO AND INCLUDING 15 YEARS): PERFORM

THE CHECKS AND TESTS OF INFLATION SYSTEM

IAW CMM

N 256200-0504-1

256200-L504-1 LIFE

JACKET F6101 155102-1

155103-1 25-65-

08 INTERVALS ARE IN ACCEPTANCE WITH

STATEMENTS OF LOCAL INSPECTION

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

ASSY AUTHORITIES. EVERY 2 YEARS: PERFORM

INSPECTION SERVICE LIFE OF THE BATTERY: 2

YEARS

N 256531-0503-1

256531-L503-1 EMERGEN

CY

LOCATOR

TRANSMIT

TER F5542 JE2 25-65-

33 NO VENDOR INTERVALS REFLECTED IN CMM

BATTERY REPLACEMENT IAW PRINTED LABEL

ON BATTERY PACK, OPERATING HOURS OR ON

CONDITION

N 256200-0504-1

256200-L504-1 LIFE

PRESERV

ER 0ACH4 5SV1025

-xxx

SERIES 25-69-

01 EVERY 1 YEAR: PERFORM AN OVERHAUL IAW

CMM

N 262411-0504-2

262411-L504-2 CABIN

FIRE

EXTINGUI

SHER F1085 1708337

B4 26-20-

01 EVERY 12 MONTHS: PERFORM AN

EXTINGUISHER TEST. EVERY 18 MONTHS:

PERFORM AN EXTINGUISHER CHECK IAW CMM

EVERY 120 MONTHS: PERFORM A HYDROSTATIC

TEST AFTER EVERY MAINTENANCE OPERATION

PERFORM A WEIGHT CHECK

R 262111-0504-2

262211-0504-2

262111-L504-2

262211-L504-2 224, 378

AND 630

CUBIC

INCH FIRE

EXTINGUI

SHERS 05167 3360000

5(-X)

3410000

5-1

3460000

6(-X) 26-20-

05 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. INSTRUCTIONS PROVIDED BY

VENDOR SERVE ONLY AS GENERAL GUIDELINE.

ALL INSPECTIONS AND TESTING SHALL BE

PERFORMED IAW. CMM AND APPLICABLE

REGULATIONS EVERY 10 YEARS: DISCARD

CARTRIDGE FOR MORE INFORMATION SEE

PACIFIC SCIENTIFIC SIL NO. 26-0233E AND SIL

NO. 26-0237D

R 262311-0504-2

262312-0504-1

262311-L504-2

262312-L504-1 630, 800

AND 1600

CUBIC

INCH FIRE

EXTINGUI

SHERS

(APU) 05167 346000X

X

3460002

5-1

3520000

X(-X) 26-20-

06 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. INSTRUCTIONS PROVIDED BY

VENDOR SERVE ONLY AS GENERAL GUIDELINE.

ALL INSPECTIONS AND TESTING SHALL BE

PERFORMED IAW. CMM AND APPLICABLE

REGULATIONS EVERY 10 YEARS: DISCARD

CARTRIDGE FOR MORE INFORMATION SEE

PACIFIC SCIENTIFIC SIL NO. 26-0233E AND SIL

NO. 26-0237D

R 262111-0504-2

262111-L504-2 FIRE

EXTINGUI

SHER

CONTAINE

R 61423 A813600

-XX 26-20-

06 NO VENDOR INTERVALS REFLECTED IN CMM

FOR HYDROSTATIC TEST REFER TO SIL 96-2,

DOT 49 CFR 180.205 and FAA INSPECTOR'S

HANDBOOK 8300.10 FOR WEIGHT CHECK REFER

TO SIL 96-2 FOR MAINTENANCE AND DISCARD

OF CARTRIDGE REFER TO CMM 26-21-34

N 262411-0504-1

262411-0504-2

262411-L504-1

262411-L504-2 FIRE

EXTINGUI

SHER 61423 870904

870905

870906 26-20-

08 EVERY 6 MONTHS: PERFORM A WEIGHT CHECK

EVERY 5 YEARS: PERFORM A HYDROSTATIC

TEST

N 262411-0504-2

262411-L504-2 PORTABL

E FIRE

EXTINGUI

SHER Z4003 BO100S

WITH

BRACKE

T 00300

(PREVIO

US PN: 26-20-

10 EVERY 5 YEARS: PERFORM OVERHAUL

INCLUDING HYDROSTATIC TEST

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

11600-9,

GRAVIN

ER PN:

HA 1002)

BO100S

WITHOU

T

BRACKE

T 00313

(PREVIO

US PN:

HA1002-

6,

GRAVIN

ER PN:

HA 1002-

06)

R 262411-0504-1

262411-L504-1 PORTABL

E FIRE

EXTINGUI

SHER U3061 BA51015

XX

BA51016

XXX

BA51012

S

BA20703

BA20789 26-20-

15 EVERY YEAR: PERFORM AN INSPECTION IAW

CMM (INCLUSIVE WEIGHT CHECK OR, IF GAUGE

IS FITTED, CHECK THAT NEEDLE IS IN GREEN

SECTOR)

N 262411-0504-1

262411-0504-2

262411-L504-1

262411-L504-2 AIRCRAFT

FIRE

EXTINGUI

SHER

LIQUID

TYPE 61423 870317

871685

890017

890275

891318

892480

893948 26-20-

20 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. ALL INSPECTIONS AND TESTING

SHALL BE PERFORMED IAW. CMM AND

APPLICABLE REGULATIONS EVERY 5 YEARS:

PERFORM A PROOF PRESSURE TEST. REFER

TO 29 CFR 1910.157 EVERY YEAR: PERFORM A

WEIGHT CHECK

N 262411-0504-1

262411-L504-1 BCF AND

WATER

GLYCOL

PORTABL

E FIRE

EXTINGUI

SHER U3061 BA20703

-SERIES

BA21775

-SERIES

BA23044

-SERIES

BA51012

-SERIES

BA51015

-SERIES

BA61016

-SERIES 26-20-

30 EVERY YEAR: PERFORM A CHECK IAW CMM

INCLUDING WEIGHT CHECK IF GAUGE IS FITTED

CHECK THAT GAGE POINTER IS IN GREEN BAND.

NO FURTHER INTERVALS REFLECTED WITHIN

CMM. FOR INTERVALS CONCERNING CLEANING,

INSPECTION AND OVERHAUL CONSULT

NATIONAL OR LOCAL AVIATION AUTHORITY

CONTAINER LIFE: 10 YEARS

N 262411-0504-1

262411-0504-2

262411-L504-1

262411-L504-2 PORTABL

E FIRE

EXTINGUI

SHER 61423 891083(-

01)

991825 26-20-

40 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. ALL INSPECTIONS AND TESTING

SHALL BE PERFORMED IAW. CMM AND

APPLICABLE REGULATIONS EVERY 6 MONTHS:

PERFORM A WEIGHT CHECK EVERY 3 YEARS: IF

CYLINDER PN IS 241914 (3HT) PERFORM A

HYDROSTATIC TEST EVERY 5 YEARS: IF

CYLINDER PN IS 62238 (3AA) PERFORM A

HYDROSTATIC TEST

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

N 262111-0504-2

262111-L504-2 FIRE

EXTINGUI

SHER

CONTAINE

R 61423 A823700

-21 26-20-

89 NO VENDOR INTERVALS REFLECTED IN CMM

FOR HYDROSTATIC TEST AND INSPECTION

INTERVALS OF CONTAINERS REFER TO SIL 96-2,

DOT 49 CFR 180.205 AND FAA INSPECTOR'S

HANDBOOK 8300.10 FOR WEIGHT CHECK REFER

TO SIL 96-2 FOR MAINTENANCE AND DISCARD

OF CARTRIDGE REFER TO CMM 26-21-34

N 262111-0504-2

262111-L504-2 FIRE

EXTINGUI

SHER

CONTAINE

R 61423 895240(-

xx)

SERIES 26-21-

10 NO VENDOR INVERVALS REFLECTED IN CMM

FOR HYDROSTATIC TEST REFER TO DOT 49 CFR

180.205 / CGA PAMPHLET C1 CONCERNING

WEIGHT CHECK REFER TO SIL 92-2 FOR

MAINTENANCE AND DISCARD OF CARTRIDGE

REFER TO CMM 26-21-34

N 262211-0504-2

262211-L504-2 FIRE

EXTINGUI

SHER

CONTAINE

R 61423 895877 /

896066

CARTRI

DGE:

876296(-

X) 26-21-

27 NO VENDOR INTERVALS REFLECTED IN CMM

FOR HYDROSTATIC TEST AND INSPECTION

INTERVALS OF CONTAINERS REFER TO SIL 96-2,

DOT 49 CFR 180.205 AND FAA INSPECTOR'S

HANDBOOK 8300.10 FOR WEIGHT CHECK REFER

TO SIL 96-2 FOR MAINTENANCE AND DISCARD

OF CARTRIDGE REFER TO CMM 26-21-34

R 262113-0504-1

262212-0504-1

262312-0504-1

262113-L504-1

262212-L504-1

262312-L504-1 POWER

DEVICE

CARTRID

GES 61423 252066,

262299-

X,

446090-

X

446158

446161-

X

446189-

X

446201

446203

446290

446307

446384-

X

446518-1

446582-

X

446616

446617

446665

446736

446738

446754

446842

446850

472001-

XX

841155-

X

872194-

01 26-21-

34 DIFFERENT LIFE LIMITS ACCORDING TO PN.

MAXIMUM 3-10 YEARS. REFER TO CMM

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

872627-

XX

873364-

X

873571-

XX

874000-

XX

874103

874310

876296-

X

876299-

XX

876561-

X

877279

877723

877744-

XX

878269-

X

878492-

X

878562-

X

878563-

X

893613-

X

894846-

X

895188-

X

895189

895408-

X

895409-

X

897776-

X

897899-

X

898760

898997

899855-

X

A800545

-X

A805300

-XX

R 262411-0504-1

262411-0504-2

262411-L504-1 HALON

1211

PORTABL 61423 466040

466090

898052 26-21-

39 EVERY 12 YEARS: PERFORM A HYDROSTATIC

TEST (REFER TO 29 CFR 1910.157) NO FURTHER

INTERVALS REFLECTED WITHIN CMM. CMM

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

262411-L504-2 E FIRE

EXTINGUI

SHERS REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. FOR INTERVALS CONCERNING

INSPECTION, OVERHAUL OR WEIGHT CHECK

CONSULT NATIONAL OR LOCAL AVIATION

AUTHORITY. ALL INSPECTIONS AND TESTING

SHALL BE PERFORMED IAW. CMM AND

APPLICABLE REGULATIONS.

N 262411-0504-2

262411-L504-2 CABIN

FIRE

EXTINGUI

SHER F1085 1708337

B4 26-24-

04 LIFE LIMIT: 10 YEARS 26-24-04 OBSOLETE AND

SUPERSEDED BY CMM 26-20-01.

N 262411-0504-2

262411-L504-2 PORTABL

E FIRE

EXTINGUI

SHER D0243 74-00

74-20

74-21

76-00 26-24-

05 EVERY 2 YEARS: PERFORM AN INSPECTION IAW

CMM INCLUDING WEIGHT CHECK EVERY 10

YEARS: PERFORM A HYDROSTATIC TEST.

(VENDOR RECOMMENDATION IS TO REPLACE

THE EXTINGUISHER)

N 262500-0504-1

262500-L504-1 DISPOSAB

LE FIRE

EXTINGUI

SHER 61423 A800100

-X

A825100

-X(X)

A826300

-X

A826700

-1

BAC10-

61909-X

G800100

-X

G825100

-XX

G826300

-1

G826700

-1

474276

474453-

X 26-25-

04 EVERY 5 YEARS: PERFORM A VISUAL CHECK

AND WEIGHT CHECK HYDROSTATIC TESTS ARE

NOT APPLICABLE. REFER TO 49 CFR 180.209(D)

N 262411-0504-2

262411-L504-2 PORTABL

E FIRE

EXTINGUI

SHER U3061 BA

51015

BA

51016

BA51015

/G

BA61016

/WG 26-90-

29 EVERY YEAR: PERFORM AN INSPECTION

INCLUDING WEIGHT CHECK. LIFE LIMIT:

10YEARS

R 313100-0503-2

313100-L503-2 UNDERWA

TER

ACOUSTIC

BEACON 94970 N15F210

B (NSN

5845-01-

009-

4702) 31-10-

15 EVERY 3 MOUNTHS (OR ON CONDITION):

BEACON CLEANING AND TESTING EVERY 18

MONTHS: BATTERY REPLACEMENT

N 313100-0503-2

313100-L503-2 RECORDE

R, 97896 980-

4100AXX 31-30-

32 EVERY 4 YEARS FOR THE DK100 ULD: ULB

BATTERY REPLACEMENT (REFER TO RELATED

# MAINTENANCE PLANNING DOCUMENT

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ION MANUFACT

URER /

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FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

UNIVERSA

L FLIGHT

DATA

(UFDR) S 980-

4100AXX

N 980-

4100AX

US 980-

4100AX

UN 980-

4100BX

US 980-

4100BX

UN 980-

4100DX

XS 980-

4100DX

XN 980-

4100DX

US 980-

4100DX

UN 980-

4101-001

980-

4101-002 TECHNICAL USER MANUAL). EVERY 6 YEARS

FOR THE ELP362D IF SERIAL NUMBER BEGINS

WITH 'S': ULB BATTERY REPLACEMENT (REFER

TO RELATED TECHNICAL USER MANUAL). IF

SERIAL NUMBER BEGINS WITH AN 'S', NO

BATTERY MAINTENANCE IS REQUIRED. DO NOT

REMOVE BATTERY AT ANY TIME. RETURN ULD

TO MANUFACTURER FOR SERVICE.

PREVENTIVE MAINTENANCE OF COMPONENTS

IAW CMM FIG 615 BEARINGS ARE TO BE

PERIODICALLY CHECKED AND REPLACED IAW

CMM FIG 603 SERVICE LIFE: 20 YEARS OR 60.000

HOURS OF OPERATION REFER ALSO TO

HONEYWELL DOCUMENT NO. 032-000

N 313100-0503-2

313100-L503-2 UNIVERSA

L FLIGHT

DATA

RECORDE

R 97896 980-

4100-

XXXX

SERIES 31-30-

33 EVERY 4 YEARS FOR THE DK100 ULD: ULB

BATTERY REPLACEMENT (REFER TO RELATED

TECHNICAL USER MANUAL). EVERY 6 YEARS

FOR THE ELP362D IF SERIAL NUMBER BEGINS

WITH 'S': ULB BATTERY REPLACEMENT (REFER

TO RELATED TECHNICAL USER MANUAL). IF

SERIAL NUMBER BEGINS WITH AN 'S', NO

BATTERY MAINTENANCE IS REQUIRED. DO NOT

REMOVE BATTERY AT ANY TIME. RETURN ULD

TO MANUFACTURER FOR SERVICE.

PREVENTIVE MAINTENANCE OF COMPONENTS

IAW CMM FIG 615 BEARINGS ARE TO BE

PERIODICALLY CHECKED AND REPLACED IAW

CMM FIG 603 SERVICE LIFE: 20 YEARS OR 60.000

HOURS OF OPERATION REFER ALSO TO

HONEYWELL DOCUMENT NO. 032-000

N 313100-0503-2

313100-0504-1

313100-L503-2

313100-L504-1 DIGITAL

FLIGHT

DATA

RECORDE

R 92685 10077A5

00-xxx

SERIES 31-31-

03 EVERY 3000 OPERATING HOURS: PERFORM

INSPECTION, CHECK AND FUNCTIONAL TEST

IAW CMM AFTER 5 YEARS OR 15.000 HOURS OF

OPERATION THE DFDR SHOULD BE RESTORED

TO ZERO TIME STATUS. BATTERY

REPLACEMENT DEPENDS ON DATE LABEL ON

BODY OF THE BEACON

N 313100-0503-2

313100-0504-1

313100-L503-2

313100-L504-1 DIGITAL

FLIGHT

DATA

RECORDE

R 92685 10077A5

00-801

(WITHO

UT

BEACON

)

10077A5

00-803 31-31-

04 NO VENDOR INTERVALS REFLECTED IN CMM

PERFORM PERIODIC MAINTENANCE IAW CMM

(FIG 501) BATTERY REPLACEMENT DEPENDS ON

DATE STAMPED ON THE BEACON

# MAINTENANCE PLANNING DOCUMENT

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ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

(WITH

BEACON

)

N 313100-0503-2

313100-0504-1

313100-L503-2

313100-L504-1 DIGITAL

FLIGHT

DATA

RECORDE

R 97896 981-

6009- xxx

SERIES 31-31-

05 N0 BATTERY MAINTENANCE IS REQUIRED FOR

THE DK100 ULD (6 YEAR WARRANTY PER

TECHNICAL MANUAL). DO NOT REMOVE

BATTERY AT ANY TIME. AT OR NEAR

EXPIRATION DATE PRINTED ON CASE, RETURN

ULD TO MANUFACTURER FOR SERVICE. FOR

TECHNICAL INFORMATION REFER TO MANUALS

OF DUKANE CORP. SERVICE LIFE BATTERY OF

N15F210B-ULD: PN: 810-418 (PRE DUKANE SB

210B-1-7) PN: 810-418A BATTERY (POST DUKANE

SB 210B-1-7) 2 YEARS IF EMERGENCY LOCATOR

BEACON ELP362D INSTALLED REFER TO ITS

TECHNICAL MANUALS FOR MAINTENANCE

INTERVALS. FOR ADDITIONAL MAINTENANCE

INFORMATION REFER TO ALLIEDSIGNAL

DOCUMENT NO. 060-1699-001

R 313100-0503-2

313100-L503-2 UNDERWA

TER

ACOUSTIC

BEACON 94970 DK100

DK120

DK130

DK140 31-31-

36 EVERY 2 YEARS: BEACON CLEANING AND

TESTING EVERY 6 YEARS: ULB BATTERY

REPLACEMENT INSTALL NEW O-RING

R 351111-0504-1

351111-L504-1 CYLINDER

AND

VALVE

ASSEMBLI

ES F5341 GSM

1114

(SCOTT

891111-

14) GSM

1414

(SCOTT

891211-

14) GSM

1814

(SCOTT

891311-

14) GSM

2214

(SCOTT

891411-

14) GSM

3214

(SCOTT

891511-

14) 35-11-

41 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. ALL INSPECTIONS AND TESTING

SHALL BE PERFORMED IAW. CMM AND

APPLICABLE REGULATIONS EVERY 3 YEARS:

PERFORM A HYDROSTATIC TEST AFTER 24

YEARS OR 4.380 PRESSURIZATIONS IF DOT 3HT

TYPE DISCARD AND REPLACE CYLINDER

N 351111-0504-1

351111-L504-1 STATIONA

RY

CYLINDER

AND

VALVE

ASSEMBL

Y 53655 891000

SERIES

P/N

ASSEMB

LY:

891XXXXX

CYLIND

ER: 35-28-

91 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. ALL INSPECTIONS AND TESTING

SHALL BE PERFORMED IAW. CMM AND

APPLICABLE REGULATIONS EVERY 3 YEARS:

FOR CYLINDER TYPE DOT 3HT-1850 (-500, -505, -

510, -515, -520) PERFORM A HYDROSTATIC TEST.

EVERY 6 YEARS: PERFORM AN OVERHAUL

SERVICE LIFE OF CYLINDER: 24 YEARS OR 4380

PRESSURISATIONS

# MAINTENANCE PLANNING DOCUMENT

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ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

6084-XX

N 352000-0504-1

352000-L504-1 PORTABL

E

OXYGEN

UNIT 53655 802501-

xx

SERIES

802502-

xx

SERIES

802511-

xx

SERIES

802512-

xx

SERIES

802093-

01 (PN

OF

OXYGE

N

GENERA

TOR) 35-31-

07 NO VENDOR INTERVALS REFLECTED IN CMM

R 352000-0504-1

352000-L504-1 PORTABL

E

CYLINDER

ASSEMBL

Y 80477 900-700-

035-XX 35-31-

07 OVERHAUL PERIOD IS INDEFINITE AS LONG AS

THE UNIT TESTS IAW CMM. PART "TESTING" ARE

SUCCESSFUL IN ADDITION CMM REFERS TO

DOT SPECIFICATIONS OR EXEMPTIONS. ALL

INSPECTIONS AND TESTING SHALL BE

PERFORMED IAW. CMM AND APPLICABLE

REGULATIONS FOR RE-QUALIFICATIONS AND

SERVICE LIFE. E.G. 3AA1800 CYLINDERS SHALL

BE RETESTED EVERY 5 TO 10 YEARS, REFER TO

TITLE 59 CFR, FOR SERVICE LIFE AND RETEST

PERIOD.

R 352000-0504-1

352000-L504-1 PORTABL

E

CYLINDER

ASSEMBL

Y 00543 900-700-

039-XX 35-31-

08 OVERHAUL PERIOD IS INDEFINITE AS LONG AS

THE UNIT TESTS IAW CMM. PART "TESTING" ARE

SUCCESSFUL IN ADDITION CMM REFERS TO

DOT SPECIFICATIONS OR EXEMPTIONS. ALL

INSPECTIONS AND TESTING SHALL BE

PERFORMED IAW. CMM AND APPLICABLE

REGULATIONS FOR RE-QUALIFICATIONS AND

SERVICE LIFE. E.G. 3AA1800 CYLINDERS SHALL

BE RETESTED EVERY 5 TO 10 YEARS, REFER TO

TITLE 59 CFR, FOR SERVICE LIFE AND RETEST

PERIOD.

N 353000-0504-1

353000-L504-1 PORTABL

E

CYLINDER

ASSEMBLI

ES 53655 9700-

SERIES

9800-

SERIES 35-31-

55 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. ALL INSPECTIONS AND TESTING

SHALL BE PERFORMED IAW. CMM AND

APPLICABLE REGULATIONS EVERY 5 YEARS:

PERFORM AN OVERHAUL FOR THE 9700-X

SERIES AND 803668-01 INCLUDING

HYDROSTATIC TEST EVERY 3 YEARS: FOR 9700-

G2A AND 9700-H2A SERIES: PERFORM A

HYDROSTATIC TEST EVERY 6 YEARS: PERFORM

AN OVERHAUL FOR THE 9700-G2A AND 9700-H2A

SERIES. EVERY 5 YEARS: PERFORM AN

# MAINTENANCE PLANNING DOCUMENT

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V. MPD REF. DESIGNAT

ION MANUFACT

URER /

VENDOR

FSCM PARTNU

MBER CMM

REF. VENDOR RECOMMENDATION / VENDOR

INTERVAL

OVERHAUL FOR THE 9800 SERIES INCLUDING

HYDROSTATIC TEST CYLINDER LIFE TIME: -

COMPOSITE (-505, -510): 15 YEARS. - STEEL (-500

THRU 500D, 500, 500A): UNLIMITED AS LONG AS

NOT FAIL INSPECTIONS AND HYDROSTATIC

TESTS

N 353000-0504-1

353000-L504-1 PORTABL

E

CYLINDER

ASSEMBL

Y 53655 5500

SERIES

5600

SERIES 35-32-

18 CMM REFERS TO DOT SPECIFICATIONS OR

EXEMPTIONS. ALL INSPECTIONS AND TESTING

SHALL BE PERFORMED IAW. CMM AND

APPLICABLE REGULATIONS FOR 3AA-1800

STEEL CYLINDER (500 THRU 555A): EVERY 5

YEARS: PERFORM AN OVERHAUL AND

HYDROSTATIC TEST IAW CMM FOR 3HT-1850

STEEL CYLINDER (560 THRU 565) AND E8162-

1850 COMPOSITE CYLINDER (570): EVERY 3

YEARS: PERFORM HYDROSTATIC TEST EVERY 6

YEARS: PERFORM AN OVERHAUL IAW CMM

SERVICE LIFE - E8162-1850 COMPOSITE

CYLINDER (570): 15 YEARS - 3AA-1800 STEEL

CYLINDER (500 THRU 555A):UNLIMITED - 3HT1850 STEEL CYLINDER (560 THRU 565): 24 YEARS

OR 4.380 PRESSURIZATIONS REFER TO CMM 35-

22-26 FOR SERVICING THE PASSENGER MASK

ASSEMBLY

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 4 — MAINTENANCE EVENT PLANNING

EXAMPLES Page 1 

# APPENDIX 4 — MAINTENANCE EVENT PLANNING EXAMPLES

1. GENERAL

The purpose of this appendix is to provide operators with a basic example of a Block Maintenance

Program containing the scheduled maintenance tasks of the A300 MPD. The planning examples should

be the basis for establishing a Block Maintenance Program. However it has to be adjusted by the

operator in accordance with the technical configuration of the aircraft. Tasks not planned in this

appendix are identified in the NC column (not considered).

2. BLOCK MAINTENANCE PROGRAM RULES

Two Block maintenance programs are provided. They are based on a study of the utilization distribution

within the A300 fleet.

1. 800 Flight Hours per Year with a ratio of 1,1 Flight Hours per Flight Cycle

2. 1500 Flight Hours per Year with a ratio of 3,8 Flight Hours per Flight Cycle

Each example covers 12 years of utilization corresponding to the second heavy check. In order to

optimize the planning, some tasks were de-escalated for packaging into the block check. Tasks subject

to sampling are not considered within the planning examples. The following chart shows the maximum

flight hours and Flight Cycles in order to assist operators in selecting their A/C utilization in one of the

three Block maintenance programs in accordance with their A/C utilization.

3. EXAMPLE FORMAT

As these Block maintenance programs are based on the MPD and a pre-determined utilization, they

cannot be used without adjustments. To facilitate operator planning , these examples are provided in

the appendix of the Excel version of this MPD.

Operators should also include all other tasks that are not covered in the MPD, recommended or

mandatory, to complete their maintenance program.

As explained in previous paragraphs, the examples are based on a Block maintenance concept,

however they may be used as a basis for different maintenance concepts. It should be reminded that

these examples are valid for specific utilization envelopes. Consequently if the operator’s utilization

differs significantly from the upper limit of the example, it is suggested that the operators review the

tasks planning in order to see if a more optimized program could be developed to benefit from the new

usage parameter intervals.

In this case AIRBUS can support the operator with maintenance planning and supporting data based on

specific operator requirements (Refer to Customer Services Catalog).

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT Page 1 

# APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT

1. GENERAL

The content of the former MPD Volumes 2 and 3 is available in the following documents:

2. FORMER VOLUME 2 & 3 CONTENT TRANSFER TABLE

CONTENT REFER TO / COMMENT

Former Section 9: Condition Monitoring Items 

# – MPD Appendix 5, below this table

Former Section 10: Aircraft Zoning 

# – AMM Chapter 06–21 (Zoning).

– MRBR Appendix 2 (Aircraft Zoning)

Former Section 11: Access Panels / Access To 

# – AMM Chapter 06–41 (Access Provision)

Former Section 12: Servicing Charts 

# – MPD Appendix 5, below this table

Former Section 13: SSI Illustrations 

# – MPD Appendix 5, below this table.

– (only available in AirN@v).

Former Section 14: Component Data 

# – MPD Appendix 5, below this table

Former Section 15: 

# – Intentionally left blank

Former Section 16: Alternative Sampling Program 

# – MPD Appendix 5, below this table

Former Section 17: Corrosion Prevention and Control

Program (CPCP) 

# – MPD Appendix 5, below this table.

Former Section 18: Vendor Recommendation 

# – MPD Appendix 3 (Vendor Recommendations)

Former Section 19: Low Utilization Program 

# – MPD Appendix 5, below this table

3. SSI ILLUSTRATIONS (only available in AirN@v/Planning)

- Introduction ()

- ATA 52 (

- ATA 53 ()

- ATA 54 ()

- ATA 55 ()

- ATA 57 ()

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT Page 2 

# 4. CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

A. ABSTRACT - APPLICABILITY

This document formalizes the recommendation of the A300 Airworthiness Assurance Task Unit

(AATU) for development of a Corrosion Prevention and Control Program on the following A300

aging airplane series.

A300B1 all series

A300B2 all series

A300B4-100 series

A300B4-200 series

A300C4-200 series

A300F4-200 series



# This document will be periodically revised to take into account reported in-service experience.

B. GENERAL

Aircraft are designed to provide corrosion protection through selection of the proper materials and

finishes, and the use of drainage, sealants, and corrosion inhibitors. These designs are based on

knowledge of what causes corrosion and the types of corrosion that occur in aircraft structure

throughout their service life.

In addition, following a corrosion control program is necessary throughout the service life of the

aircraft to maximize the corrosion protection designed into aircraft. These activities are essential for

controlling corrosion to a predictable and manageable level to ensure structural integrity and

airworthiness for continued flight safety, regardless of aircraft age.

The Structures Program includes requirements to control corrosion to Level 1 or better. To meet

these requirements, operators must have effective corrosion prevention and control procedures

incorporated into the maintenance program for all aircraft reaching or exceeding the implementation

age defined for each airplane area.

This section of MPD provides basic requirements for preventing or controlling corrosion

deteriorations that may jeopardize continuing airworthiness of the A300 fleet.

C. PURPOSE

Airworthiness Authorities require operators to establish a Corrosion Prevention and Control

Program (CPCP) for the A300 airplanes to establish minimum in-service maintenance procedures

for aging aircraft. This Program can be the A300 CPCP Baseline Program, dated Aug 90, or any

alternative program provided it complies with the chapter 1 of the French Airworthiness Directive

(A.D.) referenced 90-196-117(B), which states "control corrosion to level 1 or better".

As airplanes age, corrosion may become more widespread and is more likely to occur. Corrosion

degrades structural integrity and, if uncontrolled, can reduce the inherent ability to sustain the

required loads. To prevent this, a program.

To prevent this, a program has been developed that defines baseline requirements for preventing

or controlling related corrosion problems in the A300 fleet.

# MAINTENANCE PLANNING DOCUMENT

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# It is not the intent of this program to establish rigid requirements for eliminating all corrosion in the

fleet, but to control corrosion below a level that could jeopardize continuing airworthiness.

Operators having an existing corrosion control program that can be shown to meet the objectives of

this program are allowed to continue with their existing program.

Implementation ages and intervals given in this program are based on an “average standard

operation” and reduced values may be required to assure timely prevention of unacceptable

combinations of corrosion and other forms of damage, associated to severe operating conditions.

Guidelines for assessment of the effectiveness of a program are given in Appendix A.

Where a corrosion Service Bulletin exists for an area, it takes precedence over the CPCP task.

D. CORROSION LEVEL DEFINITION

The effectiveness of a Corrosion Control Program is determined for a given airplane area by the

''level'' of corrosion found on the Principal Structural Elements during the scheduled inspections.

For the purpose of this program, the severity of the corrosion damage is categorised into three

''levels'' as follows:

LEVEL 1 CORROSION

Corrosion damage occurring between successive inspections, that can be re-worked/blendedout

within allowable limits as defined by the manufacturer (SRM, SB, etc.).

Or,

Corrosion damage that exceeds allowable limits but can be attributed to an event not typical of

operator's usage of other airplanes in the same fleet (e.g. Mercury spillage).

Or,

Operator experience has demonstrated only light corrosion between each successive inspection

but the latest inspection and cumulative blend-out now exceeds the allowable limits.

LEVEL 2 CORROSION

Corrosion occurring between successive inspections that requires re-work/blend-out which exceeds

allowable limits as defined by manufacturer (SRM, SB, etc.), requiring a repair/reinforcement or

complete or partial replacement of applicable structure.

LEVEL 3 CORROSION

Corrosion found during first or subsequent inspection(s), which is determined (normally by the

operator) to be a potential urgent airworthiness concern requiring expeditious action.

NOTE: When LEVEL 3 corrosion is found, consideration should be given to action required on other

airplanes in the Operator's fleet. Details of the corrosion findings and planned actions should

be expeditiously reported to the appropriate regulatory authority.

NOTE: A light corrosion on the top of a fastener head will be considered Level 1 and any corrosion

on a fastener shank as Level 2.

An effective program is one that c ontrols corrosion of the principal structural elements to level 1 or

better.

Should inspections reveal that corrosion exceeds Level 1 for a given area on a part of a fleet of

aircraft, the inspection interval or the implementation age shall be reduced and/or action taken to

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT Page 4 

# minimize recurrence. In this way the program is self regulating and will adjust itself to the optimum

inspection interval.

E. GENERAL RULES FOR PROGRAM APPLICATION

The effectiveness of the Corrosion Prevention and Control Program is determined by following the

rules listed below which are applicable individually for each task:

1. Corrosion Prevention and Control requirements defined by this document are applicable to

A300 airplanes that reach or exceed the Baseline Program implementation age for each

specified airplane area as quoted in the Structure Program.

2. Maintenance programs for affected airplanes must include corrosion prevention and control

procedures that limit corrosion findings, in all defined structural areas, to Level 1 or better.

When an operator does not have a program or the existing program is shown inadequate, the

Baseline Program must be applied.

In some cases, the Baseline Program may prove inadequate for several reasons such as

continuous exposure to adverse operating conditions, leakage of corrosive cargo or an earlier

history of inadequate maintenance and/or repair. If this happens suitable adjustments must be

made to the baseline program, based on individual operator experience, until corrosion is

controlled to Level 1 or better.

Similarly, when an existing program already more stringent than the Baseline Program is

proved inadequate, suitable adjustments must be made to maintain corrosion to Level 1 or

better.

3. Implementation age and Intervals are provided for each corrosion instruction and are quoted in

calendar time (years).

•

The implementation age is the airplane age, in years since initial delivery, beyond which an

approved Corrosion Prevention and Control Program for each airplane area must be

implemented.

•

For repeat instructions, the interval commences at the time the last instruction was performed.

•

Where repeat Intervals for task instructions have been reduced at the last revision of this

CPCP, e.g. from 9 years to 5 years, the previous Interval may be maintained in an approved

maintenance schedule or reduced if dictated by corrosion findings.

•

Where repeat Intervals for task instructions have been reduced at the last revision of this

CPCP, e.g. from 9 years to 5 years, the previous Interval may be maintained in an approved

maintenance schedule or reduced if dictated by corrosion findings.

4. The program is intended to inspect all items that are susceptible to corrosion in a given area.

Adequate access shall be provided by removal of plates/fairings, equipment/furnishings,

ceiling/wall linings, insulation blankets, etc.

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT Page 5 

# Unless specifically stated in the instruction partial disassembly and lifting rather than removing

items is acceptable where adequate access for the inspection is obtained.

The extent of any suspected corrosion must be clearly identified using appropriate inspection

techniques and/or disassembly when necessary.

5. For a corrosion program to be considered "effective" and meet with the intent of this document

it shall control corrosion to Level 1 or better on all listed areas.

The effectiveness of intervals cannot be determined during program implementation.

Determination of the level at which corrosion is being controlled will be evident at the first

repeat inspection, therefore, inspection interval increase/decrease are not recommended prior

to that time.

6. Individual operators (or group of operators) having airplanes with similar operating

environments and maintenance backgrounds, can extend the Implementation Period for a

given airplane area after a sufficient number of airplane inspections show no indication of

corrosion in that area.

Similarly, extended repeat intervals (e.g. rotational sampling which examine all aircraft) are

allowable as an alternate means of compliance as long as corrosion is controlled to no finding

on an area basis

7. Whenever Level 3 corrosion is found, there shall be an immediate investigation into its cause.

If it is suspected that the condition may be typical of an operator, a fleet campaign should be

initiated and program adjustment made accordingly.

8. Operators without programs or who have ineffective programs shall implement the Baseline

Program. The Baseline Program has been developed for aircraft which experience average

exposure.

Consideration should be given to the type of environment the aircraft is operated in, severity of

past corrosion encountered, and corrosive cargo which may be carried on regular basis when

applying the Baseline Program. These conditions may render the existing program or the

Baseline Program ineffective in maintaining Level 1 or better, necessitating adjustments based

on operator experience.

9. Operators that can prove they have an effective Corrosion Prevention and Control Program in

place may continue with their program. To be effective the program shall inspect all areas

listed in corros ion instructions included in baseline program, and control corrosion to Level 1

or better. If these conditions can be satisfied, the operator may apply for an Alternate Means of

Compliance.

10. The rate at which aircraft corrode is dependant upon numerous factors. Corrosion prevention

systems applied during manufacturing and the operating environment are two major subjects to

be addressed when developing an efficient Corrosion Prevention and Control Program.

For these reasons operators may wish to subdivide their fleets and set up different inspection

intervals to take advantage of a portion of the fleet which may operate exclusively in less

severe conditions e.g. dry climate or a portion which may be newer and have advanced

corrosion protection systems installed during m anufacturing. In this way aircraft that are not

subject to corrosion as quickly as others would not suffer from reduced inspection intervals that

may be imposed on the others.

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT Page 6 

# To assist operators in subdividing a fleet, Appendix "B" contains a list of main corrosion

protection system changes employed during manufacturing. Appendix "B" contains also

general information on typical environmental effects. When using this data as guidance to subdivide a fleet, it should be remembered that the effectiveness of any corrosion protection

system or the influences of environment on corrosion can only truly be evidenced by the

inspection results of the program.

11. Newly acquired/operated used aircraft going through the first inspection in an operators fleet

should neither negatively or positively affect the operator's existing program. Inspection

findings on a newly acquired/operated aircraft reflect the adequacy of the previous operators

program but not that of the current operator. Level 3 findings on a newly acquired aircraft may

indicate the need for all corrosion instructions to be accomplished prior to being placed in

service. The previous operator should be notified of any Level 3 findings.

12. Operators acquiring/operating aircraft that are on an existing corrosion program should

evaluate its adequacy for their planned operation. As an example, aircraft previously used to

carry overnight packages that will now be used to transport livestock need to have program

adjustments made. Similar adjustment need to be considered when switching utilization on

aircraft within an existing fleet.

13. Implementation age and repeat inspection intervals have been established in calendar times

(years). This is because corrosion is most directly related to time as opposed to aircraft hours

or flight cycles. The program established includes aircraft time in and out of service. In other

words, operators will not be, in general, allowed to take credit for out of service periods to

extend corrosion inspection intervals.

14. Occasional short term extension of 10 % up to a maximum of six months, are allowed generally

on implementation age and repeat intervals to accommodate unanticipated scheduling

changes.

15. Repeat Intervals for the Baseline Program are given in calendar periods, including both time in

and out of service. Operators can convert these to equivalent periods of Flight Hours or Flight

Cycles using their current average fleet utilization data, including projected out-of-service

periods. However adjustments to repeat intervals must be made for airplanes whose calendar

to flight hour/flight cycle relationship exceeds the operator's fleet average by 10 % or more.

(e.g. airplanes that have extended out-of-service periods or significantly different operating

conditions). Such conversions must be reviewed and revised as necessary when significant

changes occur in fleet utilization and/or out-of-service periods.

F. PART 2: BASELINE PROGRAM

This section defines the A300 Baseline Corrosion Prevention and Control Program including basic

instructions, Implementation Ages and Repeat Intervals. This program is intended for use by A300

operators who do not have a proven effective Corrosion Prevention and Control Program.

This program applies to all A300 A/C listed in paragraph 1. Instructions may vary depending on the

modification status of the aircraft.

Operators having an existing program that does not control corrosion to Level 1 or better in all the

areas listed in the Baseline Program, are required to make appropriate adjustments in the affected

areas. Reviews should be made on the task content, the implementation age and the repeat

interval.

# MAINTENANCE PLANNING DOCUMENT

ISSUE:APR 01/10 APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT Page 7 

# (1) GENERAL INSTRUCTION

The following describes the general instructions to be accomplished in each defined airplane

area as part of the Baseline Program :

1. Remove equipment and interior furnishings as far as required to accomplish instruction

“3)”.

2. Prior to inspection clean the area as required to accomplish instruction “3)”.

Where existing secondary protective media (temporary corrosion protection) permits

unobscured assessment of structure condition, then that media or film may remain in

place for inspection.

3. Perform a General Visual Inspection, Detailed Visual Inspection or Special Detailed

Inspection, in accordance with inspection level column of all structure included in the

corrosion instruction in Structure Program.

Particular attention is to be given to installed repairs.

Additional non-destructive inspections or visual inspections following partial disassembly

are required, when there are indications of hidden corrosion, such as bulging skins,

discrepant attachment or corrosion running into splices, fittings, etc.

4. Remove completely all corrosion as recommended by the A300 Structural Repair

Manual, evaluate extent of damage and repair or replace all discrepant structure as

required.

5. Clear any blocked drain holes and drainage paths.

6. Apply suitable approved temporary corrosion protection in areas where it is quoted. See

SRM chapter '51-40-13 §2) Safety precautions' for the list of areas/items where

TEMPORARY CORROSION PROTECTION MUST NOT BE APPLIED.

7. Dry wet insulation blankets prior to re-installing, or replace with new.

8. Refit/re-connect/re-install parts removed during the accomplishment of instruction “1)”

and perform system check as applicable.

(2) BASELINE PROGRAM IMPLEMENTATION REQUIREMENTS

The A300 Baseline Program is sub-divided into specific airplane areas, each having an

Implementation Age and Repeat Interval(s) for application of the Basic Instruction. The

program is applicable in each area to all affected A300 airplanes reaching the Implementation

Age for the corresponding area (years since initial delivery).

For each airplane area, the program must be implemented on all affected airplanes within a

period of time not exceeding the corresponding repeat interval for that area with a minimum

implementation rate of one airplane per year for each area starting from the implementation

time or the date of effectivity of this program which ever occurs later.

It is recommended that priority for implementing the program is given to older airplanes and

areas requiring an upgrade of previous maintenance procedures to meet the program

requirements.

When Level 1 corrosion is exceeded in an area, the period for implementing the program in

that area on remaining airplanes in the operator's fleet may require further adjustment.

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# (3) BASELINE PROGRAM INSTRUCTIONS

This section provides the inspection areas, implementation ages and repeat intervals for the

A300 Corrosion Prevention and Control Baseline Program.

All parts of the Instructions apply to each area unless otherwise noted.

The following is an explanation of the form used to describe the program.

– INSTRUCTION

Identifies a specific area within the airplane area for application of the basic instruction.

Instructions for each CPCP requirement in this section are provided in the table format. In the

following a comprehensive description is provided for each table column.

The column indicates the number (XXXXXX-CYYY-Z) selected for each CPCP requirement.

• The first sixth digits are in accordance with the A310 ATA100 / aircraft zoning breakdown,

showing where the CPCP requirement is located.

• The seventh, eighth, ninth and tenth digits are for task code.

• The eleventh and twelfth digits are for technical solution applicable to same task

requirement.

• Last digit is “C” and stands for CPCP.

– ZONES

Provides the reference of the airplane zones to which the given instructions apply.

– ACCESS

Provides details of access to perform the basic instructions, unless otherwise quoted (lifting

of the insulation for example).

– DESCRIPTION OF THE AREA

Description of the area for application of the basic instruction.

– INSPECTION LEVEL

Provides details of the level of inspection for each instruction i.e. GVI for a General Visual

Inspection, DET for a Detailed Visual Inspection and SDET for Special Detailed Inspection.

– IMPLEMENTATION AGE (IA)

Airplane age, quoted in years since initial delivery, beyond which an approved Corrosion

Prevention and Control Program must be implemented.

– REPEAT INTERVAL (RI)

The interval, quoted in years, between repeat application of the basic instruction.

– TEMPORARY CORROSION PROTECTION (Temp. Prot.)

This column indicates if a Temporary Corrosion Protection System is to be applied to this

CPCP task, as indicated below :

'Yes' : temporary corrosion protection application recommended.

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operator.

'No' : temporary corrosion protection must not be applied in the area.



# Temporary Corrosion Protection product list is included in the Structural Repair Manual

(SRM) as well as in the Consumable Material List (CML).

– APPLICABILITY

The effectivity column indicates the aircraft type/series/model/mod status to which the

requirement is applicable. Some example are given below :

- All : this requirement is applicable to all A/C.

- A300B4-200 : this requirement is applicable to A300B4-200 series A/C.

- A300F4-203 : this requirement is applicable to A300F4-203 model A/C.

- Pre XXXX : this requirement is applicable to all A/C on which modification

XXX has not been embodied.



# – REMARK

Information related to the cross reference lists with zonal and SSI programs are included

into the Appendix B of this document.

G. REPORTING SYSTEM

In addition to the routine reporting procedures already established for the A300, the Aging Airplane

Corrosion Prevention and Control Program includes a mandatory reporting requirement for

corrosion findings exceeding LEVEL 1.

The reporting form included in this section is to be used for reporting all findings exceeding LEVEL

1 corrosion on the airframe to AIRBUS. Any additional comments and/or photographs, that are

available and help to identify the corrosion problem area or type, should be attached.

CORROSION PREVENTION AND CONTROL PROGRAM (CPCP) DATA: ()

5. LOW UTILIZATION PROGRAM

A. FOREWORD

It is acknowledged that the annual utilization of certain operators is outside that range which might

be termed "average" for A300 operation. For this reason, AIRBUS has introduced an alternative

program in this appendix, which, in conjunction with those tasks listed in the Structure Program of

this document, can be used to develop a Low Utilization Scheduled Maintenance Program.

B. METHODOLOGY

The Low Utilization Program was developed through a "task by task" review of the existing tasks

and intervals listed in System and Powerplant and Zonal of this document.

A working group, comprising Airline representatives, Airbus and its design office representatives

performed this review using the following as guidelines:

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# (1) The term "low utilization" is defined as operation within the parameters described in Para. 6

"SCOPE" (6.A., 6.B., 6.C. & 6.D.) of this introduction.

(2) Task intervals selected to be commensurate with low utilization operation and expressed in

the most appropriate usage parameter. During review of task intervals, discontinue the

practice of allocating "letter check" intervals and attempt to convert as follows:

1. Letter Interval "A" & multiples:

convert to interval 3 months (400 FC/500 FH) & multiples.

2. Letter Interval "C" & multiples:

convert to interval 24 months (3200 FC/4000 FH) & multiples.

3. Intervals expressed in Usage Parameter:

- calendar :

retain, but adjust if appropriate (in-service experience).

- FC & FH :

retain, unless calendar implications dictate the addition of a calendar "cap".

C. GENERAL

This appendix contains the manufacturer's scheduled maintenance recommendations for Zonal,

Systems & Components, Auxiliary Power Unit and Power plant tasks, (already listed in Sections 4,

5, 7 & 8 of this document), with task intervals expressed commensurate with a low utilization

operation.

These tasks are to be accomplished on a 100% basis, unless otherwise stated.

Limitations of life limited parts are controlled by the manufacturer and are published in AMM

Chapter 05, entitled "SERVICE LIFE LIMITS".

For servicing and lubrication items, this document provides additional information, in the Appendix

entitled "Servicing Charts".

D. PURPOSE

The purpose of this appendix is to provide an alternative list of scheduled maintenance

recommendations to assist operators in establishing a Low Utilization Program (LUP).

As previously stated, the task descriptions listed in this appendix are identical to those listed in

System and Powerplant and Zonal of this document. However, the intervals selected for each task

may be different to those listed in System and Powerplant and Zonal.

E. INTEGRATION

In establishment of a Low Utilization Program, it is necessary to combine the tasks listed in this

section with those tasks listed in Section 6 of this document. Tasks and intervals in the Structure

have not been adjusted for low utilization operation, since corrosion is controlled by calendar time

requirements and fatigue damage is controlled by dedicated FC requirements.

It is recognized that the interval framework for CPCP tasks (zonal & structure) may not be

compatible with the task intervals selected in this section. Escalation of CPCP task intervals to a

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# compatible interval can only be applied where sufficient experience is available for good corrosion

behavior (refer CPCP Rules in Structure introduction).

A number of tasks in the Zonal & Structures program make reference to CPCP requirements and

may also have a requirement for Temporary Protection System (TPS) application.

In this context, reference to the CPCP rules should be made for guidelines on interval escalation.

As a result of the CPCP requirement to control corrosion to Level 1 or better, operators shall report

corrosion findings to the manufacturer in accordance with the Structure Program Reporting System.

F. SCOPE

Airbus has developed a low utilization program using the following criteria as a datum:

Operators may elect to incorporate the tasks & intervals listed in this section into their scheduled

maintenance program, in preference to the tasks and intervals listed in System and Powrplant and

Zonal of this document provided that:

1. Aircraft annual utilization is between 500 FH and 2000 FH, with an equivalent cyclic operation

of between 400 FC and 1600 FC per year.

2. Aircraft annual utilization does not exceed 2000 FH in a twelve-month period.

3. Aircraft utilization is continuous throughout the twelve-month period.

4. Average utilization over any three-month period does not exceed 500 FH.

Adjustments to the program will be necessary:

– where aircraft are parked or in storage for extended periods of time.

– where aircraft average utilization is not uniform.

G. METHOD OF PRESENTATION.

This section and each maintenance task are arranged by ATA sequence. To differentiate task

numbers listed in this section from those in other sections, the letter "L" has been included in the

second group of digits for each task (e.g. 278124-L505-2).

(1) Movement Codes.

Where a task has been affected by change, a movement code is printed in the margin before

the task number. These movement codes signify:

“R” .......... Task revised.

“N” .......... New task introduced.

“D” .......... Task deleted.

“P” .......... Task interval provisional

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# H. LOW UTILIZATION PROGRAM DATA ( )

6. ALTERNATIVE SAMPLING PROGRAM

A. General

The Structure Program of the A300 MRB Document contains a number of SSIs controlled under a

sampling concept. Airbus however has performed a study to convert the concerned sampling

requirements into 100% requirements for an easier consolidation (refer to Structure Program).

However, where it is intended to continue the sampling concept for a certain time or indefinitely all

tasks of Section 6 where the four digits for MPD Section and task code are 0604 (i.e. all tasks

which are XXXXXX-0604-X) may be replaced by the corresponding requirement given in this MPD

Section.

NOTE: To facilitate the finding of the corresponding task in the Structure Program the task number

has been kept the same except for the task code, i.e. task XXXXXX-0604-X becomes

XXXXXX-060S-X in this Section.

NOTE: The tasks in this Section continue to reflect the sampling requirements given by the MRB

Document, however tasks for which inservice experience does not allow the continuation of

sampling have been/will be deleted from this Section and the repeat interval in Structure

Program have been/will be amended accordingly.

B. SAMPLING RULES

The sample size of inspections stated in the sampling program represents the fraction of each

operator's fleet (or group of operator's combined fleet) that must be inspected by the item specified.

e.g. for class No.1 item

– 20% of each operator's fleet must be inspected prior 20,000 FH. An additional 20% (1/5) of each

operator's fleet shall be inspected before 26,000 FH... Finally all aircraft of the operator's fleet

have been inspected once prior to or at reaching 44,000 FH (20,000 FH plus 4 times 6,000 FH)

for class No. 1 items.

Sampling inspections may be grouped or broken down in any manner convenient to the operator's

requirements, within basic interval, providing the following conditions are met:

The sampling inspections shall be accomplished on different aircraft when fleet size permits.

For sampling purposes, the fleet of an operator or a group of operators shall be arranged so that at

the end of an inspection cycle, when the last SSI's for a given class are inspected no airplane with

SSI's of the same class not yet inspected, has exceeded the inspection time by more than one

inspection interval.

If an operator's fleet is small and the fleet fraction specified for a regular structural inspection is less

than one aircraft, he may design his sampling program so that half of the structural items that are

duplicated (one or more on each side of the aircraft center line) are examined at each prescribed

interval. Unduplicated items such as keel beam, vertical fin and rudder must be inspected at each

prescribed interval.

No less than the equivalent of one airplane per operator or a group of operators shall be

accomplished at each inspection. When the sample size is a fraction, the size will be increased to

the next higher whole number if the fraction is greater than one half and decreased to the next

lower whole number if the fraction is less than one half at the end of the cycle of inspection each

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# A/C of the fleet must have been inspected once. A group of operators may combine their fleets for

purpose of accomplishing sampling inspection requirements. Sampling requirements for such

combined fleets shall be based on the sum of each operator's fleet.

Each operator, or group of operators who have combined their fleets, must maintain a master

record showing the schedule for accomplishments of the required sampling items within the flight

hours specified. This record must be available for ready reference by the appropriate regulatory

authorities until accomplished.

When an operator separates from a group of operators, the status of his airplanes is determined by

the inspections completed by that group at that time. Continuation of the inspection program shall

be in accordance with the single operator program requirements in this document, i.e.:

Any inspection completed in the same inspection cycle can be counted toward completition of the

required sampling fraction. If the group has completed 3/4 of the sample, the separated operator

must do 1/4 of his fleet during the remainder of the inspection cycle.

Example:

a group has completed 3/4 of the sample. An operator with 4 aircraft who separates from the group

then has to inspect one aircraft to complete the sample. The parent organization must complete its

remaining fleet sample requirement.

If an airplane is permanently removed from service, no adjustment in the sampling inspection

program is required unless this airplane is an airplane to which some inspections were assigned,

which have not been accomplished yet.

The sampling inspections are intended to determine the age (total time) of the fleet when fatigue or

corrosion deterioration first becomes evident. When the inspections findings indicate the evidence

of deterioration, appropriate action will be taken throughout the fleet. Such action may include:

– a one time inspection with repair action

– a one time modification of the item

– increased sample size or

– other appropriate action depending on the consequences of allowing the evident deterioration to

continue.

Operators must report all sampling inspections accomplished and all significant structural findings

to the manufacturer in accordance with the A300 structural inspection reporting system.

C. ALTERNATIVE SAMPLING PROGRAM DATA ()

7. COMPONENT DATA

A. Scope

The COMPONENT OPERATING AND STORAGE DATA (COD) section provides a direct access to

maintenance, monitoring and storage information related to a selected number of components

considered as significant with regard to one or several of the following criteria:.

– Component subject to one (or several) MRB/MPD task(s).

– Component classified as "NO GO" or "GO IF" by the AIRBUS / MMEL (Master Minimum

Equipment List).

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# – Component to be covered by a reliability program.

B. Presentation Form Lay Out

The following informations are provided for each component:

(1) ATA REFERENCE

– Component ATA reference AMM (6 digits) as provided in the "AIRBUS / ATA Breakdown".

– Component ATA reference IPC (6 digits) as provided in the "AIRBUS / ILLUSTRATED

PARTS CATALOG".

The Component Data is arranged by ATA sequence, according to "AIRBUS / ATA

Breakdown".

(2) DESIGNATION

Component functional designations as indicated in the "AIRBUS / ATA Breakdown".

(3) QTY (QUANTITY)

Number of component(s), installed on aircraft, under the subject ATA reference.

(4) FIN

Functional Identification Number (Design Office Identifier). When several units of a given

component (e.g. valve-pack) are used within a given ATA reference (e.g. 21-11-11), all

related FIN are quoted (i.e. 68 HB, 69 HB).

(5) SCHEDULED TASKS

This column provides information on scheduled tasks which permit to access the condition of

the component.

A cross in "ON A/C" column indicates that function of the component is checked by an on

aircraft scheduled maintenance task.

A cross in "OFF A/C" column indicates that subject component is subject to scheduled

removal from the A/C for shop maintenance.

In both cases details of maintenance action to be carried out on the Aircraft (e.g. on A/C

check, or component removal for shop action) are described in the respective section (

Systems, APU and Powerplant).

(6) MONITORING LEVEL

The monitoring level is intended for use by the operator for inservice monitoring of component

removals (MTBUR) and reliability (MTBF).

Three specific monitoring levels are suggested:

– 0 : no specific monitoring required for engineering purpose

– 1 : recording of number of removal and component time (A/C flight hours/cycles or component

operating hours/cycles as applicable) at removal for computation of MTBR/MTBUR.

– 2 : recording of above information together with "shop findings" for determination of

justified/unjustified removals and computation of MTBF.

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# However as monitoring is dependant on individual airline policy and experience the column is

left blank for airline input as necessary.

(7) RAR (REMOVAL AND REPLACEMENT)

This column provides the number of Men (MEN) and the elapsed time (ELT) required for

component removal and replacement. ELT is expressed in HOURS.

The figures quoted encompass the following:

– Access opening

– Disturbance (if applicable)

Removal of all items to be taken down prior to removal of the subject component.

– Component removal

– Preparation of replacement component

– Replacement component installation

– Re-installation of disturbed items

– Test after installation

– Access closing

Times quoted are given for 100% efficiency and normal conditions (environment, component

condition, etc...).

(8) P/N (PART NUMBER)

Intentionally left blank in this standard MPD

Operator customization of COD can be using IPC via cross reference table FIN to CSN.

(9) FSCM (FEDERAL SUPPLIER CODE OF MANUFACTURER)

Component manufacturer (Vendor) code in line with AIRBUS / Vendor Information Manual.

(10) STORAGE

The storage information has been deleted from this A300 MPD, since this information is

available from:

AIRBUS

MATERIAL SUPPORT CENTER

P.O. BOX 630 262

D-22312 HAMBURG

GERMANY

FAX: +49/40/503 168

TELEX: 212 742 ASDH D

SITA: HAMBI7X

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# (11) EFFECTIVITY

Column left intentionally blank to allow operator customization of COD. At this effect

reference to IPC via cross reference table FIN to P/N shall be used.

NOTE: Effectivity linked to engine installation is given by GE or PW as applicable.

When component is specific to a given model effectivity is indicated by key word as

follows:

e.g. C4 stands for A300C4

C. COMPONENT DATA IN PDF FORMAT ()