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 referenced. 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 
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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 
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MPD 

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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 
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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 
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MPD 

SEC

TASK

NUMBER

MVT DESCRIPTION REASON / JUSTIFICATION

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

REMOVED 

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

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

REMOVED 

EDITORIAL CHANGES 

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

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

REMOVED 

EDITORIAL CHANGES 

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

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

REMOVED 

EDITORIAL CHANGES 

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

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

REMOVED 

EDITORIAL CHANGES 

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

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

REMOVED 

EDITORIAL CHANGES 

2-28 281801-0502-1 R IN SOURCE: "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 
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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 
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"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 aircraft. It is intended that this 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 
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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 before 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 particular 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 from 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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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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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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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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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 
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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 

 
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SERVICE BULLETIN LIST

It is intended to supply the Service Bulletin List within this section in future revisions. 
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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. 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

N 201210-0505-1 121 AVIONICS COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7 122 SIL 20-032  CLEANING OF EWIS INSTALLED IN THE AVIONICS  COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)  ACCESS: 121AF 121AL 121BF 121BL 121CF 121DF  121EF 121FF 121GF 121HF 121JF 121KF  121LF 121MF 121NF 121PF 121QF 121RF  121SF 121TF 121UF 121VF 121WF 121XF  121YF 121ZF 131AZ 811  122AF 122AR 122BF 122CF 122CR 122DF  122EF 122FF 122GF 122HF 122JF 122KF  122LF 122MF 122NF 122PF 122QF 132AZ  811 N 201210-0505-2 121 AVIONICS COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7 122 SIL 20-032  CLEANING OF EWIS INSTALLED IN THE AVIONICS  COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)  ACCESS: 121AF 121AL 121BL 121CF 121DF 121EF  121FF 121GF 121HF 121KF 121LF 121MF  121NF 121PF 121QF 121RF 121SF 121TF  121UF 121VF 121WF 121XF 121YF 121ZF  131AZ 811  121BG 121CG 122AG 122AR 122BF 122CF  122CR 122DF 122EF 122GF 122HF 122JF  122KF 122LF 122MF 122NF 122PF 122QF  132AZ 811 N 201210-0505-3 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 122 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AVIONICS COMPARTMENT (EWIS)  ACCESS: 121AF 121AL 121BF 121BL 121CF 121DF  121EF 121FF 121GF 121HF 121JF 121KF  121LF 121MF 121NF 121PF 121QF 121RF  121SF 121TF 121UF 121VF 121WF 121XF  121YF 121ZF 131AZ 811  122AF 122AR 122BF 122CF 122CR 122DF  122EF 122FF 122GF 122HF 122JF 122KF  122LF 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 201210-0505-3 * * * * * C O N T I N U E * * * * *  811 N 201210-0505-4 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 122 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AVIONICS COMPARTMENT (EWIS)  ACCESS: 121AF 121AL 121BL 121CF 121DF 121EF  121FF 121GF 121HF 121KF 121LF 121MF  121NF 121PF 121QF 121RF 121SF 121TF  121UF 121VF 121WF 121XF 121YF 121ZF  131AZ 811  121BG 121CG 122AG 122AR 122BF 122CF  122CR 122DF 122EF 122GF 122HF 122JF  122KF 122LF 122MF 122NF 122PF 122QF  132AZ 811 N 201210-0505-5 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 122 SIL 20-032  GENERAL VISUAL INSPECTION OF G ROUTES AND 105VU,  106VU AND APU BUS (EWIS)  PREP.: ELECTRICAL PANEL COVER TO BE OPENED  ACCESS: 121AF 121AL 121BF 121BL 121CF 121DF  121EF 121FF 121GF 121HF 121JF 121KF  121LF 121MF 121NF 121PF 121QF 121RF  121SF 121TF 121UF 121VF 121WF 121XF  121YF 121ZF 131AZ 811  122AF 122AR 122BF 122CF 122CR 122DF  122EF 122FF 122GF 122HF 122JF 122KF  122LF 122MF 122NF 122PF 122QF 132AZ  811 N 201210-0505-6 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 122 SIL 20-032  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  121FF 121GF 121HF 121KF 121LF 121MF  121NF 121PF 121QF 121RF 121SF 121TF  121UF 121VF 121WF 121XF 121YF 121ZF  131AZ 811  121BG 121CG 122AG 122AR 122BF 122CF  122CR 122DF 122EF 122GF 122HF 122JF  122KF 122LF 122MF 122NF 122PF 122QF  132AZ 811 N 201210-0505-7 121 AVIONICS COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS AND  EWIS INSIDE 101VU (EWIS)  PREP.: ELECTRICAL PANEL COVER TO BE OPENED  ACCESS: 121BL 131AZ 132AZ 811 N 201230-0505-1 123 NOSE GEAR BAY MEC GVI I: 24 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  NOSE GEAR WELL (EWIS)  ACCESS: 713 714 N 201310-0505-1 131 FORWARD CARGO COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF ALL POWER FEEDER ROUTES INSTALLED (ONLY  IF CONTAMINATED) (EWIS)  PRP.: CEILING AND LINING PANELS TO BE REMOVED  ACCESS: 132BZ 132CZ 132DZ 811 N 201310-0505-2 131 FORWARD CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  FWD 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REMOVED  ACCESS: 132BZ 132CZ 132DZ 811 N 201310-0505-3 131 FORWARD CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS IN CB BOX 921 VU  (EWIS)  PRP.: CEILING AND LINING PANELS TO BE REMOVED (DOOR  AREA), ELECTRICAL PANEL COVER TO BE OPENED  ACCESS: 132AR 811 N 201330-0505-1 133 BAY UNDER FWD CARGO COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF ALL PDU SUPPLY ROUTES (ONLY IF  CONTAMINATED) (EWIS)  PRP.: ROLLERS TO BE REMOVED  ACCESS: 131AAF 131ABF 131ACF 131ADF 131AEF 131AF  131AFF 131AGF 131AHF 131AJF 131AKF 131BF  131CF 131DF 131EF 131FF 131GF 131HF  131JF 131PF 131QF 131RF 131SF 131TF  131UF 131VF 131WF 131XF 131YF 131ZF  132AF 132BF 132CF 132DF 132EF 132FF  132GF 132HF 132JF 132KF 132LF 132MF  132NF 133AL 133AR 133BL 133BR 133CL  133DL 133EL 811 N 201330-0505-2 133 BAY UNDER FWD CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPCTION OF EWIS BUNDLES WITHIN  THE ZONE (EWIS)  PRP.: ROLLERS TO BE REMOVED  ACCESS: 131AAF 131ABF 131ACF 131ADF 131AEF 131AF  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 131BF  131CF 131DF 131EF 131FF 131GF 131HF  131JF 131PF 131QF 131RF 131SF 131TF  131UF 131VF 131WF 131XF 131YF 131ZF  132AF 132BF 132CF 132DF 132EF 132FF  132GF 132HF 132JF 132KF 132LF 132MF  132NF 133AL 133AR 133BL 133BR 133CL  133DL 133EL 811 N 201370-0505-1 137 BAY AFT OF FWD CARGO COMPARTMENT MEC CLN I: 60 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF EWIS IN THE AREA AROUND OF THE PDU FEEDER  PRESSURE SEALS (ONLY IF CONTAMINATED) (EWIS)  ACCESS: 131BZ 131CZ 132EZ 811 N 201370-0505-2 137 BAY AFT OF FWD CARGO COMPARTMENT MEC DET I: 36 MO SIL AMM 249200/6 SIL 20-032  DETAILED INSPECTION OF EWIS IN AREA OF PRESSURE SEALS  LH/RH (EWIS)  ACCESS: 131BZ 131CZ 132EZ 811 N 201370-0505-3 137 BAY AFT OF FWD CARGO COMPARTMENT MEC GVI I: 60 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  ZONE (EWIS)  ACCESS: 131BZ 131CZ 132EZ 811 N 201410-0505-1 141 CENTER WING BOX MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  CENTER BOX (EWIS)  ACCESS: 147AZ 148AZ 734 744  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

N 201410-0505-2 141 CENTER WING BOX MEC DET I: 144 MO SIL AMM 249200/6 SIL 20-032  DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE  ZONE (EWIS)  ACCESS: 147AZ 148AZ 734 744 N 201430-0505-1 143 AIR CONDITIONING COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AIR CONDITIONING COMPARTMENT (EWIS)  ACCESS: 143AF 143BF 143CF 143DF 143FL 144DR  144FR 147BZ 734 744 N 201450-0505-1 145 PRESSURIZED ZONE BETWEEN WING CENTER BOX MEC CLN I: 72 MO SIL AMM 249200/7 MAIN GEAR WELL AND CABIN FLOOR SIL 20-032  CLEANING OF EWIS INSTALLED IN THE PRESSURIZED ZONE  BETWEEN WING CENTER BOX MAIN GEAR WELL AND CABIN  FLOOR (ONLY IF CONTAMINATED) (EWIS)  PRP.: TOILETS, GALLEYS (IF INSTALLED), SEATS AND  INSULATION TO BE REMOVED  ACCESS: 241AYF 241BBF 241BCF 241BDF 241BEF 241CZ  241DZ 242AAF 242ABF 242ADF 242AEF 242AFF  242AHF 242AJF 242AKF 242ALF 242AMF 242ANF  242APF 242AQF 242ARF 242ASF 242ATF 242AUF  242CZ 242DZ 242VF 242WF 242XF 242YF  242ZF 831 841 N 201450-0505-2 145 PRESSURIZED ZONE BETWEEN WING CENTER BOX MEC GVI I: 72 MO SIL AMM 249200/6 MAIN GEAR WELL AND CABIN FLOOR SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  PRESSURIZED ZONE BETWEEN WING CENTER BOX MAIN GEAR  WELL AND CABIN FLOOR (EWIS)  PRP.: TOILETS, GALLEYS (IF INSTALLED), SEATS AND  INSULATION 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  241DZ 242AAF 242ABF 242ADF 242AEF 242AFF  242AHF 242AJF 242AKF 242ALF 242AMF 242ANF  242APF 242AQF 242ARF 242ASF 242ATF 242AUF  242CZ 242DZ 242VF 242WF 242XF 242YF  242ZF 831 841 N 201470-0505-1 147 MAIN LANDING GEAR WELL AND HYDRAULIC MEC GVI I: 12 MO SIL AMM 249200/6 COMPARTMENT SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN MAIN  LANDING GEAR WELL AND HYDRAULIC COMPARTMENT (EWIS)  ACCESS: 734 744 N 201510-0505-1 151 AFT CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS IN CB BOX 923VU  (EWIS)  PRP.:CEILING AND LINING PANELS REMOVED, ELECTRICAL  PANEL COVER TO BE OPENED  ACCESS: 812 N 201510-0505-2 151 AFT CARGO COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AFT CARGO COMPARTMENT (EWIS)  PRP.:CEILING AND LINING PANELS REMOVED  ACCESS: 812 N 201530-0505-1 153 BAY UNDER AFT CARGO COMPARTMENT MEC CLN I: 72 MO SIL AMM 249200/7 SIL 20-032  CLEANING 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 201530-0505-1 * * * * * C O N T I N U E * * * * *  PRP.:ROLLERS TO BE REMOVED  ACCESS: 151AF 151BF 151CF 151DF 151EF 151FF  151GF 151HF 151JF 151KF 151LF 151MF  151NF 151PF 151QF 151RF 151SF 151TF  151UF 151VF 151WF 151XF 151YF 152AF  152BF 152CF 152DF 152EF 152FF 152GF  152HF 152JF 152KF 812 N 201530-0505-2 153 BAY UNDER AFT CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  BAY UNDER AFT CARGO COMPARTMENT (EWIS)  PRP.:ROLLERS TO BE REMOVED  ACCESS: 151AF 151BF 151CF 151DF 151EF 151FF  151GF 151HF 151JF 151KF 151LF 151MF  151NF 151PF 151QF 151RF 151SF 151TF  151UF 151VF 151WF 151XF 151YF 152AF  152BF 152CF 152DF 152EF 152FF 152GF  152HF 152JF 152KF 812 N 201610-0505-1 161 BULK CARGO COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  BULK CARGO COMPARTMENT(EWIS)  PRP.:LININGS AND CEILING PANELS TO BE REMOVED  ACCESS: 813 N 201630-0505-1 163 BAY UNDER BULK CARGO COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  BULK CARGO COMPARTMENT(EWIS)  ACCESS: 161AF 161BF 161CF 161DF 161EF 161FF  161GF 162AF 162BF 162CF 162DF 162EF  162FF 162GF 813  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AFT CABIN UNDERFLOOR COMPARTMENT(EWIS)  ACCESS: 162AZ 171AF 171AZ 172AF 172BF 813 N 202110-0505-1 211 FLIGHT COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF EWIS INSTALLED IN THE FLIGHT  COMPARTMENT(ONLY IF CONTAMINATED) (EWIS)  PRP.:(IF INSTALLED), SIDEWALL AND CEILING PANELS,  REMOVABLE VERTICAL LINING, LININGS, SEATS - ALL  ELECTRICAL PANEL COVERS "VU" TO BE OPENED  ACCESS: 211AF 211AZ 211BF 211CF 211DF 211EF  211FF 211GF 211HF 211JF 211KF 211LF  211MF 211NF 211PF 212AF 212BF 212CF  212DF 212EF 212FF 212GF 212HF 212JF  212KF 212LF 212MF 831 841 N 202110-0505-2 211 FLIGHT COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  FLIGHT COMPARTMENT (EWIS)  PRP.:(IF INSTALLED), SIDEWALL AND CEILING PANELS,  REMOVABLE VERTICAL LINING, LININGS, SEATS - ALL  ELECTRICAL PANEL COVERS "VU" TO BE OPENED  ACCESS: 211AF 211AZ 211BF 211CF 211DF 211EF  211FF 211GF 211HF 211JF 211KF 211LF  211MF 211NF 211PF 212AF 212BF 212CF  212DF 212EF 212FF 212GF 212HF 212JF  212KF 212LF 212MF 831 841 N 202110-0505-3 211 FLIGHT COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSIDE THE  PANEL 120VU (EWIS)  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 VU  TO BE OPENED  ACCESS: 831 841 N 202210-0505-1 221 FORWARD MAIN DECK UTILITY AREAS MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED AT  FORWARD MAIN DECK UTILITY AREAS (EWIS)  PRP.:(IF INSTALLED), GALLEYS AND TOILETS , (IF  INSTALLED) SIDEWALL LININGS TO BE REMOVED  ACCESS: 831 841 N 202230-0505-1 223 FWD MAIN DECK UTILITY OVERHEAD MEC CLN I: 144 MO SIL AMM 249200/7 COMPARTMENT SIL 20-032  CLEANING OF G, E AND P ROUTES WITHIN THE ZONE (ONLY  IF CONTAMINATED) (EWIS)  PRP.:(IF INSTALLED), CEILING PANELS, GALLEYS TOILETS  IF INSTALLED) TO BE REMOVED  ACCESS: 831 841 N 202230-0505-2 223 FWD MAIN DECK UTILITY OVERHEAD MEC GVI I: 72 MO SIL AMM 249200/6 COMPARTMENT SIL 20-032  GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS AND  EWIS INSIDE 800VU (EWIS)  PRP.:(IF INSTALLED), ELECTRICAL PANEL COVER TO BE  OPENED  ACCESS: 831 841  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 249200/6 COMPARTMENT SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS IN THE FWD MAIN  DECK UTILITY OVERHEAD COMPARTMENT (EWIS)  PRP.:(IF INSTALLED), CEILING PANELS, GALLEYS, TOILETS  (IF INSTALLED) TO BE REMOVED  ACCESS: 831 841 N 202310-0505-1 231 FWD MAIN DECK COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS  BETWEEN SEATS AND AIRCRAFT AND THE WIRING AT THE  SEATS INSTALLED AS FAR AS VISIBLE, IN THE FWD MAIN  DECK COMPARTMENT AREA  NOTE:THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH  SEATS ONLY, AND IF ELECTRONICALLY EQUIPED.  (EWIS)  ACCESS: 831 841 N 202310-0505-2 231 FWD MAIN DECK COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF EWIS INSTALLED FWD MAIN DECK COMPARTMENT  (ONLY IF CONTAMINATED) (EWIS)  PRP.:(IF INSTALLED),GALLEYS AND TOILETS (IF  INSTALLED, IF NECESSARY), SEATS (IF INSTALLED)  AND SIDEWALL LININGS IN EWIS AREAS  ACCESS: 831 841 N 202310-0505-3 231 FWD MAIN DECK COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  EWIS 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AREAS  ACCESS: 831 841 N 202330-0505-1 233 FWD MAIN DECK OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF EWIS INSTALLED IN THE FWD MAIN DECK  OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)  PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS  (IF INSTALLED)  ACCESS: 831 841 N 202330-0505-2 233 FWD MAIN DECK OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  FWD MAIN DECK OVERHEAD COMPARTMENT (EWIS)  PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS  (IF INSTALLED)  ACCESS: 831 841 N 202410-0505-1 241 CENTER MAIN DECK COMPARTMENT MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS  BETWEEN SEATS AND AIRCRAFT AND THE EWIS AT THE SEATS  INSTALLED AS FAR AS VISIBLE, IN THE CENTER MAIN  DECK COMPARTMENT AREA (EWIS)  NOTE:THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH  SEATS ONLY, AND IF ELECTRONICALLY EQUIPED.  ACCESS: 831 841 N 202410-0505-2 241 CENTER MAIN DECK COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 DECK  COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)  PRP.:(IF INSTALLED),GALLEYS AND TOILETS (IF  INSTALLED, IF NECESSARY), SEATS (IF INSTALLED)  AND SIDEWALL LININGS IN EWIS AREAS  ACCESS: 831 841 N 202410-0505-3 241 CENTER MAIN DECK COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  CENTER MAIN DECK COMPARTMENT (EWIS)  PRP.:(IF INSTALLED),GALLEYS AND TOILETS (IF  INSTALLED, IF NECESSARY), SEATS (IF INSTALLED)  AND SIDEWALL LININGS IN EWIS AREAS  ACCESS: 831 841 N 202430-0505-1 243 CENTER MAIN DECK OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF EWIS INSTALLED IN THE CENTER MAIN DECK  OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)  PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS  (IF INSTALLED)  ACCESS: 831 841 N 202430-0505-2 243 CENTER MAIN DECK OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  CENTER MAIN DECK OVERHEAD COMPARTMENT (EWIS)  PRP.:(IF INSTALLED),CEILING PANELS, STOWAGE BINS  (IF INSTALLED)  ACCESS: 831 841  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS  BETWEEN SEATS AND AIRCRAFT AND THE EWIS AT THE SEATS  INSTALLED AS FAR AS VISIBLE, IN THE AFT MAIN  DECK COMPARTMENT AREA (EWIS)  NOTE:THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH  SEATS ONLY, AND IF ELECTRONICALLY EQUIPED.  ACCESS: 833 843 N 202510-0505-2 251 AFT MAIN DECK COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING 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 IN  EWIS AREAS  ACCESS: 833 843 N 202510-0505-3 251 AFT MAIN DECK COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AFT MAIN DECK COMPARTMENT (EWIS)  PRP.:GALLEYS AND TOILETS (IF INSTALLED, IF NECESSARY)  SEATS (IF INSTALLED) AND SIDEWALL LININGS IN  EWIS AREAS  ACCESS: 833 843 N 202530-0505-1 253 AFT MAIN DECK OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF EWIS INSTALLED AFT MAIN DECK OVERHEAD  COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)  PRP.:CEILING PANELS, STOWAGE BINS (IF INSTALLED)  ACCESS: 833 843  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AFT MAIN DECK OVERHEAD COMPARTMENT (EWIS)  PRP.:CEILING PANELS, STOWAGE BINS (IF INSTALLED)  ACCESS: 833 843 N 202610-0505-1 261 AFT MAIN DECK UTILITY AREA MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING OF EWIS INSTALLED IN THE AFT MAIN DECK  UTILITY AREAS (ONLY IF CONTAMINATED) (EWIS)  PRP.:SEATS AND SIDEWALL LININGS, GALLEYS AND TOILETS  (IF INSTALLED, IF NECESSARY)  ACCESS: 833 843 N 202610-0505-2 261 AFT MAIN DECK UTILITY AREA MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSIDE THE  811VU PANEL (EWIS)  PRP.:ELECTRICAL PANEL COVER 811VU TO BE OPENED  ACCESS: 833 843 N 202610-0505-3 261 AFT MAIN DECK UTILITY AREA MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  AFT MAIN DECK OVERHEAD COMPARTMENT (EWIS)  PRP.:SEATS AND SIDEWALL LININGS, GALLEYS AND TOILETS  (IF INSTALLED, IF NECESSARY)  ACCESS: 833 843 N 202630-0505-1 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC CLN I: 144 MO SIL AMM 249200/7 SIL 20-032  CLEANING 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 N 202630-0505-2 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF APU FEED LINE AND POWER  G, E AND P ROUTE EWIS IN CEILING AREA (EWIS)  PRP.:CEILING PANEL (IF INSTALLED)  ACCESS: 833 843 N 202630-0505-3 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC DET I: 144 MO SIL AMM 249200/6 SIL 20-032  DETAILED INSPECTION OF APU FEEDERS AND STARTER CABLE  AT REAR BULKHEAD PRESSURE SEALS (EWIS)  PRP.: AFT G & T MOUNTS.  ACCESS: 833 843 N 202630-0505-4 263 MAIN DECK UTILITY OVERHEAD COMPARTMENT MEC GVI I: 144 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS IN MAIN DECK  UTILITY OVERHEAD COMPARTMENT (EWIS)  PRP.:CEILING PANEL (IF INSTALLED), GALLEYS AND  TOILETS (IF INSTALLED, IF NECESSARY)  ACCESS: 833 843 N 203110-0505-1 311 HORIZONTAL AND VERTICAL ATTACHMENT AREA MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 N 203130-0505-1 313 TAIL CONE - APU INTAKE AREA MEC GVI I: 48 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS AT TAIL CONE - APU  INTAKE AREA (EWIS)  ACCESS: 312AR 313AL N 203150-0505-1 315 TAIL CONE - APU AND ACCESSORY MEC CLN I: 24 MO SIL AMM 249200/7 COMPARTMENT SIL 20-032  CLEANING OF ALL POWER FEEDER ROUTES (ONLY IF  CONTAMINATED) (EWIS)  ACCESS: 315AL 316AR N 203150-0505-2 315 TAIL CONE - APU AND ACCESSORY MEC GVI I: 24 MO SIL AMM 249200/6 COMPARTMENT SIL 20-032  GENERAL VISUAL INSPECTION OF G ROUTE WITHIN THE  ZONE (EWIS)  ACCESS: 315AL 316AR N 203150-0505-3 315 TAIL CONE - APU AND ACCESSORY MEC GVI I: 24 MO SIL AMM 249200/6 COMPARTMENT SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS AT TAIL CONE - APU  AND ACCESSORY COMPARTMENT (EWIS)  ACCESS: 315AL 316AR N 203340-0505-1 334 HORIZONTAL STABILIZER TIP MEC GVI I: 72 MO SIL AMM 249200/6 SIL 20-032  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  334DB 334DT 334EB 334ET 334FT 334GT  334HT 334JT 334KT 334LT 344AB 344AT  344BB 344BT 344CB 344CT 344DB 344DT  344EB 344ET 344FT 344GT 344HT 344JT  344KT 344LT N 204110-0505-1 411 PYLON LEADING EDGE MEC GVI I: 48 MO SIL AMM 249200/6 421 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN PYLON  LEADING EDGE (EWIS)  ACCESS: 411AL  421AL N 204130-0505-1 413 FWD UPPER PYLON MEC GVI I: 48 MO SIL AMM 249200/6 423 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN FWD  UPPER PYLON (EWIS)  ACCESS: 413AL 413BL 413CL 413DL 413EL 413FL  414AR 414BR 414CR 414DR  423AL 423BL 423CL 423DL 423EL 423FL  424AR 424BR 424CR 424DR N 204130-0505-2 413 FWD UPPER PYLON MEC GVI I: 48 MO SIL AMM 249200/6 423 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN FWD  UPPER PYLON (EWIS)  ACCESS: 413AL 413BL 413DL 413EL 413FL 413GL  413HL 414AR 414BR 414CR 414DR 414ER  423AL 423BL 423DL 423EL 423FL 423GL  423HL 424AR 424BR 424CR 424DR 424ER N 204150-0505-1 415 FORWARD LOWER PYLON MEC GVI I: 48 MO SIL AMM 249200/6 425 SIL 20-032  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FWD  LOWER PYLON (EWIS)  ACCESS: 415AL 416AR  425AL 426AR N 204330-0505-1 433 ENGINE AIR INTAKE (NOSE COWL) MEC GVI I: 72 MO SIL AMM 249200/6 443 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN  ENGINE AIR INTAKE (EWIS)  ACCESS: 433AL 434AR 434BR  443AL 444AR 444BR N 204330-0505-2 433 ENGINE AIR INTAKE (NOSE COWL) MEC GVI I: 72 MO SIL AMM 249200/6 443 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN  ENGINE AIR INTAKE (EWIS)  ACCESS: 433EL 434CR 434ER 434FR  443EL 444CR 444ER 444FR N 204350-0505-1 435 FAN CASE AND FAN COWL MEC GVI I: 24 MO SIL AMM 249200/6 445 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN ENGINE  FAN CASE AND FAN COWL (EWIS)  ACCESS: 435AL 436AR  445AL 446AR N 204510-0505-1 451 THRUST REVERSER MEC GVI I: 24 MO SIL AMM 249200/6 461 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN ENGINE  THRUST REVERSER (EWIS)  PRP.:THRUST REVERSER DEPLOYED  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

N 204530-0505-1 453 HOT SECTION MEC GVI I: 24 MO SIL AMM 249200/6 463 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN ENGINE  HOT SECTION (EWIS)  ACCESS: 451AL 452AR  461AL 462AR N 204710-0505-1 471 PYLON TO WING LEADING EDGE MEC GVI I: 48 MO SIL AMM 249200/6 481 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN PYLON  TO WING LEADING EDGE (EWIS)  PRP.:SLATS TO BE EXTENDED  ACCESS: 471AL 471BL 472AR 472BR  481AL 481BL 482AR 482BR N 204730-0505-1 473 AFT UPPER PYLON MEC GVI I: 48 MO SIL AMM 249200/6 483 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN AFT  UPPER PYLON (EWIS)  ACCESS: 473AL 473BL 473DL 474AR 474BR 474CR  483AL 483BL 483DL 484AR 484BR 484CR N 205120-0505-1 512 INBOARD FIX ED L.E. AREA MEC GVI I: 72 MO SIL AMM 249200/6 612 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN SLAT  TRACK / SCREW JACK AREA (EWIS)  PRP.:SLATS TO BE EXTENDED  ACCESS: 512AB 512AT 512BB 512CB 512DB 512EB  512FB 512GB 512HB 512JB 512KB 512LB  612AB 612AT 612BB 612CB 612DB 612EB  612FB 612GB 612HB 612JB 612KB 612LB N 205120-0505-2 512 INBOARD FIX ED L.E. AREA MEC GVI I: 72 MO SIL AMM 249200/6 612 SIL 20-032  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 EXTENDED  ACCESS: 512AB 512AT 512BB 512CB 512DB 512EB  512FB 512GB 512HB 512JB 512KB 512LB  612AB 612AT 612BB 612CB 612DB 612EB  612FB 612GB 612HB 612JB 612KB 612LB N 205130-0505-1 513 FORWARD WING ROOT AND KRUEGER FLAP MEC GVI I: 72 MO SIL AMM 249200/6 613 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  ZONE (EWIS)  PRP.:KRUEGER FLAP EXTENDED, COVER PLATE REMOVED  ACCESS: 513AB 513BB 513CB  613AB 613BB 613CB N 205130-0505-2 513 FORWARD WING ROOT AND KRUEGER FLAP MEC GVI I: 72 MO SIL AMM 249200/6 613 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  ZONE (EWIS)  PRP.:KRUEGER FLAP EXTENDED, COVER PLATE REMOVED  ACCESS: 513AB  613AB N 205230-0505-1 523 CENTER FIXED L.E. AREA (FROM RIB7 TO 17) MEC GVI I: 72 MO SIL AMM 249200/6 623 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN SLAT  TRACK / SCREW JACK AREA (EWIS)  PRP.:SLATS TO BE EXTENDED  ACCESS: 523AB 523BB 523CB 523DB 523EB 523FB  523GB 523HB 523JB 523KB 523LB 523MB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 249200/6 623 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  CENTER FIXED L.E. AREA (EWIS)  PRP.:SLATS TO BE EXTENDED  ACCESS: 523AB 523BB 523CB 523DB 523EB 523FB  523GB 523HB 523JB 523KB 523LB 523MB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB N 205240-0505-1 524 OUTBOARD FIXED L.E. AREA (FROM RIBS 17 MEC GVI I: 72 MO SIL AMM 249200/6 624 TO 28) SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN SLAT  TRACK / SCREW JACK AREA (EWIS)  PRP.:SLATS TO BE EXTENDED  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB N 205240-0505-2 524 OUTBOARD FIXED L.E. AREA (FROM RIBS 17 MEC GVI I: 72 MO SIL AMM 249200/6 624 TO 28) SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  OUTBOARD FIXED L.E. AREA (EWIS)  PRP.:SLATS TO BE EXTENDED  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB N 205300-0505-1 530 FLAP TRACK FAIRING AND WING TIP MEC GVI I: 72 MO SIL AMM 249200/6 630 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE  FLAP 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 MOVING  FAIRINGS TO BE REMOVED  ACCESS: 531AB 531BB 532AB 532BB 533AB 533BB  534AB 534BB 535AB 535BB 536AB 536BB  631AB 631BB 632AB 632BB 633AB 633BB  634AB 634BB 635AB 635BB 636AB 636BB N 205410-0505-1 541 FWD INBOARD SECTION OF INNER FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6 641 SIL 20-032  DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUEL  TANK (EWIS)  ACCESS: 541AB 541BB 541CB 542EB  641AB 641BB 641CB 642EB N 205410-0505-2 541 FWD INBOARD SECTION OF INNER FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6 641 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS IN FWD INBOARD  SECTION OF INNER FUEL TANK AREA (EWIS)  ACCESS: 541AB 541BB 541CB 542EB  641AB 641BB 641CB 642EB N 205420-0505-1 542 AFT INBOARD SECTION OF INNER FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6 642 (RIBS 1 TO 9) SIL 20-032  DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUEL  TANK (EWIS)  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB N 205420-0505-2 542 AFT INBOARD SECTION OF INNER FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6 642 (RIBS 1 TO 9) SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS IN THE AFT INBOARD  SECTION 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 205420-0505-2 * * * * * C O N T I N U E * * * * *  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB N 205430-0505-1 543 OUTBOARD SECTION OF INNER FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6 643 (RIBS 9 TO 14) SIL 20-032  DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUEL  TANK (EWIS)  ACCESS: 543AB 543BB 543CB 543DB  643AB 643BB 643CB 643DB N 205430-0505-2 543 OUTBOARD SECTION OF INNER FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6 643 (RIBS 9 TO 14) SIL 20-032  GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE  FUEL TANK (EWIS)  ACCESS: 543AB 543BB 543CB 543DB  643AB 643BB 643CB 643DB N 205500-0505-1 550 OUTBOARD FUEL TANK MEC DET I: 144 MO SIL AMM 249200/6 650 SIL 20-032  DETAILED INSPECTION OF EXPOSED EWIS WITHIN THE FUEL  TANK (EWIS)  ACCESS: 550BB 550DB 550EB 550FB 550GB 550HB  550JB 550KB 550LB 550MB 550NB 550PB  550QB  650BB 650DB 650EB 650FB 650GB 650HB  650JB 650KB 650LB 650MB 650NB 650PB  650QB N 205500-0505-2 550 OUTBOARD FUEL TANK MEC GVI I: 144 MO SIL AMM 249200/6 650 SIL 20-032  GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE  FUEL TANK (EWIS)  ACCESS: 550BB 550DB 550EB 550FB 550GB 550HB  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 550PB  550QB  650BB 650DB 650EB 650FB 650GB 650HB  650JB 650KB 650LB 650MB 650NB 650PB  650QB N 205710-0505-1 571 MAIN GEAR WELL MEC GVI I: 144 MO SIL AMM 249200/6 671 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  FAIRINGS (EWIS)  PRP.:UNDER WING FAIRINGS TO BE REMOVED N 205710-0505-2 571 MAIN GEAR WELL MEC GVI I: 48 MO SIL AMM 249200/6 671 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  ZONE (EWIS) N 205720-0505-1 572 TRAILING EDGE AREA (SHROUD BOX) MEC GVI I: 48 MO SIL AMM 249200/6 672 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN FLAP  TRACK 2 GEARBOX AREA (EWIS)  PRP.:FLAPS AND SPOILERS TO BE EXTENDED  ACCESS: 572AB 572CB 572DB 572EB 572FB 572GB  572HB 572JB 572KB 572LB 572PB  672AB 672CB 672DB 672EB 672FB 672GB  672HB 672JB 672KB 672LB 672PB N 205720-0505-2 572 TRAILING EDGE AREA (SHROUD BOX) MEC GVI I: 48 MO SIL AMM 249200/6 672 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  ZONE (EWIS)  PRP.:FLAPS AND SPOILERS TO BE EXTENDED  ACCESS: 572AB 572CB 572DB 572EB 572FB 572GB  572HB 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  672HB 672JB 672KB 672LB 672PB N 205750-0505-1 575 FIXED TRAILING EDGE AREA (FROM SHROUD MEC GVI I: 72 MO SIL AMM 249200/6 675 BOX TO RIB 9) SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE FIXED  TRAILING EDGE AREA (EWIS)  PRP.:FLAPS TO BE EXTENDED  ACCESS: 575AB 575BB 575CB 575DB 575EB 575FB  575GB  675AB 675BB 675CB 675DB 675EB 675FB  675GB N 205770-0505-1 577 AFT WING ROOT MEC GVI I: 72 MO SIL AMM 249200/6 677 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE AFT  WING ROOT AREA (EWIS)  PRP.:FLAPS TO BE EXTENDED  ACCESS: 577AB 577AT 577BB 577BT 577CT 577DT  577ET 577FT 577GT  677AB 677AT 677BB 677BT 677CT 677DT  677ET 677FT 677GT N 205810-0505-1 581 FIXED TRAILING EDGE AREA (RIBS 9 TO 25) MEC GVI I: 144 MO SIL AMM 249200/6 681 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  FAIRING (EWIS)  PRP.:UNDER WING FAIRINGS TO BE REMOVED N 205810-0505-2 581 FIXED TRAILING EDGE AREA (RIBS 9 TO 25) MEC GVI I: 48 MO SIL AMM 249200/6 681 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  FAIRING (EWIS)  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 EXTENDED  ACCESS: 581AB 581BB 581CB 581DB 581EB 581FB  581GB 581HB 581JB  681AB 681BB 681CB 681DB 681EB 681FB  681GB 681HB 681JB 681KB N 205910-0505-1 591 TRAILING EDGE AREA BETWEEN REAR SPAR AND MEC GVI I: 72 MO SIL AMM 249200/6 691 LOW SPEED AILERON SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  ZONE (EWIS)  ACCESS: 591AB 591BB 591CB 591DB  691AB 691BB 691CB 691DB N 207110-0505-1 711 NOSE LANDING GEAR AND DOORS MEC GVI I: 12 MO SIL AMM 249200/6 SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  ZONE (EWIS)  ACCESS: 713 714 N 207310-0505-1 731 MAIN LANDING GEAR INCLUDING FIXED AND MEC GVI I: 12 MO SIL AMM 249200/6 MOVABLE DOORS SIL 20-032  GENERAL VISUAL INSPECTION OF EWIS WITHIN THE  ZONE (EWIS)  ACCESS: 734 744  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STANDARD PRACTICES - AIRFRAME REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 212000-0505-1 200 DISTRIBUTION MEC CLN I: 5 A MPD AMM 212100/3 OR AMM 212200/3 CLEAN LAVATORY AIR EXTRACTION GRILLS NOTE 5-2  212100-0503-1 131 AIR DISTR/EXTR. FWD FUSELAGE MEC FUC I: 3 C MRB ** AMM 212100/5 FUNCTIONAL CHECK OF PRESSURE SWITCH (35 HR).  PREP.: REMOVE LININGS BETWEEN FR.20 AND 24 IN FWD  CARGO COMPARTMENT L/H.  212100-0503-2 121 AIR DISTR/EXTR. FWD FUSELAGE MEC FUC I: 3 C MRB AMM 212400/5 FUNCTIONAL TEST, IN SITU, OF FLOW DETECTOR SETTING  SWITCH (77 HQ).  ACCESS: 131AZ  212100-0503-3 121 AIR DISTR/EXTR. FWD FUSELAGE MEC FUC I: 3 C MRB AMM 212400/5 FUNCTIONAL TEST,IN SITU,OF FAN SPEED SWITCH (69 HQ)  ACCESS: 131AZ  212100-0503-4 210 AIR DISTR/EXTR. FWD FUSELAGE MEC OPC I: 1 C MRB AMM 212400/5 OPERATIONAL 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 212421/4 OR AMM 212422/4 - CLEAN (AFTER DISASSEMBLY) DUST SEPARATOR UNIT, NOTE 5-2 AMM 212423/4 - CLEAN DUST SEPARATOR SCAVENGE LINE, SIL 21-017  - CLEAN AIR INLET GRILL OF SOUND REDUCER,  - REPLACE FILTER CARTRIDGE.  PREP.: REMOVE AIR FILTER UNIT AND SOUND REDUCER.  ACCESS: 121BL 131AZ  SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 212100-0505-2 121 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 5 A MPD AMM 212421/4 OR AMM 212422/4 01. REMOVE SOUND REDUCER NOTE 5-2  02. CLEAN MESHED FILTER AT AIR INLET TO SOUND  REDUCER  03. REMOVE AND REPLACE FILTER ELEMENT  04. REINSTALL SOUND REDUCER  ACCESS: 121BL 131AZ  212100-0505-3 131 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 2 C MPD AMM 212100/7 CLEAN VENTURI GRIDS IN AIR EXTRACTION DUCT.  PREP.: REMOVE SIDE WALL LINING BETWEEN FR.22 AND  FR.23 IN FWD CARGO COMPARTMENT.  212100-0505-4 122 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 2 C MPD AMM 212100/7 CLEAN GRIDS OF RELAY BOXES.  PREP.: REMOVE COVERS OF RELAY BOXES 250VU, 251VU,  252VU, IN AVIONICS COMPARTMENT.  ACCESS: 132AZ  212100-0505-5 210 AIR DISTR/EXTR. FWD FUSELAGE MEC CLN I: 2 C MPD AMM 212500/7 CLEAN GRIDS BEHIND INSTRUMENT PANELS.  PREP.: REMOVE INSTRUMENT PANELS OF PILOT,CO-PILOT,F/E  AND C/B PANEL AS REQUIRED.  212200-0505-1 154 AIR DISTR/EXTR. AFT FUSELAGE MEC CLN I: 2 C MPD AMM 212200/7 CLEAN GRIDS IN AIR EXTRACTION DUCTS BELOW AFT  CARGO COMPARTMENT.  PREP.: REMOVE AFT CARGO COMPARTMENT FLOOR PANELS AS  REQUIRED.  SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 212200-0505-2 130 AIR DISTR/EXTR. FORWARD FUSELAGE MEC CLN I: 2 C MPD AMM 212100/7 CLEAN GRIDS IN AIR EXTRACTION DUCTS BELOW FWD.  CARGO COMPARTMENT (ZONES 133/134/135/136).  PREP.: REMOVE FWD.CARGO COMPARTMENT FLOOR PANELS AS  REQUIRED.  212200-0505-3 100 AIR DISTRIBUTION/EXTRACTION FUSELAGE MEC CLN I: 1 C MPD AMM 212100/3 200 AMM 212200/3 CLEAN TOILET AIR EXTRACTION DUCTS OF  ALL LAVATORIES  ACCESS: LAVATORY FLOOR  ACCESS: 162AZ 812  131AZ 811  212200-0505-4 100 AIR DISTRIBUTION/EXTRACTION FUSELAGE MEC CLN I: 4 A MPD AMM 212200/3 200 AMM 261711/4 1. REMOVE LAVATORY SMOKE DETECTORS SIL 26-018  2. REMOVE AIR EXTRACTION DUCTS BETWEEN  SMOKE DETECTORS AND EXTRACTION DUCT INLET  3. CLEAN DUCTS  4. REINSTALL LAVATORY AIR EXTRACTION DUCTS  5. REINSTALL LAVATORY SMOKE DETECTOR  ACCESS: 131AZ 131HF 162AZ  212200-0505-5 131 DOOR ACCESS AIR CONDITIONING SYSTEM MEC DET I: 4 C SB SB 21-0120  SIL SIL 21-0148  DETAILED INSPECTION OF LOW PRESSURE GROUND CONNECTION  COVER ASSEMBLY.  212300-0502-1 121 AIR DISTR/EXTR. - BATTERIES MEC GVI I: 1 A MRB AMM 212300/0 CHECK EXTERNAL BATTERY COOLING ORIFICES FOR  OBSTRUCTION  SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 212300-0503-1 121 AIR DISTR/EXTR. - BATTERIES ERI OPC I: 3 C MPD AMM 212300/6 OPERATIONAL TEST OF BATTERY COOLING SYSTEM  ACCESS: 131AZ  212300-0505-1 222 AIR DISTR/EXTR. - BATTERIES ERI CLN I: 2 C MPD AMM 212300/7 232 AMM 212400/7 CLEAN AIR EXTRACTION GRIDS/BAFFLES OF BATTERY AND  ELECTRONIC RACK 90 VU.  PREP.: REMOVE LOWER SIDEWALL/DADO PANELS BETWEEN  FRAME 17 AND FRAME 19 ABOVE PASS.CABIN FLOOR  AS REQUIRED.  212400-0503-1 121 AIR DISTR/EXTR.ELECTR.RACKS ERI FUC I: 3 C MPD AMM 212400/5 FUNCTIONAL TEST OF ELECTRONIC RACKS, VENTILATION,  OVERHEAT DETECTOR AND ASSOCIATED CIRCUIT  ACCESS: 131AZ  212700-0505-1 200 GALLEY VENTILATION FILTER MEC CLN I: NOTE 5-2 MPD AMM 253000/3 CLEAN GALLEY VENTILATION FILTERS - CHANGE IF  NECESSARY  213100-0503-1 137 RECIRCULATION VALVE MEC OPC I: 1 C MRB ** AMM 213114/5 171  OPERATIONAL TEST OF RECIRCULATING VALVE AS FOLLOWS:  01. MANUALLY CHECK THAT FLAPS MOVE FULLY AND SMOOTHLY  (FOR INFORMATION: THE VALVE STARTS OPENING WHEN  DIFFERENTIAL PRESSURE IS 6 MB.)  02. ENSURE THAT VALVE SEAT AND GRID ARE CLEAN  ACCESS: 131BZ  162AZ 171AZ  213100-0503-2 134 NEGATIVE PRESS.SAFETY VALVE MEC OPC I: 1 C MRB AMM 213115/5 171  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 VALVE  AS FOLLOWS:  01. MANUALLY CHECK THAT FLAP MOVES FULLY AND SMOOTHLY  (FOR INFORMATION: THE VALVE STARTS OPENING WHEN  DIFFERENTIAL PRESSURE IS 6 MB.)  02. ENSURE THAT VALVE SEAT AND GRIDS ARE CLEAN  ACCESS: 132JF  162AZ 171AZ  213100-0503-3 210 VALVE - PRESSURE REGULATING MEC OPC I: 3 C MRB ** AMM 213100/5 OPERATIONAL TEST OF ELECTRICAL CLOSING OF  PRESS.REGULATING VALVES (DITCHING CONFIGURATION)  213100-0503-4 210 RECIRCULATION VALVE MEC OPC I: 1 C MRB AMM 213100/5 ON PANEL 433 VU:  01. OPERATIONAL TEST OF STEADY "CAB RATE" WARNING  02. OPERATIONAL TEST OF DEPRESS.VALVE "FAULT" WARNING  (POSITION DISAGREE)  03. OPERATIONAL TEST OF DEPRESS VALVE IN "MAN CTL"  (MANUAL CONTROL) MODE  213100-0503-5 210 AUTO CABIN PRESSURE CONTROL MEC OPC I: WEEKLY MRB AMM 213100/5 "TEST OK" OF AUTOMATIC CABIN PRESSURE CONTROL SYSTEM  213100-0505-1 136 VALVE - PRESSURE REGULATING MEC CLN I: 5 A MRB AMM 213100/3 170  CLEAN PRESSURE REGULATING VALVE SEAT AND GRID  (MAY BE CARRIED OUT IN SITU)  ACCESS: 136AR  171AZ  SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 213100-0505-2 136 VALVE - PRESSURE REGULATING MEC CLN I: 2 C MRB AMM 213100/3 170  FOWARD AND AFT VALVES:  01. CLEAN TEFLON COATING OF PRESSURE REGULATING  VALVES SEATS  02. CLEAN ANNULAR GRIDS  (TASK MAY BE CARRIED OUT IN SITU)  ACCESS: 136AR  171AZ  213117-0503-1 137 VALVE-PRESS.RELIEF,GRD.AUTO MEC FUC I: 3 C MRB AMM 213117/5 FUNCTIONAL TEST OF PNEUMATIC LOCKING  ACCESS: 131CZ  213400-0503-1 121 CABIN PRESSURE RELIEF ERI FUC I: 3 C MRB AMM 213411/5 FUNCTIONAL TEST OF "CAB.PRESS." MANOMETRIC SWITCH AND  ASSOCIATED WARNING  ACCESS: 131AZ  213500-0503-1 212 EMERGENCY CABIN DEPRESS. MEC OPC I: 2 C MRB ** AMM 213500/5 MANUAL OPERATIONAL TEST OF EMERGENCY CABIN  DEPRESSURIZATION AS FOLLOWS:  01. ROTATE HANDWHEEL ON FLIGHT ENGINEER ́S PANEL IN  THE OPEN DIRECTION UNTIL IT STOPS,THE MOVEMENT  MUST BE SMOOTH WITHOUT ANY HARD POINTS  02. TURN THE HANDWHEEL IN CLOSE DIRECTION UNTIL IT  STOPS (FULL CLOSING OF THE VALVE) THEN LOCK HAND-  WHEEL  215000-0502-1 140 RAM AIR INLET MEC GVI I: 1 A MRB AMM 215100/6 CHECK COOLING AIR INLETS/OUTLETS FOR GENERAL  CONDITION  SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 215115-0504-1 135 CHECK VALVE - CABIN MEC OPC I: 4 C MRB AMM 215115/4 AMM 215115/6 CHECK VALVE FOR WEAR AND FREEDOM OF FLAPPERS,  CHECK MANUALLY THAT VALVE OPERATES CORRECTLY.  PREP.: REMOVE/INSTALL CHECK VALVE.  ACCESS: 131BZ 137ALF  215116-0505-1 143 SEPARATOR - WATER MEC CLN I: 5 A MRB AMM 215116/3 144  CHECK COALESEUR FOR CONDITION AND CLEANINESS:  01. REMOVE COALESEUR FROM WATER SEPARATOR,  02. CLEAN COALESEUR AND CHECK FOR EVIDENCE OF DAMAGE  OR CONTAMINATION,  03. REINSTALL COALESEUR (ENSURE INDICATOR ROD OF  CLOGGING INDICATOR IS NOT PROTRUDING  (PRE MOD 03696 ONLY)  ACCESS: 147FZ  215121-0503-1 143 REFRIGERATION UNIT MEC OPC I: 3 C MRB AMM 215000/5 144  LEAK CHECK OF REFRIGERATION UNIT WITH RUNNING PACK:  01. PERFORM OPERATIONAL TEST OF REFRIGERATION UNIT.  02. CHECK UNIT AND DUCTS WITHIN AIRCONDITIONING  COMPARTMENT FOR CONDITION AND LEAKS.  ACCESS: 147FZ  215300-0503-1 143 EMERGENCY RAM AIR INLET MEC OPC I: 2 C MRB ** AMM 215300/5 AMM 215300/6 - OPERATIONAL TEST OF EMERGENCY RAM AIR INLET SCOOP.  - GENERAL VISUAL INSPECTION OF EMERGENCY RAM AIR  SCOOP AND DUCT.  ACCESS: 147FZ  215300-0504-1 135 RAM AIR INLET CHECK VALVE MEC OPC I: 4 C MRB AMM 215312/4 AMM 215312/6 CHECK 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: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 215300-0504-1 * * * * * C O N T I N U E * * * * *  01. REMOVE CHECK VALVE  02. CLEAN VALVE AND CHECK FOR WEAR AND FREEDOM OF  FLAPPERS  03. REINSTALL CHECK VALVE  ACCESS: 131CZ  215311-0502-1 140 ACTUATOR-EMER.RAM AIR INLET MEC GVI I: DY-TERM MRB AMM 215300/6 CHECK THAT RAM AIR INLET FLAP IS CLOSED  215500-0503-1 210 GROUND COOLING ERI OPC I: 2 C MPD AMM 212400/5 OPERATIONAL CHECK OF ELECTRIC RACKS GROUND COOLING  SYSTEM "FAULT" WARNING  216200-0503-1 211 COCKPIT & CABIN DUCT TEMP. ERI OPC I: 5 A MPD AMM 216216/4 232 AMM 216222/4 242 REMOVE SENSORS AND INSPECT SENSORS AND SCREENS  252 FOR CLEANLINESS, SATISFACTORY CONDITION AND PERFORM  OPERATIONAL TEST OF SENSOR AIRFLOW FAN  216200-0505-1 200 COCKPIT & CABIN TEMP.CONTR. ERI CLN I: 1 C MRB AMM 216218/4 AMM 216222/4 REMOVE, CLEAN AND REINSTALL COCKPIT TEMPERATURE  SENSOR, TRANSMITTER AND VENT LINE (BETWEEN FRAMES  8 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 216217/4 AMM 216221/4 REMOVE, CLEAN AND REINSTALL DUCT TEMPERATURE  SENSORS 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: 
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A300 MAINTENANCE PLANNING D

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 216300-0503-1 136 TRIM AIR TEMP.CONTROL MEC FUC I: 3 C MRB AMM 216313/5 FUNCTIONAL TEST OF TRIM AIR DIFFERENTIAL PRESSURE  SWITCH.  ACCESS: 136AR  216311-0503-1 143 VALVE-TRIM AIR PRESS.REGUL. MEC FUC I: 4 C MPD AMM 216311/5 FUNCTIONAL TEST OF TRIM AIR PRESSURE REGULATING  VALVES.  ACCESS: 147FZ  216312-0504-1 136 CHECK VALVE, HOT AIR MANIF. MEC OPC I: 4 C MRB AMM 216312/4 AMM 216312/6 CHECK FOR WEAR AND FREEDOM OF FLAPPERS:  01. REMOVE CHECK VALVE  02. CLEAN CHECK VALVE WITH MEK - SOLVENT (MATERIAL  11-003) AND INSPECT FOR CONDITION  03. OPERATE FLAPS OF CHECK VALVE MANUALLY AND CHECK  THAT THEY MOVE FREELY WITH NO HARD POINTS  04. REINSTALL CHECK VALVE  NOTE: TORQUE VALUE IS GIVEN ON THE CLAMPS  ACCESS: 136AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : AIR CONDITIONING REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 221000-0503-1 210 AUTOPILOT ELO OPC I: 4000 FH MRB AMM 221000/5 CN  OPERATIONAL TEST OF AP DISCONNECTION WHEN AP PITCH 94-185-165(B ACTUATOR IS MANUALLY OVERRIDDEN  221000-0503-2 210 AUTOPILOT ELO OPC I: 2000 FH AD AD  CN 2007-04-05 C OPERATIONAL TEST FOR AP DISCONNETION BY STICK FORCE FAA AD CN  APPLICATION ISB F-2005-107(B FAA AD  2007-04-5  ISB 22-0118  221100-0503-1 210 AP/FD ROLL / YAW CHANNEL ELO FUC I: 1 A MRB ** AMM 224200/5 FUNCTIONAL TEST OF COMPARATOR THRESHOLD BY AFCS  SAFETY TEST:  01. AP/FD ROLL/YAW CHANNEL  02. AP/FD PITCH CHANNEL  03. AP/FD LOGIC/MONITOR CHANNEL  04. YAW DAMPER COMPUTER  05. AUTOMATIC PITCH TRIM COMPUTER  06. AUTOTHROTTLE CONTROL COMPUTER  221200-0503-1 210 AP/FD MECHANICAL OVERRIDE ELO OPC I: 1 C MRB ** AMM 221000/5 OPERATIONAL TEST OF MECHANICAL OVERRIDE LEVERS  (TORQUE LIMITER LEVERS) FOR CORRECT OPERATION OF:  - ROLL MECHANICAL OVERRIDE  - YAW MECHANICAL OVERRIDE  - PITCH MECHANICAL OVERRIDE  221512-0503-1 210 FLIGHT CONTROL UNIT ELO OPC I: DY-TERM MRB AMM 220000/5 LAMP TEST OF THE UNIT TO CHECK CORRECT OPERATION OF  DISPLAY  SYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 221521-0503-1 210 FLIGHT MODE ANNUNCIATOR ELO OPC I: DY-TERM MRB AMM 220000/5 LAMP TEST OF THE FLIGHT MODE ANNUNCIATOR TO CHECK  CORRECT OPERATION OF DISPLAY.  222000-0503-1 210 SPEED - ATTITUDE CORRECTION ELO OPC I: 1 A MRB AMM 222700/5 - OPERATIONAL TEST OF ELECTRIC PITCH TRIM MECHANICAL  DISCONNECTION AND OVERRIDE.  - OPERATIONAL TEST OF AUTOTRIM MECHANICAL OVERRIDE  TO CHECK PITCH TRIM DISENGAGEMENT.  222000-0503-2 210 SPEED - ATTITUDE CORRECTION ELO OPC I: 1 A MRB AMM 224000/5 READ "MTP" SEQUENCE TO ASSESS STATUS OF ANGLE  OF ATTACK SENSORS  222000-0504-1 210 SPEED - ATTITUDE CORRECTION MEC DET I: 500 FH AD AD 2006-15-0 CN CN 2005-111( DETAILED VISUAL INSPECTION OF THE AUTOTRIM FUNCTION. ISB ISB 22A0115  222100-0503-1 210 YAW DAMPER ELO OPC I: WEEKLY MRB ** AMM 222100/5 OPERATIONAL TEST TO VERIFY CORRECT OPERATION OF  MECHANICAL CONTROL BETWEEN YAW DAMPER SYSTEM 2 AND  THE RUDDER  222300-0503-1 210 AUTOMATIC PITCH TRIM ELO OPC I: 3000 FH MRB ** AMM 222300/5 CN  OPERATIONAL TEST OF SAFETY DEVICE IN PITCH TRIM 1980-222-030 ENGAGEMENT (ENGAGEMENT AND WARNING TEST) FAA AD 80-18 222300-0503-2 210 MICROSWITCHES - THS ELO FUC I: 1 C MRB ** AMM 222300/5 310  FUNCTIONAL 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: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 222300-0503-2 * * * * * C O N T I N U E * * * * *  ACCESS: 312AR  222300-0503-3 210 AUTOMATIC PITCH TRIM ELO OPC I: 1000 FH AD AD 2006-25-0 CN CN  OPERATIONAL TEST OF PITCH TRIM SYSTEM 2 AT HIGH ISB CN  SPEED OF TRIM F-2005-157(B ISB 22-0121  222300-0504-1 311 SPEED - ATTITUDE CORRECTION MEC RAR I: 12000 FH AD AD 2006-26-1 312 CN CN  REMOVAL OF PITCH TRIM SERVOMOTOR FOR RESTORATION ISB CN  F-2005-109(B ISB 22-0120  222339-0504-1 110 AUTOMATIC PITCH TRIM MEC RAR I: 8000 FH CN CN  OR FAA AD F-2003-457(B REMOVE HONEYWELL AOA SENSOR P/N 965-4020-007 FOR 8 YE OIT FAA AD  SHOP INSPECTION 2006-01-03  OIT SE  ACCESS: 110AL 999.0029/03/ 222600-0503-1 210 YAW DAMPER ELO OPC I: WEEKLY MRB ** AMM 222600/5 OPERATIONAL TEST TO VERIFY CORRECT OPERATION OF  MECHANICAL CONTROL BETWEEN YAW DAMPER SYSTEM 2 AND  THE RUDDER  222634-0504-1 121 FLIGHT AUGMENTATION COMPUT. ELO FUC I: SHOP VIS MRB AMM 222634-4 A COMPLETE ATEC TEST OF THE FAC INCLUDING FOLLOWING  FUNCTIONS:  - ALPHA-FLOOR PROTECTION  - AIRCRAFT CONFIGURATION SIGNALS  ACCESS: 131AZ  SYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 222700-0503-1 210 ELECTRIC PITCH TRIM ELO OPC I: 3000 FH MPD AMM 222700/5 OPERATIONAL TEST OF SAFTY DISENGAGEMENT DEVICES IN  PITCH TRIM ENGAGEMENT  (OVERRIDE TEST)  222700-0503-2 210 MICROSWITCHES-THS ELO OPC I: 1 C MPD AMM 222700/5 310  OPERATIONAL CHECK OF THS TRAVEL LIMIT SWITCHES  ACCESS: 312AR  223000-0503-1 210 AUTOTHROTTLE SYSTEM ELO OPC I: 5 A MRB AMM 341700/5 AMM 342000/5 CHECK CORRECT OPERATION OF ATTITUDE HEADING  REFERENCE UNITS (AHRU) AND HYBRID AIR DATA COMPUTERS  (HADC) SWITCHING.  223100-0503-1 210 AUTOTHROTTLE CONTROL ELO FUC I: 5 A MPD AMM 223100/5 FUNCTIONAL TEST OF FULL THROTTLE LIMIT STOP AND N1  LIMIT STOP.  223100-0503-2 210 AUTOTHROTTLE CONTROL ELO FUC I: 5 A MPD AMM 223100/5 FUNCTIONAL TEST OF FULL THROTTLE LIMIT STOP AND EPR  LIMIT STOP.  223512-0503-1 210 THRUST RATING PANEL ELO OPC I: 1 C MRB AMM 223000/5 CHECK CORRECT OPERATION OF AUTOMATIC CHANGE  OVER OF T.A.T. DISPLAY (HADC1 / HADC2)  223512-0503-2 210 THRUST RATING PANEL ELO OPC I: DY-TERM MRB AMM 220000/5 LAMP TEST OF THE PANEL TO CHECK CORRECT OPERATION OF  DISPLAY  SYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 223634-0503-1 210 THRUST CONTROL COMPUTER ELO OPC I: DY-TERM MRB  OPERATIONAL TEST OF EPR LIMIT COMPUTATION (WITH  THRUST RATING PANEL).  223634-0503-2 210 THRUST CONTROL COMPUTER ELO OPC I: DY-TERM MRB AMM 220000/5 OPERATIONAL TEST OF N1 LIMIT COMPUTATION (WITH  THRUST RATING PANEL).  224200-0502-1 210 AUTOMATIC FLIGHT CONTROL SYSTEM TEST ELO OPC I: NOTE MRB AMM 224200/5 CHECK THE STATE OF TEST PANEL MAGNETIC INDICATORS.  NOTE: AFTER EACH AUTOMATIC LANDING OR AUTOMATIC  LANDING ATTEMPT WITH AP1 AND AP2 ENGAGED  (CAT III CONDITIONS)  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : AUTO FLIGHT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 231100-0503-1 210 HF-SYSTEM RAD OPC I: DY-TERM MRB ** AMM 231100/5 OPERATIONAL TEST OF HF SYSTEM (IF REQUIRED FOR  FLIGHT).  235100-0503-1 210 AUDIO INTERGRATING RAD OPC I: WEEKLY MRB ** AMM 235100/5 OPERATIONAL TEST OF AUDIO INTEGRATING SYSTEM  236000-0502-1 300 STATIC DISCHARGING RAD GVI I: 1 A MRB AMM 236000/0 500  600 CHECK PRESENCE OF ALL STATIC DISCHARGERS LOCATED  ON THE WINGS AND EMPENNAGE  236000-0503-1 500 STATIC DISCHARGING RAD FUC I: 2 C MRB AMM 236000/6 600  FUNCTIONAL TEST OF STATIC DISCHARGERS ON THE WING:  01. CHECK RESISTANCE BETWEEN RETAINER AND AIRCRAFT  STRUCTURE (MAX. AUTHORIZED VALUE: 1 OHM),  02. CHECK FOR CONDITION.  236000-0503-2 300 STATIC DISCHARGING RAD FUC I: 2 C MRB AMM 236000/6 FUNCTIONAL TEST OF STATIC DISCHARGERS ON THE RUDDER  AND ELEVATOR:  01. CHECK RESISTANCE BETWEEN RETAINER AND AIRCRAFT  STRUCTURE.(MAX.AUTHORIZED VALUE: 1 OHM),  02. CHECK FOR CONDITION.  237100-0503-1 171 COCKPIT VOICE RECORDER RAD FUC I: 2 C MRB AMM 237100/5 CMM 277001  FUNCTIONAL TEST OF UNDERWATER LOCATOR BEACON AND  REPLACE BATTERY IF NECESSARY  ACCESS: 162AZ  237100-0503-2 210 COCKPIT VOICE RECORDER RAD OPC I: DY-TERM MRB ** AMM 237100/5 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : COMMUNICATIONS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 237100-0503-2 * * * * * C O N T I N U E * * * * *  SELF TEST OF COCKPIT VOICE RECORDING SYSTEM  237100-0504-1 171 COCKPIT VOICE RECORDER RAD RAR I: VR MRB CMM 237001  REMOVE AND REPLACE BATTERY OF UNDERWATER  LOCATOR BEACON ATTACHED TO THE COCKPIT VOICE RECORDER  ACCESS: 162AZ  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : COMMUNICATIONS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 240000-0503-1 120 ELECTRICAL POWER GENERAL ERI DET I: 18 MO CN CN  FAA AD 1994-187-163 DETAILED INSPECTION OF 104 VU ELECTRICAL LOOM FAA AD 95-10 INSTALLATION ISB 24-0087  NOTE: THIS TASK IS RELATED TO MECHANICAL INSPECTION  OF AVIONIC COMPARTMENT LADDER, REF TASK  532411-0502-1.  ACCESS: 121BL  240000-0503-2 200 ELECTRICAL POWER-GENERAL ERI OPC T: 24 MO SIL AMM 240000/6 I: 36 MO SIL 20-0017  OPENING AND CLOSING OF ALL CIRCUIT BREAKERS.  PREP.: ELECTRICAL POWER OFF  241111-0503-1 436 CONSTANT SPEED DRIVE ENG OPC I: CSD CHG MRB ** AMM 241100/5 446 ENG.CHG  OPERATIONAL TEST OF CSD DISCONNECT AND RESET SYSTEM  (WITH ENGINE STOPPED)  ACCESS: 435AL 436AR  445AL 446AR  241111-0504-1 435 CONSTANT SPEED DRIVE MEC RAR I: 4 C MPD AMM 241121/4 445 OR NOTE SIL SUN 192  01. REMOVE CSD OIL HEAT EXCHANGER AND OIL COOLING  TUBING  02. CLEAN CSD OIL HEAT EXCHANGER AND OIL COOLING  TUBING  03. REINSTALL CSD OIL HEAT EXCHANGER AND OIL COOLING  TUBING  NOTE: TASK MAY BE ACCOMPLISHED AT THE OPPORTUNITY  OF THE ENGINE SHOP VISIT  ACCESS: 435AL 436AR  445AL 446AR  SYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION: 
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 241111-0504-2 435 CONSTANT SPEED DRIVE MEC RAR I: 4 C MPD AMM 792106/4 445 OR NOTE SIL SUN 192  01. REMOVE CSD OIL HEAT EXCHANGERS AND OIL COOLING  TUBING  02. CLEAN CSD OIL HEAT EXCHANGERS AND OIL COOLING  TUBING  03. REINSTALL CSD OIL HEAT EXCHANGERS AND OIL COOLING  TUBING  NOTE: TASK MAY BE ACCOMPLISHED AT THE OPPORTUNITY  OF THE ENGINE SHOP VISIT  ACCESS: 435AL 436AR  445AL 446AR  241111-0505-1 436 CONSTANT SPEED DRIVE ENG RPL I: 1 A MRB AMM 121324/0 446 AMM 241100/3 01. CHECK OIL LEVEL OF CONSTANT SPEED DRIVE AND AMM 241100/6 REPLENISH IF NECESSARY  02. CHECK CSD SCAVENGE FILTER AND CHARGE FILTER  CLOGGING INDICATORS ARE NOT PROTRUDING (AS  APPLICABLE)  03. CHECK MANUALLY THE QAD RING FOR EVIDENCE OF PLAY  ACCESS: 436AR  446AR  241111-0505-2 436 CONSTANT SPEED DRIVE ENG RPL I: 3 A MRB AMM 241100/3 446 OR SB SUN 24-13 REPLACE SCAVENGE FILTER ELEMENT AND CHECK FOR SB SUN  CONTAMINATION 24-1341  ACCESS: 436AR  446AR  242111-0505-1 436 GENERATOR - AC - ENGINE ENG RPL I: 3 A MRB AMM 121324/0 446  CHECK OIL LEVEL OF GENERATOR AND REPLENISH IF  NECESSARY  ACCESS: 436AR  446AR  SYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 242112-0503-1 121 GENERATOR CONTROL UNIT ERI OPC I: 1 C MRB ** AMM 242112/4 OPERATIONAL TEST OF GENERATOR CONTROL UNITS (APU GCU  INCLUSIVE)  ACCESS: 132AZ  242200-0502-1 261 APU GENERATOR FEEDER CABLES ERI GVI I: 200 FC CN CN  262 FAA AD 1981-058-033 VISUAL INSPECTION OF APU GENERATOR FEEDER CABLE FAA AD 80-26 SLICES AT FRAME 78 AND 79 FOR SATISFACTORY CONDITION. ISB 24-0048  242200-0503-2 471 AC GENER.FEEDERS/ENG.WIRING ENG DET I: 1000 FH CN CN 2001-555( 481 FAA AD FAA AD  CHECK CONDITION OF FILLET SEAL, GENERATOR 2002-04-05  FEEDERS AND ENGINE WIRING HARNESS IN PYLON ISB 24-0053  (INCLUDING ZONE 472 AND 482) ISB 24-0083  ACCESS: 471AL 472AR  481AL 482AR  242211-0505-1 315 GENERATOR-AC-APU ENG RPL I: 3 A MRB AMM 121324/0 CHECK OIL LEVEL OF GENERATOR AND REPLENISH IF  NECESSARY  ACCESS: 315AL 316AR  242311-0503-1 210 INVERTER-115V/600VA STATIC ERI OPC I: DY-TERM MRB ** AMM 242311/4 OPERATIONAL TEST OF STATIC INVERTERS  242400-0503-1 210 SWITCHING-AC GEN./ESS.CIRCT ERI OPC I: ENG. CHG MRB ** AMM 242400/5 OPERATIONAL TEST OF THE AC ESS BUS OVERRIDE SUPPLY  SYSTEMS AND POWERPLANT PROGRAM : ELECTRICAL POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 242400-0503-2 210 SWITCHING-AC GEN./ESS.CIRCT ERI OPC I: ENG. CHG MRB AMM 242400/5 OPERATIONAL TEST OF THE SMOKE DRILL CONFIGURATION  (OVRD SUPPLY 1 AND 2) INCLUDING THE AUTOMATIC CHANGE  OVER  243100-0503-1 210 BATTERIES ERI OPC I: DY-TERM MRB AMM 243111/4 CHECK BATTERIES FOR CORRECT VOLTAGE  243111-0502-1 122 BATTERIES ERI DET I: 750 FH MRB AMM 243100/3 01. CHECK ACCUMULATORS AND CONNECTIONS FOR SIGNS OF  OVERHEATING OR ELECTROLYTE OVERFLOW  02. CHECK NO-LOAD VOLTAGE OF ACCUMULATORS  03. CHECK BATTERY MOUNTING RACK FOR CLEANLINESS,  SECURITY OF ATTACHMENTS AND SATISFACTORY CONDI-  TION  ACCESS: 132AZ  243111-0504-1 122 BATTERIES ERI RAR I: NOTE 5-1 MRB AMM 243111/4 REMOVE BATTERIES FOR SHOP VISIT  ACCESS: 132AZ  243112-0503-1 121 MONITORING UNIT-BATT CHARGE ERI OPC I: 1 C MRB ** AMM 243112/4 OPERATIONAL TEST OF BATTERY CHARGE LIMITER (CHARGE  MONITORING UNIT) BY BITE  ACCESS: 132AZ  243211-0503-1 120 TRANSFORMER RECTIFIER-150A ERI OPC I: 2 A MPD AMM 243211/6 SIL 24-025  OPERATIONAL TEST OF TRANSFORMER RECTIFIER COOLING  FANS, 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: 
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 243211-0503-1 * * * * * C O N T I N U E * * * * *  ACCESS: 132AZ  245000-0503-1 210 ELECTR.LOAD DISTRIBUTION ERI OPC I: 1 C MRB ** AMM 245000/5 OPERATIONAL TEST OF "NORM EQPT/ESS BUS MIN EQPT"  SWITCH AND "SMOKE DRILL NAV SELECT" SWITCH  245000-0503-2 210 ELECTR.LOAD DISTRIBUTION ERI OPC I: 1 C MRB ** AMM 245000/5 OPERATIONAL 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: 
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INTERVAL (I)

 251100-0502-1 210 FLIGHT COMPARTMENT SEATS MEC DET I: 2 C MRB AMM 251111/6 AMM 251112/6 DETAILED INSPECTION OF CREW SEAT STRUCTURE AND AMM 251113/6 SEAT TO FLOOR ATTACHMENTS  251100-0503-1 210 FLIGHT COMPARTMENT SEATS MEC OPC I: 2 C MRB AMM 251111/5 AMM 251112/5 OPERATIONAL TEST OF CREW SEATS IN MECHANICAL AND AMM 251113/5 ELECTRICAL MODES, CHECK PROPER OPERATION OF INERTIA  REELS AND GENERAL CONDITION OF HARNESS.  252100-0502-1 200 PASSENGER COMPARTMENT SEATS MEC DET I: 2 C MRB AMM 252000/0 1. DETAILED INSPECTION OF PASSENGER AND  CABIN ATTENDANT SEAT TO FLOOR ATTACHMENTS FOR  SATISFACTORY CONDITION, CRACKS, AND CORROSION  2. GENERAL VISUAL INSPECTION OF SEATS INCLUDING  LEGS, FRAME, BACKREST, ARMREST AND TABLE  RETAINER FOR SATISFACTORY CONDITION, CRACKS  AND CORROSION  252100-0502-2 200 CREW REST UNIT MEC GVI I: 2 C MRB AMM 253111/6 GENERAL VISUAL INSPECTION OF CREW REST UNIT SEATS AND  FURNISHING INCLUDING SEAT BELT ASSY AND FLOOR  ATTACHMENT STRUCTURE.  252331-0502-1 200 PANELS-LOWER SIDEWALL MEC DET I: 1 C MPD SIL 25-085  REMOVE PANEL AND CARRY OUT DETAILED INSPECTION  OF LOWER SIDE WALL PANEL AND OF AREA BEHIND LOWER  SIDE WALL PANEL FOR FOREIGN MATERIAL ACCUMULATION.  NOTE: 01. ONE LOWER SIDE WALL PANEL IN FWD MID AND  AFT PASSENGER CABIN SHOULD BE REMOVED IN  ORDER TO ACCESS THE NEED FOR MORE  EXTENSIVE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 RECOMMENDED  AT NEXT INSPECTION.  03. INTERVAL MAY BE ADJUSTED ACCORDING TO  OPERATOR EXPERIENCE.  252331-0503-1 200 PANELS-LOWER SIDE WALL MEC OPC I: 2 C MRB ** AMM 256610/2 OPERATIONAL TEST OF DECOMPRESSION PANELS, TEST AT  LEAST ONE PANEL IN EACH ZONE:  01. PRESS SPRING-LOADED MOVABLE (DECOMPRESSION)  PANELS AT LOWER REGION OF GRILL TOWARDS REAR  02. PANEL MUST BE CLOSED AUTOMATICALLY  253000-0502-1 200 BUFFET AND GALLEY MEC GVI I: 1 C MRB AMM 253000/6 GENERAL 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 253111/4 AMM 253211/4 DETAILED INSPECTION OF GALLEY LOWER AMM 253311/4 ATTACHMENTS.  EFERENC REMARKS: CARRY OUT THIS TASK TOGETHER WITH  ZL-220-0403-5  254000-0502-1 200 LAVATORY COMPARTMENTS MEC DET I: NOTE 5-3 MPD FAA AD 74-08 OR  DETAILED INSPECTION OF ALL LAVATORY PAPER AND C  LINEN WASTE RECEPTACLE ENCLOSURE ACCESS DOORS AND  DISPOSAL DOORS FOR PROPER OPERATION, FIT, SEALING AND  LATCHING FOR THE CONTAINMENT OF POSSIBLE TRASH FIRES  NOTE: 1000 FH INTERVAL FOR OPERATORS FLYING  UNDER FAA REGULATIONS AS PER AD 74-08-09R2  255000-0502-1 100 CARGO COMPARTMENTS MEC GVI I: 1 A MRB AMM 255180/0 AMM 255280/0 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 523000/3 COMPARTMENTS, INCL. DOORS AND CARGO LOADING SYSTEM  FOR CONDITION AND CLEANLINESS (CHECK DRAIN PANS FOR  ANY EVIDENCE OF DRAINAGE SYSTEM OBSTRUCTION).  255120-0502-1 100 LININGS AND CEILINGS MEC GVI I: DY-TERM CN CN  FAA AD 1982-022-044 GENERAL VISUAL INSPECTION OF DECOMPRESSION PANELS FAA AD 85-17 IN PARTITION WALL, SIDEWALLS AND CEILING LININGS FOR ISB 25-0138  CONDITION AND CORRECT ATTACHMENT IN PANEL CUT-OUT.  255120-0502-2 100 LININGS AND CEILINGS MEC GVI I: 600 FH CN CN  FAA AD 1982-022-044 CHECK FWD,AFT AND BULK CARGO COMPARTMENTS MRB ** FAA AD 85-17 DECOMPRESSION PANELS IN POSITION AND CORRECTLY ISB 25-0138  ATTACHED (ZONE 130,150,160)  255130-0502-1 130 FWD CARGO COMPARTMENT MEC GVI I: NOTE 5-2 MRB AMM 255100/7 01. VACUUM CLEANING OF FWD CARGO CONVEYANCE  SYSTEM.  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 255100/7 01. 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 255800/6 GENERAL VISUAL INSPECTION OF BARRIER NET AND SMOKE  PROTECTIVE CURTAIN IN CABIN.  SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 255853  I: 1 YE  REMOVE TEST NET STRAP AND PERFORM FUNCTIONAL  TEST (A SAMPLE TEST PROOF LOADING)  255820-0504-1 200 BARRIER NET AND SMOKE CURT. MEC RAR I: NOTE 5-1 MRB ** AMM 255823/4 AMM 255824/4 REMOVE BARRIER NET AND SMOKE CURTAIN, SEND TO  WORKSHOP OR MANUFACTURER FOR OVERHAUL  255830-0502-1 200 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 3 A MRB AMM 255810/0 GENERAL VISUAL INSPECTION OF CARGO LOADING SYSTEM,  CLEAN IF NECESSARY.  255830-0502-2 200 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: NOTE 5-2 MRB AMM 255800/7 01. 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 SYSTEM  INSTALLATION.  256100-0502-1 830 ESCAPE FACILITIES MEC GVI I: WEEKLY MRB ** AMM 256100/6 840  CHECK ESCAPE SLIDE/RAFT BOTTLES FOR CORRECT  PRESSURE AND CONTAINER FOR SATISFACTORY CONDITION (IN  SITU)  256111-0503-1 830 SLIDE/RAFT - ESCAPE MEC FUC I: 6 MO MRB ** AMM 256100/5 840  01. FUNCTIONAL TEST OF ESCAPE SLIDE/RAFT LIGHTING REFERENC SYSTEM (BATTERY CAPACITY CHECK).  02. BULB CONTINUITY CHECK.  256111-0503-2 830 SLIDE/RAFT ESCAPE MEC OPC I: 18 MO MRB ** AMM 256100/3 840 OR AMM 256100/5 OPERATIONAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 DOOR  POSITION, (831 OR 841), (832 OR 842),  (833 OR 843), (834 OR 844).  - ONE SAMPLE PER OPERATOR FLEET.  - ALTERNATE DOOR POSITION AT NEXT INTERVAL  RECOMMENDED.  - CREW TRAINING MAY BE USED TO SATISFY THIS  REQUIREMENT.  NOTE: REFER TO TASK 256111-0504-2  256111-0503-3 830 SLIDE/RAFT - ESCAPE MEC RAR I: NOTE 5-3 MRB ** AMM 256111/4 840 AMM 256112/4 REMOVE ESCAPE SLIDE/RAFTS FOR SHOP RESTORATION AMM 256115/4 256111-0504-2 830 SLIDE/RAFT-ESCAPE BATTERIES MEC RAR I: 4 YE MRB ** AMM 256100/5 840  REPLACE ESCAPE SLIDE/RAFT BATTERIES (MODEL  BAS 10-1 OR BAS 19)  NOTE: REFER TO TASK 256111-0503-2  256111-0504-3 830 SLIDE/RAFT - AIR BOTTLE MEC RAR I: NOTE 5-3 MRB ** AMM 256111/4 840 AMM 256112/4 HYDROSTATIC TEST OF AIR BOTTLES IN ACCORD. WITH LOCAL AMM 256115/4 NATIONAL REQUIREMENTS OR PRIOR TO NEXT FULL OR  PARTIAL REFILLING AFTER 36 MONTHS SINCE LAST  HYDROSTATIC TEST. (MAX. SERVICE LIFE IN ACCORD. WITH  NAT.REQTS/MANUF. RECOMMENDATIONS).  256113-0503-1 210 DESCENT DEVICE-EMERGENCY MEC RAR I: 60 MO MRB AMM 256113/4 REMOVE EMERGENCY DECENT DEVICES AND SEND TO  VENDOR  SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 256200-0502-1 200 FLOTATION & SURVIVAL EQUIP. MEC GVI I: WEEKLY MRB ** AMM 256200/6 GENERAL VISUAL INSPECTION OF FLOTATION AND SURVIVAL  EQUIPMENT.  256200-0504-1 200 FLOAT. AND SURVIVAL EQUIP. MEC RAR I: NOTE 5-3 MRB ** AMM 256200/0 - REMOVE/REPLACE LIFE VESTS FOR OVERHAUL.  (IF INSTALLED).  256300-0503-1 210 EVACUATION SIGNALING EQUIP. MEC OPC I: 2 A MRB ** AMM 256300/5 OPERATIONAL TEST OF EVACUATION SIGNALING EQUIPMENT.  256531-0503-1 200 TRANSMITTER-BEACON ERI OPC I: NOTE 5-1 MRB ** AMM 256533/4 REMOVE EMERGENCY LOCATOR TRANSMITTER FOR  WORKSHOP TEST (BATTERY CHECK AND FUNCTIONAL  TEST)  256532-0503-1 200 MEGAPHONE ERI OPC I: 1 C MRB AMM 256532/6 OPERATIONAL TEST OF MEGAPHONE  256532-0504-1 200 MEGAPHONE ERI RAR I: NOTE 5-1 MRB ** AMM 256532/6 CMM 256504  DISCARD MEGAPHONE BATTERIES.  257200-0502-1 147 WHEEL WELLS MEC DET I: 2 YE ISB ISB 25-0477  148  DETAILED INSPECTION OF THE ATTACHMENT FITTINGS  OF THE ACCESS PANELS BETWEEN THE AIR CONDITIONING-  AND THE MAIN LANDING GEAR BAYS  ACCESS: 147FZ 147GZ 147MZ  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 257200-0502-1 * * * * * C O N T I N U E * * * * *  148GZ 148HZ  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : EQUIPMENT/FURNISHINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 261100-0503-1 120 AVIONICS COMP. SMOKE DETECT. ERI FUC I: 1 C MRB ** AMM 261100/5 FUNCTIONAL TEST OF POWER SUPPLY AND FAULT MONITORING  CIRCUIT  ACCESS: 132AZ  261100-0503-2 210 AVIONICS COMP. SMOKE DETECT. ERI OPC I: WEEKLY MRB ** AMM 261100/5 AMM 261400/5 OPERATIONAL TEST OF SMOKE DETECTION SYSTEM AMM 261700/5 AVIONICS/CARGO COMPARTMENT, TOILET VENTILATION SYSTEM  261112-0505-1 100 DETECTOR-SMOKE ERI CLN I: 4000 FH MRB ** AMM 261112/4 NOTE AMM 261411/4 REMOVE,CLEAN AND INSPECT SMOKE DETECTORS FOR SIL 26-015  SATISFACTORY CONDITION IN ZONES 120,130,150,160  AND 170 AND CLEAN ASSOCIATED INLET AND OUTLET  DUCTINGS OF DUCT SMOKE DETECTORS IN ZONE 120  NOTE: INTERVAL 4000 FH RECOMMENDED BUT TO BE  ADJUSTED TO SUIT OPERATING ENVIRONMENT  ACCESS: 132AZ 134AR  261112-0505-2 100 DETECTOR SMOKE ERI CLN I: 4000 FH MRB ** AMM 261112/4 NOTE AMM 261411/4 01. REMOVE CLEAN AND CHECK SMOKE DETECTORS IN FWD SIL 26-015  CARGO COMPARTMENT INCLUDING DUCT SMOKE DETECTORS  IN ZONE 133/134 FOR SATISFACTORY CONDITION  02. REMOVE LININGS IN ZONE 162 AS REQUIRED  03. REMOVE SMOKE DETECTORS OF AFT AND REAR CARGO  COMPARTMENT INCLUDING DUCT SMOKE DETECTORS IN  ZONE 162, CLEAN AND INSPECT FOR SATISFACTORY  CONDITION  04. CLEAN ASSOCIATED INLET AND OUTLET DUCTINGS  OF DUCT SMOKE DETECTORS IN ZONE 133/134/162  05. INSTALL SMOKE DETECTORS  06. REINSTALL LININGS  NOTE: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 261112-0505-2 * * * * * C O N T I N U E * * * * *  ADJUSTED TO SUIT OPERATING ENVIRONMENT  ACCESS: 134AR 162AZ  261121-0503-1 210 FAN-SMOKE DETECTION SNIFFER ERI OPC I: 1 C MRB ** AMM 261121/4 OPERATIONAL TEST OF SMOKE DETECTION SNIFFER FAN (MIN  EQT BAY SNIFFER FAN)  261200-0503-1 122 ENGINE FIRE DETECTION ELO OPC I: 1 C MPD AMM 261200/5 BITE TEST OF ENGINE FIRE DETECTION CONTROL UNITS  ACCESS: 131AZ 132AZ  261200-0503-2 210 ENGINE FIRE DETECTION ELO OPC I: 2 C MPD AMM 261200/5 EXTENDED "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 261200/5 AMM 261300/5 OPERATIONAL TEST OF ENGINE AND APU FIRE DETECTION  SYSTEM (LOOP TEST)  261200-0503-4 210 ENGINE FIRE DETECTION ELO OPC I: DY-TERM MPD AMM 261200/5 "LOOP TEST" ON ENGINE FIRE CONTROL PANELS (FIRE  DETECTION IN "LOOP A AND LOOP B" CONFIGURATION).  261600-0503-1 210 OVERHEAT DETECTION ERI OPC I: WEEKLY MRB ** AMM 261600/5 OPERATIONAL TEST OF MANIFOLD FAULT DETECTION SYSTEM  (LOOPS TEST ON PANEL 59VU).  SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 261600-0503-2 210 OVERHEAT DETECTION ELO OPC I: WEEKLY MRB ** AMM 261600/5 OPERATIONAL TEST OF MANIFOLD "LEAK" DETECTION  SYSTEM.(LOOPS TEST ON PANEL 471VU)  261700-0503-1 120 SMOKE DETEC-LAVATORY VENT. ERI FUC I: 1 C MRB AMM 261700/5 FUNCTIONAL TEST OF POWER SUPPLY AND FAULT MONITORING  CIRCUIT  ACCESS: 132AZ  261900-0503-1 120 SMOKE DETECTION - CABIN CARGO ERI FUC I: 1 C MRB ** AMM 261900/5 FUNCTIONAL TEST OF POWER SUPPLY AND FAULT MONITORING  CIRCUIT.  NOTE: IN CARGO CONFIGURATION ONLY.  261900-0503-2 210 SMOKE DETECTION - CABIN CARGO ERI OPC I: DY-TERM MRB ** AMM 261900/5 OPERATIONAL TEST OF SMOKE DETECTION SYSTEM CABIN  CARGO  NOTE: IN CARGO CONFIGURATION ONLY  261911-0505-1 200 DETECTOR - SMOKE ERI CLN I: 2 C MRB ** AMM 261912/4 SIL 26-015  CLEAN UPPER (MAIN) DECK SMOKE DETECTORS AND INSPECT  FOR SATISFACTORY CONDITION.  PREP.: REMOVE/INSTALL SMOKE DETECTORS.  SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 262100-0502-1 415 ENGINE FIRE EXTINGUISHING MEC DET I: 8000 FH CN AMM 262100/6 425 FAA AD CN  DETAILED INSPECTION OF FIRE EXTINGUISHER PIPE 1990-056-106 AT RIB 12 OF ENGINE PYLON. FAA AD 92-23 ACCESS: 415AL 416AR 473AL 474AR  425AL 426AR 483AL 484AR  262100-0503-1 473 ENGINE FIRE EXTINGUISHING ENG FUC I: 3 C MRB ** AMM 262100/5 484  FUNCTIONAL TEST OF ELECTRICAL PERCUSSION CIRCUIT  AND EXTINGUISHER BOTTLE LOW PRESSURE INDICATING  ELECTRICAL CIRCUIT.  ACCESS: 473AL  484AR  262100-0503-2 473 ENGINE FIRE EXTINGUISHING ENG OPC I: 3 C MRB ** AMM 262100/5 484  OPERATIONAL TEST OF CHECK VALVE AND CHECK  EXTINGUISHER LINES FOR LEAKAGE AND SATISFACTORY  CONDITION  ACCESS: 435AL 436AR 473AL  445AL 446AR 484AR  262100-0503-3 474 ENGINE FIRE EXTINGUISHING ENG FUC I: NOTE CN AMM 262111/4 484 FAA AD CN  BONDING CHECK OF FIRE-EXTINGUISHER BOTTLE 1988-181-089 INSTALLATION FAA AD 89-09 NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY  OF TASK 262111-0504-1 AND 262113-0504-1  ACCESS: 473AL  484AR  262100-0503-4 210 ENGINE FIRE EXTINGUISHING ENG OPC I: DY-TERM MRB ** AMM 262100/5 OPERATIONAL TEST OF ENGINE FIRE EXTINGUISHING  CIRCUITS (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: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 262100-0503-4 * * * * * C O N T I N U E * * * * *  DOES NOT INDICATE DISCHARGE  262111-0503-1 474 BOTTLE - FIRE EXTING.ENGINE ENG FUC I: 2 C MRB AMM 262111/6 484  FUNCTIONAL CHECK OF SHOCK-ABSORBERS:  01. COMPRESS SHOCK-ABSORBERS BY APPLICATION OF A  FORCE EQUAL TO 1/4 OF BOTTLE WEIGHT  02. CHECK HEIGHT OF SHOCK-ABSORBERS BETWEEN UPPER  AND LOWER FASTENING POINT  03. IF DIMENSION IS LOWER THAN, OR EQUAL TO, 8MM RE-  PLACE SHOCK ABSORBERS  ACCESS: 473AL  484AR R 262111-0504-1 474 BOTTLE - FIRE EXTING.ENGINE ENG RAR I: NOTE 5-3 MRB ** AMM 262111/6 484 OR  WEIGHT CHECK OF ENGINE FIRE EXTINGUISHER BOTTLES. NOTE 5-1  NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY  OF TASK 262100-0503-3  ACCESS: 473AL  484AR R 262111-0504-2 474 BOTTLE - FIRE EXTING.ENGINE ENG RAR I: NOTE 5-3 MRB ** AMM 262111/4 484 OR  HYDROSTATIC TEST OF ENGINE FIRE EXTINGUISHER NOTE 5-1  BOTTLES  ACCESS: 473AL  484AR  262111-0504-3 474 ENGINE FIRE EXTING. BOTTLE ENG RAR I: 6 MO ISB AMM 262111/6 484 ISB 26-025  REMOVE FIRE EXTINGUISHING BOTTLE FOR WEIGHT  CHECK, 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: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 262111-0504-3 * * * * * C O N T I N U E * * * * *  ACCESS: 473AL  484AR  262113-0504-1 474 CARTRIDGE-DISCHARGE-ENGINE ELO RAR I: NOTE 5-1 MRB AMM 262113/4 484  REPLACE DISCHARGE CARTRIDGE OF ENGINE FIRE  EXTINGUISHERS  NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY  OF TASK 262100-0503-3  ACCESS: 473AL  484AR  262200-0502-1 313 APU FIRE EXTINGUISHING ENG GVI I: DY-TERM MRB AMM 262200/0 CHECK APU FIRE EXTINGUISHER BOTTLE DISCHARGE  INDICATOR FOR PRESENCE  262200-0503-1 313 APU FIRE EXTINGUISHING ERI FUC I: 3 C MRB ** AMM 262200/5 01. FUNCTIONAL TEST OF ELECTRICAL PERCUSSION CIRCUIT  02. FUNCTIONAL TEST OF AUTOMATIC EXTINGUISHING  CIRCUIT  03. FUNCTIONAL TEST OF THE EXTINGUISHER BOTTTLE  PRESSURE DROP INDICATING CIRCUIT  ACCESS: 313AL  262200-0503-2 210 APU FIRE EXTINGUISHING ERI OPC I: WEEKLY MRB ** AMM 262200/5 OPERATIONAL TEST OF APU FIRE EXTINGUISHING CIRCUIT  (SQUIB TEST) PERFORM GROUND TEST OF THE APU AUTOMATIC  EXTINGUISHING CIRCUIT.  262211-0504-1 313 BOTTLE - FIRE EXTING. APU ENG RAR I: NOTE 5-3 MRB ** AMM 262211/4 OR  WEIGHT 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: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 262211-0504-1 * * * * * C O N T I N U E * * * * *  ACCESS: 313AL  262211-0504-2 313 BOTTLE - FIRE EXTING. APU ENG RAR I: NOTE 5-3 MRB ** AMM 262211/4 HYDROSTATIC TEST OF APU FIRE EXTINGUISHER BOTTLE 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)  ACCESS: 313AL  262212-0504-1 313 CARTRIDGE - DISCHARGE APU ELO RAR I: NOTE 5-1 MRB AMM 262212/4 REPLACE DISCHARGE CARTRIDGE OF APU FIRE EXTINGUISHER.  ACCESS: 313AL  262300-0503-1 132 CARGO COMPART FIRE EXTING. ELO FUC I: 3 C MRB ** AMM 262300/5 01. FUNCTIONAL TEST OF ELECTRICAL PERCUSSION CIRCUIT  02. FUNCTIONAL TEST OF EXTINGUISHER BOTTLE PRESSURE  DROP INDICATING CIRCUIT  ACCESS: 132DZ  262300-0503-2 210 CARGO COMPART.FIRE EXTING. ELO OPC I: DY-TERM MRB ** AMM 262300/5 OPERATIONAL TEST OF CARGO COMPARTMENTS FIRE  EXTINGUISHING CIRCUITS (SQUIB TEST). CHECK THAT AGENT  INDICATOR DOES NOT INDICATE DISCHARGE  262300-0503-3 210 CARGO COMPART.FIRE EXTING. ELO OPC I: DY-TERM MPD AMM 262300/5 VALVE POSITION TEST OF AFT/BULK CARGO COMPARTMENT  FIRE EXTINGUISHING DIRECTION VALVE  SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 262311-0504-1 132 BOTTLE - FIRE EXTING. CARGO MEC RAR I: NOTE 5-3 MRB ** AMM 262311/4 OR  WEIGHT CHECK OF FWD CARGO COMPARTMENT FIRE 1 YE  EXTINGUISHER BOTTLES  ACCESS: 132DZ  262311-0504-2 132 BOTTLE - FIRE EXTING.CARGO MEC RAR I: NOTE 5-3 MRB ** AMM 262311/4 HYDROSTATIC TEST OF FWD CARGO COMPARTMENT FIRE  EXTINGUISHER BOTTLES 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)  ACCESS: 132DZ R 262312-0504-1 132 BOTTLE - FIRE EXTING.CARGO MEC RAR I: NOTE 5-1 MRB AMM 262312/4 REPLACE DISCHARGE CARTRIDGE OF FWD CARGO COMPARTMENT  FIRE EXTINGUISHERS.  ACCESS: 132DZ  262411-0502-1 120 PORTABLE FIRE EXTINGUISHER MEC GVI I: 1 A MRB ** AMM 262400/0 CHECK PRESSURE OF PORTABLE FIRE EXTINGUISHER  AT GAUGE IN AVIONICS COMPARTMENT  262411-0502-2 200 PORTABLE FIRE EXTINGUISHER MEC GVI I: 1 A MRB ** AMM 262400/0 CHECK PRESSURE OF PORTABLE FIRE EXTINGUISHERS  AT GAUGE IN CABIN AREA  262411-0502-3 210 PORTABLE FIRE EXTINGUISHER MEC GVI I: 1 A MRB ** AMM 262400/0 CHECK PRESSURE OF PORTABLE FIRE EXTINGUISHER  AT GAUGE IN FLIGHT COMPARTMENT  SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 262411-0504-1 121 PORTABLE FIRE EXTINGUISHER MEC RAR I: NOTE 5-3 MRB ** AMM 262400/0 200 OR  WEIGHT CHECK OF PORTABLE FIRE EXTINGUISHER BOTTLES. 1 YE  262411-0504-2 121 PORTABLE FIRE EXTINGUISHER MEC RAR I: NOTE 5-3 MRB ** AMM 262400/0 200  HYDROSTATIC TEST OF PORTABLE FIRE EXTINGUISHER  BOTTLES IN ACCORDANCE WITH LOCAL NATIONAL REQUIRE-  MENTS, OR PRIOR TO NEXT FULL OR PARTIAL REFILLING  AFTER 60 MONTHS SINCE LAST HYDROSTATIC TEST.  (MAXIMAL SERVICE LIFE IN ACCORDANCE WITH NATIONAL  REQUIREMENTS/VENDOR RECOMMENDATIONS)  262411-0504-3 200 PORTABLE FIRE EXTINGUISHER MEC RAR I: NOTE 5-3 MRB ** AMM 262400/0 OR  WEIGHT CHECK OF UPPER (MAIN) DECK CARGO COMPARTMENT 1 YE  FIRE EXTINGUISHER BOTTLES.  262500-0502-1 220 LAVATORY FIRE EXTINGUISHING MEC GVI I: 400 FH ISB AMM 262500/2 ISB 26-057  GENERAL VISUAL INSPECTION IN-SITU OF THE  LAVATORY FIRE EXTINGUISHER AND DISCHARGE TUBES  262500-0502-2 200 LAVATORY FIRE EXTINGUISHING MEC GVI I: WEEKLY MRB ** AMM 262500/2 VISUAL INSPECTION OF LAVATORY FIRE EXTINGUISHING  BOTTLE FOR SIGNS OF DISCHARGE  262500-0504-1 200 LAVATORY FIRE EXTINGUISHING MEC RAR I: 2 C MRB ** AMM 262500/2 01. REMOVE BOTTLE FOR WEIGHT CHECK  02. INSPECT BOTTLE AND PIPES FOR SATISFACTORY CON-  DITION  03. CHECK DISCHARGE INDICATORS  04. INSPECT MOUNTING BRACKETS FOR DAMAGE AND SECURITY  OF ATTACHMENTS  05. REINSTALL BOTTLE  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FIRE PROTECTION REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 271100-0503-1 575 MECHANICAL CONTROL,AILERON MEC FUC I: 3 C MRB AMM 271000/6 675  CHECK CONTROL CABLE OF AILERON TRIM IN WING AREA  FOR CORRECT TENSION WITH TENSIOMETER IN ACCORDANCE  WITH THE RESP. AMM CABLE TENSION AND ADJUSTMENT  GRAPH.  ACCESS: 575AB  675AB  271100-0503-2 210 MECHANICAL CONTROL-LSA MEC OPC I: WEEKLY MRB ** AMM 271100/5 OPERATIONAL TEST OF LOW SPEED AILERON LOCK OUT SYSTEM  271116-0503-1 120 SPRING ROD-INTERCONNECTING MEC OPC I: 4 C MPD AMM 271100/6 210  CHECK COMPRESSION AND EXTENSION OF SPRING ROD:  (LOCATED BETWEEN PILOT/CO-PILOT CONTROL COLUMN IN  ZONE 120)  - SIMULATE PILOT OR CO-PILOT CONTROL SYSTEM JAMMING  BY INSERTING APPROPRIATE RIGGING PIN.  ACCESS: 132AZ  271117-0503-1 120 REGULATOR - CABLE TENSION MEC FUC I: 3 C MPD AMM 271000/6 AMM 272000/6 01. CHECK IN ACCORDANCE WITH THE RESPECTIVE AMM CABLE AMM 273000/6 TENSION ADJUSTMENT GRAPH THE FOLLOWING MECHANICAL AMM 274000/6 CONTROL CABLES IN ZONES 121/122 FOR CORRECT AMM 275000/6 TENSION: AMM 761100/5 - ALL SPEED AILERON, AILERON TRIM  - RUDDER CONTROL, RUDDER TRIM  - ELEVATOR CONTROL  - TRIMABLE HORIZONTAL STABILIZER CONTROL  - FLAP CONTROL  - THROTTLE CONTROL  NOTE: USE CABLE TENSIOMETER AND PLACE IT APPROX. ONE  (1) METER NEAR THE CABLE TENSION REGULATOR  02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLE  TENSION REGULATOR IS WITHIN LIMITS  03. 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 271117-0503-1 * * * * * C O N T I N U E * * * * *  SECURITY OF ATTACHMENT AND INSTALLATION  ACCESS: 121TF 121XF 132AZ  271122-0504-1 575 MECH.DIFF.DROOP&FEEL LH-RH MEC RAR I: NOTE MRB ** AMM 271122/4 675 ISB 05-0004  SAMPLING INSPECTION OF DIFFERENTIAL DROOP AND FEEL  MECHANISM ASSEMBLY IN ACCORDANCE WITH MANUFACTURERS  INSTRUCTIONS SAMPLE SIZE - ONE ITEM FROM EACH  OPERATORS FLEET  NOTE: INSPECTION TO BE CARRIED OUT BETWEEN  23000 FH AND 27000 FH  ACCESS: 131DZ 132DZ 575AB 575AT 575BB 575BT  575CB 575DB 575FB 575GB  131DZ 132DZ 675AB 675AT 675BB 675BT  675CB 675DB 675FB 675GB  271122-0505-1 575 MECH.DIFF.DROOP & FEEL MEC LUB I: 1 C MRB AMM 122227/0 675  CLEAN, INSPECT AND LUBRICATE DROOP INPUT MECHANISM  (AEROSOL SPRAY APPLICATION USING MINERAL OIL).  NOTE: AILERON TO BE UNDROOPED AND FULLY UP ON SIDE  TO BE LUBRICATED  ACCESS: 575AB  675AB  271122-0505-2 575 MECH.DIFF.DROOP & FEEL MEC LUB I: 2 C MPD AMM 122227/0 675  LUBRICATE TRIM SCREW JACK AND CHAIN OF AILERON  ACCESS: 575AB  675AB  271122-0505-3 121 MECH.DIFF.DROOP & FEEL MEC LUB I: 2 C MPD AMM 122227/0 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AND  RUDDER (BRUSH APPLICATION)  ACCESS: 132AZ  271122-0505-4 143 MECH.DIFF.DROOP & FEEL MEC LUB I: 2 C MPD AMM 122227/0 LUBRICATE CHAIN IN AILERON TRIM SYSTEM (BRUSH  APPLICATION)  ACCESS: 143BF  271141-0502-1 581 DETENT UNIT-FULL STROKE MEC DET I: 1 C MRB AMM 271100/0 681  DETAILED INSPECTION OF AILERON FULL STROKE  DETENT UNIT FOR CLEANLINESS, SECURITY OF ATTACHMENTS,  SATISFACTORY CONDITION AND IDLER (ROLLER) AND CAM FOR  WEAR.  ACCESS: 575FB 575GB 581CB  675FB 675GB 681CB  271141-0503-1 581 DETENT UNIT-FULL STROKE MEC FUC I: 6 C MRB ** AMM 271141/4 681 AMM 271141/6 CHECK BREAK OUT LOAD OF AILERON FULL STROKE  DETENT UNIT BY EITHER OF FOLLOWING METHODS:  A. WITH DETENT UNIT REMOVAL  01. REMOVE FULL STROKE DETENT UNIT  02. CHECK BREAK OUT LOAD (REFER TO OVERHAUL  MANUAL)  03. REINSTALL FULL STROKE DETENT UNIT  B. WITHOUT DETENT UNIT REMOVAL  01. CHECK BREAK OUT LOAD USING SPECIAL TOOL  98A 27308031  ACCESS: 575FB 575GB 581CB  675FB 675GB 681CB  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 271142-0503-1 581 REGULATOR CABLE TENSION-LSA MEC FUC I: 3 C MRB AMM 271000/6 681  01. CHECK IN ACCORDANCE WITH THE RESPECTIVE AMM CABLE  TENSION ADJUSTMENT GRAPH THE LOW SPEED AILERON  CONTROL CABLES FOR CORRECT TENSION  NOTE: USE CABLE TENSIOMETER AND PLACE IT APPROX.  ONE METER NEAR THE CABLE TENSION REGULATOR  02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLE  TENSION REGULATOR IS WITHIN LIMITS  03. CHECK REGULATOR FOR CLEANLINESS,WEAR,CORROSION,  SECURITY OF ATTACHMENT AND INSTALLATION  ACCESS: 581CB 581EB  681CB 681EB  271200-0503-1 210 AILERON TRIM-MECH.CONTROL MEC OPC I: 1 A MRB AMM 271200/5 OPERATIONAL TEST OF AILERON TRIM BY MEANS OF CONTROL  WHEEL AND FLIGHT CONTROLS POSITION INDICATOR  271216-0502-1 147 BRACKET - PULLEY MEC GVI I: 4400 FH ISB ISB 27-0107  148  GENERAL VISUAL INSPECTION OF MACHINED AILERON TRIM  CONTROL PULLEYS FOR HYDR. FLUID CONTAMINATION.  271216-0502-2 500 BRACKET - PULLEY MEC GVI I: 4400 FH ISB ISB 27-0107  600  GENERAL VISUAL INSPECTION OF MACHINED ALL SPEED  AILERON, AILERON TRIM, RAT, SPEED BRAKE AND LOW  SPEED AILERON CONTROL PULLEYS FOR HYDR. FLUID  CONTAMINATION  ACCESS: 571DB 575AB 581CB 581EB 591AB  671DB 675AB 681CB 681EB 691AB  271400-0503-1 210 SERVO CONTROLS MEC OPC I: 1 C MRB ** AMM 271400/5 OPERATIONAL TEST OF SERVO CONTROL JAMMING DETECTION  SYSTEM ( PITCH,ROLL,YAW )  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 271400-0504-1 500 LOW SPEED AILERON MEC RAR I: 9000 FC ISB ISB 27-0109  600  REMOVE AND REPLACE LOW SPEED AILERON FLEXIBLE  HYDRAULIC PRESSURE HOSES P/N:A2714201001000 AND  P/N: 660000040165RRK.  ACCESS: 591AT  691AT  271412-0502-1 575 SERVO CONTROLS - AILERON MEC DET I: 1 C SIL AMM 271412/6 675 SIL 27-087  DETAILED INSPECTION OF ALL SPEED  AILERON SERVO CONTROL BEARINGS FOR  EVIDENCE OF EXTRUSION OF THE SELF  LUBRICATION COATING AND FOR GENERAL  CONTION  ACCESS: 575CB  675CB  271412-0503-1 210 SERVO CONTR.-ALL SPEED AIL. MEC OPC I: 5 A MRB ** AMM 271400/5 OPERATIONAL TEST OF ALL SPEED AND LOW SPEED AILERON  SERVO CONTROLS WITH INDIVIDUAL HYDRAULIC SYSTEMS.  271412-0503-2 210 SERVO CONTROLS MEC FUC I: 1300 FH ISB ISB 27-0189  FUNCTIONAL TEST OF AILERON AND ELEVATOR SERVO  CONTROLS WITH EACH HYDRAULIC SYSTEM PRESSURIZED  IN TURN.  271414-0503-1 210 VALVE-PRIORITY MEC FUC I: 3 C MRB ** AMM 274200/5 AMM 275200/5 FUNCTIONAL TEST OF PRIORITY VALVES (GREEN, BLUE, AMM 278200/5 YELLOW).  271414-0504-1 147 VALVE-PRIORITY MEC RAR I: 10000 FC MPD AMM 271414/4 148 AMM 274216/4 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 HYDRAULIC  SYSTEMS (TOTAL 3 OFF).  271414-0504-2 147 VALVE-PRIORITY MEC RAR I: 10000 FC MPD AMM 271414/4 REPLACE PRIORITY VALVE IN GREEN HYDRAULIC SYSTEM. R 272100-0502-1 311 RUDDER MECHANICAL CONTROL MEC GVI SI: 2 C MRB ** AMM 272000/6 323 I: COVERED  GENERAL VISUAL INSPECTION OF DUPLEX LINKAGE FOR BY AMM  INTEGRITY, SECURITY OF ATTACHMENTS, SATISFACTORY 272000/  CONDITION, WEAR, CORROSION AND CLEANLINESS. 601  ACCESS: 312AR 313AL  325AL 325BL 325CL 325DL  272100-0504-1 325 RUDDER MECHANICAL CONTROL MEC RAR I: NOTE MRB ** AMM 272117/4 ISB 05-0004  SAMPLING INSPECTION OF DRIVE SHAFT ASSY AND BELLCRANK  IN ACCORDANCE WITH MANUFACTURERS INSTRUCTIONS.  SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́S  FLEET.  NOTE: INSPECTION TO BE CARRIED OUT BETWEEN  23000 FH AND 27000 FH  ACCESS: 312AR 325DL  272200-0503-1 210 RUDDER TRIM-MECH.CONTROL MEC OPC I: 1 A MRB AMM 272200/5 OPERATIONAL TEST OF RUDDER TRIM BY MEANS OF CONTROL  WHEEL AND FLIGHT CONTROLS POSITION INDICATOR  272200-0505-1 311 RUDDER TRIM-MECHANICAL CONTROL MEC LUB I: 2 C MPD AMM 122227/0 LUBRICATE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 272200-0505-1 * * * * * C O N T I N U E * * * * *  ACCESS: 312AR  272311-0503-1 311 ARTIFICIAL FEEL-RUDDER MEC FUC I: 6 C MRB AMM 272100/5 WITH THREE (3) HYDRAULIC SYSTEMS PRESSURIZED:  OPERATE RUDDER TO LEFT AND RIGHT FULL TRAVEL.  OPERATING FORCES MUST INCREASE WITH INCREASING  RUDDER PEDAL DEFLECTION. CHECK THAT OPERATING FORCES  AT 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 272118/4 AMM 272311/4 SAMPLING INSPECTION OF ISB 05-0004  - ARTIFICIAL FEEL AND TRIM UNIT  - MAIN SHAFT, INNER SHAFT AND BELLCRANK ASSY  IN ACCORDANCE WITH MANUFACTURERS INSTRUCTIONS.  SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́S FLEET.  NOTE: INSPECTION TO BE CARRIED OUT BETWEEN  23000FH AND 27000FH.  ACCESS: 312AR 325DL  272312-0503-1 210 VARIABLE LEVER ARM UNIT MEC FUC I: 950 FH MRB ** AMM 272300/5 FUNCTIONAL TEST OF RUDDER DEFLECTION VERSUS AIRSPEED  272312-0503-2 210 VARIABLE LEVER ARM MEC OPC I: 1 A ISB AMM 272300/5 ISB 27-0093  JAMMING DETECTION TEST OF VARIABLE LEVER ARM UNIT  272312-0504-1 311 VARIABLE LEVER ARM UNIT MEC RAR I: NOTE MRB ** AMM 272312/4 ISB 05-0004  SAMPLING INSPECTION OF VARIABLE LEVER ARM UNIT IN  ACCORDANCE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 BETWEEN  23000 FH AND 27000 FH  ACCESS: 312AR 325DL  272400-0503-1 210 HYDRAULIC ACTUATION MEC OPC I: 1300 FH CN CN F-2004-09 FAA AD FAA AD  OPERATIONAL TEST OF RUDDER SYSTEM USING EACH 2005-17-14  HYDRAULIC SYSTEM IN TURN AND CHECK FOR RUDDER ISB 27-0188  DESYNCHRONIZATION FROM THE GROUND.  272411-0502-1 320 SERVO CONTROL MEC DET I: 1 C SIL AMM 272411/6 SIL 27-087  DETAILED INSPECTION OF RUDDER SERVO CONTROL  BEARINGS FOR EVIDENCE OF EXTRUSION OF THE SELF  LUBRICATION COATING AND FOR GENERAL CONDITION  ACCESS: 325DL 326DL  272411-0503-1 210 SERVO CONTROL - RUDDER MEC OPC I: 1 A MRB ** AMM 271400/5 OPERATIONAL TEST OF RUDDER SERVO CONTROLS (WITH  INDIVIDUAL HYDRAULIC SYSTEM) BY MOVING RH RUDDER  PEDAL FULL FORWARD AND VISUALLY OBSERVE THAT RUDDER  MOVES TO RIGHT. CHECK THAT RUDDER TRAVEL IS CONFIRMED  ON THE FLIGHT CONTROL POSITION INDICATOR (FCPI).  RELEASE RH PEDAL. REPEAT ABOVE TEST BY MOVING LH  RUDDER PEDAL.  273100-0502-1 310 ELEVATOR MECHANICAL CONTROL MEC GVI I: 2 C MRB ** AMM 273000/6 334  344 VISUAL INSPECTION OF DUPLEX LINKAGE FOR  INTEGRITY,SECURITY OF ATTACHMENTS,SATISFACTORY  CONDITION,WEAR,CORROSION AND CLEANLINESS.  ACCESS: 312AR 313AL  334AB 334BB  344AB 344BB  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 273100-0503-1 210 ELEVATOR CHANNEL UNCOUPLING ERI OPC I: 2500 FH MRB ** AMM 273100/5 OPERATIONAL TEST OF ELEVATOR CHANNEL UNCOUPLING  COMPUTER  273100-0503-2 210 ELEVATOR CHANNEL UNCOUPLING ERI FUC I: 12000 FH MRB ** AMM 273100/5 FUNCTIONAL TEST OF ELEVATOR CHANNEL UNCOUPLING  (SYSTEM)  273100-0504-1 313 ELEVATOR MECHANICAL CONTROL MEC RAR I: 23000 FH MRB ** AMM 273121/4 TO ISB 05-0004  INSPECTION OF DRIVE SHAFT ASSY IN ACCORDANCE WITH 27000 FH  MANUFACTURERS INSTRUCTIONS.  NOTE: SAMPLE SIZE - ONE ITEM FROM EACH OPERATOR ́S  FLEET.  ACCESS: 313AL  273311-0503-1 210 ARTIFICIAL FEEL - ELEVATOR MEC OPC I: 1 C MRB AMM 273300/5 OPERATIONAL TEST OF PITCH ARTIFICIAL FEEL BY  COMPARING QUALITATIVELY OPERATING LOADS IN HIGH-SPEED  AND LOW-SPEED CONFIGURATIONS (WITH EACH INDIVIDUAL  HYDRAULIC SYSTEM)  NOTE: REFER TO REFERENCED AMM CHAPTER SEC.2  273311-0503-2 210 ARTIFICIAL FEEL - ELEVATOR MEC FUC I: 6 C MRB AMM 273300/5 FUNCTIONAL TEST OF PITCH ARTIFICIAL FEEL BY MEASURING  OPERATING LOADS IN HIGH-SPEED AND LOW-SPEED  CONFIGURATION  273311-0504-1 311 ARTIFICIAL FEEL UNIT MEC RAR I: NOTE MRB ** AMM 273311/4 ISB 05-0004  SAMPLING INSPECTION OF ARTIFICIAL FEEL UNIT IN  ACCORDANCE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 BETWEEN  23000 FH AND 27000 FH  ACCESS: 312AR 313AL  273313-0503-1 210 COMPUTER-ARTIFICIAL FEEL ELO OPC I: 3500 FH MRB ** AMM 272300/5 AMM 273300/5 OPERATIONAL TEST OF ARTIFICIAL FEEL "PITCH  FEEL"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 273411/6 344 SIL 27-087  DETAILED INSPECTION OF ELEVATOR SERVO CONTROL  BEARINGS FOR EVIDENCE OF EXTRUSION OF THE SELF  LUBRICATION COATING AND FOR CONDITION.  ACCESS: 334CB  344CB  273411-0503-1 210 SERVO CONTROL-ELEVATOR MEC OPC I: 5 A MRB ** AMM 271400/5 OPERATIONAL TEST OF SERVO CONTROLS WITH INDIVIDUAL  HYDRAULIC SYSTEMS  273600-0503-1 210 AIR DATA WARN.(STALL WARN.) ELO FUC I: 6000 FH MRB ** AMM 273600/5 FUNCTIONAL TEST OF STALL WARNING IN ACCORDANCE WITH  SLAT POSITION  273600-0503-2 210 AIR DATA WARN.(STALL WARN.) ELO OPC I: 1200 FH MRB ** AMM 273600/5 OPERATIONAL TEST OF MONITORING CIRCUIT AND STALL  WARNING  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 274100-0505-1 121 THS-MECHANICAL CONTROL MEC LUB I: 1 C MPD AMM 122227/0 310  LUBRICATE CHAINS IN TRIM SYSTEM (BRUSH APPLICATION).  ACCESS: 132AZ  312AR  274211-0502-1 312 ACTUATOR GEARBOX - THS MEC GVI I: 1 C MRB AMM 274211/6 CHECK GEARBOX MAGNETIC DRAIN PLUG FOR EVIDENCE  OF METAL PARTICLES  ACCESS: 312AR R 274211-0502-2 311 ACTUATOR - THS MEC FUC T: NOTE AD AMM 274211/6 312 I: 2500 FH MRB AD 2009-0111  FUNCTIONAL CHECK OF PHASING BETWEEN THSA MOTORS SB SB  PHASING FOLLOWED BY, CHECK GEARBOX MAGNETIC DRAIN SB-A300-27-0 PLUG FOR EVIDENCE OF METAL PARTICLES  NOTE: THRESHOLD IS 4000 FH AFTER THE LAST THSA  OVERHAUL OR WITHIN 250 FH AFTER THE EFFECTIVE  DATE OF THE AD WHICHEVER OCCURS LATER.  ACCESS: 312AR  274211-0503-1 210 ACTUATOR - THS MEC OPC I: 2 C MRB ** AMM 274200/5 CONTROL VALVE JAMMING DETECTION TEST TO CHECK  OPERATION OF JAMMING DETECTION CIRCUITS  ACCESS: 312AR  274211-0503-2 210 ACTUATOR - THS MEC OPC I: 1 C MRB AMM 274100/5 CHECK TRAVEL RANGE OF THS ACTUATOR IN ACCORDANCE  WITH TRIM WHEEL POSITION POINTER AND INDEX ON FLIGHT  CONTROL POSITION INDICATOR (WITH INDIVIDUAL HYDRAULIC  SYSTEM).  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 274211-0503-3 210 ACTUATOR - THS MEC OPC I: 1000 FH MRB ** AMM 274211/6 CN  CONTROL VALVE JAMMING DETECTION CHECK TO DETECT 1981-085-036 POSSIBLE HIDDEN JAMMED CONTROL VALVE FAA AD 85-09 ISB 27-0132  ACCESS: 312AR  274211-0503-4 210 ACTUATOR - THS MEC OPC I: 550 FH MRB ** AMM 274211/6 CN  CONTROL VALVE JAMMING DETECTION CHECK TO DETECT 1981-085-036 POSSIBLE HIDDEN JAMMED CONTROL VALVE FAA AD 85-09 ISB 27-0132  274211-0504-1 310 ACTUATOR - THS MEC RAR I: 12500 FH MRB ** AMM 274211/4 REMOVE THS ACTUATOR FOR OVERHAUL  ACCESS: 312AR  274211-0504-2 310 ACTUATOR - THS MEC RAR I: 7500 FH MRB ** AMM 274211/4 CN  REMOVE THS ACTUATOR FOR OVERHAUL 1981-085-036 FAA AD 85-09 ACCESS: 312AR  274211-0505-1 312 ACTUATOR - THS MEC RPL I: 5 A MRB AMM 121327/0 CHECK GEARBOX OIL LEVEL AS FOLLOWS:  01. REMOVE OIL LEVEL AND FILLER PLUGS  02. REPLENISH GEARBOX OIL AS NECESSARY UNTIL OIL  OVERFLOWS FROM THE LEVEL PLUG  03. 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 274211-0505-1 * * * * * C O N T I N U E * * * * *  RECOMMENDED TORQUE VALUES  04. SAFETY PLUGS WITH LOCKWIRE  ACCESS: 312AR  274211-0505-2 312 ACTUATOR BALL NUT - THS MEC LUB I: 2 A MRB AMM 121327/0 LUBRICATE BALL NUT AND CHECK THS HYDROMECHANICAL  ACTUATOR UNIT FOR FREEDOM OF OIL AND HYDRAULIC LEAKS.  ACCESS: 312AR  274211-0505-3 312 ACTUATOR GEARBOX - THS MEC RPL I: 1 C MRB AMM 121327/0 AMM 274211/6 CHANGE OIL OF THS GEARBOX AS FOLLOWS:  01. REMOVE OIL LEVEL AND FILLER PLUG  02. REMOVE MAGNETIC DRAIN PLUG AND CHECK THE AMOUNT  OF METAL PARTICLES AND DRAIN OIL  03. INSTALL DRAIN PLUG WITH NEW O-RING  04. FILL GEARBOX WITH OIL MIL-L-7808/G/2 (MAT.03-003)  UNTIL OIL OVERFLOWS THE LEVEL PORT  05. REINSTALL LEVEL AND FILLER PLUGS WITH NEW  O-RINGS AND TIGHTEN TO RECOMMENDED TORQUE VALUES  06. SAFETY PLUGS WITH LOCKWIRE  ACCESS: 312AR  274211-0505-4 312 ACTUATOR GEARBOX - THS MEC RPL I: 2 C MRB AMM 121327/0 AMM 274211/6 CHANGE OIL OF THS GEARBOX AS FOLLOWS:  01. REMOVE OIL LEVEL AND FILLER PLUG  02. REMOVE MAGNETIC DRAIN PLUG AND CHECK THE AMOUNT  OF METAL PARTICLES AND DRAIN OIL  03. INSTALL DRAIN PLUG WITH NEW O-RING  04. FILL GEARBOX WITH OIL MIL-L-7808/G/2 (MAT.03-003)  UNTIL OIL OVERFLOWS THE LEVEL PORT  05. REINSTALL LEVEL AND FILLER PLUGS WITH NEW  O-RINGS AND TIGHTEN TO RECOMMENDED TORQUE VALUES  06. 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 274211-0505-4 * * * * * C O N T I N U E * * * * *  ACCESS: 312AR N 274211-0505-5 310 ACTUATOR THS MEC DET T: 2500 FH EASA AD EASA AD  A. EFFECT ISB 2010-0019  DETAILED INSPECTION OF THSA UPPER ATTACHMENTS DATE OF ISB 27-0203  AND BALL SCREW: THE AD  01. CHECK FOR PRESENCE OF METALLIC PARTICLES. I: 2500 FH  02. CHECK FOR CRACKS, SCRATCHES OR MATERIAL MISSING.  ACCESS: 312AR  274300-0503-1 210 CONTROL SURFACES POS.INDIC. MEC OPC I: 1 A MRB AMM 274300/5 OPERATIONAL TEST OF VISUAL AND AURAL STAB.TRIM  WARNINGS (STAB.TRIM OUT OF TAKE OFF RANGE)  275100-0503-1 145 MECHANICAL CONTROL MEC FUC I: 3 C MRB AMM 275000/6 AMM 278000/6 CHECK 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 TENSION  ADJUSTMENT GRAPH.  ACCESS: 241AQ 241CZ  275121-0504-1 147 SHOCK ABSORBER FLAP MEC RAR I: 12000 FC MRB AMM 275121/4 148 CMM 270901  REMOVE FLAP SHOCK ABSORBER FOR WORKSHOP CHECK  (COMPRISING OIL LEVEL CHECK AND FUNCTIONAL TEST).  ACCESS: 147SZ  148SZ  275121-0505-1 147 SHOCK ABSORBER FLAP MEC RPL I: 3 C MRB AMM 121327/0 148  CHECK 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 LEVEL  03. 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 LEVEL  PORT  04. REPLACE SEALS,INSTALL PLUGS AND FULLY TIGHTEN OIL  LEVEL AND VENT PLUG  ACCESS: 147SZ  148SZ  275122-0505-1 147 TORQUE LIMITER FLAP MEC RPL I: 1 C MRB AMM 121327/0 148  CHECK TORQUE LIMITER FOR CORRECT OIL LEVEL AS  FOLLOWS:  01. REMOVE OIL LEVEL PLUG  02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILL  FLUID OVERFLOWS THROUGH OIL LEVEL PORT  03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TO  RECOMMENDED VALUE  ACCESS: 147UZ  148UZ  275123-0504-1 577 TEE GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275123/4 677 SB 27-0101  REMOVE TEE GEARBOX FOR OVERHAUL OF HALO TYPE  UNIVERSAL JOINT POSITION 4  275123-0504-2 577 TEE GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275123/4 677 SB 27-0101  REMOVE TEE-GEARBOX FOR OVERHAUL OF HOOKES-TYPE  UNIVERSAL JOINT POSITION 4.  275123-0505-1 500 GEARBOXES - FLAP MEC RPL I: 1 C MRB AMM 121327/0 600  CHECK 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 DROOP  AS FOLLOWS:  01. REMOVE OIL LEVEL PLUG  02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILL  FLUID OVERFLOWS THROUGH OIL LEVEL PORT  03. REPLACE PLUG SEAL.INSTALL PLUG AND TORQUE  TO RECOMMENDED VALUE  ACCESS: 575DB 577CT 577ET 577FT  675DB 677CT 677ET 677FT  275124-0504-1 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275124/4 148 SB 27-0101  REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FOR  OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 6  275124-0504-2 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 8000 LG MRB AMM 275124/4 148 SB 27-0101  REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FOR  OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 6  275124-0504-3 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 16000 LG MRB AMM 275124/4 148 SB 27-0101  REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FOR SB 27-0159  OVERHAUL OF HOOKE-TYPE UNIVERSAL JOINT POSITION 6  275124-0504-4 147 SIMPLEX BEVEL GEARBOX-FLAP MEC RAR I: 8000 LG MRB AMM 275124/4 148 CN  REMOVE SIMPLEX OR SWINGING BEVEL GEAR BOX FOR 1983-147-055 OVERHAUL OF HOOKE-TYPE UNIVERSAL JOINT POSITION 6 FAA AD 84-06 SB 27-0101  SB 27-0159  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 275000/6 600  CHECK INTEGRITY OF PRIMARY AND SECONDARY LOAD  PATHS IN SCREWJACK,DUPLEX AND TEE GEARBOXES,SCREWJACK  SHAFT AND SECONDARY TIE ROD.  ACCESS: 577AB 577BB 577ET  677AB 677BB 677ET  275125-0504-1 500 SCREWJACK 1 MEC CHK I: 6500 FC MRB ** AMM 275000/6 600  CHECK INTEGRITY OF PRIMARY LOAD PATHS AND SCREWJACK  SHAFT. REMOVE DUPLEX GEARBOX AND CHECK INTEGRITY  OF SECONDARY LOAD PATH IN TEE GEARBOX, DUPLEX SHAFT  AND TIE ROD. MANUALLY CHECK PRIMARY AND SECONDARY  DRIVES OF DUPLEX GEARBOX BEFORE REINSTALLATION.  ACCESS: 577AB 577BB 577ET  677AB 677BB 677ET  275126-0502-1 500 SCREWJACK 2 TO 6 MEC CHK I: 6500 FC MRB ** AMM 275000/6 600  CHECK INTEGRITY OF PRIMARY AND SECONDARY LOAD  PATHS IN SREWJACK,DOWNDRIVE GEARBOX AND DUPLEX SHAFT  AND SCREWJACK SECONDARY TIE ROD  ACCESS: 572DB 572FB 572HB 572JB 581CB 581DB  581EB 581FB 581GB 581HB 581JB 581KB  672DB 672FB 672HB 672JB 681CB 681DB  681EB 681FB 681GB 681HB 681JB 681KB  275126-0502-2 500 SCREWJACK 1 TO 6 MEC CHK T: 10000 FC MRB AMM 275100/6 600 NOTE SIL 27-076  CHECK BACKLASH BETWEEN FLAP SCREWJACK BALL NUT AND I: 2500 FC  SCREW 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 275126-0502-2 * * * * * C O N T I N U E * * * * *  NOTE: POSITION 1 10000 CY  POSITIONS 2 TO 6 12000 CY  275126-0502-3 500 SCREW JACK 4,5 AND 6 MEC FUC I: ISB CN CN  600 27-0172 FAA AD 1984-066-061 CHECK BACKLASH OF FLAP SCREWJACK NO-BACK DEVICE NOTE CN 2001-184( FAA AD 87-21 NOTE: DETAILS OF INSPECTION PROGRAM SEE LUCAS FAA AD 91-05 SB 1058-27-608 0R AI.ISB 27-172. ISB 27-0172  FOR SREWJACKS WITH BACKLASH LESS THAN  0,331 MM (0,013 INCH) INSPECT EACH  3600 LDGS  275126-0502-4 500 SCREW JACK 4,5 AND 6 MEC FUC I: 12000 LG MPD AMM 275100/6 600 NOTE  CHECK BACKLASH OF FLAP SCREWJACK NO-BACK  DEVICE  NOTE: -INTERVAL OF 12000 LG TO BE CONFIRMED AFTER  SAMPLING INSPECTION AT 6500 LG.  -ONE A/C OF EACH OPERATOR ́S FLEET  275126-0505-1 500 SCREWJACK 1 TO 6 MEC LUB I: 2 A MRB AMM 122227/0 600 SIL 27-063  LUBRICATION OF FOLLOWING ITEMS:  01. BALL NUTS OF SCREW JACKS 1 TO 6  02. CARRIAGE ROLLERS OF FLAP TRACK 1 TO 6  03. RUBBING PADS (CARRIAGE SIDE LOCATION) TRACK NO.1  ONLY  (FLAPS EXTENDED)  275126-0505-2 500 SCREWJACK 1 TO 6 MEC RPL I: 1 C MRB AMM 121327/0 600 SIL 27-081  CHECK FLAP SCREW-JACKS NO.1 TO 6 FOR CORRECT  OIL LEVEL  NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY OF  TASK 283100-0502-1  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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.5  275126-0505-3 500 SCREWJACK 1 TO 6 MEC RPL I: 5 A MRB AMM 121327/0 600 SIL 27-081  CHECK FLAP SCREWJACKS NO.1 TO 6 FOR CORRECT  OIL LEVEL  ACCESS: MOVABLE FLAP-TRACK FAIRINGS NO.1 TO 6,  FIXED FAIRING NO.5  275134-0505-1 500 GEARBOX - DOWNDRIVE,FLAP MEC RPL I: 1 C MRB AMM 121327/0 600  CHECK INNER/CENTER AND OUTER FLAP GEARBOX -  DOWN DRIVES FOR CORRECT OIL LEVEL:  01. EXTEND FLAPS AND LOCK FLAP CONTROL LEVER USING  TOOL P/N 98A27901022000  02. REMOVE OIL LEVEL PLUG  03. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILL  FLUID OVERFLOWS THROUGH OIL LEVEL PLUG  04. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TO  RECOMMENDED VALUE  275136-0504-1 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 5/6 AND  15/16 FOR OVERHAUL OF HALO-TYPES UNIVERSAL JOINT  POSITION 5 AND 15  275136-0504-2 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 8000 FC MRB AMM 275136/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 5/6 AND 15/16  FOR OVERHAUL OF HALO-TYPES UNIVERSAL JOINT POSITION  5 AND 15.  275136-0504-3 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 5/6 AND SB 27-0159  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  5 AND 15  275136-0504-4 500 SHAFT TRANSMISSION - FLAP MEC RAR I: 8000 FC MRB AMM 275136/4 600 CN  REMOVE TRANSMISSION SHAFT POSITION 5/6 AND 1983-147-055 15/16 FOR OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINTS FAA AD 84-06 5 AND 15 SB 27-0101  SB 27-0159  275136-0504-5 575 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4 675 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 13/14 FOR  OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 13  275136-0504-6 575 SHAFT TRANSMISSION - FLAP MEC RAR I: 16000 FC MRB AMM 275136/4 675 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 13/14 FOR SB 27-0159  OVERHAUL OF HOOKES TYPE UNIVERSAL JOINT POSITION 13  275137-0504-1 581 COUPLING BOX - FLAP MEC RAR I: 16000 FC MRB AMM 275137/4 681 SB 27-0101  REMOVE COUPLING BOX FOR OVERHAUL OF HALO-TYPE  UNIVERSAL JOINT POSITION 14  ACCESS: 581AB  681AB  275137-0504-2 581 COUPLING BOX - FLAP MEC RAR I: 8000 FC MRB AMM 275137/4 681 SB 27-0101  REMOVE COUPLING BOX FOR OVERHAUL OF HALO TYPE  UNIVERSAL JOINT POSITION 14  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 275137-0504-2 * * * * * C O N T I N U E * * * * *  ACCESS: 581AB 581CB  681AB 681CB  275137-0504-3 581 COUPLING BOX MEC RAR I: 16000 FC MRB AMM 275137/4 681 SB 27-0101  REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPE SB 27-0159  UNIVERSAL JOINT POSITION 14.  ACCESS: 581AB  681AB  275137-0504-4 581 COUPLING BOX MEC RAR I: 8000 FC MRB AMM 275137/4 681 CN  REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPE 1983-147-055 UNIVERSAL JOINT POSITION 14. FAA AD 84-06 SB 27-0101  ACCESS: 581AB SB 27-0159  681AB  275138-0502-1 571 BEARING-STEADY MEC DET I: 350 FH ISB ISB 27-0044  671  DETAILED INSPECTION OF FLAP TRANSMISSION NO.1  BEARING AND SUPPORT BRACKETS FOR CRACKS.  275138-0502-2 571 BEARING-STEADY MEC DET I: 2000 FH ISB ISB 27-0044  671  DETAILED INSPECTION OF FLAP TRANSMISSION NO.1  BEARING AND SUPPORT BRACKETS FOR CRACKS.  275153-0502-1 500 CARRIAGE-FLAP TRACK 1 TO 6 MEC DET I: 4 C MRB AMM 275100/6 600 AMM 275153/6 CHECK 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 WEAR  PARTICULARY AT SELECTED POSITIONS  02. CHECK WEAR OF RUBBING PLATES (TRACK 1)  03. DETAILED INSPECTION OF INNER FLAP  HINGE FOR CONDITION AND SECURITY (TRACK 1)  275154-0502-1 500 FRONT CARRIAGE - TRACK 2 MEC CHK I: 9000 FH MRB AMM 275100/6 600  CHECK CLEARANCE BETWEEN MAIN ROLLERS AND FLAP  TRACK 2 AT SELECTED POSITION  (LEAD A/C PER OPERATOR ONLY)  275211-0503-1 147 CONTROL UNIT-FLAP ERI OPC I: 1 C MRB AMM 275400/5 CHECK JAMMING DETECTION ELECTRICAL CIRCUIT FOR  CORRECT OPERATION  ACCESS: 147SZ 148SZ  275211-0504-1 147 CONTROL UNIT-FLAP ERI RAR I: 12000 FC MRB AMM 275211/4 REMOVE CONTROL UNIT FLAP FOR OVERHAUL  ACCESS: 148SZ  275211-0505-1 147 CONTROL UNIT-FLAP ERI RPL I: 1 C MRB AMM 121327/0 CHECK CONTROL UNIT - FLAP FOR CORRECT OIL LEVEL:  01. REMOVE OIL LEVEL FILLER PLUG  02. FILL UP WITH OIL MIL-L-7808/G/2 TILL OIL OVER-  FLOWS THROUGH OIL LEVEL PORT  03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TO  RECOMMENDED VALUE  ACCESS: 148SZ  275400-0503-1 210 FLAP ASYMMETRY MEC OPC I: 1 A MRB ** AMM 275400/5 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 275400/5 OPERATIONAL TEST OF PRESSURE-OFF BRAKE  275421-0505-1 570 SCREWJACK NO.1 MEC LUB I: 5 A MPD AMM 122227/0 670  LUBRICATION OF INNER FLAP UPLOCK ROLLER  NOTE: FLAPS TO BE EXTENDED  275512-0502-1 147 FLAP INSTRUMENTATION UNIT ELO GVI I: 3 A MPD AMM 275512/6 GENERAL VISUAL INSPECTION OF ELECTRICAL CONNECTORS AT  FLAP INSTRUMENTATION UNIT FOR SATISFACTORY CONDITION  AND DETERIORATION BY FLUID.  ACCESS: 148SZ  276100-0503-1 575 SPOILER & AIRBRAKE CABLES MEC FUC I: 3 C MRB AMM 276000/6 675  CHECK CONTROL CABLES OF SPOILER AND AIRBRAKES  FOR CORRECT TENSION WITH TENSIOMETER IN ACCORDANCE  WITH AMM CABLE TENSION ADJUSTMENT GRAPH.  ACCESS: 575AB 575FB  675AB 675FB  276100-0503-2 210 ELECTRICAL & MECH.CONTROL ELO OPC I: WEEKLY MRB ** AMM 276100/5 OPERATIONAL TEST OF GROUND SPOILER ELECTRICAL CIRCUIT  (ELECTRICAL AND MECHANICAL CONTROL AIRBRAKES AND  SPOILERS)  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 276114-0503-1 147 REGULATOR-CABLE TENSION MEC FUC I: 3 C MRB AMM 276000/5 01. CHECK (IN ACCORDANCE WITH THE RESPECTIVE AMM  CABLE TENSION ADJUSTMENT GRAPH) SPEEDBRAKE AND  SPOILER CONTROL CABLES FOR CORRECT TENSION  NOTE: USE CABLE TENSIOMETER AND PLACE IT APPROX.  ONE METER NEAR THE CABLE TENSION REGULATOR  02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLE  TENSION REGULATOR IS WITHIN LIMITS  03. CHECK REGULATOR FOR CLEANLINESS,WEAR,CORROSION,  SECURITY OF ATTACHMENT AND INSTALLATION  ACCESS: 147DZ 148DZ  276122-0503-1 581 DETENT-SPOILER & OUT.AIRBR. MEC FUC I: 6 C MRB AMM 276122/6 681 AMM 276129/6 CHECK DETENT SPRING CHARACTERISTICS AND ROLLER AMM 276132/6 -CAM DISCONNECT FORCE (SPOILERS,INNER AND OUTER  AIRBRAKES)  ACCESS: 572CB 572GB 572LB 581EB 581FB 581GB  581HB 581JB  672CB 672GB 672LB 681EB 681FB 681GB  681HB 681JB  276161-0505-1 572 MICROSWITCH INNER SPEEDBR. INP LUB I: 1 C MPD AMM 122227/0 672  LUBRICATE CONTROL LINKAGE/MICROSWITCHES OF  INNER SPEEDBRAKES  ACCESS: 572GB 572LB  672GB 672LB  278100-0503-1 210 SLAT RETRACTION INTERLOCK MEC OPC I: 1 A MRB ** AMM 278100/5 OPERATIONAL TEST OF SLAT RETRACTION INTERLOCK  (MECHANICAL CONTROL)  278112-0504-1 144 SHOCK ABSORBER SLAT MEC FUC I: 12000 FC MRB AMM 278112/4 CMM 270901  CHECK 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  278112-0505-1 144 SHOCK ABSORBER SLAT MEC RPL I: 3 C MRB AMM 121327/0 CHECK OIL LEVEL OF SHOCK ABSORBER:  01. ALIGN OIL LEVEL OF SHOCK ABSORBER HORIZONTALLY  02. REMOVE OIL LEVEL PLUG AND CHECK OIL LEVEL  03. 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 LEVEL  PORT  04. REPLACE SEALS,INSTALL PLUGS AND FULLY TIGHTEN OIL  LEVEL AND VENT PLUG  ACCESS: 147GZ  278113-0505-1 143 TEE GEARBOX-SLAT MEC RPL I: 1 C MRB AMM 121327/0 CHECK FOLLOWING ITEMS FOR CORRECT OIL LEVEL  - TEE GEARBOX - SLAT  - TORQUE LIMITER - SLAT (INCLUDING ZONE 144)  01. REMOVE OIL LEVEL PLUG  02.FILL UP WITH HYDR.FLUID MIL-H-5606/C/1 TILL  FLUID OVERFLOWS THROUGH OIL LEVEL PORT  03. REPLACE PLUG SEAL,INSTALL PLUG AND TORQUE  TO RECOMMENDED VALUE  ACCESS: 147GZ  278115-0505-1 512 GEARBOX BEVEL - SLAT MEC RPL I: 1 C MPD AMM 121327/0 612  CHECK FOR CORRECT OIL LEVEL:  01. REMOVE OIL LEVEL PLUG  02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILL  FLUID OVERFLOWS THROUGH OIL LEVEL PORT  03. 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278115-0505-1 * * * * * C O N T I N U E * * * * *  RECOMMENDED VALUE  ACCESS: 512BB  612BB  278116-0505-1 512 GEARBOX STEPBACK - SLAT MEC RPL I: 1 C MRB AMM 121327/0 612  CHECK GEARBOX FOR CORRECT OIL LEVEL:  01. REMOVE THE TWO OIL LEVEL/FILLER PLUGS (ONE PLUG  FOR EACH GEARBOX)  02. FILL UP WITH MATERIAL NO.02-001 TILL FLUID OVER-  FLOWS THROUGH OIL LEVEL/FILLER PORT  03. REPLACE PLUG SEALS, INSTALL PLUGS AND TIGHTEN TO  RECOMMENDED TORQUE VALUES  ACCESS: 512JB 512KB  612JB 612KB  278117-0504-1 523 STEADY BEARING - SLAT MEC RAR I: 12000 FC MRB AMM 278117/4 623 SB 27-0101  REMOVE STEADY BEARING FOR OVERHAUL OF HALO-TYPE SB 27-0158  UNIVERSAL JOINTS POSITION 20 AND 21.  ACCESS: 512KB 512LB 523AB 523BB  612KB 612LB 623AB 623BB  278117-0504-2 523 STEADY BEARING - SLAT MEC RAR I: 3500 FC MRB AMM 278117/4 623 CN  REMOVE STEADY BEARING FOR OVERHAUL OF HAL0-TYPE 1983-148-056 UNIVERSAL JOINT POSITION 20 AND 21. FAA AD 84-06 SB 27-0101  ACCESS: 512KB 512LB 523AB 523BB SB 27-0158  612KB 612LB 623AB 623BB  278117-0504-3 523 STEADY BEARING - SLAT MEC RAR I: 12000 FC MRB AMM 278117/4 623 SB 27-0101  REMOVE STEADY BEARING FOR OVERHAUL OF HOOKES-TYPE  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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.  ACCESS: 512KB 512LB 523AB 523BB  612KB 612LB 623AB 623BB  278117-0504-4 523 STEADY BEARING - SLAT MEC RAR I: 8000 FC MRB AMM 278117/4 623 SB 27-0101  REMOVE STEADY BEARING FOR OVERHAUL OF HOOKES  TYPE UNIVERSAL JOINTS POSITION 20 AND 21  ACCESS: 512KB 512LB 523AB 523BB  612KB 612LB 623AB 623BB  278118-0504-1 512 COUPLING BOX - SLAT MEC RAR I: 16000 FC MRB AMM 278118/4 612 SB 27-0101  REMOVE COUPLING BOX FOR OVERHAUL OF HALO-TYPE SB 27-0158  UNIVERSAL JOINT POSITION 8  ACCESS: 147GZ 512BB  148GZ 612BB  278118-0504-2 512 COUPLING BOX - SLAT MEC RAR I: 5000 FC MRB AMM 278118/4 612 CN  REMOVE COUPLING BOX FOR OVERHAUL OF HALO-TYPE 1983-148-056 UNIVERSAL JOINT POSITION 8. FAA AD 84-06 SB 27-0101  ACCESS: 147GZ 512BB SB 27-0158  148GZ 612BB  278118-0504-3 512 COUPLING BOX - SLAT MEC RAR I: 16000 FC MRB AMM 278118/4 612 SB 27-0101  REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPE  UNIVERSAL JOINT POSITION 8.  ACCESS: 147GZ 512BB  148GZ 612BB  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278118-0504-4 512 COUPLING BOX - SLAT MEC RAR I: 8000 FC MRB AMM 278118/4 612 CN  REMOVE COUPLING BOX FOR OVERHAUL OF HOOKES-TYPE 1983-148-056 UNIVERSAL JOINT POSITION 8. FAA AD 84-06 SB 27-0101  ACCESS: 147GZ 512BB  148GZ 612BB  278119-0504-1 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 12000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 9/10 FOR SB 27-0158  OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 9  ACCESS: 512AB 512BB  612AB 612BB  278119-0504-2 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 3500 FC MRB AMM 278119/4 600 CN  REMOVE TRANSMISSION SHAFT POSITION 9/10 FOR 1983-148-056 OVERHAUL OF HALO-TYPE UNIVERSAL JOINT POSITION 9 FAA AD 84-06 SB 27-0101  ACCESS: 512AB 512BB SB 27-0158  612AB 612BB  278119-0504-3 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 12000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 9/10 FOR  OVERHAUL OF HOOKES TYPE UNIVERSAL JOINT POSITION 9  ACCESS: 512AB 512BB  612AB 612BB  278119-0504-4 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4 600 CN  REMOVE TRANSMISSION SHAFT POSITION 9/10 FOR 1983-148-056 OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 9 FAA AD 84-06 SB 27-0101  ACCESS: 512AB 512BB  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278119-0504-4 * * * * * C O N T I N U E * * * * *  612AB 612BB  278119-0504-5 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFTS POSITION 9/10 AND SB 27-0158  21/22 FOR OVERHAUL OF HALO-TYPE UNIVERSAL JOINTS  POSITIONS 9 AND 22  ACCESS: 523CB 523EB  623CB 623EB  278119-0504-6 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFTS POSITION 9/10 AND SB 27-0158  21/22 FOR OVERHAUL OF HALO-TYPE UNIVERSAL JOINTS  POSITIONS 9 AND 22  ACCESS: 523CB 523EB  623CB 623EB  278119-0504-7 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFTS POSITION 21/22 FOR  OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 22.  ACCESS: 523CB 523EB  623CB 623EB  278119-0504-8 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFTS POSITION 21/22 FOR  OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 22.  ACCESS: 523CB 523EB  623CB 623EB  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278120-0504-1 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 11/12 AND SB 27-0158  21/22 FOR OVERHAUL OF HALO TYPE UNIVERSAL JOINTS  POSITION 12 AND 22  ACCESS: 523CB 523EB  623CB 623EB  278120-0504-2 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFT POSITION 11/12 AND SB 27-0158  21/22 FOR OVERHAUL OF HALO TYPE UNIVERSAL JOINTS  POSITION 12 AND 22  ACCESS: 523CB 523EB  623CB 623EB  278120-0504-3 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 16000 FC MRB AMM 278119/4 600 SB 27-0101  REMOVE TRANSMISSION SHAFTS POSITION 11/12 FOR  OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 12.  ACCESS: 512BB 523CB 523EB  612BB 623CB 623EB  278120-0504-4 500 SHAFT TRANSMISSION - SLAT MEC RAR I: 8000 FC MRB AMM 278119/4 600 CN 1983-148- REMOVE TRANSMISSION SHAFTS POSITION 11/12 FOR FAA AD 84-06 OVERHAUL OF HOOKES-TYPE UNIVERSAL JOINT POSITION 12. SB 27-0101  ACCESS: 512BB 523CB 523EB  612BB 623CB 623EB  278121-0504-1 143 STEADY BEARING - SLAT MEC RAR I: 16000 FC MRB AMM 278121/4 SB 27-0101  REMOVE STEADY BEARING FOR OVERHAUL OF HAL0-TYPE SB 27-0158  UNIVERSAL JOINT POSITION 2.  ACCESS: 147GZ 148GZ  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278121-0504-2 143 STEADY BEARING - SLAT MEC RAR I: 8000 FC MRB AMM 278121/4 SB 27-0101  REMOVE STEADY BEARING FOR OVERHAUL OF HAL0-TYPE SB 27-0158  UNIVERSAL JOINT POSITION 2.  ACCESS: 147GZ 148GZ  278121-0504-3 143 STEADY BEARING - SLAT MEC RAR I: 16000 FC MRB AMM 278121/4 SB 27-0101  REMOVE STEADY BEARING FOR OVERHAUL OF HOOKES-TYPE  UNIVERSAL JOINT POSITION 2.  ACCESS: 147GZ 148GZ  278121-0504-4 143 STEADY BEARING - SLAT MEC RAR I: 8000 FC MRB AMM 278121/4 SB 27-0101  REMOVE STEADY BEARING FOR OVERHAUL OF HOOKES-TYPE  UNIVERSAL JOINT POSITION 2.  ACCESS: 147GZ 148GZ  278124-0502-1 500 SCREW JACKS - SLAT MEC DET T: 12000 FC MRB AMM 278100/6 600 I: 2500 FC  CHECK PLAY OF JACK SCREW (BALL IN SCREW NUT)  AND PERFORM DETAILED INSPECTION OF MOUNTING  TRUNNIONS FOR CONDITION AND SECURITY,JACK 1 TO 6  278124-0505-1 500 SCREW JACKS - SLAT MEC RPL I: 1 C MPD AMM 121327/0 600 SIL 27-081  CHECK SLAT SCREW JACK 1 TO 6 FOR CORRECT OIL LEVEL:  ACCESS: 512CB 512GB 523DB 523KB 524DB 524JB  612CB 612GB 623DB 623KB 624DB 624JB  278124-0505-2 500 SCREW JACKS - SLAT MEC LUB I: 3 A MRB AMM 122227/0 600  LUBRICATION OF SLAT SCREWJACKS BALL NUTS (SCREWJACK  NO.1 TO 6)  ACCESS: 512CB 512GB 523DB 523KB 524DB 524JB  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  278124-0505-3 500 SCREW JACKS - SLAT MEC RPL I: 5 A MPD AMM 121327/0 600 SIL 27-081  CHECK SLAT SCREW JACK 1 TO 6 FOR CORRECT OILLEVEL.  ACCESS: 512CB 512GB 523DB 523KB 524DB 524JB  612CB 612GB 623DB 623KB 624DB 624JB  278141-0502-1 500 SEALING SHUTTERS-SLAT TRACK MEC DET I: 1 C MPD SIL 27-077  600  DETAILED INSPECTION AT TRACK POSITIONS 4 TO  11, OF SHUTTER MECHANISM CAM BLOCKS AND VISIBLE  LENGTH OF FORWARD AND AFT DRESSING ANGLES FOR WEAR  AND/OR DAMAGE  278147-0504-1 524 FRICTION BRAKE - SLAT MEC RAR I: 12000 FC MRB AMM 278147/4 624  REMOVE SLAT FRICTION BRAKE FOR OVERHAUL  ACCESS: 524KB  624KB  278147-0505-1 524 FRICTION BRAKE - SLAT MEC RPL I: 1 C MRB AMM 121327/0 624  CHECK OIL LEVEL OF SLAT FRICTION BRAKE:  01. REMOVE FILLER PLUG  02. FILL UP WITH MATERIAL NO.03-004(REFER TO MM 20-31  -00/12)TILL OIL OVERFLOWS  03. DRAW OFF 25 C.C. OF MATERIAL NO.03-004 IN ORDER  TO MAINTAIN A VOLUME OF AIR EQUAL TO 25 C.C. IN  THE FRICTION BRAKE  04. REPLACE PLUG SEAL,INSTALL PLUG AND TORQUE TO  RECOMMENDED VALUE  ACCESS: 524KB  624KB  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278149-0504-1 513 MOVABLE VANE - KRUEGER FLAP MEC RAR I: 8 C MPD AMM 278149/4 613 SIL SIL 27-112  REMOVE KRUEGER FLAP SPRING ROD FOR OVERHAUL.  ACCESS: 513AT  613AT  278149-0505-1 513 MOVABLE VANE - KRUEGER FLAP MEC LUB I: 1 C MPD SIL 27-020  613 SIL  CLEAN AND LUBRICATE PISTON OF SPRING ROD (ATTACHED TO  MOVABLE VANE) AND CHECK OVERLAP AND CONDITION OF  KRUEGER 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 278153/4 612 SB 27-0101  REMOVE STEPBACK GEARBOX FOR OVERHAUL OF SB 27-0158  HALO-TYPE UNIVERSAL JOINT POSITION 10  ACCESS: 512BB  612BB  278153-0504-2 512 STEPBACK GEARBOX - SLAT MEC RAR I: 3500 FC MRB AMM 278153/4 612 CN  REMOVE STEPBACK GEARBOX FOR OVERHAUL OF 1983-148-056 HALO-TYPE UNIVERSAL JOINT POSITION 10 FAA AD 84-06 SB 27-0101  ACCESS: 512BB SB 27-0158  612BB  278153-0504-3 512 STEPBACK GEARBOX - SLAT MEC RAR I: 12000 FC MRB AMM 278153/4 612 SB 27-0101  REMOVE STEPBACK GEARBOX FOR OVERHAUL OF  HOOKES-TYPE UNIVERSAL JOINT POSITION 10  ACCESS: 512BB  612BB  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278153-0504-4 512 STEPBACK GEARBOX - SLAT MEC RAR I: 8000 FC MRB AMM 278153/4 612 CN  REMOVE STEPBACK GEARBOX FOR OVERHAUL OF 1983-148-056 HOOKES-TYPE UNIVERSAL JOINTS POSITION 10 AND 11 FAA AD 84-06 SB 27-0101  ACCESS: 512BB  612BB  278153-0504-5 512 STEPBACK GEARBOX - SLAT MEC RAR I: 16000 FC MRB AMM 278153/4 612 SB 27-0101  REMOVE STEPBACK GEARBOX FOR OVERHAUL OF SB 27-0158  HALO-TYPE UNIVERSAL JOINT POSITION 11  ACCESS: 512BB  612BB  278153-0504-6 512 STEPBACK GEARBOX - SLAT MEC RAR I: 8000 FC MRB AMM 278153/4 612 SB 27-0101  REMOVE STEPBACK GEARBOX FOR OVERHAUL OF SB 27-0158  HALO-TYPE UNIVERSAL JOINT POSITION 11  ACCESS: 512BB  612BB  278153-0504-7 512 STEPBACK GEARBOX - SLAT MEC RAR I: 16000 FC MRB AMM 278153/4 612 CN  REMOVE STEPBACK GEARBOX FOR OVERHAUL OF 1983-148-056 HOOKES-TYPE UNIVERSAL JOINT POSITITION 11 FAA AD 84-06 SB 27-0101  ACCESS: 512BB  612BB  278153-0505-1 512 STEPBACK GEARBOX - SLAT MEC RPL I: 1 C MPD AMM 121327/0 612  CHECK FOR CORRECT OIL LEVEL:  01. REMOVE OIL LEVEL PLUG  02. FILL UP WITH HYDRAULIC FLUID MIL-H-5606/C/1 TILL  FLUID OVERFLOWS THROUGH OIL LEVEL PORT  03. 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 278153-0505-1 * * * * * C O N T I N U E * * * * *  RECOMMENDED VALUE  ACCESS: 512BB  612BB  278211-0503-1 147 CONTROL UNIT-SLAT ERI OPC I: 1 C MRB AMM 278300/5 CHECK JAMMING DETECTION ELECTRICAL CIRCUIT FOR  CORRECT OPERATION  278211-0504-1 147 CONTROL UNIT-SLAT MEC RAR I: 12000 FC MRB AMM 278211/4 REMOVE CONTROL UNIT-SLAT FOR OVERHAUL  ACCESS: 147CZ  278211-0505-1 147 CONTROL UNIT-SLAT MEC RPL I: 1 C MRB AMM 121327/0 CHECK CONTROL UNIT, SLAT FOR CORRECT OIL LEVEL:  01. REMOVE OIL LEVEL FILLER PLUG  02. FILL UP WITH OIL MIL-L-7808/G/2 TILL OIL OVER-  FLOWS THROUGH OIL LEVEL PORT  03. REPLACE PLUG SEAL, INSTALL PLUG AND TORQUE TO  RECOMMENDED VALUE  ACCESS: 147CZ  278300-0503-1 210 SLAT ASYMMETRY MEC OPC I: 1 A MRB ** AMM 278300/5 OPERATIONAL TEST OF SLAT ASYMMETRY MONITORING CIRCUIT  278300-0503-2 210 SLAT - PRESSURE OFF BRAKE MEC OPC I: 1000 FH MRB ** AMM 278300/5 OPERATIONAL TEST OF PRESSURE-OFF BRAKE  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 278400/5 OPERATIONAL TEST (BITE TEST) OF THE KRUEGER AND SLOT  FLAP INDICATING UNIT  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FLIGHT CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 281100-0502-1 500 FUEL TANKS MEC GVI I: DY-TERM MRB AMM 121128/0 600  CHECK THAT DIPSTICKS ARE RETRACTED AND IN SECURED  POSITION (LH AND RH WING) AND NO LEAKS ARE PRESENT  281100-0502-2 500 FUEL TANKS MEC GVI I: 1 A MRB AMM 281100/6 600  CHECK FUEL TANK AREAS FOR FUEL LEAKS ESPECIALLY  IN AREAS OF PYLON ATTACHMENT AND INBOARD OF RIB 1.  281100-0503-1 140 FUEL TANKS MEC DET I: NOTE 5-2 MPD AMM 123228/0 500 SIL SIL 28-079  600 SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATION  ANALYSIS  281100-0503-2 500 FUEL TANKS MEC DET I: NOTE 5-2 MPD AMM 123228/0 600 SIL SIL 28-079  SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATION  ANALYSIS  281100-0503-3 140 CENTER TANK MEC DRN I: WEEKLY MPD AMM 123228/0 SIL SIL 28-079  WATER DRAIN CHECK  281100-0505-1 500 FUEL TANKS MEC CHK I: DY-TERM MPD AMM 123228/0 600 OR SIL SIL 28-079  CHECK WATER CONTENT OF ALL FUEL TANKS AT DRAIN NOTE 5-2  VALVES  NOTE: INTERVAL MAY BE INCREASED DEPENDING  ON INDIVIDUAL OPERATORS OPERATING  INVIRONMENT  281115-0503-1 500 VALVES-FLAP MEC OPC I: 4 YE MRB AMM 281115/4 600  VISUAL INSPECTION AND MANUAL OPERATION TO REVEAL ANY  TENDENCY 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 MANHOLES  02. CHECK THAT FLAP VALVE WILL CLOSE WITH LIGHT PUSH  03. CHECK FLAP VALVE FOR FREEDOM OF MOVEMENT OVER  COMPLETE RANGE  ACCESS: 541AB 542CB 550BB  641AB 642CB 650BB  281300-0503-1 140 WING CENT.BOX/TANK VENT.SYS MEC OPC I: 4 C MRB ** AMM 251300/5 AMM 281312/6 01. VISUAL INSPECTION OF WING CENTER BOX VENTILATION  SYSTEM AIR INLET AND OUTLET SCREENS FOR CLEAN-  INLESS  02. OPERATIONAL TEST OF CHECK VALVE  ACCESS: 148AZ 148GZ 241ZF  281300-0503-2 140 WING CENT.BOX/TANK VENT.SYS MEC OPC I: 4 C MRB ** AMM 281312/6 01. INSPECT CENTER TANK VENTILATION SYSTEM AIR INLET  SCREEN FOR CLEANLINESS  02. PERFORM OPERATIONAL TEST OF CHECK VALVE  ACCESS: 241ZF  281300-0503-3 140 WING CENT.BOX/TANK VENT SYS MEC OPC I: 4 C MRB ** AMM 281312/6 OPERATIONAL TEST OF CHECK VALVE  ACCESS: 241ZF  281800-0502-1 143 IGNITION PREVENTION MEC FUC I: 6 YE EUAD AMM 281800/5 144 EUAD 2007-00 145 FUNCTIONAL CHECK OF CENTER TANK VAPOUR SEAL FAL 95A.1928 146  ACCESS: 147FZ 147GZ 147HZ  148GZ 148HZ  241AAF 241ABF 241ZF  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 281800-0502-1 * * * * * C O N T I N U E * * * * *  242VF 242WF  281800-0502-2 541 IGNITION PREVENTION MEC DET I: 12 YE MRB 9 AMM 281800/6 542  543 DETAILED INSPECTION OF THE WING TANK BONDING LEADS.  550  560  641  642  643  650  660 R 281800-0502-3 141 IGNITION PREVENTION MEC DET I: 12 YE FAL AMM 281800/6 142  541 DETAILED VISUAL INSPECTON OF WING AND CENTER TANK  542 BONDING LEADS.  543  550  560  641  642  643  650  660  281800-0502-4 541 IGNITION PREVENTION MEC GVI I: 12 YE MRB 9 AMM 281800/6 542  543 GENERAL VISUAL INSPECTION OF INTERNAL WING TANK  550 WIRING AND PROBE ATTACHMENTS.  560  641  642  643  650  660 R 281800-0502-5 141 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6 142  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AND  542 CENTER TANK WIRING AND PROBE ATTACHMENTS.  543  550  560  641  642  643  650  660 R 281800-0502-6 130 IGNITION PREVENTION MEC GVI I: 6 YE FAL AMM 281800/6 GENERAL VISUAL INSPECTION OF CENTER TANK FORWARD  CARGO BAY INSULATION MATS. R 281800-0502-7 145 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6 146  GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE  CENTER TANK. R 281800-0502-8 512 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6 523  524 GENERAL VISUAL INSPECTION OF WING LEADING - AND  572 TRAILING EDGE ELECTRICAL WIRING CONNECTIONS.  575  581  591  612  623  624  672  675  681  691 R 281800-0502-9 500 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6 600  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 281800-0502-9 * * * * * C O N T I N U E * * * * *  ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL  SUPPLY CABLE.  281800-0503-1 143 IGNITION PREVENTION MEC FUC I: 6 YE EUAD AMM 281800/6 144 EUAD 2007-00 147 DETAILED INSPECTION OF CENTER TANK VAPOUR SEAL. FAL 95A.1928 148  ACCESS: 147FZ 147GZ 147MZ  148GZ 148HZ  734  744  281800-0503-2 141 IGNITION PREVENTION MEC OPC I: NOTE EUAD AMM 281800/5 142 EUAD 2007-00 540 OPERATIONAL CHECK OF FUEL QUANTITY INDICATING AND FAL 95A.1928 550 LEVEL SENSING FOR ELECTRICAL CONTINUITY.  640  650 NOTE: TO BE CARRIED OUT IN ACCORDANCE WITH THE AD.  ACCESS: TANK ACCESS PANELS R 281801-0502-1 140 IGNITION PREVENTION MEC GVI I: 12 YE FAL AMM 281800/6 500  600 GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS.  282100-0503-1 141 FUEL-CENTER TANK INSPECTION OF FUEL NDT SDI T: 19600 FC CN CN F-2005-19 142 PUMPS AND PUMP CANISTERS I: 3000 FC FAA AD FAA AD  ISB 2006-12-05  REMOVE CENTRE FUEL TANK BOOSTER PUMPS FOR: . ISB 28-0084  01. DETAILED INSPECTION.  02. SPECIAL DETAILED INSPECTION OF THE BOOSTER PUMP  CANISTERS.  PREP.: INNER TANKS AND CENTER TANK TO BE DEFUELED  ACCESS: 147AZ 147HZ 734  148AZ 148HZ 744  SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 282112-0503-1 500 PUMP BOOSTER ENG OPC I: ENG. CHG MRB AMM 710000/5 600  OPERATE ENGINE ON SUCTION FEED AND MONITOR  ENGINE FUEL PRESSURE INDICATOR.(WITHOUT BOOSTER  PUMPS)  282116-0503-1 210 VALVES-ISOLATION (SHUT OFF) MEC OPC I: 1 C MRB ** AMM 282117/4 OPERATIONAL TEST OF INBOARD,OUTBOARD TANK ISOLATION  SHUT-OFF VALVE AND ACTUATORS USING KNOB INDICATOR  LIGHTS TO VERIFY VALVE POSITION  ACCESS: 575BB 675BB  282116-0503-2 210 VALVES-ISOLATION (SHUT OFF) MEC OPC I: 1 C MRB ** AMM 282117/4 OPERATIONAL TEST OF INBOARD,OUTBOARD AND CENTER TANK  ISOLATION SHUT OFF VALVES AND ACTUATORS USING KNOB  INDICATOR LIGHTS TO VERIFY VALVE POSITION  ACCESS: 575BB 675BB  282116-0503-3 210 VALVES - ISOLATION (S/O) MEC DET I: 500 FH CN AMM 282100/4 FAA AD CN  OPERATIONAL TEST OF ISOLATION VALVE AND CROSS-FEED 1991-173-126 VALVE CONTROL UNIT. FAA AD 97-07 282118-0503-1 500 LOW PRESSURE FUEL FIRE SHUT OFF VALVE MEC OPC I: ENG. CHG MRB ** AMM 282118/5 600  CHECK FOR LEAKAGE:  01. BEFORE RECONNECTION OF FUEL LINE MAKE CERTAIN  THAT LP FIRE SHUT OFF VALVES ARE CLOSED (BY USING  FIRE CONTROL HANDLE)  02. START UP BOOSTER FUEL PUMPS (TANK 1 AND 2)  03. LEAVE THE SYSTEM PRESSURIZATED FOR SEVERAL  MINUTES  04. MAKE CERTAIN THAT THERE IS NO FUEL FLOW FROM END  OF ENGINE PYLON FUEL LINE  05. SHUT DOWN FUEL PUMPS  SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 282124-0503-1 550 JET PUMP-OUTBOARD TANKS MEC FUC I: 4 C MRB ** AMM 282124/5 650  FUNCTIONAL TEST OF JET PUMP OUTBOARD TANKS  282125-0503-1 210 VALVE CROSSFEED ELO OPC I: 4000 FH MRB ** AMM 282100/5 OPERATIONAL TEST OF VALVE AND ACTUATOR CROSSFEED WITH  EACH ACTUATOR INCLUSIVE POSITION INDICATOR  ACCESS: 147DZ  282200-0503-1 144 VALVE - OVERFLOW MEC OPC I: DY-TERM MRB AMM 282200/0 OPERATIONAL TEST OF OVERFLOW VALVE AT REFUELING  PANEL:  - MANUALLY OPERATE THE HANDLE AND CHECK FOR FREE  MOVEMENT  ACCESS: 144ER  282214-0502-1 523 COUPLING REFUEL/DEFUEL MEC GVI I: 6 C MRB AMM 282214/6 623  INSPECT REFUEL/DEFUEL COUPLING FOR EVIDENCE OF  DEMAGE AND WEAR,CAP-ROLLERS FOR FREEDOM,CABLE AND  CHAIN FOR CHAFING.ENSURE SEAL SUPPORT PLATE CAN BE  DEPRESSED AND RETURNED BY SPRING  ACCESS: 523HB  623HB  282400-0502-1 310 APU FUEL DUCT DRAIN MAST MEC GVI I: 1 A MRB AMM 282400/6 CHECK APU FUEL DUCT DRAIN MAST HOLES (AT FRAME  54) FOR OBSTRUCTION AND FOR FUEL LEAKAGE WITH TANK 1  BOOSTER PUMP OPERATING  282414-0502-1 313 VALVE-LP FUEL FIRE SHUT OFF ENG GVI I: 1 C MRB ** AMM 282400/5 INSPECT 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: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 282414-0502-1 * * * * * C O N T I N U E * * * * *  SWITCH AND APU FUEL FIRE SHUT OFF VALVE FOR  SATISFACTORY 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  282611-0502-1 147 VALVE-ECOLOGICAL DISCHARGE MEC GVI I: 1 C MRB AMM 282611/6 148  CHECK THAT DISCHARGE VALVE DIFFERENTIAL  PRESSURE INDICATOR IS NOT PROTRUDING  283100-0502-1 535 FUEL JETTISON - FLEX. HOSE MEC DET T: 4 C MPD AMM 275165/4 635 I: 1 C  DETAILED INSPECTION OF THE FUEL JETTISION  SYSTEM FLEXIBLE HOSE FOR PROPER INSTALLATION,  EVIDENCE OF DAMAGE AND/OR LEAKAGE.  NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY OF  TASK 275126-0505-2  ACCESS:-LH MOVABLE AND FIXED FLAP-TRACK FAIRING NO.5  -RH MOVABLE AND FIXED FLAP-TRACK FAIRING NO.5  283100-0503-1 535 FUEL JETTISON SYSTEM MEC OPC I: 3 C MRB ** AMM 283100/5 635  01. OPERATIONAL TEST OF JETTISON VALVE  CONTROL AND INDICATING CIRCUITS  02. OPERATIONAL TEST OF JETTISON VALVE  03. FUNCTIONAL TEST OF FUEL JETTISON SYSTEM  04. CHECK JETTISON PIPE BETWEEN WING  LOWER SKIN AND END OF FLAP TRACK FAIRING  FOR LEAKAGE  283111-0503-1 542 CHECK VALVE-FUEL FEED MEC OPC I: 6 C MRB AMM 283111/5 642  OPERATIONAL TEST OF CHECK VALVE - FUEL FEED  SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 283114-0502-1 535 NOZZLE JETTISON MEC GVI I: 1 A MRB  635  CHECK JETTISON DISCHARGE NOZZLE (AT FLAP TRACK  NO. 5) FOR GENERAL CONDITION  284200-0503-1 210 CAPACITANCE QUANTITY INDIC. ERI FUC I: 4 C MRB AMM 284200/5 FUNCTIONAL TEST OF FUEL QUANTITY AMPLIFIER ( 15QT )  WITH TANKS DRY  ACCESS: 144ER 523JB 623JB  284200-0503-2 210 CAPACITANCE QUANTITY INDIC. ERI FUC I: 4 C MRB AMM 284200/5 FUNCTIONAL TEST OF FUEL QUANTITY AMPLIFIER ( 15QT )  WITH TANKS DRY  ACCESS: 144ER 523JB 623JB  284300-0503-1 210 FUEL LOW PRESSURE INDICAT. ERI OPC I: PRE-ACPT MRB AMM 331400/5 LIGHT TEST OF FUEL LOW PRESSURE INDICATORS.  284600-0503-1 210 FUEL LOW LEVEL INDICATING ERI OPC I: 1 C MRB ** AMM 284600/5 OPERATIONAL TEST OF LOW LEVEL INDICATING SYSTEM.  ( ALTERNATIVE WITHOUT TEST EQUIPMENT: TRANSFER FUEL  FROM ONE TANK TO THE OTHER )  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FUEL REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 290000-0502-1 570 HYDRAULIC POWER MEC DET T: 27000 FH ISB ISB 29-0122  670 OR  DETAILED INSPECTION OF HYDRAULIC PIPES IN WING AREA 13500 FC  LH/RH BETWEEN RIB 5A AND RIB 9. I: 24 MO  ACCESS: 575CB 575DB  675CB 675DB  291000-0502-1 147 MAIN SYSTEM - FILTERS MEC GVI I: WEEKLY MPD AMM 290000/3 571  671 CHECK THAT RETURN FILTER CLOGGING INDICATOR  BUTTONS ARE NOT PROTRUDING (GREEN,BLUE AND YELLOW)  ACCESS: 147SZ  291000-0502-2 147 MAIN SYSTEM - FILTERS MEC GVI I: 1 A MPD AMM 290000/3 CHECK THAT CLOGGING INDICATORS OF GROUND SERVICE,  HIGH PRESSURE, BRAKE FILTER AND RETURN FILTER ARE  NOT PROTRUDING.  291000-0502-3 435 E.D.P. CASE DRAIN FILTER MEC GVI I: 1 A MRB AMM 290000/3 445  CHECK THAT EDP CASE DRAIN FILTERS CLOGGING  INDICATORS ARE NOT PROTRUDING  ACCESS: 435AL  445AL  291000-0503-1 147 HYDRAULIC POWER MEC FUC I: 3 C MRB AMM 290000/6 CHECK AND MEASUREMENT OF HYDRAULIC COMPONENTS  INTERNAL LEAKAGE AS FOLLOWS:  MEASURE AND RECORD LEAKAGE RATE PER GROUP OF USER  SERVICES IN GREEN,BLUE AND YELLOW SYSTEM AND COMPARE  WITH "NOMINAL"FLOW RATE OF EACH GROUP (FOR MONITORING  PURPOSE)  ACCESS: 147DZ  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 291000-0503-2 210 HYDR.FLUID TEMP.INDICATING MEC OPC I: 1 A MRB ** AMM 293300/5 OPERATIONAL TEST OF HYDRAULIC FLUID TEMPERATURE  OVERHEAT WARNING SYSTEM (PUSH TO TEST)  291000-0503-3 210 HYDRAULIC QTY, INDICATING MEC FUC I: 3 C MRB AMM 293100/5 FUNCTIONAL TEST OF QUANTITY AND LOW LEVEL  WARNING.(MAIN AND AUXILARY SYSTEMS)  ACCESS: 147SZ 148SZ  291000-0503-4 210 HYDRAULIC POWER MEC FUC I: 1 C MPD AMM 290000/6 INTERNAL LEAKAGE CHECK OF HYDRAULIC SYSTEM BY MEANS  OF ELECTRIC PUMP PRESSURE  291000-0503-5 147 HYDRAULIC SYSTEM FLUID SAMPLING MEC CHK I: 1 C SIL AMM 123229/0 148 SIL 29-034  SAMPLING OF HYDRAULIC FLUID. SIL 29-081  ACCESS: 734  744  291000-0505-1 148 HYDRAULIC PRESSURE FILTERS MEC DET I: 1 C MRB AMM 291142/3 AMM 292117/3 CHECK PRESSURE FILTER ELEMENTS FOR PARTICLES: AMM 292213/3 01. REMOVE FILTER ELEMENTS (1048,1049,2048,3049,AND AMM 292412/3 1079,2091,3084,3090)  02. DETAILED INSPECTION FOR SATISFACTORY  CONDITION AND METAL PARTICLES  03. REINSTALL A NEW OR RECONDITIONED FILTER ELEMENT  ACCESS: 147LZ 147SZ 148LZ  291000-0505-2 148 RETURN MANIFOLD FILTERS (G) MEC CLN I: 3 C MPD AMM 291114/3 REMOVE,INSPECT AND CLEAN GREEN RETURN MANIFOLD  FILTER ELEMENT (1066)  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 291000-0505-2 * * * * * C O N T I N U E * * * * *  ACCESS: 148SZ  291000-0505-3 147 RETURN FILTERS MEC RAR I: 3 C MRB AMM 291115/3 571  671 REPLACE RETURN FILTER ELEMENT AND CHECK FOR  PARTICLES (1002,2002,3002)  ACCESS: 147BL  571EB  671EB  291000-0505-4 147 GROUND SERVICE FILTER MEC DET I: 4 C MRB AMM 291164/3 INSPECT GROUND SERVICE FILTER ELEMENT FOR  PARTICLES AS FOLLOWS:  01. REMOVE FILTER ELEMENT  02. DETAILED INSPECTION FOR SATISFACTORY  CONDITION AND METAL PARTICLES.  03. REINSTALL NEW OR RECONDITIONED FILTER ELEMENT  ACCESS: 147BL  291000-0505-5 671 RAM AIR TURBINE FILTER MEC DET I: 4 C MRB AMM 292535/3 INSPECT RAM AIR TURBINE FILTER ELEMENT FOR PARTICLES:  01. REMOVE FILTER ELEMENT  02. DETAILED INSPECTION FOR SATISFACTORY  CONDITION AND METAL PARTICLES  03. REINSTALL NEW OR RECONDITIONED FILTER ELEMENT  291000-0505-6 430 E.D.P.SHAFT SEAL DRAINS MEC SER I: 5 A MPD AMM 290000/6 440  DRAIN INDIVIDUAL COLLECTOR OF EACH E.D.P.SHAFT  SEAL DRAIN,TO MONITOR SHAFT SEAL LEAKAGE  ACCESS: 435AL 436AR  445AL 446AR  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 291000-0505-7 450 E.D.P.SHAFT SEAL DRAINS MEC SER I: 5 A MRB AMM 290000/6 460  DRAIN INDIVIDUAL VALVE OF EACH E.D.P.SHAFT SEAL  DRAIN,ON GEARBOX SEAL DRAIN MANIFOLD ASSY,TO MONITOR  SHAFT SEAL LEAKAGE  ACCESS: 451AL 452AR  461AL 462AR  291000-0505-8 435 MAIN HYDRAULIC POWER MEC RAR I: EDP CHG MRB AMM 291136/3 445 ENG. CHG  REMOVE EDP CASE DRAIN FILTER ELEMENTS (GREEN, BLUE,  YELLOW), INSPECT FILTER ELEMENTS FOR PARTICLES,  INSTALL NEW FILTER ELEMENTS.ENSURE CLOGGING INDICATOR  IS NOT PROTRUDING  NOTE: AFTER ENGINE OR EDP CHANGE  ACCESS: 435AL  445AL  291111-0505-1 140 HYDR.QUANTITY INDICATING MEC RPL I: 1 A MRB AMM 121229/0 CHECK FLUID LEVEL OF HYDRAULIC TANKS (BLUE-GREEN-  YELLOW).  ACCESS: 147BL 147RZ 147SZ 147XZ 148RZ 148SZ  291132-0503-1 210 PUMP-ENGINE DRIVEN (G&B&Y) MEC OPC I: 1 A MRB AMM 291000/5 DEPRESSURATION OPERATIONAL TEST OF ENGINE DRIVEN  PUMPS (GREEN-BLUE-YELLOW)  291133-0503-1 210 SHUT OFF VALVE-FIRE (G&B&Y) MEC FUC I: 4000 FH MRB ** AMM 291000/5 FUNCTIONAL TEST OF FIRE SHUT OFF VALVES.  NOTE: TASK TO BE CARRIED OUT AT THE OPPORTUNITY  OF TASK 762000-0503-1 AND 762000-0503-2  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 291133-0503-3 210 SHUT OFF VALVE-FIRE (G&B&Y) MEC OPC I: 3 A MRB ** AMM 291000/5 OPERATIONAL 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 29-052  OPERATIONAL TEST OF FIRE VALVES.  291136-0502-1 450 EDP CASE DRAIN FILTER MEC DET I: 50 FH CN AMM 291136/3 460 CN F-1991-14 REMOVE AND INSPECT EDP CASE DRAIN FILTER FOR EVIDENCE  OF STEEL PARTICLES.  291156-0505-1 147 HYDR. ACCUMULATOR (G&B&Y) MEC RPL I: 1 A MRB AMM 121429/0 CHECK CHARGE PRESSURE OF HYDR.ACCUMULATORS  (BLUE-GREEN-YELLOW) AND BRAKE ACCUMULATOR  ACCESS: 147RZ 147SZ 148RZ 148XZ  291400-0502-1 571 TANK PRESSURATION FILTER MEC GVI I: 1 A MPD AMM 291400/3 CHECK BY-PASS OPENING INDICATOR ON PRESSURISATION  LINE FILTER OF "ENG I" AIR BLEED IS NOT PROTRUDING.  291400-0505-1 450 HYDR.TANK PRESSURE FILTER MEC CLN I: ENG. CHG MPD AMM 291415/4 460  CLEAN PRESSURIZATION LINE FILTER SCREEN  (BETWEEN RIB 5 AND 6 IN LOWER PYLON SECTION)  NOTE: AFTER 1ST ENGINE RUN-UP.  ACCESS: 435AL 455AL 456AR  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 291400-0505-1 * * * * * C O N T I N U E * * * * *  445AL 465AL 466AR  292000-0502-1 147 AUXILARY SYSTEM MEC GVI I: 1 A ISB ISB 29-0015  148  CHECK GREEN SYSTEM ELECTRIC PUMPS (ABEX MODEL PMP 09  V01 P/N: 4007) AT PORT CAPS FOR LEAKS, WHEN PUMPS ARE  OPERATING.  CAUTION: PORT CAP LEAKAGE SHOULD NOT BE CONFUSED WITH  DRAINAGE FROM DRAIN HOLE BETWEEN PUMP AND  MOTOR  ACCESS: 147SZ  148SZ  292211-0503-1 210 POWER TRANSFER UNIT MEC OPC I: 2 A MRB AMM 292200/5 AMM 292300/5 OPERATIONAL TEST OF POWER TRANSFER UNITS (GREEN/BLUE  AND GREEN/YELLOW)  292527-0503-1 210 TURBINE-RAM AIR MEC FUC I: 2 C MRB ** AMM 292500/3 AMM 292500/5 FUNCTIONAL TEST OF TURBINE - RAM AIR  292527-0503-2 132 TURBINE-RAM AIR MEC FUC I: 3 C MRB AMM 292500/5 CHECK CABLES OF TURBINE - RAM AIR CONTROL WITH  TENSIOMETER FOR CORRECT TENSION (REFER TO CABLE  TENSION ADJUSTMENT GRAPH IN THE RESP. AMM 292500/501)  292527-0503-3 671 TURBINE - RAM AIR MEC FUC I: 600 FH CN AMM 292500/3 OR FAA AD AMM 292500/5 FUNCTIONAL TEST OF TURBINE - RAM AIR 6 MO CN  1985-146-IMP * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 292527-0503-3 * * * * * C O N T I N U E * * * * *  ACCESS: 671BB 671CB FAA AD 90-23 292527-0503-4 671 TURBINE - RAM AIR MEC FUC I: 3000 FH CN AMM 292500/3 OR FAA AD AMM 292500/5 FUNCTIONAL TEST OF TURBINE - RAM AIR 1 YE CN  NOTE 1985-146-IMP NOTE: FOR INITIAL INSPECTION 9000 FH OR 3 YE FAA AD 90-23 SUBJECT TO A ONCE ONLY CHECK PER AIRCRAFT ISB 29-0087  292527-0503-5 671 TURBINE - RAM AIR MEC RAR I: 20000 FH CN AMM 292527/4 OR FAA AD CN  REMOVE RAM AIR TURBINE FOR OVERHAUL 10 YE 1985-146-IMP FAA AD 90-23 ACCESS: 671BB 671CB ISB 29-0087  292527-0503-6 671 TURBINE - RAM AIR MEC DET I: 30 MO CN AMM 292500/5 FAA AD CN  DETAILED INSPECTION, CLEANING AND GREASING OF 1991-124-122 RAT EXTENSION CONTROL CABLES. FAA AD 92-19 ISB 29-0097  NOTE: TASK MAY BE ACCOMPLISHED DURING FUNCTIONAL  TEST OF RAT.  ACCESS: 671BB 671CB  292527-0503-7 671 TURBINE - RAM AIR MEC FUC I: 10 MO CN AMM 292500/5 FAA AD CN  01. DEPLOY RAM AIR TURBINE 2000-259-315 02. CHECK FOR CORRECT ADJUSTMENT OF FAA AD  RAM AIR TURBINE LOCKING ROD. 2001-01-06  ISB 29-0101  ACCESS: 671BB 671CB  292527-0503-8 671 TURBINE - RAM AIR MEC RAR I: 20 YE CN AMM 292527/4 FAA AD CN 2001-212( REMOVE RAM AIR TURBINE FOR OVERHAUL FAA AD  2002-02-05  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 292527-0503-8 * * * * * C O N T I N U E * * * * *  ACCESS: 671BB 671CB SB 29-0118  292527-0504-1 671 TURBINE-RAM AIR MEC RAR I: 30 MO CN AMM 292526/4 FAA AD CN  REMOVE THE LEVER ASSEMBLY OF THE RAT UPLOCK 1995-163-182 FEEDTHROUGH MECHANISM FOR STRIP INSPECTION FAA AD 98-21 ISB 29-0108  PREP.: RAT EXTENSION  ACCESS: 671BB  292527-0505-1 671 TURBINE-RAM AIR MEC LUB I: 2 C MPD AMM 122229/0 LUBRICATE RAM AIR TURBINE DOOR HINGES AND  EXTENSION JACK ROD END FITTING  292527-0505-2 671 TURBINE-RAM AIR MEC LUB I: 2 C MPD AMM 122229/0 LUBRICATE RAM AIR TURBINE DOOR HINGES AND  EXTENSION JACK ROD END FITTING AND LOCKING  ROD ASSEMBLY  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : HYDRAULIC POWER REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 301100-0503-1 210 WING ICE PROTECTION ERI OPC I: 2 C MRB AMM 301100/5 OPERATIONAL TEST OF EMERGENCY IN FLIGHT ICE  PROTECTION (APU SUPPLY) CONTROL AND INDICATING  CIRCUIT.  301100-0503-2 140 UNDERPRESSURE SWITCH ERI FUC I: 3 C MRB AMM 301112/5 FUNCTIONAL TEST OF BOTH UNDERPRESSURE SWITCHES 137 DM  AND 138 DM  NOTE: ON A/C FUNCTIONAL TEST WITH PRESSURE  SWITCHES REMOVED  ACCESS: 147FZ  301100-0503-3 210 WING ICE PROTECTION ERI OPC I: 2 C MPD AMM 301100/5 OPERATIONAL TEST OF OVERHEAT WARNING CIRCUITS  301100-0503-4 210 WING ICE PROTECTION ERI OPC I: 2 A MRB ** AMM 301100/5 ON PANEL 38VU:  01. OPERATIONAL TEST OF ANTI-ICE VALVES FAULTY  POSITION 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 301100/5 ON PANEL 426 VU:  01. OPERATIONAL TEST OF "ALTERNATE" MODE  02. OPERATIONAL TEST OF "FAULT" WARNING (EACH VALVE  DISAGREE DETECTION)  301100-0503-6 210 WING ICE PROTECTION ERI OPC I: 2 A MRB ** AMM 301100/5 ON PANEL 38 VU  01. OPERATIONAL GROUND TEST OF ICE PROTECTION UNDER  PRESSURE AND EXCESSIVE PRESSURE WARNING CIRCUITS  02. 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: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 301100-0503-6 * * * * * C O N T I N U E * * * * *  INHIBITION WITH EMERGENCY INFLIGHT ICE PROTECTION  CONTROLLED BY APU  301112-0503-1 512 SWITCH - UNDERPRESSURE ERI FUC I: 2 C MPD AMM 301112/5 612  FUNCTIONAL TEST OF UNDERPRESSURE SWITCH AND  ASSOCIATED WARNING CIRCUITS  ACCESS: 512KB  612KB  301113-0503-1 512 SWITCH - EXCESSIVE PRESSURE ERI FUC I: 2 C MPD AMM 301113/5 612  FUNCTIONAL TEST OF EXESSIVE PRESSURE SWITCH AND  ASSOCIATED CIRCUITS  ACCESS: 512KB  612KB  302100-0503-1 210 ENGINE AIR INTAKE ANTI-ICE ERI OPC I: 3 C MRB AMM 302100/5 OPERATIONAL TEST OF ENGINE ANTI ICE INDICATING SYSTEM  302100-0503-2 430 ENGINE AIR INTAKE ANTI-ICE ERI FUC I: 3 C MRB AMM 302112/5 440  FUNCTIONAL TEST OF POD ANTI ICE PRESSURE SWITCHES  ACCESS: 436AR  302100-0503-3 210 ENGINE-AIR INTAKE ANTI-ICE ERI OPC I: DY-TERM MRB ** AMM 302100/5 OPERATIONAL TEST OF ENGINE ANTI-ICE SYSTEM  303100-0503-1 210 SENSORS,PITOT PROBES/STATIC ERI OPC I: DY-TERM MRB ** AMM 303100/5 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ICE AND RAIN PROTECTION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 303100-0503-1 * * * * * C O N T I N U E * * * * *  OPERATIONAL TEST OF PITOT PROBES AND STATIC PORTS  HEATING SYSTEM  304100-0502-1 210 WINDSHIELD RAIN REMOVAL SYS ERI GVI I: C MPD AMM 304100/6 NOTE  GENERAL VISUAL INSPECTION OF WINDSHIELD WIPERS FOR  SATISFACTORY CONDITION  NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH  OPERATIONAL ENVIRONMENT AND OPERATOR EXPERIENCE  304100-0502-2 210 WINDSHIELD RAIN REMOVAL SYS ERI GVI I: DY-TERM MRB AMM 304151/4 CHECK QUANTITY AND PRESSURE OF RAIN REPELLENT  SYSTEM  304200-0502-1 210 WINDSHIELD PANEL ANTI-ICE AND DE-FOGGING ERI DET T: 15000 FH ISB ISB 30-0047  I: 1 C  DETAILED INSPECTION OF PILOT AND COPILOT OR  SLIDING WINDOWS ELECTRICAL HARNESS AND METALLIC 5000 FH  CONDUIT  304200-0503-1 210 WINDSHIELD ANTI ICE/DEFOG. ERI OPC I: 1 C MRB AMM 304200/5 AMM 304300/5 OPERATIONAL TEST OF ANTI-ICING AND DE-FOGGING  OVERCURRENT PROTECTION  307200-0503-1 136 WATER SERV.PANELS HEATING MEC OPC I: 1 C MPD AMM 307200/4 220  OPERATIONAL TEST OF THE WATER SERVICING PANEL HEATING  ACCESS: 136BR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ICE AND RAIN PROTECTION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 310000-0502-1 210 INDICATING/RECORDING SYSTEM MEC OPC I: PRE-ACPT MRB AMM 311500/0 CHECK ENGINE OIL, APU OIL AND HYDRAULIC TANK FLUID  FOR CORRECT LEVELS AT FLIGHT COMPARTMENT INDICATORS  311500-0502-1 210 LATERAL PANEL ELO OPC I: PRE-ACPT MPD AMM 242100/0 CHECK STATUS OF AC GENERATORS "BEARING RUB"  LATCHING MAGNETIC INDICATORS  311500-0502-2 210 LATERAL PANEL ELO OPC I: DY-TERM MRB AMM 311500/0 ON LATERAL PANEL:  01. SELECT ANNUNCIATOR LIGHTS SWITCH TO "READ" POSI-  TION:  - CHECK STATUS OF "OPEN / SHUT" INDICATING  LIGHTS (HYDRAULIC FIRE SHUT-OFF VALVES AND  APU ISOLATING VALVE)  - CHECK STATUS OF "DC BUS TIE CONTACTOR" INDI-  CATING LIGHT  02. CHECK STATUS OF ALL LATCHING MAGNETIC INDICATORS  03. MAKE CERTAIN THAT ALL TEST ROTARY SELECTORS ARE  IN "NORMAL FLT" POSITION  TAKE APPROPRIATE ACTION ACCORDING TO FINDINGS  313100-0503-1 171 DIGITAL FLIGHT DATA RECORD. ELO FUC I: NOTE 5-3 MRB AMM 313135/4 OR  DFDR TAPE READ OUT FOR AQUISITION CHECK OF MANDATORY 2 C  PARAMETERS AS DEFINED BY OPERATORS AIRWORTHINESS  AUTHORITY  ACCESS: 162AZ  313100-0503-2 171 UNDERWATER LOCATOR BEACON ELO FUC I: NOTE 5-1 MRB AMM 313100/4 NOTE 5-3  FUNCTIONAL TEST OF UNDERWATER LOCATOR BEACON AND  REPLACE BATTERY IF NECESSARY  ACCESS: 162AZ  SYSTEMS AND POWERPLANT PROGRAM : INSTRUMENTS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 313100/4 DISCARD AND REPLACE BATTERY OF UNDERWATER LOCATOR  BEACON ATTACHED TO THE DIGITAL FLIGHT DATA RECORDER  ACCESS: 162AZ  314211-0503-1 210 COMPUTER - N1 LIMIT ELO OPC I: DY-TERM MRB AMM 314200/5 OPERATIONAL TEST OF N1 LIMIT COMPUTER  314211-0503-2 210 COMPUTER EPR LIMIT ELO OPC I: DY-TERM MRB AMM 314200/5 OPERATIONAL TEST OF EPR LIMIT COMPUTER  314213-0503-1 122 FAN COOLING - N1 ELO OPC I: 3 C MRB AMM 314213/4 OPERATIONAL TEST OF N1 LIMIT COMPUTER COOLING FAN  (AURAL CHECK)  314213-0503-2 122 FAN COOLING - EPR ELO OPC I: 3 C MRB AMM 314213/4 OPERATIONAL TEST OF EPR LIMIT COMPUTER COOLING FAN  (AURAL CHECK)  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : INSTRUMENTS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 321000-0502-1 731 MAIN GEAR AND DOORS MEC GVI I: WEEKLY MRB AMM 321000/6 741  CHECK ATTACHMENTS AND INSTALLATIONS FOR SECURITY  AND 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 32-0233  740  DETAILED INSPECTION OF SHOCK ABSORBER LOWER  BEARING HOUSING FOR CORROSION  321100-0502-2 731 MAIN GEAR MEC DET I: REFER CN CN CN  741 FAA AD 1981-174-041 DETAILED CHECK OF MLG HINGE ARMS FAA AD 84-02 (PIN C65381-2) IN THE VICINITY OF THE RETRACTION ISB 32-0328  MECHANISM ATTACHING TRUNNIONS FOR CORROSION AND  CRACKS  321100-0502-3 731 MAIN GEAR MEC GVI I: PRE-ACPT MRB AMM 321000/6 741  CHECK MAIN GEAR FOR GENERAL CONDITION,FLUID  LEAKAGE,TYRES FOR EVIDENCE OF UNDERINFLATION,AND  BRAKES FOR EXTERNAL LEAKAGE.(DOORS CLOSED) CHECK THAT  PITCH DAMPER DROOP INDICATOR IS NOT PROTRUDING  (IF INSTALLED)  321100-0502-4 731 MAIN GEAR MEC GVI I: DY-TERM MRB AMM 321000/6 741 AMM 324100/6 CHECK NORMAL EXTENSION AND GENERAL CONDITION OF  SLIDING TUBE, WHEELS AND TYRES FOR DAMAGE, WEAR  (DEFORMATION,CUTS,FLAT SPOTS) AND CORRECT PRESSURE,  BRAKES FOR GENERAL CONDITION AND EXTERNAL LEAKS  321100-0503-1 731 MLG - HINGE ARM MEC FUC I: ISB CN CN  741 32-356 FAA AD 1982-160-049 AT HINGE ARMS MEASURE SIDE PLAY OF BRONZE BUSH, CN  LOCATED BETWEEN STIRRUP AND HINGE ARM TRUNNION 1983-051-050 AT ACTUATING CYLINDER SIDE. FAA AD 84-03 ISB 32-0356  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 321100-0503-1 * * * * * C O N T I N U E * * * * *  321100-0503-2 730 MLG - HINGE ARM NDT SDI T: REFER CN CN CN  740 I: 400 FC FAA AD 1983-052-051 SPECIAL DETAILED INSPECTION (ULTRA SONIC) FAA AD 84-02 -PROBE PARALLEL AND PROBE AT 45 DEGREES- ISB 32-0365  ON THE LATERAL INBOARD TRUNNION OF HINGE ARM ON ISB 470-32-4 ACTUATOR SIDE.  321100-0503-3 730 MLG - HINGE ARM NDT SDI I: REFER CN CN CN  740 FAA AD 1987-029-078 SPECIAL DETAILED INSPECTION (ULTRASONIC) ON THE TWO FAA AD 88-03 LOWER FLANGE TIE RODS ON HINGE ARM. ISB 32-0369  ISB 470-32-4 321112-0502-1 731 MAIN LANDING GEAR ASSY MEC DET I: 1 C MRB ** AMM 321000/6 741  DETAILED INSPECTION OF MAIN LANDING GEAR  STRUCTURE, RELATED COMPONENTS AND ATTACHMENTS  (WITH DOORS OPEN)  - SHOCK STRUT (OUTER CYLINDER), HINGE ARM (TRUNNION)  AND BEARING, MULTIPLE CLEVIS ASSY, CROSS BRACE AND  UP-LOCK ROLLER, TORQUE LINKS, SLIDING TUBE,BOGIE BEAM  (TRUCK BEAM),PITCH DAMPER,BRAKE BAR (BRAKE EQUALIZING  RODS), BRACE STRUT (SIDE STRUT), LOCK LINK ASSY,  SPRINGS, BRACE STRUT HINGE POINT AT FRAME 50, SHAFT  (VISIBLE PART ONLY) FOR:  CLEANLINESS,CORROSION,PROTECTIVE PAINTWORK,SECURITY  OF ATTACHMENT,LEAKAGE,IDENTIFICATION PLATES CORRECTLY  ATTACHED,BONDING JUMPERS FOR CORRECT CONDITION AND  FLAKED AREAS ON THE CHROMIUM PLATED RODS.  321112-0502-2 731 MLG - UPLOCK ROLLERS MEC GVI I: 5 A MRB AMM 321000/6 741  CHECK UPLOCK ROLLERS OF STRUT ASSY FOR FREE  ROTATION  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 321112-0504-1 700 MAIN LANDING GEAR ASSY MEC RAR I: 12000 FC MRB ** AMM 321111/4 OR  REMOVE AND REPLACE FOLLOWING COMPONENTS FOR 8 YE  OVERHAUL:  - STRUT ASSY - MAIN GEAR SHOCK  - ABSORBER MAIN GEAR SHOCK  - BEAM ASSY - BOGIE  - STRUT BRACE  - LINK ASSY LOCK  321112-0505-1 731 MAIN LANDING GEAR ASSY MEC LUB I: 3 A MRB AMM 122232/0 741  CLEAN 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 SIDE  NOTE: BRAKE UNIT ON WHEEL SIDE AT OPPORTUNITY OF  WHEEL CHANGE  321112-0505-2 731 MAIN LANDING GEAR ASSY MEC LUB I: 2 A MRB AMM 122232/0 741  CLEAN AND LUBRICATE FOLLOWING POINTS:  - BOGIE BEAM ARTICULATION  - PITCH DAMPER ATTACH POINTS  - BRAKE BARS ATTACH POINTS  321112-0505-3 731 MAIN LANDING GEAR ASSY MEC LUB I: 1 A SIL AMM 122232/0 741 SIL 32-111  LUBRICATION OF LOWER BEARING - SHOCK STRUT  (BARREL LOWER BEARING)  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 321113-0505-1 731 ABSORBER-MAIN GEAR SHOCK MEC RPL I: 1 C MRB AMM 121232/0 741  CHECK MLG SHOCK ABSORBER CHARGE PRESSURE  321113-0505-2 731 ABSORBER-MAIN GEAR SHOCK MEC RPL I: 2 C MRB AMM 121232/0 741  CHECK MLG SHOCK ABSORBER FLUID LEVEL AND  CHARGE PRESSURE  321114-0502-1 731 BOGIE BEAM ASSEMBLY MEC DET I: ISB CN AMM 321114/6 741 32-394 FAA AD CN  DETAILED INSPECTION OF THE INNER SIDE OF THE 1990-005-101 BOGIE BEAM BETWEEN THE TWO AXLES. FAA AD 90-26 ISB 32-0394  SB MHB  470-32-659  321115-0505-1 731 DAMPER-PITCH MEC RPL I: 1 C MRB ** AMM 121232/0 741  CHECK MLG PITCH DAMPER CHARGE PRESSURE  321115-0505-2 731 DAMPER-PITCH MEC RPL I: 2 C MRB AMM 121232/0 741  CHECK MLG PITCH DAMPER FLUID LEVEL  321115-0505-3 731 DAMPER - PITCH MEC RPL I: 1 C MRB AMM 121232/0 741  CHECK MLG PITCH DAMPER FLUID LEVEL  321115-0505-4 731 DAMPER - PITCH MEC RPL I: 3 A MRB AMM 121232/0 741  CHECK MLG PITCH DAMPER FLUID LEVEL  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 321118-0502-1 147 MULTIPLE CLEVIS ASSY MEC DET I: 1 C MRB ** AMM 321000/6 148  DETAILED INSPECTION OF MULTIPLE CLEVIS ASSY AT  FRAME 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 321118/4 148 OR  REMOVE UPPER SHAFT OF MULTIPLE CLEVIS AT 8 YE  FR.50 AND INSPECT FOR WEAR AND CORROSION  321124-0504-1 700 FWD SPHERICAL BEARING HOUS. MEC RAR I: 12000 FC MPD AMM 321124/4 OR SIL 32-038  REMOVE SPHERICAL BEARING ASSY FROM FORWARD 8 YE  PICK-UP AND INSPECT HOUSING AND SCREW THREADS  NOTE: TO BE PERFORMED AT OPPORTUNITY OF LANDING  GEAR OVERHAUL  321127-0502-1 731 TORQUE LINKS - MAIN GEAR MEC GVI I: 4 C MPD AMM 321127/4 741  CHECK TORQUE LINKS FOR EXESSIVE FREEPLAY  322000-0502-1 711 NOSE GEAR AND DOORS MEC GVI I: WEEKLY MRB AMM 322000/6 CHECK NLG FOR SECURITY AND DAMAGE OF ATTACHM.  INSTALLATIONS AND EXTERNAL LEAKAGE OF ALL COMPONENTS,  DOORS UP-LOCK ASSY, DOORS STRUCTURE AND HINGES, NOSE  GEAR UP-LOCK ASSY AND TAXI-LIGHTS FOR DAMAGE (WITH  DOORS OPEN)  322100-0502-1 711 NOSE GEAR MEC GVI I: PRE-ACPT MRB AMM 322000/0 AMM 324100/6 CHECK 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 322000/0 AMM 324100/6 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 322100-0502-2 * * * * * C O N T I N U E * * * * *  CHECK NORMAL EXTENSION AND GENERAL CONDITION  OF SLIDING TUBE,WHEELS AND TYRES FOR DAMAGE,WEAR  (DEFORMATION,CUTS,FLAT SPOTS) AND CORRECT PRESSURE  322112-0502-1 711 STRUT-NOSE- GEAR SHOCK MEC DET I: 1 C MRB ** AMM 322000/6 DETAILED INSPECTION OF NOSE LANDING GEAR  STRUCTURE, RELATED COMPONENTS AND ATTACHMENTS (WITH  DOORS 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,SECURITY  OF ATTACHMENT,EXTERNAL LEAKAGE IDENTIFICATION PLATES  CORRECTLY ATTACHED,BONDING JUMPERS FOR CORRECT CON-  DITION AND FLAKED AREAS ON THE CHROMIUM PLATED RODS  322112-0504-1 711 NOSE LANDING GEAR ASSY MEC RAR I: 12000 FC MRB ** AMM 322111/4 OR  REMOVE AND REPLACE FOLLOWING COMPONENTS FOR 8 YE  OVERHAUL:  - STRUT ASSY - NOSE GEAR SHOCK  - ABSORBER - NOSE GEAR SHOCK  - STRUT ASSY - NOSE GEAR TELESCOPIC DRAG  322112-0504-2 711 NOSE LANDING GEAR ASSY. NDT SDI I: REFER CN CN CN  MRB 1987-100-080 SPECIAL DETAILED INSPECTION (ULTRASONIC) OF NOSE GEAR ISB 32-0382  BARREL. SB MHB  470-32-604  322112-0504-3 711 NOSE LANDING GEAR ASSY NDT SDI I: REFER CN CN CN  FAA AD 1988-143-088 SPECIAL DETAILED INSPECTION (ULTRASONIC) OF NOSE GEAR FAA AD 69-23 LOWER 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 322112-0504-3 * * * * * C O N T I N U E * * * * *  SB MHB  470-32-641  322112-0505-1 710 STRUT-NOSE- GEAR SHOCK MEC LUB I: 3 A MRB AMM 122232/0 CLEAN 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 PIN  322114-0505-1 710 ABSORBER-NOSE GEAR SHOCK MEC RPL I: 1 C MRB AMM 121232/0 CHECK OF NOSE LANDING GEAR SHOCK ABSORBER CHARGE  PRESSURE.  322114-0505-2 711 ABSORBER-NOSE GEAR SHOCK MEC RPL I: 2 C MRB AMM 121232/0 CHECK NOSE LANDING GEAR FLUID LEVEL AND CHARGE  PRESSURE  322114-0505-3 711 ABSORBER-NOSE GEAR SHOCK MEC RPL T: NOTE EASA AD EASA AD  I: 3200 FC ISB 2008-0052  NOSE LANDING GEAR ASSY SHOCK ABSORBER/BARREL OR ISB 32-0447  ATTACHMENT BOLTS - INSPECTION 30 MO  NOTE: REFER TO EASA AD FOR APPLICABLE THRESHOLD  322115-0502-1 711 TORQUE LINKS - NOSE GEAR MEC GVI I: 4 C MPD AMM 322115/8 CHECK TORQUE LINKS FOR EXESSIVE FREEPLAY  322116-0502-1 123 UPLOCK/DRAG STRUT FITTING MEC DET I: 1 C MRB ** AMM 322000/6 124  IN 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 (REAR  ATTACHMENT)  - TELESCOPIC DRAG STRUT HINGE PIN  FOR CRACKS AND CORROSION  322116-0504-1 120 UPLOCK/DRAG STRUT FITTING MEC RAR I: 12000 FC MRB ** AMM 323121/4 OR AMM 323124/4 REMOVE FOLLOWING PARTS FROM NOSE GEAR: 8 YE  - UPLOCK BOX MECHANICAL LINK AND ASSOCIATED ATTACH  BOLTS (REAR ATTACHMENT)  - TELESCOPIC DRAG STRUT HINGE PIN  AND INSPECT FOR WEAR AND CORROSION.  NOTE: TASK SHOULD BE ACCOMPLISHED AT THE OPPORTUNITY  OF LDG REMOVAL.  322200-0502-1 123 NOSE GEAR DOORS MEC LUB I: 1 C MPD AMM 323000/5 124 SIL 32-055  01. DISASSEMBLE, CLEAN AND LUBRICATE NOSE GEAR DOOR  GROUND OPENING MECHANISM  02. LUBRICATE THE TORSION TUBE CENTRE BEARINGS  03. REASSEMBLE NOSE GEAR DOOR GROUND OPENING  MECHANISM  04. PERFORM GROUND DOOR OPENING AND CLOSING TEST  ACCESS: 713  714  322200-0505-1 123 NOSE GEAR DOORS MEC LUB I: 4 A MPD AMM 122232/0 124 SIL 32-055  LUBRICATION OF THE MECHANICAL LINKAGE OF THE  BELLCRANKS OF THE GROUND OPENING CONTROL MECHANISM.  ACCESS: 713  714  323100-0503-1 210 NORMAL EXTENSION/RETRACTION MEC OPC I: 6400 FH MRB ** AMM 323000/5 OPERATIONAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 ELECTRICAL  SYSTEM 1 AND 2,AS FOLLOWS:  - GEAR RETRACTION INHIBITION WITH SHOCK ABSORBERS  COMPRESSED (AMM 323000/501 "D. SYSTEM TEST 4.D)  - GEAR RETRACTION INHIBITION WITH NOSE WHEEL STEERING  LEFT 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.SYSTEM  TEST 4.F)  323100-0503-2 210 NORMAL EXTENSION/RETRACTION MEC OPC I: 3 C MRB ** AMM 323000/6 CHECK ELECTRIAL CIRCUITS ASSOCIATED WITH LANDING  GEAR NORMAL CONTROL (MICROSWITCH UNIT).  323112-0503-1 210 ELECTROVALVE-LANDING GEAR ERI OPC I: 15000 FH MRB ** AMM 323112/6 ISB 32-0055  OPERATIONAL TEST OF ELECTROVALVE LANDING GEAR  NOTE: ACCOMPLISHMENT OF THIS TASK SATISFIES  REQUIREMENTS OF TASK 323112-0503-4  323112-0503-2 210 ELECTROVALVE-LANDING GEAR ERI OPC I: 3000 FH MRB ** AMM 323112/6 ISB 32-0055  OPERATIONAL TEST OF ELECTROVALVE LANDING GEAR  323112-0503-3 210 ELECTROVALVE-LANDING GEAR ERI OPC I: 1000 FH MRB ** AMM 323112/6 ISB 32-0055  OPERATIONAL TEST OF ELECTROVALVE LANDING GEAR  323112-0503-4 210 ELECTROVALVE LANDING-GEAR ERI OPC T: 32000 FC CN AMM 323112/6 I: 2800 FC FAA AD CN 2001-603( OPERATIONAL TEST OF ELECTROVALVE LANDING GEAR OR 18 MO FAA AD  2004-04-10  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 323112-0503-4 * * * * * C O N T I N U E * * * * *  NOTE: ACCOMPLISHMENT OF THIS TASK SATISFIES  REQUIREMENTS OF TASK 323112-0503-1  323112-0503-5 210 ELECTROVALVE LANDING-GEAR ERI OPC I: 32000 FC CN AMM 323112/6 FAA AD CN 2001-603( DISCARD ELECTROVALVE LANDING GEAR FAA AD  2004-04-10  323114-0503-1 711 NLG - DOOR UPLOCKS MEC FUC T: 3000 LG ISB AMM 323114/6 I: 5 A SB MHB  CHECK LOAD REQUIRED TO CLOSE UPLOCK HOOK 470-32-206  USING DYNAMOMETER  323118-0502-1 120 VALVE-NOSE GEAR-SEQUENCE MEC GVI I: 5 A MRB AMM 323118/8 CHECK FLEXIBLE DIAPHRAGM OF VALVE-NOSE GEAR  SEQUENCE (LH/RH) FOR RED WITNESS MARK  323124-0502-1 120 NLG - DOWN LOCK INDICATING MEC GVI I: 2 A MRB ** AMM 326100/6 CHECK VISUAL INDICATOR FROM ELECTRONIC BAY FOR  CLEANLINESS,CORROSION,CORRECT INDICATION AND  CLEAN INDICATOR WINDOW  323133-0503-1 147 MLG - DOOR UPLOCKS MEC FUC T: 3000 LG ISB AMM 323133/6 148 I: 1 C SB MHB  CHECK LOAD REQUIRED TO CLOSE UPLOCK HOOK 470-32-206  USING DYNAMOMETER  323200-0503-1 145 EMERGENCY EXTENSION MEC FUC I: 3 C MRB AMM 323200/6 CHECK EMERGENCY EXTENSION CONTROL CABLES FOR  CORRECT TENSION:  01. CHECK CABLE TENSION WITH TENSIOMETER (ACCESS  241AEF)  02. CHECK THAT POINTER ON COMPENSATION SCALE OF CABLE  TENSION REGULATOR IS WITHIN LIMITS.  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 323200-0503-2 121 EMERGENCY EXTENSION MEC FUC I: 3 C MRB AMM 323226/4 122 AMM 324500/5 CHECK EMERGENCY EXTENSION,PARKING AND ULTIMATE AMM 324500/6 EMERGENCY BRAKING AND STEERING CONTROL CABLES FOR AMM 325100/6 CORRECT TENSION WITH TENSIOMETER  ACCESS: 132AZ  323200-0503-3 711 NLG - DOWNLOCK FRICT. CHECK MEC FUC I: 3 C ISB AMM 322100/6 ISB 32-0353  FRICTION CHECK OF NLG COMPONENTS WITH A/C ON JACKS OR SB MHB  NOSE GEAR JACKED UP: 470-32-409  01. MEASURE TOTAL FRICTION OF COMPONENTS  02. MEASURE FRICTION OF TELESCOPIC STRUT  03. MEASURE FRICTION OF NLG-ACTUATOR AND ATTACHEMENT  04. PERFORM SWING TEST OF NLG HINGE POINTS  NOTE: TASK CANCELLED AFTER EMBODIMENT OF ALL  THE FOLLOWING MODS  MOD 1033 (S 6237)/MHB 606  MOD 1033 (S 6384)/MHB 657  MOD 1257 (S 4482)/MHB 457  323200-0503-4 700 EMERGENCY EXTENSION MEC DET I: 1000 FH ISB ISB 32-0298  SB MHB  MEASUREMENT OF PRESSURE REQUIRED TO EXTENT THE MAIN 470-32-349  GEAR BRACE STRUT ACTUATING CYLINDER ROD.  323200-0503-5 210 EMERGENCY EXTENSION MEC FUC I: 2 C MPD AMM 323000/5 FUNCTIONAL TEST OF LANDING GEAR EMERGENCY EXTENSION R 323300-0503-1 210 FREE FALL EXTENSION MEC OPC I: 2000 FH ISB AMM 323000/5 MRB ** ISB 32-0335  OPERATIONAL TEST OF FREE FALL EXTENSION LIMITED TO  UNLOCKING OF LANDING GEAR DOORS AND GEAR UPLOCKS (A/C  ON WHEELS)  323300-0503-2 210 FREE FALL EXTENSION MEC FUC I: 3 C MRB ** AMM 323000/5 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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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 EXTENSION  NOTE: CARRY OUT TOGETHER WITH TASK 325000-0503-1 R 323300-0503-4 210 FREE FALL EXTENSION MEC FUC I: 12 MO AOT AMM 323000/5 CN AOT 32-14  FUNCTIONAL TEST OF LANDING GEAR FREE FALL EXTENSION. FAA AD CN 1997-113- FAA AD 99-25 324111-0504-1 730 WHEELS - MAIN LANDING GEAR MEC DET I: TIRE CHG MRB AMM 123732/0 740 SB MHB  01. DETAILED INSPECTION OF WHEEL HALVES AND 470-32-001  TIE-BOLTS FOR GENERAL CONDITION,CRACKS,CORROSION  AND DAMAGE  02. DETAILED INSPECTION OF BEARINGS FOR GEN-  ERAL CONDITION AND EVIDENCE OF OVERHEATING  03. LUBRICATION OF BEARINGS  324111-0504-2 730 WHEELS - MAIN LANDING GEAR NDT SDI I: TIRE CHG MRB AMM 123732/0 740 SB MHB  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF WHEEL 470-32-001  HALVES AND MAGNAFLUX INSPECTION OF TIE-BOLTS IN  ACCORDANCE WITH VENDOR RECOMMENDATIONS.  324111-0504-4 730 WHEELS.- MAIN LANDING GEAR MEC DET I: 4 C MPD AMM 324227/4 740  DETAILED INSPECTION OF SLEEVE AND AXLE FOR  SATISFACTORY CONDITION.  PREP.: REMOVE AXLE SLEEVES.  324111-0504-5 730 WHEELS - MAIN LANDING GEAR MEC GVI I: BRAKE MPD AMM 324227/4 740 UNIT CHG  GENERAL VISUAL INSPECTION OF MAIN WHEEL AXLE SLEEVE  FOR SHOCKS, CORROSION, CHROME PLATING DAMAGE AND  OVERHEATING.  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

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THRESHOLD (T) 

INTERVAL (I)

 324112-0504-1 710 WHEEL NOSE LANDING GEAR MEC DET I: TIRE CHG MRB AMM 123732/0 SB MHB  01. DETAILED INSPECTION OF WHEEL HALVES AND 470-32-001  TIE-BOLTS FOR GENERAL CONDITION,CRACKS,CORROSION  AND DAMAGE  02. DETAILED INSPECTION OF BEARINGS FOR GEN-  ERAL CONDITION AND EVIDENCE OF OVERHEATING  03. LUBRICATION OF BEARINGS  324112-0504-2 710 WHEEL-NOSE LANDING GEAR NDT SDI I: TIRE CHG MRB AMM 123732/0 SB MHB  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF WHEEL 470-32-001  HALVES AND MAGNAFLUX INSPECTION OF TIE-BOLTS IN  ACCORDANCE WITH VENDOR RECOMMENDATIONS.  324200-0503-1 210 STAND-BY BRAKING MEC OPC I: 1 C MRB ** AMM 324300/5 ISB 32-0373  OPERATIONAL TEST OF STAND-BY BRAKING SYSTEM  NC 324200-0503-2 210 NORMAL BRAKING MEC OPC I: 1 C MRB ** AMM 324200/5 OPERATIONAL TEST TO CHECK AUTOBRAKE MAX. MODE  ENGAGEMENT  324200-0503-3 210 STANDBY BRAKING MEC OPC I: 1 A MRB ** AMM 324300/5 OPERATIONAL TEST OF STANDBY BRAKING SYSTEM  324200-0505-1 121 NORMAL BRAKING MEC RPL I: 2 A MRB AMM 121232/0 CHECK FLUID LEVEL IN BRAKE RESERVOIR AND  TOP-UP AS NECESSARY  ACCESS: 132AZ  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 324200-0505-2 147 NORMAL BRAKING MEC CLN I: 3 C MRB AMM 324212/3 CHECK BRAKE SYSTEM FILTER ELEMENT 1298 (NORMAL  BRAKING SYSTEM-GREEN HYDRAULIC):  - REMOVE FILTER ELEMENT AND INSPECT FOR SATISFACTORY  CONDITION AND PARTICLES  - INSTALL A NEW OR CLEAN FILTER ELEMENT  ACCESS: 147SZ  324227-0502-1 731 BRAKE UNIT MEC GVI I: WEEKLY MRB AMM 324227/6 741  CHECK BRAKES FOR WEAR  324227-0504-1 730 BRAKE UNIT MEC DET I: BRAKE MRB AMM 324227/4 740 UNIT CHG AMM 324227/6 DETAILED INSPECTION OF WHEEL AXLE, BRAKE  HOUSING 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 324200/6 FAA AD CN  DETAILED CHECK OF REAR ATTACHMENTS OF 1980-151-027 BRAKE PEDAL TRANSMITTER SUPPORT FOR CRACKS FAA AD 80-16 ISB 32-0264  ACCESS: 132AZ  324257-0503-1 700 ANTI-SKID TACH.GENERATORS MEC OPC I: 3 C MPD AMM 324200/5 OPERATIONAL TEST OF BRAKE ANTI-SKID SYSTEM.  324272-0503-1 210 CONTROL BOX,BRAKE SYSTEM MEC OPC I: 1 A MRB AMM 324272/4 TEST OF ANTI-SKID SYSTEM 1 & 2  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 324314-0505-1 148 EMERGENCY BRAKE DISTRIBUTION - DUAL MEC SER I: 4 A CN AMM 324314/6 VALVE FAA AD CN  1998-263-255 DRAIN WATER ACCUMULATION IN THE DRAIN TUBE OF THE FAA AD  BRAKE DUAL DISTRIBUTION VALVE (BDDV). 2001-15-10  324500-0503-1 210 PARK/ULTIMATE EMERGENCY BRAKING MEC OPC I: 1 C MRB ** AMM 324500/5 OPERATIONAL TEST OF PARKING AND ULTIMATE EMERGENCY  BRAKING SYSTEM.  325000-0503-1 210 STEERING MEC FUC I: 3 C MRB ** AMM 325100/5 FUNCTIONAL TEST OF ELECTRO/HYDRAULIC SELECTOR VALVE  WITH ELECTRICAL POWER ALTERNATIVELY SUPPLIED THROUGH  MICROSWITCHES ASSOCIATED WITH ENGINE 1 AND 2 HP FUEL  LEVERS (HP FUEL LEVERS ALTERNATIVELY SET TO "ON" THEN  TO "OFF" POSITION).  NOTE: CARRY OUT TOGETHER WITH TASK 323300-0503-2  325000-0503-2 210 STEERING MEC FUC I: 3 C MRB AMM 325100/5 FUNCTIONAL TEST OF ELECTRO/HYDRAULIC SELECTOR VALVES  (GREEN/YELLOW HYDRAULIC SYSTEM) WITH ELECTRICAL POWER  ALTERNATIVELY SUPPLIED THROUGH MICROSWITCHES  ASSOCIATED WITH ENGINE 1 AND 2 HP FUEL LEVERS (HP  FUEL LEVERS ALTERNATIVELY SET TO OFF POSITION) MOD  3070 EMBODIED  325000-0503-3 210 STEERING MEC FUC I: 6 C MPD AMM 325100/5 FUNCTIONAL TEST OF ELECTRO/HYDRAULIC SELECTOR VALVES  (GREEN/YELLOW HYDRAULIC SYSTEM)  325100-0502-1 710 STEERING MEC GVI I: 4400 FH ISB ISB 27-0107  GENERAL VISUAL INSPECTION OF MACHINED NOSE GEAR  EMERG/ULTIMATE EMERG. EXTENSION, PARKING BRAKE AND  NOSE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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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 326100/5 OPERATIONAL TEST OF AURAL WARNING MICROSWITCH ON  SYSTEM 1 AND 2  326112-0503-1 122 MODUL UNIT-PROX.DETECTOR ERI FUC I: 600 FH MRB ** AMM 320000/5 CONTINUITY TEST OF MODUL UNIT-PROXIMITY DETECTOR.  ACCESS: 132AZ  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : LANDING GEAR REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 331300-0503-1 210 INSTRUMENT AND PANEL INTEGRAL LIGHTING ERI OPC I: 700 FH EUAD AMM 331300/5 FAA AD EUAD 2006-03 OPERATIONAL CHECK OF STANDBY HORIZON INTEGRAL FAA AD  LIGHTING LOGIC. 2005-20-06  331500-0503-1 210 MASTER WARNING ERI OPC I: DY-TERM MRB ** AMM 331400/5 CHECK LIGHTS OF MASTER WARNING SYSTEM AND  ANNOUNCIATOR PANEL  331500-0503-2 210 MASTER WARNING ERI OPC I: 2 A MRB ** AMM 331500/5 OPERATIONAL TEST OF MASTER WARNING SYSTEM  332100-0502-1 200 GENERAL ILLUMINATION ERI GVI I: 1 A MPD AMM 332600/5 CHECK ALL INTERNAL FLIGHT COMPARTMENT AND PASSENGER  COMPARTMENT LIGHTS (INCLUDING FASTEN SEAT BELT /  NO SMOKING SIGNS) FOR BURNT OUT BULBS, MISSING SPARE  BULBS AND FUSES (SPARE BOX)  334000-0502-1 100 EXTERIOR LIGHTS ERI GVI I: WEEKLY MRB AMM 334300/6 AMM 334900/5 CHECK RUNWAY TURNOFF LIGHTS AND WING/ENGINE SCAN  LIGHTS FOR DAMAGE, GENERAL CONDITION AND FOR BURNT  OUT BULBS  334000-0502-2 500 EXTERIOR LIGHTS ERI GVI I: WEEKLY MRB AMM 334100/6 600 AMM 334200/5 CHECK LANDING/TAKEOFF, NAVIGATION/TOWING LIGHTS AMM 334600/5 FOR DAMAGE, GENERAL CONDITION AND FOR BURNT OUT BULBS  334000-0502-3 300 EXTERIOR LIGHTS ERI GVI I: WEEKLY MRB AMM 334700/0 CHECK EXTERIOR LIGHTS OF AFT FUSELAGE FOR DAMAGE,  GENERAL CONDITION AND FOR BURNT OUT BULBS  SYSTEMS AND POWERPLANT PROGRAM : LIGHTS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 335100-0502-1 200 PASS COMPT EMERGENCY LIGHT ERI GVI I: 1 C MRB AMM 335100/5 CHECK PASSENGER COMPARTMENT EMERGENCY LIGHTS FOR  FAILED BULBS  335100-0503-1 200 PASS COMPT/EXT EMERG LIGHT ERI FUC I: 6 C MRB ** AMM 335100/5 FUNCTIONAL TEST OF ELECTRICAL CIRCUITS AND INVERSE  BREAKDOWN CHARACTERISTICS OF DIODES  335100-0503-2 200 PASS COMPT/EXT EMERG LIGHT ERI OPC I: WEEKLY MRB ** AMM 335100/5 OPERATIONAL TEST OF PASSENGER COMPARTMENT EMERGENCY  LIGHTING (28V/6V).  335100-0503-3 200 PASS COMP/EXT EMERG LIGHT ERI OPC I: 1 A MPD AMM 335100/5 OPERATIONAL TEST OF EMERGENCY ESCAPE PATH MARKING  LIGHTING.  335100-0504-1 200 PASS COMPT/EXT EMERG LIGHT ERI RAR I: 2 YE MRB ** AMM 335111/3 AMM 335114/4 REMOVE PASSENGER CABIN EMERGENCY LIGHT BATTERIES  FOR BENCH TEST AND CHECK CAPACITY.  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : LIGHTS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 340000-0502-1 100 NAVIGATION-GENERAL ELO GVI I: DY-TERM MRB WDM 910004/0 CHECK 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 273615/6 AMM 341115/6 CHECK PITOT PROBES, STATIC PORTS, TEMPERATURE SENSORS AMM 341116/6 AND ANGLE OF ATTACK SENSORS FOR SECURITY OF AMM 341218/6 ATTACHMENT, SATISFACTORY CONDITION AND CLEAR APPEAR-  ENCE OF MARKINGS AND PLACARDS  341100-0503-1 100 AIR DATA-PRESSURE SYSTEM ELO FUC I: 1 C MRB AMM 122434/0 AMM 341110/5 DRAIN AND LEAK TEST OF PITOT AND STATIC SYSTEM.  ENSURE VALVE IS PROPERLY SEATED AFTER DRAINING.  ACCESS: 133AL 133BL 133CL  341100-0505-1 100 AIR DATA-PRESSURE SYSTEM ELO CLN I: 2 C MRB AMM 341110/3 NOTE SIL 34-084  FLUSHING OF PITOT AND STATIC SYSTEM  (AFTER FLUSHING PERFORM LEAK TEST)  NOTE: INTERVAL 2C-CHECK RECOMMENDED BUT CAN BE  ADJUSTED WITH EXPERIENCE TO SUIT OPERATING  ENVIRONMENT  ACCESS: 133AL 133BL 133CL  341120-0503-1 210 AIR DATA-COMPUTATION ELO OPC I: 2 A MRB ** AMM 341120/5 BITE TEST OF AIR DATA COMPUTER, INDICATORS AND  OVERSPEED FUNCTION SYSTEM 1+2.  341134-0503-1 120 AIR DATA COMPUTER ELO OPC I: 2 A MRB AMM 341800/5 BITE TEST OF HYBRID AIR DATA COMPUTER SYSTEM 1 AND 2  TO 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: 
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A300 MAINTENANCE PLANNING D

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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 RESPECTIVE  INDICATORS  342100-0503-1 210 MAGNETIC HEADING REFERENCE ELO OPC I: 2 C MRB AMM 342100/5 OPERATIONAL TEST OF COMPASS AND MAGNETIC HEADING  SYSTEM; INCLUSIVE COMPASS SWITCHING DEVICE.  342122-0503-1 210 INDICATOR-HORIZONTAL SITU. ELO OPC I: 3 A MRB AMM 342100/5 OPERATIONAL TEST OF HSI MAGNETIC MODE AND MONITORING.  342400-0503-1 210 SPEED REFERENCE SYSTEM ELO OPC I: 1 C MRB ** AMM 342400/5 OPERATIONAL TEST OF ALPHA-FLOOR PROTECTION.  342400-0503-2 210 SPEED REFERENCE SYSTEM ELO FUC I: 2 C MRB ** AMM 342400/5 FUNCTIONAL TEST OF SRS COMPUTER FOR CORRECT OPERATION  OF SLAT INSTRUMENTATION UNIT, FLAP MICROSWITCHES AND  MAIN GEAR RELAYS  342400-0503-3 210 SPEED REFERENCE SYSTEM ELO OPC I: DY-TERM MRB ** AMM 342400/5 CHECK SPEED REFERENCE SYSTEM ENGAGEMENT  342500-0503-1 210 ATTITUDE AND HEADING SYSTEM ELO OPC I: 5 A MRB AMM 342000/5 BITE TEST OF ATTITUDE AND HEADING REFERENCE SYSTEMS  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 342500-0503-1 * * * * * C O N T I N U E * * * * *  (AHRS 1, 2 AND 3) TO COVER OPERATIONAL TEST OF  FOLLOWING FUNCTIONS:  - ATTITUDE (ADI)  - HEADING (HSI AND RDMI)  - GROUND SPEED (AHRS/ONS GROUND SPEED DISPLAY ON  ONS CONTROL DISPLAY UNIT)  - VERTICAL SPEED (VSI)  - INSTRUMENTS SWITCHING (SYS 3)  CHECK INDICATIONS, LIGHTS AND FLAGS ON AHRU AND  RESPECTIVE INDICATORS.  342500-0503-2 210 INERTIAL REFERENCE SYSTEM ELO OPC I: 1 C MRB AMM 342000/5 OPERATIONAL TEST OF "ATT" SWITCHING (DATA SUPPLY FROM  IRS 3) THROUGH "ATT/SYS 3" PUSH BUTTONS ON CAPT AND  F/O SWITCHING PANEL.  342500-0504-1 121 INERTIAL NAVIGATION UNIT ELO RAR I: 1 C MPD SIL 34-055  01. REMOVE INERTIAL NAVIGATION UNITS  02. CLEAN AIR FILTER OF EACH INU IN THE WORKSHOP  03. INSTALL INERTIAL NAVIGATION UNITS  ACCESS: 132AZ  342523-0503-1 210 INDICATOR-ATTITUDE DIRECTOR ELO OPC I: WEEKLY MRB ** AMM 342523/4 BITE TEST OF ATTITUDE DIRECTOR INDICATOR.  342538-0504-1 121 BATTERY - ISS/INS ELO RAR I: NOTE 5-1 MRB ** AMM 342538/4 SIL 34-005  REMOVE BATTERY FOR RESTORATION / CAPACITY CHECK (SHOP  VISIT). CLEAN BATTERY UNIT SHELF.  NOTE: INTERVAL SHOULD BE IN ACCORDANCE WITH THE  VENDOR RECOMMENDATIONS.  ACCESS: 132AZ  SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 342723-0503-1 210 DIGITAL ATTITUDE DIRECTOR INDICATOR ELO OPC I: WEEKLY MPD AMM 342500/5 TEST OF A.D.I. 1 AND 2 BY MEANS OF PUSH-TO-TEST  BUTTON  343600-0503-1 210 ILS (INSTR. LANDING SYSTEM) ELO OPC I: 2 A MRB ** AMM 343600/5 OPERATIONAL TEST OF INSTRUMENT LANDING SYSTEM BY BITE  343600-0503-2 210 ILS (INSTR. LANDING SYSTEM) ELO OPC I: 2 A MRB AMM 343600/5 AMM 343636/4 BITE TEST OF ILS 1 AND 2 TO COVER OPERATIONAL TEST OF  FOLLOWING FUNCTIONS:  - ILS RECEPTION AND INDICATION (ADI,HSI)  - OPERATIONAL TEST OF DIGITAL/ANALOGIC CONVERTER  FOR GPWS AND FDAU.  CHECK INDICATIONS,LIGHTS AND FLAGS ON RECEIVERS  AND RESPECTIVE INDICATORS.  344200-0503-1 210 RADIO ALTIMETER ELO OPC I: 2 A MRB ** AMM 344200/5 SELF TEST OF SYSTEM 1 AND 2 USING THE TEST KNOB ON  INDICATORS. N 344200-0503-2 150 RADIO ALTIMETER MEC CLN I: 6 MO SIL AMM 20-31-00  PAGE1  RADIO ALTIMETER ANTENNAS EXTERNAL SURFACE TO BE SIL 34-099  CLEANED.  344243-0503-1 152 FAN - RADIO ALTIMETER ELO OPC I: 1 C MRB AMM 344200/5 AURAL OPERATIONAL TEST OF RADIO ALTIMETER TRANSCEIVER  CASE COOLING FAN  344800-0503-1 210 GROUND PROXIMITY WARNING SYSTEM ELO FUC I: 1 C MPD AMM 344800/5 FUNCTIONAL TEST OF GPWC MODES  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 344800-0503-1 * * * * * C O N T I N U E * * * * *  344800-0503-2 210 GROUND PROX.WARNING SYSTEM ELO OPC I: 2 A MRB ** AMM 344800/5 OPERATIONAL TEST OF GPW SYSTEM BY BITE  345100-0503-1 210 DME (DISTANCE MEASUR.EQUIP) ELO OPC I: 2 A MPD AMM 345100/5 BITE TEST OF DME 1 AND 2 TO COVER OPERATIONAL TEST OF  FOLLOWING FUNCTIONS:  - DME INTERROGATION AND INDICATION (RDMI,HSI)  CHECK INDICATIONS,LIGHTS AND FLAGS ON  TRANSCEIVERS AND INDICATORS.  345233-0503-1 200 ATC TRANSPONDER ELO FUC I: 2 YE MPD AMM 345200/5 FUNCTIONAL TEST AS PER FAR 91.413  NOTE: TASK APPLICABLE TO AIRCRAFT OPERATED UNDER  FAA REQUIREMENTS  345300-0503-1 210 ADF (AUTOMAT.DIRECT.FIND.) ELO OPC I: 2 A MRB ** AMM 345300/5 OPERATIONAL TEST OF ADF SYSTEM BY BITE  345300-0503-2 210 ADF (AUTOMAT.DIRECT.FIND.) ELO OPC I: 2 A MRB AMM 345300/5 BITE TEST OF ADF 1 AND 2 TO COVER OPERATIONAL TEST OF  FOLLOWING FUNCTIONS:  - ADF RECEPTION AND INDICATION (HSI)  CHECK INDICATIONS,LIGHTS AND FLAGS ON RECEIVERS  AND INDICATORS.  345500-0503-1 210 VOR (VHF OMNI RANGE) ELO OPC I: 2 A MRB ** AMM 345500/5 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 345500-0503-1 * * * * * C O N T I N U E * * * * *  OPERATIONAL TEST OF VOR SYSTEM BY BITE  345500-0503-2 210 VOR (VHF OMNI RANGE) ELO OPC I: 2 A MRB AMM 345500/5 BITE TEST OF VOR 1 AND 2 TO COVER OPERATIONAL TEST OF  FOLLOWING FUNCTIONS:  -VOR RECEPTION AND INDICATION  (RDMI,HSI COURSE POINTER)  -MARKER BEACON MONITORING  CHECK INDICATIONS,LIGHTS AND FLAGS ON  RECEIVERS AND INDICATORS.  345600-0503-1 210 OMEGA NAVIGATION SYSTEM ELO OPC I: 2 A MPD AMM 345600/5 TEST OF ONS 1 AND 2 USING THE TEST KNOB ON ONS  CONTROL DISPLAY UNITS.  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : NAVIGATION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 351111-0502-1 132 CYLINDER - OXYGEN STORAGE INS GVI I: 1 A MRB AMM 351300/6 CHECK CREW OXYGEN BY COMPARING PRESSURE INDICATOR  WITH GAUGES ON OXYGEN CYLINDERS IN FWD CARGO  COMPARTMENT.  351111-0504-1 132 CYLINDER - OXYGEN STORAGE INS RAR I: NOTE 5-3 MRB ** AMM 351111/4 OR  REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST 3 YE  ACCESS: 132BZ  351200-0502-1 132 OXYGEN DISCHARGE DISCS INS GVI I: DY-TERM MRB AMM 351100/6 CHECK OXYGEN DISCHARGE DISCS ARE MAINTAINED  ON INDICATORS  351200-0503-1 132 OXYGEN DISTRIBUTION INS FUC I: 2 C MRB AMM 351000/5 LEAK TEST OF CREW OXYGEN SYSTEM:  01. CLOSE OXYGEN CYLINDER VALVE (ZONE 132)  02. MONITOR AT COCKPIT OXYGEN GAGES FOR CONSTANT  PRESSURE (ZONE 210)  03. OPEN OXYGEN CYLINDER VALVE (ZONE 132)  ACCESS: 132BZ 132CZ  351241-0502-1 210 MASK ASSY-CREW OXYGEN INS GVI I: 1 C MRB AMM 351241/7 GENERAL VISUAL INSPECTION OF CREW OXYGEN MASK (MASK  OUT OF THE BOX) FOR CLEANLINESS AND SATISFACTORY  CONDITION  351241-0502-2 210 MASK ASSY - CREW OXYGEN MEC GVI I: 6 MO ISB AMM 351241/4 ISB 35-0009  GENERAL VISUAL INSPECTION OF QUICK DONNING MASK  REGULATORS 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: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 351241-0503-2 210 MASK ASSY-CREW OXYGEN INS OPC I: DY-TERM MRB ** AMM 351241/5 "IN SITU" OPERATIONAL TEST OF CREW OXYGEN MASK  ASSEMBLY  351241-0504-1 210 MASK ASSY-CREW OXYGEN INS FUC I: 4 YE MRB AMM 351241/4 REMOVE QUICK DONNING OXYGEN MASKS AND PERFORM  FUNCTIONAL TEST OF DEMAND REGULATOR ASSEMBLY  (OFF AIRCRAFT)  352000-0503-1 200 PASSENGER OXYGEN SYSTEM INS FUC I: 6 C MRB ** AMM 352100/5 U1. FUNCTIONAL TEST OT AUTOMATIC RELEASE OF PASSENGER  OXYGEN MASKS  02. DETAILED INSPECTION OF MASKS, GENERATORS  (INCLUSIVE SENSITIVE TAPE) AND RELEASE CATCHES  NOTE: TO BE ACCOMPLISHED WITH 352000-0503-2.  352000-0503-2 200 PASSENGER OXYGEN SYSTEM INS OPC I: 2 C MRB ** AMM 352100/5 OPERATIONAL TEST OF PASSENGER MASK RELEASE:  01. SET ALL DOOR STOPS OF EMERGENCY OXYGEN CONTAINERS  TO THE "TEST" POSITION  02. ON "PASSENGER OXYGEN PANEL" SET GUARDED SWITCH  TO "MANUAL OVERRIDE" POSITION AND CHECK THAT  INDICATOR LIGHT "SYS.ACTUATED" COMES ON.  03. CHECK THAT ALL DOORS OF EMERGENCY OXYGEN CONTAIN-  ERS OPEN TO MAXIMUM PERMITTED BY DOOR STOPS  04. ON "PASSENGER OXYGEN PANEL" PRESS "RESET" PUSH  BUTTON AND CHECK THAT INDICATOR LIGHT GOES OFF.  05. CLOSE DOORS OF ALL EMERGENCY OXYGEN CONTAINERS  BY DEPRESSING THE SPRING LOADED LATCH WITH THE  MANUAL RELEASE TOOL  NOTE: TO BE ACCOMPLISHED WITH 352000-0503-1  352000-0504-1 200 PASSENGER OXYGEN SYSTEM INS RAR I: NOTE 5-1 MRB ** AMM 352113/4 SIL 35-003  REMOVE AND REPLACE OXYGEN GENERATORS  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : OXYGEN REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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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 353121/7 VISUAL INSPECTION OF FULL FACE SMOKE MASK FOR  SATISFACTORY CONDITION - CLEAN MASK AND CONTAINER IF  NECESSARY  353000-0502-2 200 PORTABLE OXYGEN INS GVI I: WEEKLY MRB AMM 353111/6 CHECK 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 353100/5 OPERATIONAL TEST OF PORTABLE OXYGEN SUPPLY AND  REGULATION:  01. TURN REGULATOR "ON-OFF VALVE" TO "ON" POSITION  02. CONNECT MASK TO THE DEMAND REGULATOR, PUT MASK ON  AND BREATH IN TO ENSURE THAT REGULATOR OPERATES  CORRECTLY  03. DISCONNECT MASK AND STORE IN CONTAINER  04. TURN REGULATOR "ON-OFF VALVE" TO "ON" POSITION  353000-0504-1 200 PORTABLE OXYGEN INS RAR I: NOTE 5-3 MRB ** AMM 353111/6 OR  REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST 5 YE  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : OXYGEN REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 361100/5 OPERATIONAL TEST OF TEMP HI WARNING CIRCUIT  361100-0503-2 210 ENGINE BLEED AIR SUPPLY SYS ENG OPC I: 3 A MRB AMM 361100/5 OPERATIONAL TEST OF PNEUMATIC SYSTEM CONTROLLER BY  BITE  361100-0503-3 210 ENGINE BLEED AIR SUPPLY SYS ENG OPC I: 5 A MRB ** AMM 361100/5 OPERATIONAL TEST OF MANIFOLD FAULT WARNING WITH BLEED  VALVE CONTROL SWITCH IN AUTO POSITION  361100-0503-4 210 ENGINE BLEED AIR SUPPLY SYS ERI OPC I: 5 A MRB ** AMM 361100/5 OPERATIONAL TEST OF MANIFOLD "LEAK" WARNING WITH  BLEED VALVE IN "AUTO" CONTROL MODE  361111-0503-1 210 VALVE ISOLATION ERI OPC I: 2 A MRB AMM 361100/5 OPERATIONAL TEST OF ENGINE BLEED AIR ISOLATION VALVE  ("X"-BLEED VALVE) IN "AUTO NORM" AND "AUTO ALT"  POSITION  361111-0503-2 210 VALVE ISOLATION ERI OPC I: 2 A MRB AMM 361100/5 OPERATIONAL TEST OF ENGINE BLEED AIR ISOLATION AND  CROSS BLEED VALVE ("X"-BLEED VALVE) IN "AUTO" AND  "MAN" (MANUAL) CONTROL MODES  361113-0504-1 410 LP CHECK VALVE MEC RAR I: 3000 FH MPD AMM 360000/4 420 SB GARRETT  CHECK THE FLAPPER BUSHING/HINGE PIN FOR WEAR. 123894-36-12 SIL 36-026  PREP.: VALVE TO BE REMOVED.  SYSTEMS AND POWERPLANT PROGRAM : PNEUMATIC REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 361113-0504-2 410 LP CHECK VALVE MEC CHK T: ENG. CHG ISB AMM 360000/4 420 OR SB GARRETT  CHK STOP TUBE FOR WEAR. 1200 HSN 123894-36-12 I: 3000 FH SIL 36-026  361115-0502-1 410 PRECOOLER - BLEED AIR MEC DET T: 8000 FH ISB AMM 361100/6 420 I: 1 C ISB 36-0031  DETAILED INSPECTION OF THE PRECOOLER DUCTS.  ACCESS: 413BL  423BL  361116-0502-1 450 VALVE-FAN AIR MEC DET T: 4 C MPD AMM 361116/6 460 I: 1 C SIL 36-023  DETAILED INSPECTION OF VORTEX GENERATOR  ASSEMBLY FOR INTEGRITY AND ABSENCE OF CRACKS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  361117-0503-1 413 VALVE-PNEUMA SYS OVERPRESS. ERI FUC I: 2 C MRB ** AMM 361117/5 423  FUNCTIONAL TEST OF PNEUMATIC SYSTEM OVERPRESSURE  VALVE  ACCESS: 413FL 423FL  414CR 424CR  361119-0502-1 453 ENGINE BLEED PRESS.SEN.LINE MEC DET I: 2 A MPD AMM 361114/6 463  DETAILED INSPECTION OF ENGINE BLEED PRESSURE  SENSING LINE FOR EVIDENCE OF CRACKS.  NOTE: PAY PARTICULAR ATTENTION TO SLIGHT CONTOUR  VARIATIONS (WAVES) AND SURFACE (SCORES AND  SMALL FOLDS)  ACCESS: 451AL  461AL  SYSTEMS AND POWERPLANT PROGRAM : PNEUMATIC REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 361121-0503-1 471 SENSOR-PNEUMA SYS TEMP CONT ERI FUC I: 4 C MRB AMM 361121/4 482  01. REMOVE TEMPERATURE CONTROL SENSOR.  02. CLEAN SENSOR AND INSPECT FOR SATISFACTORY  CONDITION.  03. PERFORM FUNCTIONAL TEST.  04. RE-INSTALL SENSOR.  05. PERFORM BITE TEST OF PNEUMATIC SYSTEM CONTROLLER.  ACCESS: 471AL  482AR  361200-0503-1 100 APU BLEED AIR SUPPLY SYSTEM ENG OPC I: 4 C MRB AMM 361200/6 300 AMM 361211/6 01. LEAK CHECK OF APU BLEED AIR SUPPLY DUCTING  02. OPERATIONAL CHECK OF APU BLEED AIR LP-CHECK VALVE  BY OPERATING MANUALLY THE FLAPPERS FOR FREEDOM OF  MOVEMENT  03. VISUAL INSPECTION OF COMPONENTS (CHECK-VALVES,  DUCTS, COUPLINGS) FOR GENERAL CONDITION,  CLEANLINESS AND SECURITY OF ATTACHMENTS.  ACCESS: 147FZ 151MF 161AF  312AR 313AL 315AL 316AR  361311-0502-1 143 GROUND CONNECTOR-HP ENG DET I: 4 C MRB AMM 361300/6 DETAILED INSPECTION OF GROUND CONNECTOR WITH  NIPPLE-CHECK VALVE ASSEMBLY FOR SATISFACTORY  CONDITION, SECURITY OF CAP AND ATTACHMENT CHAIN AND  CLEANLINESS.  ACCESS: 143FL  361415-0505-1 512 VALVE-LEADING EDGE VENT. MEC LUB I: 5 A MPD AMM 122257/0 612  LUBRICATE SPRING STRUT PLUNGER OF VENTILATION  VALVE  ACCESS: 512EB  612EB  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : PNEUMATIC REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 381100-0505-1 100 WATER STORAGE, DISTRIBUTION MEC RPL I: 2 A MRB AMM 381000/3 OR AMM 381200/5 01. FLUSH, REFILL AND STERILIZE THE POTABLE WATER NOTE 5-3  SYSTEM (INCLUDING WATER TAPS) AND  - CLEAN WASTE WATER PIPES IF NECESSARY -  02. PERFORM OPERATIONAL TEST OF POTABLE  WATER SYSTEM  ACCESS: 122BR 172BR  383000-0503-1 200 WASTE DISPOSAL MEC CLN I: 2 C MPD AMM 383000/3 CLEAN TOILET VENT LINES OF ALL  LAVATORIES  ACCESS: TOILET SHROUD  383100-0502-1 200 TOILET SYSTEM MEC GVI I: 1 C SIL SIL 38-013  VISUAL CHECK OF WASTE HOLDING TANK, LAVATORY FLOOR  AND WASTE LINE CONNECTION FOR SIGNS OF "BLUE FLUID"  LEAKAGE AND CHECK OF ADJACENT UNDERFLOOR AREA.  PREP: REMOVE TOILET SHROUD  ACCESS: 121DL 172AR  383100-0503-1 200 TOILET SYSTEM MEC OPC I: 2 A MRB AMM 383100/5 OR  OPERATIONAL TEST OF FLUSHING SYSTEM. NOTE 5-3  ACCESS: 121DL 172AR  383200-0502-1 200 WATER WASTE DRAIN MEC GVI I: 3 A MRB AMM 383215/4 CHECK OVERFLOWS AND PAN DRAIN FOR OBSTRUCTION  AND CLEAN IF NECESSARY  384100-0505-1 138 AIR SUPPLY FILTER MEC RAR I: 2 C MRB AMM 384112/3 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : WATER/WASTE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 384100-0505-1 * * * * * C O N T I N U E * * * * *  REPLACE FILTER ELEMENT AND CHECK TANK-PRESSURIZATION  SYSTEM AND COMPONENTS FOR CLEANLINESS AND  SATISFACTORY CONDITION  ACCESS: 131BZ 131CZ 132EZ  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : WATER/WASTE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 491200-0703-1 310 APU-MOUNTS ENG DET I: APU CHG MRB  01. DETAILED INSPECTION OF APU MOUNTS  02. DETAILED INSPECTION OF APU ATTACH FITTINGS  AND SUPPORT STRUCTURE AT FRAME 95, 97 AND 98  (SSI NO.530905) INTERNAL IN ZONES 315 AND 316  03. DETAILED INSPECTION OF FRAMES, STRINGERS  AND SKIN IN APU COMPARTMENT AREA FROM FRAME 95  TO 100 (SSI NO.530907) INTERNAL IN ZONES 315/316  ACCESS: 315AL 315AZ 316AR 316AZ 316BZ  491600-0703-1 313 AIR INTAKE SYSTEM ENG DET I: APU CHG MRB AMM 491000/4 314  DETAILED INSPECTION OF APU AIR INTAKE AREA,  DUCTS AND SUPPORTS FOR SATISFACTORY CONDITION,  CRACKS, WEAR, CORROSION AND SECURITY OF ATTACHMENTS.  ACCESS: 313AL  491600-0703-2 310 AIR INLET SCREEN ENG GVI I: 1000 AH MRB AMM 492000/7 VISUAL INSPECTION OF APU - AIR INLET SCREEN FOR  SATISFACTORY CONDITION AND CLEANLINESS  ACCESS: 313AL  491700-0702-1 316 ENGINE DRAIN SYSTEM ENG DRN I: 3 A MPD AMM 491700/6 DRAINAGE OF COLLECTOR SIGHT GLASSES  ACCESS: 315AL 316AR  492000-0703-1 315 APU COMPRESSOR, FIRST STAGE ENG DET I: 500 AH MRB AMM 492000/6 01. REMOVE THE AIR INTAKE DUCT OR REMOVE INSPECTION  PLUG FROM BOTTOM OF INLET CYLINDER  02. DETAILED INSPECTION OF LP COMPRESSOR  FIRST STAGE ROTOR BLADES FOR CRACKS, CORROSION  AND FOD OR PERFORM BOROSCOPE INSPECTION OF LP  COMPRESSOR 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: 
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A300 MAINTENANCE PLANNING D

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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 FREE  ROTATION.  ACCESS: 313AL 315AL 316AR  492000-0703-2 315 ENGINE - APU ENG DET I: 2000 FC CN CN  FAA AD 1977-163-IMP DETAILED INSPECTION OF 1 ST STAGE LP FAA AD 77-17 COMPRESSOR DISK SB G  TSCP700-49-A ACCESS: 315AL 316AR 2  493000-0703-1 315 ENGINE FUEL AND CONTROL ENG GVI I: 500 AH MRB AMM 493114/3 CHECK THAT THE FUEL FILTER DIFFERENTIAL PRESSURE  INDICATOR IS NOT PROTRUDING.  ACCESS: 315AL 316AR  493000-0703-2 315 ENGINE FUEL AND CONTROL ENG RAR I: 1000 AH MRB AMM 493114/3 - REMOVE THE PRIMARY FUEL FILTER AND INSPECT FOR  SATISFACTORY CONDITION AND PARTICLES  - INSTALL A NEW FILTER ELEMENT  ACCESS: 315AL 316AR N 493000-0703-3 315 APU FUEL SHROUD LINE ENG FUC I: 10 YE SIL AMM 493100/5 SIL 49-056  FUNCTIONAL CHECK (AIR PRESSURE CHECK) OF APU FUEL  SHROUD LINE  494000-0702-4 315 IGNITION AND STARTING ENG OPC I: 3 A MPD AMM 494000/5 TEST OF "SELF TEST" CAPABILITY FOR APU STARTER  CIRCUIT (USING TEST SWITCH 14 KA)  ACCESS: 315AL 316AR  SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 494000-0703-1 315 APU-IGNITER PLUGS ENG DET I: 500 AH MRB AMM 494212/2 01. REMOVE IGNITER PLUGS  02. CLEAN PLUGS  03. DETAILED INSPECTION OF IGNITER PLUGS  FOR CERAMIC CRACKING AND ALUMINIUM SPRAY DEPOSITS  04. INSPECT THREADS FOR CORROSION AND DAMAGE  05. REINSTALL IGNITER PLUGS.  ACCESS: 315AL 316AR  494000-0703-2 315 APU-ELECTRIC STARTER MOTOR ENG GVI I: 500 AH MRB AMM 494411/6 GENERAL VISUAL INSPECTION OF APU ELECTRICAL STARTER  MOTOR BRUSHES AND BRUSH LEADS FOR SATISFACTORY  CONDITION, WEAR, CORROSION AND DAMAGED LEADS.  ACCESS: 315AL 316AR  494000-0703-3 315 APU STARTER MOTOR CLUTCH ENG DET I: 1000 AH MRB AMM 494412/6 DETAILED INSPECTION OF APU STARTER MOTOR  CLUTCH COMPONENTS AND PAWL STROKE.  ACCESS: 315AL 316AR  495000-0703-1 316 AIR - BLEED ENG CLN I: 1000 AH MRB AMM 495114/3 REMOVE AIRFLOW SENSOR FOR CLEANING AND INSPECT  FOR CRACKS AND OBVIOUS DAMAGE  ACCESS: 315AL 316AR  495000-0703-2 316 AIR ENG DET I: 600 FH ISB AMM 495116/6 ISB 49-0031  DETAILED INSPECTION OF HOUSING (FLEXIBLE  COUPLING) BETWEEN SURGE BLEED VALVE AND AIR DUCT  SUPPORT STRUTS FOR WEAR  ACCESS: 315AL 316AR  SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 495000-0703-3 315 COOLING FAN ENG DET I: 500 AH MPD AMM 495211/6 DETAILED INSPECTION OF FAN IMPELLER FOR FOD  AND EVIDENCE OF OIL LEAKS.  INSPECT INLET DUCT FOR GENERAL CONDITION  PREP.: REMOVE COOLING FAN INLET DUCTING.  ACCESS: 315AL 316AR  495000-0703-4 315 APU COMPARTMENT ENG GVI I: 3 A MRB AMM 495200/6 VISUAL INSPECTION OF APU COMPARTMENT FOR GENERAL  CONDITION AND EXTERNAL LEAKS (DOOR OPEN)  ACCESS: 315AL 316AR  495000-0703-5 315 AIR ENG GVI I: 2A ISB ISB 49-0017  OR  REMOVE COOLING AIR INLET DUCT AND CHECK DUCT FOR APU CHG  SATISFACTORY CONDITION AND CRACKS - COOLING FAN  FOR F.O.D. AND OIL LEAKS  ACCESS: 315AL 316AR  495000-0703-6 316 SURGE AIR VALVE FILTER ENG CLN I: 500 AH MRB AMM 495113/3 REMOVE,INSPECT AND CLEAN THE SURGE AIR VALVE  FILTER AND FILTER SCREEN  ACCESS: 315AL 316AR  498000-0703-1 310 EXHAUST DUCT AND MUFFLER ENG DET I: APU CHG MRB AMM 491000/4 DETAILED INSPECTION OF APU EXHAUST DUCT  AND MUFFLER FOR SATISFACTORY CONDITION, CRACKS AND  CORROSION IN ZONES 315, 316, 317 AND 318  ACCESS: 315AL 316AR 317AL  SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 499000-0703-1 315 APU OIL QUANTITY INDICATION ENG DET I: APU CHG MPD AMM 499312/4 COMPARE BY READING OF QUANTITY INDICATOR IN  FLIGHT COMPARTMENT AGAINST DIPSTICK THE CORRECT  FUNCTIONING OF LIQUID QUANTITY TRANSMITTER  (AFTER APU REPLACEMENT)  ACCESS: 315AL 316AR  499000-0705-1 315 APU - OIL FILTER ENG RPL I: 500 AH MRB AMM 499112/3 AMM 499113/3 01. REMOVE OIL FILTER FOR INSPECTION AND CHANGE  FILTER ELEMENT  02. REMOVE MAGNETIC PLUG/CHIP DETECTOR FOR CONTAMINA-  TION CHECK OF OIL PER MAGNETIC PLUG FINDINGS  NOTE: CHANGE OIL IF OIL IS FOUND CONTAMINATED  DETERIORATED OR IF OIL BRAND IS CHANGED  ACCESS: 315AL 316AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : AUXILIARY POWER UNIT REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 513000-0502-1 100 FUSELAGE DRAIN VALVES MEC GVI I: C MPD AMM 513041/6 OR SIL 53-060  CHECK 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 VALVES  BETWEEN FR. 19 AND FR. 65,  FOR FREEDOM OF OBSTRUCTION ( FROM OUTSIDE ONLY )  NOTE: INSPECTION MAY BE NEED TO BE PERFORMED  MORE FREQUENTLY IN CERTAIN OPERATING  CONDITIONS  513000-0502-2 100 FUSELAGE DRAIN VALVES MEC DET I: 4 YE MPD AMM 513011/6 AMM 513021/6 DETAILED INSPECTION OF FUSELAGE DRAIN VALVES AMM 513031/6 (INCLUDING RUBBER SEALING FLAP) IN INTERNAL FUSELAGE AMM 513041/6 BILGE AREA (ZONE: 121/122, 133/134, 135/136, 143/144,  153/154, 164, 171/172, 311, 312).  NOTE: INSPECTION TO BE DONE AT THE OPPORTUNITY  OF ZONAL INSPECTIONS IN CORRESPONDING  ZONES  513000-0502-3 100 PRESSURE BULKHEADS DRAINS MEC GVI I: 1 C MPD AMM 513011/6 AMM 513041/6 CHECK DRAIN HOLES AT THE:  - LOWER AREA OF THE FORWARD PRESSURE BULKHEAD  - LOWER AREA OF THE AFT PRESSURE BULKHEAD  FOR FREEDOM OF OBSTUCTION (FROM INSIDE)  ACCESS: 132AZ 162AZ  513000-0502-4 311 FUSELAGE DRAIN MAST MEC OPC I: 4 MO SIL AMM 513041/6 312 OR SIL 53-060  CHECK FUSELAGE DRAINAGE AND DRAIN PATH AT DRAIN MAST NOTE  AFT OF FR 80 FOR FREEDOM OF OBSTRUCTION ( FROM  INSIDE)  NOTE: INSPECTION MAY BE NEEDED TO BE PERFORMED MORE  FREQUENTLY IN CERTAIN OPERATING CONDITIONS  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STRUCTURES REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 513000-0502-4 * * * * * C O N T I N U E * * * * *  ACCESS: 312AR  518061-0502-1 400 PYLON DRAINAGE MEC CHK I: 1 C MPD AMM 513061/6 OIT  CHECK PYLON UPPER SPAR DRAIN INLETS ST/999.0108/ FOR BLOCKAGE  518061-0502-2 400 PYLON DRAINAGE MEC BSI I: 2 C MPD AMM 513061/6 OIT  BOROSCOPE INSPECTION OF PYLON LOWER SPAR INLETS FOR ST/999.0108/ SIGNS OF CONTAMINATION  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STRUCTURES REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 520000-0502-1 800 DOORS AND PANELS MEC GVI I: 1 A MRB AMM 520000/6 AMM 522200/6 CHECK FUSELAGE DOORS AND SERVICE PANELS FOR  SATISFACTORY CONDITION  520000-0502-2 100 SERVICE PANELS MEC GVI I: 3 A MRB SIL 38-013  CHECK DRAIN AND FILLER CAPS ARE CORRECTLY INSTALLED  AND SEALS ARE SERVICEABLE.  NOTE: ACCESS 134 BR IS OPTIONAL ACCORDING TO GALLEY/  TOILETS CONFIGURATION.  ACCESS: 121DL 134BR 136BR 172AR  521000-0502-1 831 PASSENGER/CREW DOOR MEC DET I: 36 MO CN CN  832 1999-410-294 833 DETAILED INSPECTION OF DOOR DAMPER/EMERGENCY FAA AD  841 ACTUATOR STRIKER MECHANISM FOR CORROSION. 2003-03-04  842 ISB 52-0168  843  521000-0502-2 831 PASSENGER/CREW DOOR MEC DET I: 36 MO CN CN  841 1999-410-294 DETAILED INSPECTION OF DOOR DAMPER/EMERGENCY FAA AD  ACTUATOR STRIKER MECHANISM FOR CORROSION. 2003-03-04  ISB 52-0168  521014-0504-1 830 CYLINDER - DOOR DAMPER MEC RAR I: 18 MO CN AMM 521014/4 840 FAA AD CN  REMOVE PERCUSSION MECHANISM FROM EACH DOOR DAMPER 1989-092-095 AND INSPECT FOR CORROSION FAA AD 90-17 ISB 52-0130  NOTE: DEPENDING ON DAMPER TYPE,DAMPER MAY HAVE TO BE  REMOVED FROM DOOR FIRST  ACCESS: UPPER SUPPORT ARM LINING  SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 521022-0505-1 800 MECHANISM SLIDE RELEASE MEC LUB I: NOTE 5-2 MPD SIL 52-029  APPLY LPS 3 TO GIRT BAR SLIDERS AND FITTINGS  521031-0502-2 830 PASSENGER/CREW DOORS MEC DET I: 3000 FH ISB ISB 52-0014  840  WEAR CHECK OF PAX/CREW DOOR STOP  FITTINGS ON DOOR AND ON FUSELAGE.  521031-0502-3 830 PASSENGER/CREW DOORS MEC DET T: 12000 FH ISB ISB 52-0014  840 I: 9000 FH  WEAR CHECK OF PAX/CREW DOOR STOP  FITTINGS ON DOOR AND FUSELAGE STRUCTURE  521114-0502-1 830 CYLINDER - DOOR DAMPER MEC GVI I: 1 A MRB ** AMM 521014/6 840  CHECK DOOR DAMPER / EMERGENCY CYLINDER FOR  CORRECT PRESSURE  CAUTION: WHEN REFILLING A BOTTLE DO NOT EXCEED THE  MAXIMUM PRESSURE,INDICATED ON THE PLACARD  521114-0505-1 830 CYLINDER - DOOR DAMPER INP LUB I: 1 C MPD AMM 122252/0 840  LUBRICATE DAMPER/TELESCOPIC RODS OF  PASSENGER DOORS  521121-0503-1 830 MECHANISM - DOOR LOCKING MEC FUC I: 6 C MRB AMM 521020/6 840  ON THE LOCKING MECHANISM OF THE PASSENGER/CREW DOORS:  01. FUNCTIONAL TEST OF LOCKING MECHANISM ON DOORS  02. DETAILED INSPECTION OF INTERNAL LOCKING  MECHANISM FOR SATISFACTORY CONDITION,CORROSION,  WEAR AND SECURITY OF ATTACHMENT  PREP.: REMOVE LININGS.  521121-0505-1 830 MECHANISM - DOOR LOCKING MEC LUB I: 1 C MPD AMM 122252/0 840  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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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 521030/6 832 AMM 522222/6 833 01. REMOVE ESCAPE SLIDE AND DOOR LINING  834 02. PERFORM FUNCTIONAL TEST OF ESCAPE SLIDE RELEASE  841 MECHANISM  842 (FWD, MID, AFT PASSENGER/CREW DOORS AND  843 PASSENGER COMPARTMENT EMERGENCY EXIT  844 DOORS)  03. REINSTALL DOOR LINING AND ESCAPE SLIDE  521131-0505-1 831 FWD PAX DOOR LATCHING LINK. MEC LUB I: 1 C MPD AMM 521022/4 841 SIL 52-030  LUBRICATE LATCHING LINKAGE ASSEMBLY ROD  PREP.: REMOVE DOOR LININGS  522221-0503-1 834 LOCKING MECHANISM,EMER.EXIT MEC FUC I: 6 C MRB AMM 522200/6 844 AMM 522213/4 01. DO A FUNCTIONAL TEST OF LOCKING MECHANISM OF AMM 522221/6 EMERGENCY EXIT DOORS.  02. REMOVE ESCAPE SLIDES, LININGS AND INSULATION  03. DO A DETAILED INSPECTION OF INTERNAL  LOCKING MECHANISM FOR SATISFACTORY CONDITION,  CORROSION, WEAR AND SECURITY OF ATTACHMENT  04. REINSTALL ESCAPE SLIDES, LININGS AND ISOLATION  522231-0502-2 834 PASSENGER COMPARTMENT EMERGENCY EXIT MEC DET T: 12000 FH ISB ISB 52-0014  844 I: 6000 FH  WEAR CHECK ON EMERGENCY EXIT DOOR STOP FITTINGS ON  DOOR AND ON FUSELAGE.  522231-0502-3 834 PASSENGER COMPARTMENT EMERGENCY EXIT MEC DET T: 12000 FH ISB ISB 52-0014  844 I: 9000 FH  WEAR CHECK ON EMERGENCY EXIT DOOR STOP FITTINGS ON  DOOR AND FUSELAGE STRUCTURE  SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 523011-0502-1 811 CARGO COMPARTMENT DOORS MEC GVI I: 2400 FC ISB ISB 52-0048  812  REMOVE AND CHECK SHEAR BOLT OF ACTUATOR  ATTACHMENT FITTING AT CARGO DOORS FOR CRACKS  523011-0504-1 811 CARGO COMPARTMENT DOORS MEC RAR I: 4800 FC ISB ISB 52-0048  812  REPLACE SHEAR BOLT OF ACTUATOR ATTACHMENT FITTING  AT CARGO DOOR  523100-0505-1 811 FWD CARGO COMPARTMENT DOOR MEC LUB I: 1 C MPD AMM 122252/0 LUBRICATE THE FOLLOWING CARGO COMPARTMENT DOOR  COMPONENTS:  - 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  523121-0503-1 811 LOCK.MECHANM.FWD CARGO DOOR MEC FUC I: 3 C MRB ** AMM 523021/6 - FUNCTIONAL TEST OF LOCKING MECHANISM  - VISUAL INSPECTION OF INTERNAL DOOR LOCKING  MECHANISM  ACCESS: 811AR 811BR 811CR 811DR  523200-0505-1 812 AFT CARGO COMPARTMENT DOOR MEC LUB I: 1 C MPD AMM 122252/0 LUBRICATE THE FOLLOWING CARGO COMPARTMENT DOOR  COMPONENTS:  - 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  523221-0503-1 812 LOCK.MECHANM.AFT CARGO DOOR MEC FUC I: 3 C MRB ** AMM 523021/6 - FUNCTIONAL TEST OF LOCKING MECHANISM  - VISUAL INSPECTION OF INTERNAL DOOR LOCKING  MECHANISM  ACCESS: 812AR 812BR 812CR 812DR  523307-0502-1 811 ACTUATOR ATTACHMENT FITTING CARGO DOOR NDT SDI I: ISB ISB ISB 52-0101  52-101  DETAILED CHECK AND SPECIAL DETAILED INSPECTION  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 523300/6 812  OPERATIONAL TEST OF CARGO DOOR SEQUENCE VALVE  523351-0502-1 835 ACTUATOR - DOOR, UDC COMPARTMENT MEC GVI I: 5 A MRB ** AMM 523600/5 01. PERFORM GAP-CHECK OF HOOK  02. CHECK THAT THE HYDRAULIC PRESSURE HOLDS THE DOOR  IN SELECTED POSITIONS BY VISUAL OBSERVATION  523351-0503-1 835 ACTUATOR - DOOR, UDC COMPARTMENT MEC OPC I: 1 C MRB ** AMM 523600/5 CHECK FOR CORRECT OPERATION OF DETENT HOOK IN  SELECTED POSITIONS (70 DEG. AND 145 DEG.) WITH  BYPASS CHECK VALVE MANUALLY OPENED.  523400-0502-1 813 BULK CARGO COMPARTMENT DOOR MEC GVI I: 6 C MPD AMM 523441/6 ON THE BALANCE MECHANISM:  01. INSPECT MECHANISM FOR CORROSION AND GENERAL  CONDITION  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 523400-0502-1 * * * * * C O N T I N U E * * * * *  02. CHECK FORCE REQUIRED TO OPERATE MECHANISM  523400-0505-1 813 BULK CARGO COMPARTMENT DOOR MEC LUB I: 1 C MPD AMM 122252/0 LUBRICATE THE FOLLOWING CARGO COMPARTMENT DOOR  COMPONENTS:  - ROD EYE END BOLTS,UNIVERSAL JOINT AND FLANGE  ASSEMBLY BEARING AT MAIN SHAFT OF LOCKING MECHA-  NISM  - DOOR OPERATING HANDLE MECHANISM  - SPRING HOOK/BOX ASSEMBLY  PREP.: REMOVE DOOR LININGS  523500-0503-1 200 ELECTR. CONTR. SYST. DOORS MEC OPC I: WEEKLY MRB AMM 527111/5 OPERATIONAL TEST OF MONITORING SYSTEM (DOOR TEST  SWITCH) OF THE ELECTRICAL CONTROL AND DOORWARNING  SYSTEM  523500-0503-2 835 ELEC.CONT.SYS.(UDC-DOOR) ERI OPC I: 5 A MRB AMM 523600/5 UDC-COMPARTMENT DOOR - ELECTRICAL CONTROL AND DOOR  WARNING SYSTEM  - CHECK ELECTRICAL CUT-OFF FROM THE UDC-DOOR TO MID  PASSENGER/CREW DOOR  CAUTION: TO AVOID DAMAGE TO UDC-COMPARTMENT DOOR  AND LH MID PASS./CREW DOOR, DO NOT FULLY  OPEN LH MID PASS./CREW DOOR.  523600-0502-1 835 MAIN DECK CARGO DOOR MEC DET I: 500 FH AOT AOT 52-11  DETAILED INSPECTION OF MAIN DECK CARGO DOOR  - SLEEVES AT DOOR ACTUATOR ATTACHMENT POINTS FOR  DENTS  - ROD EYE ENDS FOR CRACKS AND DENTS.  SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 523600-0505-1 835 UDC - COMPARTMENT DOOR MEC LUB I: 5 A MPD AMM 122252/0 LUBRICATE THE FOLLOWING UDC-COMPARTMENT DOOR  COMPONENTS:  - 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  835GR  523619-0503-1 835 LOCKING MECHANISM - UDC DOOR MEC OPC I: 5 A MRB AMM 523600/5 OPERATIONAL TEST OF SAFETY LEVER AND DOOR  LOCKING/UNLOCKING MECHANISM TO ENSURE PROPER  OPERATION OF DECOMPRESSION FLAP AND VISUAL (RED) DOOR  LOCKING INDICATOR BUTTONS  523619-0503-2 835 LOCKING MECHANISM - UDC DOOR MEC FUC I: 3 C MRB AMM 523600/5 FUNCTIONAL TEST OF DOOR LOCKING/ UNLOCKING MECHANISM  524200-0505-1 121 FWD TOIL.SERVICE PANEL MEC LUB I: 3 A MPD AMM 122252/0 LUBRICATE SPRING DEVICE (HOLD OPEN MECHANISM)  OF PANEL 121DL  ACCESS: 121DL  524215-0502-1 120 FWD CARGO COMPT DOOR CONTL NDT SDI I: 500 FC ISB ISB 52-0151  SPECIAL DETAILED INSPECTION OF ACCESS PANEL HINGES OF  FWD CARGO DOOR CONTROL PANEL FOR CRACKS.  ACCESS: 122DR  SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 527300-0503-1 800 EMERG ESCAPE SLIDE WARNING ELO OPC I: 1 C MPD AMM 527300/5 OPERATIONAL TEST OF ESCAPE SLIDE RELEASE WARNING  SYSTEM (FLASHING WARNING LIGHT AND BUZZER TONE)  IN ZONE 831/841, 832/842, 834/844 AND 833/843.  ACCESS: 831  527300-0503-2 800 RESIDUAL PRESSURE WARNING ELO FUC I: 1 C SIL AMM 527300/5 SIL 52-043  01. OPERATIONAL TEST OF RESIDUAL CABIN  PRESSURE WARNING.  02. FUNCTIONAL TEST OF ASSOCIATED  PRESSURE SWITCH.  IN ZONE 831/841, 832/842, 834/844,  833/843 AND 100.  ACCESS: 131AZ 811 811CR 812CR 831  527300-0503-3 121 RESIDUAL PRESSURE WARNING ELO FUC I: 4 A SIL AMM 527300/5 SIL 52-043  01. CAPACITY TEST OF AUTONOMOUS  STANDBY SUPPLY UNIT.  02. BITE TEST OF AUTONOMOUS STANDBY  POWER SUPPLY UNIT.  ACCESS: 131AZ 811  528212-0503-1 715 SECONDARY NOSE LANDING GEAR DOORS NDT SDI T: 8000 FC CN NTM 528211  716 I: 700 FC FAA AD PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF NLG OR CN  DOOR HINGE FITTINGS. NOTE 1995-011-174 FAA AD 95-12 NOTE: AS AN ALTERNATIVE COMPLIANCE, REMOVE AND ISB 52-0161  REPLACE NLG DOOR FITTINGS AT INTERVAL 8000 FC.  ACCESS: 713  714  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 530000-0502-1 100 FUSELAGE GENERAL MEC GVI I: PRE-ACPT MRB  VISUAL INSPECTION OF FORWARD AND AFT FUSELAGE FROM  GROUND FOR GENERAL CONDITION AND POSITIVE LOCKING OF  FORWARD, 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 MRB  VISUAL INSPECTION OF EXTERNAL APU AREA, HORIZONTAL  STABILIZER (INCLUDING ELEVATORS AND RUDDER) FROM  GROUND FOR GENERAL CONDITION, VISIBLE DAMAGE, LEAKS  AND APU BAY DOORS CLOSED. CHECK TAIL SKID NOT DAMAGED  530000-0502-3 100 FUSELAGE GENERAL MEC GVI I: DY-TERM MRB  VISUAL INSPECTION OF EXTERIOR FUSELAGE, INLETS/  OUTLETS, TEMPERATURE AND ANGLE OF ATTACK SENSORS  AND PITOT PROBES/STATIC PORTS FOR GENERAL CONDITION  AND DAMAGE.  531300-0502-1 220 FUSELAGE FORWARD SECTION MEC GVI T: 3 YE ISB ISB 53-0155  230 I: 3 YE  VISUAL INSPECTION OF FORWARD PASSENGER/CREW DOOR  FRAME AT FRAME 14 AND 16A AND MID PASSENGER/CREW DOOR  FRAME AT FRAME 28A AND 30A FOR CORROSION.  532411-0502-1 120 EXTENDING LADDER MEC FUC I: 1050 FH CN CN  FAA AD 1994-187-163 1. FUNCTIONAL CHECK OF LADDER FOR INTERFERENCE. FAA AD 95-10 2. DETAILED INSPECTION OF LADDER SUPPORT ISB 24-0087  SHAFT AND ATTACHMENT RIVETS.  NOTE: THIS TASK IS RELATED TO INSPECTION OF 104 VU  PANEL ELECTRICAL INSTALLATION REF TASK  240000-0503-1.  ACCESS: 121BL  SYSTEMS AND POWERPLANT PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 534212-0502-1 230 MID/PAX DOOR ATTACH FITTG. MEC GVI T: 4000 FC ISB ISB 53-0165  I: 2000 FC  DETAILED INSPECTION OF THE GUIDE ARM SUPPORT  FITTINGS AT THE UPPER DOOR FRAME OF THE MID/PASSENGER  CREW DOOR  534600-0505-1 319 HORIZ. STAB. ATTACH FITTING MEC LUB I: 1 C MPD AMM 122253/0 LUBRICATE HORIZONTAL STABILIZER HINGE BEARING  SUPPORT FITTINGS  ACCESS: 313AL  534700-0502-1 311 TAIL CONE ATTACH FITTING MEC GVI I: 2 YE MPD SIL 53-043  01. CHECK FOR CLEANLINESS OF DRAIN HOLE AT FRAME 91.  02. APPLY CORROSION INHIBITOR AND WATER REPELLENT  ON CENTERING FITTINGS.  535100-0502-1 110 RADOME MEC GVI I: PRE-ACPT MRB  VISUAL INSPECTION OF RADOME FOR DAMAGE  535112-0505-1 110 LATCH-RADOME ADJUST. HOOK MEC LUB I: 1 C MPD AMM 122253/0 LUBRICATE CABLE ASSY AND LOCKING MECHANISM  MOVING PARTS (ENSURE NO PAINT ON LOCKING HOOK)  ACCESS: 110AL  535300-0502-2 311 THS APRON TRAVEL AREA MEC GVI T: 1600 FH ISB ISB 53-0068  312 I: 400 FH  313 GENERAL VISUAL CHECK OF TRIMMABLE HORIZONTAL  314 STABILIZER APRON TRAVEL AREA FOR GENERAL CONDITION,  SCRATCHES AND DAMAGE  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 540000-0502-1 470 NACELLE/PYLON MEC DET I: 1 C ISB ISB 54-0029  480  DETAILED INSPECTION OF PIPES, CLAMPS AND  SUPPORTS FOR DAMAGE AND SECURITY OF ATTACHMENT  ACCESS: 413AL 413BL 413EL 413FL 414BR 435AL  475AL 475BL 475CL 475DL 476AR 476BR  423AL 423BL 423EL 423FL 424BR 445AL  485AL 485BL 485CL 485DL 486AR 486BR  540000-0502-2 470 LOWER AFT PYLON ENG GVI I: 1 A MRB AMM 543000/6 480  CHECK LOWER AFT PYLON FOR CORROSION, CRACKS,  FUEL LEAKS, SECURITY OF FASTENERS AND DETERIORATION  OF TREATMENT  541000-0502-1 470 ENGINE PYLON MEC GVI I: 3000 FH ISB ISB 54-0042  480  VISUAL INSPECTION OF SPIGOT BALL JOINT TO MAKE  CERTAIN THAT THE AIR-FLON LINER IS IN PLACE  ACCESS: 471AL 472AR 473AL  481AL 482AR 484AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 551100-0505-1 319 HORIZ.STABILIZER HINGE PINS MEC LUB I: 1 C MPD AMM 122255/0 LUBRICATE HINGE PINS OF TRIMMABLE HORIZONTAL  STABILIZER  ACCESS: 313AL  552111-0504-1 334 ELEVATOR SERVO CONTROLS MEC RAR I: 6000 FH ISB ISB 55-0032  344  REPLACE ABRASION WASHERS AND BUSHES OF  ELEVATOR SERVO CONTROLS AT ELEVATOR HINGE FITTINGS  ACCESS: 334BB 335BB  344BB 345BB  553645-0505-1 326 RUDDER HINGE BEARING NO.4 MEC LUB I: 1 C MPD AMM 122227/0 SIL 55-019  LUBRICATE RUDDER HINGE BEARING NO.4  ACCESS: 325DL 326DL  555100-0503-1 334 ELEVATOR HINGE ARMS MEC OPC I: 4 C MPD AMM 555000/6 344 SIL 55-023  CHECK PLAY AT EACH BEARING LOCATION AT TRAILING EDGE  OF TRIMMABLE HORIZONTAL STABILIZER.  ACCESS: 334BT 334DT 334FT 334HT 334KT  344BT 344DT 344FT 344HT 344KT  555200-0503-1 335 ELEVATOR ATTACH FITTINGS MEC OPC I: 4 C MPD AMM 555000/6 345 SIL 55-023  CHECK PLAY AT EACH BEARING LOCATION AT LEADING EDGE  OF ELEVATOR.  ACCESS: 334AB 334BB 334CB 334DB 334EB  344AB 344BB 344CB 344DB 344EB  555300-0503-1 325 RUDDER HINGE ARMS MEC OPC I: 4 C MPD AMM 555000/6 SIL 55-023  CHECK 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: 
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A300 MAINTENANCE PLANNING D

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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  555400-0503-1 326 RUDDER ATTACH FITTINGS MEC OPC I: 4 C MPD AMM 555000/6 SIL 55-023  CHECK PLAY AT EACH BEARING LOCATION AT LEADING EDGE  OF RUDDER.  ACCESS: 326AL 326AR 326BL 326BR 326CL 326CR  326DL 326DR 326EL 326ER  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 561000-0502-1 210 COCKPIT WINDOWS MEC DET I: 1 A MRB AMM 561111/6 SIL AMM 561112/6 DETAILED INSPECTION OF ALL COCKPIT WINDOWS AMM 561211/6 FROM INSIDE SIL 56-017  561100-0502-1 210 COCKPIT FIXED SIDE WINDOWS MEC DET I: 1 C MPD AMM 561112/6 SIL 56-011  DETAILED INSPECTION OF COCKPIT SIDE WINDOWS IN  AREA OF BUS BARS  NOTE: FROM INSIDE COCKPIT  561100-0502-2 210 COCKPIT FIXED SIDE WINDOWS MEC DET I: 7 DAYS CN AMM 561112/6 FAA AD CN  DETAILED INSPECTION OF COCKPIT FIXED SIDE ISB 1994-104-160 WINDOWS FOR EVIDENCE OF ELECTRICAL ARCING. FAA AD 94-10 ISB 56-0008  NOTE: 01. EFFECTIVITY DEPENDS ON P/N OF INSTALLED SIL 56-011  WINDOWS, 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 56-017  SIL  DETAILED INSPECTION OF ALL COCKPIT WINDOWS  FROM OUTSIDE  561200-0502-1 210 COCKPIT SLIDING WINDOWS MEC DET I: 2 C SIL SIL 56-017  DETAILED INSPECTION OF WINDOW SEALS.  561200-0505-1 210 COCKPIT SLIDING WINDOWS MEC LUB I: 4 A MPD AMM 122256/0 SIL 56-009  CLEANING AND LUBRICATION OF COCKPIT SLIDING WINDOW  MECHANISM AND TRACKS  ACCESS: SLIDING WINDOW OPENED  SYSTEMS AND POWERPLANT PROGRAM : WINDOWS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 562100-0502-1 200 PASS. COMPARTMENT WINDOWS MEC GVI I: 1 C ISB ISB 56-0002  VISUAL INSPECTION OF CABIN WINDOWS IN PASSENGER  COMPARTMENT AND ALL DOORS  (ZONE 800) FOR BULGING, CRAZING AND SCRATCHES.  562100-0502-2 200 PASS. COMPARTMENT WINDOWS MEC GVI I: 1000 FH ISB ISB 56-0007  VISUAL INSPECTION OF CABIN WINDOWS IN PASSENGER  COMPARTMENT AND ALL DOORS  (ZONE 800) FOR BULGING, CRAZING AND SCRATCHES.  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : WINDOWS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 570000-0502-1 500 WING MEC GVI I: PRE-ACPT MRB  600  01. CHECK LOWER SURFACE FROM GROUND AND UPPER SURFACE  THROUGH CABIN WINDOWS OF WING EXTERIOR AND  LEADING EDGE SLATS FOR GENERAL CONDITION AND FUEL  LEAKAGE  02. CHECK WING TRAILING EDGE, AILERONS, SPOILERS,  AIRBRAKES, FLAPS AND FLAP TRACK FAIRINGS FOR  GENERAL CONDITION, DAMAGE AND SIGNS OF LEAKS  570000-0502-2 513 WING MEC GVI I: PRE-ACPT MRB  613  CHECK KRUEGER FLAP AND SLOT FLAP FOR GENERAL  CONDITION  570000-0502-3 500 WING MEC GVI I: 3 A MRB AMM 570000/6 600  CHECK WING EXTERIOR FOR DAMAGE, GENERAL CONDITION,  VORTEX GENERATORS, SLAT SEALS AND SHUTTERS FOR  COMPLETENESS (SLATS EXTENDED).  571119-0504-1 571 MLG-PICK UP AT RIB 5 MEC DET I: AT LDG. MRB AMM 574211/6 671 GEAR CHG  CLEAN AREA AND CARRY OUT DETAILED INSPECTION  OF 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 574211/6 671 GEAR CHG  CLEAN AREA AND CARRY OUT DETAILED INSPECTION  OF MAIN LANDING GEAR RETRACTION ROD ATTACHMENTS AND  LINKS AT RIB 5.  571127-0504-1 571 MLG-PICK UP AT REAR SPAR MEC DET I: AT LDG. MRB AMM 574211/6 671 GEAR CHG  CLEAN AREA AND CARRY OUT DETAILED INSPECTION  OF 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 574211/6 671 GEAR CHG  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571138-0504-1 * * * * * C O N T I N U E * * * * *  CLEAN AREA AND CARRY OUT DETAILED INSPECTION  OF MAIN GEAR PIVOT PICK-UP LUGS AT RIB 5, AFT OF  REAR SPAR.  572030-0502-1 731 MAIN LANDING GEAR ATTACHMENT MEC DET T: 9 YE ISB ISB 57-0212  741 I: 5 YE  DETAILED INSPECTION OF THE FORWARD AND AFT  FACES OF:  - MAIN LANDING GEAR ATTACHMENT LUGS  - FORWARD CROSS BRACE ATTACHMENT LUG  - AFT CROSS BRACE ATTACHMENT LUG  PREP.:MAIN LANDING GEAR REMOVED.  572500-0502-2 500 FLAP TRACK BEAMS MEC DET I: 2400 FC ISB ISB 57-0122  600  CHECK BOLTS AT FLAP TRACK BEAM NO. 2, 3, 4, 5 AND 6  FORWARD ATTACHMENT BRACKETS FOR LOOSENESS AND  RETIGHTEN AS NECESSARY  ACCESS: MOVABLE AND FIXED FARINGS  572500-0505-1 500 FLAP TRACK BEAM NO. 1 TO 6 MEC LUB I: 5 A MPD AMM 572511/7 600  01. CLEAN CHANNELS WITH LINT-FREE CLOTH  02. CHECK FOR CORROSION  03. RE-APPLY GREASE MIL-G-23827  NOTE: IN CASE OF CORROSION PITS WITHIN  ALLOWABLE LIMITS, ARDOX 3302 MUST BE  APPLIED ON CORROSION PITS BEFORE  GREASING, AS TEMPORARY PROTECTION  BEFORE REPAIR  572512-0502-1 532 FLAP TRACK BEAM NO.2 TO 6 MEC DET T: REFER CN CN CN  632 I: 700 FC FAA AD 1987-121-081 DETAILED INSPECTION OF BOLTING AT THE AFT FAA AD 88-22 ATTACHMENT OF FLAP TRACK BEAMS 2 TO 6. ISB 57-0150  SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 573100-0505-1 500 ACCESS DOORS MEC LUB I: 1 C MPD AMM 122257/0 600  LUBRICATION OF PIANO HINGES OF ACCESS DOORS AND  SPRING STRUT PLUNGER (INNER DEFLECTORS FLAP).  NOTE: -FLAP TO BE EXTENDED TO GAIN ACCESS TO  PIANO HINGES  -ACCESS TO INNER FLAP DEFLECTOR SPRING  STRUT PLUNGER IF GAINED THROUGH ACCESS  PANELS LOCATED IN MLG WHEEL ON REAR  FALSE BAR  ACCESS: 572FB 572KB 572PB  672FB 672KB 672PB  573111-0503-1 500 DOOR-ACCESS-WING SKIN,LH/RH MEC FUC I: 10000 FH MRB AMM 281114/5 600 OR ISB 57-0089  BONDING CHECK OF NON-LOAD CARRYING FUEL TANK MANHOLE 5 YE  COVERS  573111-0503-2 500 DOOR ACCESS WING SKIN,LH/RH MEC FUC I: 6300 FH ISB AMM 281114/5 600 OR ISB 57-0089  BONDING CHECK OF NON-LOAD CARRING FUEL TANK MANHOLE 3 YE  COVERS  574413-0505-1 500 ALL SPEED AILERON HINGES MEC LUB I: 5 A MPD AMM 122227/0 600  LUBRICATION OF ALL HINGE BEARINGS OF ALL SPEED  AILERON AND SERVO CONTROL ATTACHMENT POINTS  ACCESS: 575CB 575GB  675CB 675GB  574414-0502-1 582 ATTACHMENT OUTER AIRBRAKE LH/RH MEC GVI I: 3 A ISB ISB 57-0052  583  682 GENERAL VISUAL CHECK OF OUTER AIRBRAKE  683 INNERMOST OUTER HINGE BRACKETS FOR CRACKS  SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 574600-0505-1 520 ATTACHMENT-FLIGHT SURFACES MEC LUB I: 3 A MRB AMM 122227/0 620  CLEAN, INSPECT AND LUBRICATE:  - SLAT TRACK ROLLERS (BRUSH APPLICATION)  - SLAT TRACKS  - SLAT TRACK ROLLER PINS  ACCESS: 512CB 523DB 523KB 524DB 524JB  612CB 623DB 623KB 624DB 624JB  574600-0505-2 500 ATTACHMENT-FLIGHT SURFACES MEC LUB I: 1 C MPD AMM 122257/0 600  LUBRICATION OF THE SLAT TO TRACK ATTACHMENT BOLTS  ACCESS: SLAT EXTENDED  574600-0505-3 500 ATTACHMENT-FLIGHT SURFACES MEC LUB I: 1 C MPD AMM 122227/0 600  LUBRICATION OF CLOSING PLATE SPRING STRUT PLUNGER  ACCESS: 512FB  612FB  575000-0502-1 500 FLIGHT SURFACES MEC GVI I: 1 A ISB ISB 57-0076  600  CHECK TAPE AT SLAT LEADING EDGE SKIN SPLICES  FOR PRESENCE  575900-0505-1 500 FLAP DEFLECTORS MEC LUB I: 3 A MPD AMM 122257/0 600  LUBRICATION OF PIANO HINGES ON:  - FLAPS DEFLECTOR DOORS AT INBOARD, INTERMEDIATE AND  OUTER POSITION. (FLAPS MUST BE EXTENDED)  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 711000-0802-1 450 COWLINGS ENG DET I: NOTE MPD AMM 711300/3 460  01. CHECK CORRECT OPERATION AND TENSION OF FAN  AND THRUST REVERSER COWL LATCHES  02. DETAILED INSPECTION OF HINGED AND SLIDING  COWLS FOR SECURITY OF ATTACHMENT, SEALS FOR  SCRAPES, BINDING, FLUID STREAKING  03. INSPECT COWL DOORS INNER AREA FOR EVIDENCE OF  CRACKS, HOT SPOTS AND DISTORTION  NOTE: TASK DUE AT ENGINE CHANGE OR ONE YEAR  OR 2000 FH WHICHEVER OCCURS FIRST  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  711000-0802-2 430 COWLINGS ENG FUC I: 1 C MPD AMM 711300/3 440  FAN COWL LATCH TENSION CHECK  ACCESS: 435AL 436AR  445AL 446AR  711000-0812-1 450 COWLINGS ENG DET I: ENG. CHG MPD AMM 711300/3 460 OR NOTE  01. CHECK CORRECT OPERATION AND TENSION OF FAN  AND THRUST REVERSER COWL LATCHES  02. DETAILED INSPECTION OF HINGED AND SLIDING  COWLS FOR SECURITY OF ATTACHMENT, SEALS FOR  SCRAPES, BINDING, FLUID STREAKING  03. INSPECT COWL DOORS INNER AREA FOR EVIDENCE OF  CRACKS, HOT SPOTS AND DISTORTION  NOTE: TASK DUE AT ENGINE CHANGE OR ONE YEAR  OR 2000 FH WHICHEVER OCCURS FIRST  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  711000-0812-2 430 COWLINGS ENG FUC I: 1 C MPD AMM 711305/5 440  FAN 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 711000-0812-2 * * * * * C O N T I N U E * * * * *  ACCESS: 435AL 436AR  445AL 446AR  711100-0802-1 430 NOSE COWL ENG GVI I: WEEKLY MPD AMM 711100/6 440  VISUAL INSPECTION OF NOSE COWL FOR LIP SKIN CRACKS  AND SATISFACTORY CONDITION  711100-0812-1 430 NOSE COWL ENG GVI I: WEEKLY MPD AMM 711100/6 440  VISUAL INSPECTION OF NOSE COWL FOR LIP SKIN CRACKS  AND SATISFACTORY CONDITION  711300-0802-1 430 COWL DOORS ENG GVI I: PRE-ACPT MRB  440  CHECK ALL R/H AND L/H ENGINE COWLS CLOSED AND  LATCHED  711300-0805-1 450 COWL DOORS ENG LUB I: 1 C MPD AMM 122271/0 460  CLEAN AND LUBRICATE LATCHES OF:  - FAN COWL DOORS  - THRUST REVERSER DOORS  - CORE COWL DOORS  - PRESSURE RELIEF DOORS  ACCESS: 435AL 435CL 436AR 451AL 451CL 452AR  455AL 455BL 456AR 456BR  445AL 445CL 446AR 461AL 461CL 462AR  465AL 465BL 466AR 466BR  711300-0812-1 430 COWL DOORS ENG GVI I: PRE-ACPT MRB  440  CHECK ALL R/H AND L/H ENGINE COWLS CLOSED AND  LATCHED  SYSTEMS AND POWERPLANT PROGRAM : POWER PLANT REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 711300-0815-1 450 COWL DOORS ENG LUB I: 1 C MPD AMM 122271/0 460  CLEAN AND LUBRICATE LATCHES OF  - FAN COWL DOORS  - THRUST REVERSER DOORS  - PRESSURE RELIEF DOORS  ACCESS: 435AL 436AR 436DR 451AL 451CL 452AR  445AL 446AR 446DR 452AR 461AL 461CL  711301-0802-1 430 COWL CORE ENG GVI I: DY-TERM CN AMM 711300/5 440 FAA AD CN  CHECK CORE COWL DOOR LATCHES 1987-132-082 FAA AD  88-11-10R1  ISB 71-0054  712000-0802-1 450 MOUNTS-ENGINE ENG DET I: C MRB AMM 712000/6 460 OR AMM 722300/6 DETAILED INSPECTION OF: ENG. CHG  - THE FWD MOUNT, THE FRONT FLANGE OF THE HP  COMPRESSOR STATOR AND THE FAN FRAME ASSY FOR  SATISFACTORY CONDITION, SECURITY OF ATTACHMENTS  AND CORROSION  - THE AFT MOUNT, ATTACHMENT FITTINGS ON THE TURBINE  MID FRAME FOR SATISFACTORY CONDITION, SECURITY  OF ATTACHMENTS AND CORROSION  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  712000-0802-2 450 MOUNTS-ENGINE ENG NDT I: ENG. CHG MRB AMM 710000/4 460 CMM 712013/3 NDT INSPECTION OF FORWARD AND AFT ENGINE MOUNT BOLTS  AND RUNNING CHECK ON NUTS  712000-0812-1 450 MOUNTS-ENGINE ENG DET I: C MRB AMM 712002/4 460 OR AMM 712003/4 DETAILED 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FOR  SATISFACTORY CONDITION, SECURITY OF ATTACHMENTS  AND CORROSION.  - THE AFT MOUNT, ATTACHMENT FITTINGS ON THE ENGINE  FLANGES OF THE EXHAUST CASE FOR SATISFACTORY  CONDITION, SECURITY OF ATTACHMENTS AND CORROSION.  712000-0812-2 450 MOUNTS-ENGINE ENG NDT I: ENG. CHG MPD AMM 710000/4 460 CMM 712013/3 NDT INSPECTION OF FORWARD AND AFT ENGINE MOUNT BOLTS.  ( 4 BOLTS ATTACHING THE ENGINE FWD MOUNT TO THE  PYRAMID AND 4 BOLTS ATTACHING THE ENGINE AFT MOUNT TO  THE PYLON BEAM. )  712000-0812-3 450 MOUNTS ENGINE ENG FUC I: ENG. CHG MPD AMM 710000/4 460  RUNNING CHECK TORQUE OF FWD AND AFT ENGINE MOUNT  BOLTS AND NUTS  712003-0802-1 430 MOUNT - FORWARD ENG DET I: 750 FH CN CN  440 OR FAA AD 1995-225-IMP DETAILED INSPECTION OF ENGINE FORWARD MOUNT 350 FC MPD FAA AD 95-17 SIDE LINKS. SB GE 72-109 NOTE: TASK NOT REQUIRED IF SIDE LINKS REFURBISHED  WITH SERMETAL IN ACCORDANCE WITH  CF6-50 SB 72-1092 (SHOP MANUAL ESM 72-23-11)  ACCESS: 435AL 436AR  445AL 446AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : POWER PLANT REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 720000/7 GASPATH WATER WASH  720000-0802-1 430 ENGINE ENG GVI I: PRE-ACPT MRB  440  GENERAL VISUAL INSPECTION OF THE FOLLOWING AREAS FOR  CONDITION AND EVIDENCE OF FOREIGN OBJECT DAMAGE:  (COWLINGS CLOSED)  01. ENGINE INLET  - AIR INTAKE  - FAN ROTOR BLADES AND SPINNER (AND CHECK FREE  ROTATION BY HAND)  - N1 SPEED SENSOR AND AREA  - LOW PRESSURE COMPRESSOR INLET VANES  - ACOUSTIC PANELS  - ABRADABLE SHROUDS  02. FAN REVERSER  - DUCTS AND OUTLET GUIDE VANES  03. ENGINE OUTLET  - EXIT VANES  - ACOUSTIC PANELS  - EXHAUST DUCTS FOR FREEDOM OF FOREIGN OBJECT  720000-0802-2 450 ENGINE ENG GVI I: DY-TERM MRB  460  VISUAL INSPECTION OF THE FOLLOWING AREAS (COWLING  CLOSED)  01. COWLING INLET FOR GENERAL CONDITION  02. DRAIN MAST FOR OBSTRUCTION OR EVIDENCE OF  LEAKAGE  03. HYDRAULIC PUMPS SHAFT SEAL DRAIN OUTLET FOR  EVIDENCE OF LEAKAGE  04. COWLING OUTLET FOR GENERAL CONDITION  05. EXHAUST AREA FOR EVIDENCE OF OIL LEAKAGE  06. TAIL PIPE FOR METAL DEPOSIT  07. LAST LP TURBINE STAGE BLADES FOR GENERAL  CONDITION  720000-0802-3 430 ENGINE ENG GVI I: 3 A MRB C 440  VISUAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 STARTER  AIR SUPPLY)  - OIL  - IGNITION  - HYDRAULIC POWER  - ELECTRICAL POWER  - THRUST REVERSER DRIVE AND AIR SUPPLY  FOR SECURITY OF ATTACHMENT, GENERAL CONDITION, DAMAGE  AND FREEDOM FROM FUEL, OIL AND AIR LEAKS  ACCESS: 435AL 455AL 456AR  445AL 465AL 466AR  720000-0803-1 400 ENGINE ENG FUC I: AT SHOP MRB AMM 710000/4 VISIT  FUNCTIONAL BENCH TEST IN LIEU OF DISASSEMBLY FOR THE  FOLLOWING ENGINE ITEMS:  - MAIN FUEL PUMP  - MAIN ENGINE CONTROL  - PNEUMATIC DRIVE UNIT AND CONTROL  - OIL AND SCAVENGE PUMP  NOTE: REFER TO RULES 1 AND 2 (SECTION 8 INTRUDUCTION)  720000-0803-2 400 ENGINE ENG GVI I: AT SHOP MRB AMM 710000/4 VISIT  OPPORTUNITY INSPECTION AT SHOP DISASSEMBLY FOR  FOLLOWING 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 GEARBOX  NOTE: 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 720000/7 GASPATH WATER WASH  720000-0812-1 430 ENGINE ENG GVI I: PRE-ACPT MRB  440  GENERAL VISUAL INSPECTION OF THE FOLLOWING AREAS FOR  CONDITION AND EVIDENCE OF FOREIGN OBJECT DAMAGE:  (COWLINGS CLOSED)  01. ENGINE INLET  - AIR INTAKE  - FAN ROTOR BLADES AND SPINNER (AND CHECK FREE  ROTATION BY HAND)  - N1 SPEED SENSOR AND AREA  - LOW PRESSURE COMPRESSOR INLET VANES  - ACOUSTIC PANELS  - ABRADABLE SHROUDS  02. FAN REVERSER  - DUCTS AND OUTLET GUIDE VANES  03. ENGINE OUTLET  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 OBJECT  720000-0812-2 450 ENGINE ENG GVI I: DY-TERM MRB  460  VISUAL INSPECTION OF THE FOLLOWING AREAS (COWLING  CLOSED)  01. COWLING INLET FOR GENERAL CONDITION  02. DRAIN MAST FOR OBSTRUCTION OR EVIDENCE OF  LEAKAGE  03. HYDRAULIC PUMPS SHAFT SEAL DRAIN OUTLET FOR  EVIDENCE OF LEAKAGE  04. COWLING OUTLET FOR GENERAL CONDITION  05. EXHAUST AREA FOR EVIDENCE OF OIL LEAKAGE  06. TAIL PIPE FOR METAL DEPOSIT  07. LAST LP TURBINE STAGE BLADES FOR GENERAL  CONDITION  720000-0812-3 430 ENGINE ENG GVI I: 3 A MRB  440  VISUAL INSPECTION OF ENGINE COMPONENTS IN FOLLOWING  SYSTEMS:  - FUEL FEED  - ENGINE CONTROL AND INDICATING  - ENGINE VANE AND ENGINE BLEED AIR  - BLEED AIR AND PNEUMATIC (INCLUDING STARTER  AIR SUPPLY)  - OIL  - IGNITION  - HYDRAULIC POWER  - ELECTRICAL POWER  - THRUST REVERSER DRIVE AND AIR SUPPLY  FOR SECURITY OF ATTACHMENT, GENERAL CONDITION, DAMAGE  AND FREEDOM FROM FUEL, OIL AND AIR LEAKS  ACCESS: 435AL 455AL 456AR  445AL 465AL 466AR  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 720000-0813-1 400 ENGINE ENG FUC I: AT SHOP MRB AMM 710000/4 VISIT  FUNCTIONAL - BENCH TEST IN LIEU OF DISASSEMBLY FOR  FOLLOWING ENGINE ITEMS:  - MAIN FUEL PUMP  - FUEL CONTROL UNIT  - ENGINE VANE AND BLEED CONTROL  - PNEUMATIC DRIVE UNIT & CONTROL  NOTE: REFER TO RULES 1 AND 2 (SECTION 8 INTRODUCTION)  720000-0813-2 400 ENGINE ENG GVI I: AT SHOP MRB AMM 710000/4 VISIT  OPPORTUNITY INSPECTION AT SHOP DISASSEMBLY FOR  FOLLOWING 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 NOZZLE  GUIDE VANE ASSY  - REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY  - FRONT COMPRESSOR DRIVE TURBINE ROTOR AND STATOR  ASSY  - TURBINE EXHAUST CASE  - MAIN GEAR BOX AND DRIVE SHAFT ASSY  NOTE: REFER TO RULES 1 AND 2 (SECTION 8 INTRODUCTION)  722100-0802-1 430 FAN ROTOR ASSEMBLY MEC NDT T: REFER AD CN CN  440 I: REFER AD FAA AD 1991-053-IMP AN ULTRASONIC AND FLUORESCENT PENETRANT (FPI) FAA AD 91-01 INSPECTION OF THE STAGE 1 FAN DISK DOVETAIL POST. SB GE 72-999  722100-0802-2 430 FAN AND LP COMPRESSOR SECT. ENG DET I: 1 A MRB AMM 722100/6 440 AMM 722200/6 DETAILED INSPECTION OF:  - FAN ROTOR BLADES (WITH PARTICULAR ATTENTION TO  BLADES LEADING AND TRAILING EDGES, TIPS AND MID  SPAN SHROUDS) FOR DAMAGE  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE 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 722100/6 440 GE-CESM 76 R 01. DETAILED INSPECTION OF FAN BLADES 9  AND FAN DISK  02. RELUBE DOVETAILS AND MIDSPAN SHROUDS WITH SPRAY  LUBE  - MOLYBDENUM DISULFIDE C02-004  PREP.: FAN SPINNER AND BLADES REMOVE  722100-0812-1 430 FAN AND LP COMPRESSOR SECTION MEC DET I: 1 A MRB AMM 722105/6 440 AMM 723102/6 DETAILED INSPECTION OF:  - FAN ROTOR BLADES (WITH PARTICULAR ATTENTION TO  BLADES LEADING AND TRAILING EDGES,TIPS AND MID  SPAN 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 720000/2 440  VISUAL CHECK OF PIPES AND WIRINGS OF FUEL  HEATER, IGV ANTI-ICING TURBINE CASE COOLING FOR SECU-  RITY AND DAMAGE OF ATTACHMENTS INSTALLATIONS EXTERNAL  LEAKAGE AND SIGNS OF OVERHEATING  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  722100-0815-1 430 FAN ROTOR ASSEMBLY ENG LUB I: 1 A MPD AMM 722103/2 440  01. CLEAN BOTH SIDES OF PART SPAN SHROUDS  02. APPLY LUBRICANT ON BOTH SIDES OF ALL  PART SPAN SHROUDS  722300-0802-1 430 FAN FRAME ASSEMBLY ENG GVI I: C MPD AMM 722300/6 440 OR  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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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 EVIDENCE  OF DAMAGE  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  722300-0812-1 430 FAN FRAME ASSEMBLY ENG GVI I: C MPD AMM 722000/0 440 OR  GENERAL VISUAL INSPECTION OF ENGINE FAN SECTION SHOP VIS  (FAN FRAME AND CASING) FOR CONDITION AND EVIDENCE  OF DAMAGE  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723000-0802-1 430 ENGINE COMPRESSOR SECTION ENG DET I: C MPD AMM 723100/0 440 OR  DETAILED INSPECTION OF ENGINE COMPRESSOR SHOP VIS  SECTION FOR SATISFACTORY CONDITION, CRACKS, DENTS,  INSTALLATION FOR SECURITY OF ATTACHMENT, HOT SPOTS  AND MISSING, LOOSEN OR BROKEN BOLTS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723000-0812-1 430 ENGINE COMPRESSOR SECTION ENG DET I: C MPD AMM 723200/2 440 OR  DETAILED INSPECTION OF ENGINE COMPRESSOR SHOP VIS  SECTION FOR SATISFACTORY CONDITION, CRACKS, DENTS,  INSTALLATION FOR SECURITY OF ATTACHMENT, HOT SPOTS  AND MISSING, LOOSEN OR BROKEN BOLTS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723100-0802-2 450 COMPRESSOR ROTOR BLADES ENG BSI T: NOTE CESM AMM 723100/2 460 I: 450 FC NTM GE 72300 BOROSCOPE INSPECTION OF COMPRESSOR ROTOR BLADES STAGE PART 7  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 723100-0802-2 * * * * * C O N T I N U E * * * * *  14 FOR DOMESTIC OBJECT DAMAGE GE-CESM 76 R 9  NOTE:1 IF T/E DAMAGE IS FOUND INSPECT FOR POSSIBLE  STG.14 JOINT BOLT FAILURE  NOTE:2 TH= 750 FC PRE 72-724  TH= 300 FC POST 72-724  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723100-0802-3 450 COMPRESSOR ROTOR BLADES ENG BSI I: 1000 FC CESM AMM 723100/2 460 NTM 723000  BOROSCOPE INSPECTION OF STAGE 1 HPC BLADES FOR PART 7  MIDSPAN COATING WEAR. GE-CESM 76 R 9  NOTE: FIRST INSPECTION SINCE NEW : 2400 CY IF  OPERATING IN A HOSTILE ENVIRONMENT  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723100-0804-1 450 COMPRESSOR ROTOR MEC NDT I: NOTE CN CN  460 FAA AD 1991-135IMP( A FLUORESCENT PENETRANT INSPECTION ON THE HPC REAR FAA AD  SHAFT. 91-10-03R1  NOTE: INITIAL AND SUBSEQUENT INSPECTIONS AS PER  AD 91-10-03R1 / CN 1991-135-IMP(B).  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723100-0813-1 450 COMPRESSOR ROTOR ENG NDT T: 7500 FC AOW AOW PW JT9/  460 I: 4000 FC 72-35/PSE:LE 01. REMOVE ENGINE NOTE 2 8-4-25-1  02. SHOP DISASSEMBLY FOR INSPECTION OF THE 14TH STAGE SB PW A5806  COMPRESSOR DISK REAR FLANGE  03. REINSTALL ENGINE  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 723100-0813-1 * * * * * C O N T I N U E * * * * *  NOTE 1:TASK BE PERFORMED AT THE OPPORTUNITY OF AN  ENGINE CHANGE  NOTE 2:THE CYCLES QUOTED ARE PART CYCLES  723200-0802-1 450 COMPRESSOR VARIABLE STATOR ENG DET I: 5 A MPD AMM 723200/2 460  DETAILED INSPECTION OF VSV ACTUATING SYSTEM  WITH PARTICULAR ATTENTION TO VSV LEVERS FOR BENDING  AND LOOSENESS (STAGE 3 TO 6)  723200-0802-2 450 COMPRESSOR VANES ENG BSI T: 650 FC CESM AMM 723100/2 460 I: 450 FC NTM 723000  BOROSCOPE INSPECTION COMPLETE CIRCUMFERENCE PART 7  ( PORTS B1-6 AND B1-7 ) OF HPC. GE-CESM REV  VANES STAGE 6 AND 7 TRAILING EDGE ROOT FOR NOTCHES.  NOTE : INSPECTION NOT REQUIRED IF NO EROSION PROBLEM  EXIST OR IF SHOP WORKSHOP ENTAILS PEVENTION  PLAN  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723200-0802-3 450 COMPRESSOR VARIABLE STATOR ENG DET T: 1500 FC MPD AMM 723200/2 460 I: 1500 FC  DETAILED INSPECTION OF VSV ACTUATING SYSTEM  WITH PARTICULAR ATTENTION TO VSV LEVERS FOR BENDING  AND LOOSENESS (STAGE 3 TO 6)  723200-0812-1 430 COMPRESSOR VARIABLE STATOR ASSEMBLY MEC GVI I: 1 C EMP PW JT9D EMP  440  GENERAL VISUAL INSPECTION OF VARIABLE VANE ARMS FOR  ENTRAPPED FOREIGN MATERIAL, BENT, DISTORTED OR  DETACHED VANE ARMS.  ACCESS: 435AL 436AR  445AL 446AR  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 723300-0802-1 450 COMPRESSOR REAR STATOR ASSY ENG DET I: SB SB AMM 723300/2 460 GE-CESM 76 R DETAILED INSPECTION OF REAR COMPRESSOR CASE 9  AFT FLANGE BOLT HOLES AND HORIZONTAL FLANGE WELD SB GE 72-898  JOINT FOR CRACKING.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723300-0802-2 450 COMPRESSOR REAR STATOR ASSY ENG DET I: 250 FC SB AMM 723300/2 460 GE-CESM 76 R DETAILED INSPECTION OF REAR COMPRESSOR CASE 9  HORIZONTAL FLANGE WELD JOINT FOR CRACKING. SB GE 72-861  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723300-0802-3 450 COMPRESSOR REAR STATOR ASSY ENG GVI T: 1200 CSN SB SB GE 72-099  460 I: 250 FC  VISUAL INSPECTION OF CIRCUMFERENTIAL RIB OF HPC  CASE FOR CRACKS, NICKS, DENTS, GOUGES AND SCRATCHES  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723300-0802-4 450 COMPRESSOR REAR STATOR ASSY. MEC GVI I: 600 FH MRB AMM 723300/2 460 OR  VISUAL INSPECTION OF REAR COMPRESSOR CASE FLANGES AND 400 FC  WELD JOINTS FOR CRACKING  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723400-0802-2 450 COMPRESSOR REAR FRAME ASSEMBLY NDT SDI T: SB 72-839 SB NTM 723000  460 I: SB 72-839 PART 6  EDDY CURRENT/FLUORESCENT PENETRANT INSPECTION OF CRF SB GE 72-839  IGNITER PORTS AND FUEL NOZZLE PADS FOR CRACKING  NOTE: APPLICABLE ON FRAMES AFFECTED BY SB 72-839  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 723400-0802-3 450 COMPRESSOR REAR FRAME ASSEMBLY NDT SDI T: 5000 CSN CESM AMM 723400/6 460 I: 1000 FC NTM 723000  ULTRASONIC/FLUORESCENT PENETRANT/ EDDY CURRENT PART 4/6  INSPECTION OF CRF MID FLANGE SB GE 72-780  SB GE 72-837  NOTE : FOR POST SB GE 72-0853 AND SB GE 72-0820,  FIRST INSPECTION IS NOT REQUIRED UNTIL  8500 CSN.  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  723400-0802-4 450 COMPRESSOR REAR FRAME ENG DET T: 1750 CSN SB AMM 723400/6 460 I: 250 FC SB GE 72-750  VISUAL INSPECTION OF:  - FIRE WALL AND SEAL FOR GENERAL CONDITION  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723400-0802-5 450 COMPRESSOR REAR FRAME ASSY. MEC DET T: NOTE SB GE-CESM 76 R 460 I: 450 FC 9  DETAILED INSPECTION OF COMPRESSOR REAR FRAME SB GE 72-758  FORWARD FLANGES (WITHOUT DOUBLERS INSTALLED) FOR  CRACKS  NOTE: FIRST INSPECTION: 1750 CSN (PRE SB GE 72-876)  3500 CSN (POST SB GE 72-876)  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  723400-0802-6 450 COMPRESSOR REAR FRAME ASSY. MEC DET I: SB SB GE-CESM 76 R 460 9  DETAILED INSPECTION OF COMPRESSOR REAR FRAME SB GE 72-758  FORWARD FLANGES (WITH DOUBLERS INSTALLED) FOR CRACKS.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 724000-0812-1 430 DIFFUSER CASE ASSY ENG NDT I: PW SB CN AMM 724103/6 440 5749 FAA AD CN  NDT INSPECTION OF DIFFUSER CASE REAR RAIL FOR CRACKS 1999-292-IMP FAA AD 99-11 ACCESS: 435AL 436AR 451AL 452AR SB PW 5749  445AL 446AR 461AL 462AR  724000-0812-2 430 DIFFUSER CASE ASSY ENG GVI I: C MRB AMM 724103/6 440 OR  VISUAL INSPECTION OF DIFFUSER CASE ASSY (WITH SHOP VIS  PARTICULAR ATTENTION TO CIRCUMFERENTIAL FLANGES) FOR  DAMAGE, WELD CRACKS SCORES AND SCRATCHES CHECK FIRE  WALL AND SEAL FOR GENERAL CONDITION  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  724100-0802-1 450 COMBUSTION LINER ASSEMBLY INP BSI T: 900 CSI CESM AMM 724100/6 460 I: 450 FC MRB NTM GE 72400 BOROSCOPE INSPECTION OF COMBUSTION LINER ASSEMBLY AND PART 7  DOME AREAS IN ACCORDANCE WITH GE NTM. GE-CESM 76 R 9  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  724100-0802-2 450 COMBUSTION LINER ASSEMBLY INP BSI T: 75 HSN CESM NTM GE 72510 460 I: 450 FC PART 7  BOROSCOPE INSPECTION OF COMBUSTION LINER FOR GE-CESM 76 R INDICATION OF "FISHMOUTH SEAL" FAILURE (INNER). 9  INSPECT HPT NOZZLE VANE LEADING EDGE AT 5-7 O ́CLOCK SB GE 72-688  POSITION FOR INDICATION OF DISCOLORATION AND BURNING.  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  724100-0802-4 450 COMBUSTION LINER ASSEMBLY MEC GVI I: 450 FC CESM AMM 724100/6 460 GE-CESM 76 R VISUAL INSPECTION OF COMBUSTOR MOUNTING PINS FOR WEAR 9  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 724100-0802-4 * * * * * C O N T I N U E * * * * *  445AL 446AR 461AL 462AR 465AL 466AR  724400-0812-1 450 COMBUSTION CHAMBER INP BSI T: 1000 HSN MRB AMM 720000/6 460 OR  BOROSCOPE INSPECTION OF COMBUSTION CHAMBER 750 CSN  I: 600 FH  NOTE: INSPECTION TO BE CARRIED OUT TOGETHER WITH OR  REFER TO 725100-0812-1 400 FC  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  724400-0812-2 450 COMBUSTION CHAMBER INP BSI I: 125 FC MPD AMM 720000/6 460  BOROSCOPE INSPECTION OF COMBUSTION CHAMBER  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  725000-0812-1 450 TURBINE SECTION MEC NDT I: PW SB CN CN 1994-213( 460 5979 FAA AD FAA AD 94-10 AN EDDY CURRENT INSPECTION OF THE TURBINE 6TH STAGE SB PW 5979  AIRSEAL KNIFE EDGES.  725000-0812-2 450 TURBINE SECTION MEC NDT I: REFER CN CN CN  460 FAA AD 1991-070-IMP NDT INSPECTION OF THE HPT FIRST STAGE DISK COOLING FAA AD 91-04 AIR HOLES.  725000-0812-3 450 TURBINE SECTION MEC NDT I: PW SB CN CN 1994-213( 460 5978 FAA AD FAA AD 94-10 A BORESCOPE AND EDDY CURRENT INSPECTION OF THE SB PW 5978  TURBINE 6TH STAGE AIRSEAL RETAINING WING.  725000-0814-1 450 TURBINE SECTION ENG NDT I: 2000 FC MPD AMM 710000/4 460 SB PW SB 566 - REMOVE ENGINE  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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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 2ND  STAGE TURBINE AIRSEAL (LENTICULAR AIRSEAL)  IN ACCORDANCE WITH PW SB 5668  - REINSTALL HPT MODULE ASSEMBLY  - REINSTALL ENGINE  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  725000-0814-2 450 TURBINE SECTION ENG NDT I: 3000 FC MPD AMM 710000/4 460 SB PW SB 578 - REMOVE ENGINE  - SHOP VISIT FOR HPT MODULE DISASSEMBLY  - PERFORM EDDY CURRENT CRACK INSPECTION OF THE 2ND  STAGE TURBINE AIRSEAL (LENTICULAR AIRSEAL)  IN ACCORDANCE WITH PW SB 5786  - REINSTALL HPT MODULE ASSEMBLY  - REINSTALL ENGINE  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  725100-0802-1 450 HP-TURBINE STAGE 1 INP BSI I: 450 FC CESM AMM 725100/6 460 MRB NTM GE 72510 BOROSCOPE INSPECTION OF HPT NOZZLE STAGE 1 (HPTN-1) PART 7  VIA COMBUSTION PORTS AND PORTS BETWEEN 5 AND 7 GE-CESM 76  O ́CLOCK POSITION  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  725100-0812-1 450 HP-TURBINE, STAGE 1 INP BSI I: 600 FH MRB AMM 720000/6 460 OR  BOROSCOPE INSPECTION OF HPT NOZZLE GUIDE VANES STAGE 400 FC  1 (NGV-1) VIA COMBUSTION PORTS  NOTE: INSPECTION TO BE CARRIED OUT TOGETHER WITH  COMBUSTION CHAMBER INSPECTION, REFER TO  724400-0812-1  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 725200-0812-1 450 2ND STAGE HP-TUR.STAT.VANES ENG BSI T: REFER AD CN AMM 720000/6 460 I: 1000 FH FAA AD CN  BORESCOPE INSPECTION OF SECOND STAGE HP TURBINE VANES 1993-159-IMP FAA AD 93-14 ACCESS: 435AL 436AR 451AL 452AR SB PW 5667  445AL 446AR 461AL 462AR  725300-0802-1 450 HP-TURBINE ASSY. INP BSI T: NOTE CESM AMM 725300/2 460 I: 450 FC MRB NTM GE 72530 BOROSCOPE INSPECTION OF HP TURBINE ROTOR BLADES PART 7  STAGE 1 GE-CESM 76  NOTE: FIRST INSPECTION  - 4500 TSN/800 CSN FOR BLADES CONFIGURATION  2 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  445AL 446AR 461AL 462AR 465AL 466AR  725300-0802-3 450 HP-TURBINE ASSY. INP BSI T: 1200 CSN CESM AMM 725300/2 460 I: 450 FC NTM GE 72530 BOROSCOPE INSPECTION OF HP TURBINE ROTOR BLADES STAGE PART 7  2.PAY PARTICULAR ATTENTION TO BLADE LEADING EDGE FOR GE-CESM 76 R DAMAGE INDICATING POSSIBLE STAGE 2 NOZZLE DEFECTS 9  SUCH AS BENDING OR TORSION OR SAG  (REPAIRED STG 2 NOZZLE ASSEMBLIES.)  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  725300-0802-4 450 HP TURBINE ASSY NDT SDI I: 400 FC CN CN  460 NOTE FAA AD 1991-232-IMP NDT (EDDY CURRENT) OF THE HPTR THERMAL SHIELD FAA AD 91-15 GE-CESM 109  NOTE: INSPECTION IS NOT REQUIRED IF THE THERMAL SB GE 72-879  SHIELD IS INSTALLED WITH PIP INTERSTAGE SEALS  OR HAS NEVER BEEN INSTALLED WITH PRE-PIP  INTERSTAGE 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: 
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A300 MAINTENANCE PLANNING D

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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  445AL 446AR 461AL 462AR 465AL 466AR  725300-0803-1 450 HP TURBINE ASSY NDT SDI I: NOTE CN CN  460 FAA AD 1983-011-IMP FLUORESENT PENETRANT INSPECTION OF HPT FAA AD 82-25 SPACER/IMPELLER SB GE 72-748  NOTE: INITIAL AND SUBSEQUENT INSPECTION AS PER  AD 82-25-08/CN 1983-011-IMP(B)  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  725300-0812-1 450 HP-TURBINE ASSY. INP BSI T: 1000 HSN MRB AMM 720000/6 460 OR  BOROSCOPE INSPECTION OF HP TURBINE ROTOR BLADES 750 CSN  STAGE 1 I: 600 FH  OR  ACCESS: 451AL 452AR 400 FC  461AL 462AR  725300-0812-2 450 HP TURBINE ASSY ENG GVI I: 1500 FC MPD SB PW 5551  460 NOTE  INSPECT NO.4 OIL PRESSURE TUBE, P/N 738535 OR 785544  FOR EVIDENCE OF COKING AND CLEAN AS NECESSARY  NOTE: IF LITTLE OR NO COKING IS FOUND INSPECTION  INTERVAL CAN BE EXTENDED TO 2500 CY.  725400-0802-2 450 TURBINE MID-FRAME ASSEMBLY ENG NDT I: REFER AD CN CN  460 FAA AD 1991-019-IMP VISUAL AND ULTRASONIC INSPECTION OF TURBINE MID-FRAME FAA AD 90-23 AFT FLANGE FOR CRACKS SB GE 72-957  NOTE: INITIAL AND SUBSEQUENT INSPECTIONS AS PER  AD 90-23-15/CN 1991-019-IMP(B).  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 725400-0802-3 450 ENGINE TURBINE MID FRAME ENG GVI T: NOTE CESM AMM 725400/2 460 I: NOTE GE-CESM 76 R VISUAL INSPECTION OF THE ENGINE TURBINE MID FRAME 9  (TMF): SB GE 72-658  - LINER FOR CLOCKING  - HAT SECTION AND T/C BOSS FOR CRACKING  NOTE: -FOR LINER CLOCKING PRE GE SB 72-658  FIRST INSPECTION : 1500 CSN  I : 750 FC  -FOR OUTER CASE CRACKING (HAT SECTIONS, INSTRU-  MENTATION BOSSES,SKIN WELDS):  FIRST INSPECTION : 1500 CSN  I : 450 FC  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  725600-0802-1 450 LOW PRESSURE TURBINE STATOR ENG GVI I: 750 FH CN CN  460 FAA AD 2001-108-IMP GENERAL VISUAL INSPECTION OF LPT NOZZLE LOCKS FAA AD  2001-04-16  SB GE 72-A11 725700-0802-1 430 LP TURBINE ROTOR BLADES ENG DET I: 1 A MRB AMM 725700/2 440  DETAILED INSPECTION OF LP TURBINE ROTOR BLADES  FOR DAMAGE (LAST STAGE)  725700-0802-2 450 LOW PRESSURE TURBINE ROTOR ENG BSI I: 150 FC CESM AMM 725700/2 460 NTM GE 72570 BORESCOPE/VISUAL INSPECTION OF STAGE 4 BLADES/TIP PART 7  INTERLOCK WEAR. GE-CESM 76 R 9  ACCESS: 435AL 436AR 455AL 456AR SB GE 72-227  445AL 446AR 465AL 466AR  725700-0802-3 450 LOW PRESSURE TURBINE ROTOR ENG BSI I: 450 FC CESM AMM 725700/2 460 NTM GE 72570 BORESCOPE/DETAILED INSPECTION OF STAGE 4 BLADE PART 7  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 725700-0802-3 * * * * * C O N T I N U E * * * * *  TIP INTERLOCKS FOR WEAR GE-CESM 76 R 9  ACCESS: 435AL 436AR 455AL 456AR SB GE 72-675  445AL 446AR 465AL 466AR  725700-0802-4 450 LOW PRESSURE TURBINE ROTOR ENG BSI I: NOTE SB GE-CESM 76 R 460 9  BORESCOPE INSPECTION OF LOW PRESSURE TURBINE STAGE 1 SB GE 72-125 BLADES/DISK FOR RUBS FROM TMF STRUT STUD FAILURE  NOTE: INTERVAL IN ACCORDANCE WITH VENDOR  RECOMMENDATIONS  ACCESS: 435AL 436AR 455AL 456AR  445AL 446AR 465AL 466AR  725700-0812-1 430 LP TURBINE ROTOR BLADES MEC DET I: 1 A MRB AMM 725000/6 440  DETAILED INSPECTION OF LP TURBINE ROTOR BLADES  FOR DAMAGE (LAST STAGE)  725800-0812-1 450 TURBINE EXHAUST CASE ASSY ENG GVI I: C MPD AMM 725800/6 460 OR  GENERAL VISUAL INSPECTION OF TURBINE EXHAUST CASE FOR SHOP VIS  CONDITION, HOT SPOTS AND CRACKS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  726000-0802-1 450 ACCESSORY DRIVE SECTION ENG GVI I: 1000 FH MRB AMM 726500/6 460  VISUAL INSPECTION OF ENGINE ACCESSORY DRIVE SECTION  FOR SATISFACTORY CONDITIONS, CRACKS, FREEDOM FROM  LEAKAGE (WITH PARTICULAR ATTENTION TO MOUNTING LUGS  AND BRACKETS).  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 726000-0802-2 450 ACCESSORY DRIVE SECTION ENG GVI I: 450 FC CESM AMM 726500/6 460 GE-CESM 76 R VISUAL INSPECTION OF LH LINK MOUNT SPHERICAL BEARING 9  FOR EVIDENCE OF WEAR AND MOUNT BRACKET FOR CRACKING  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  726000-0812-1 450 ACCESSORY DRIVE SECTION ENG GVI I: C MRB AMM 726500/0 460 OR  VISUAL INSPECTION OF ENGINE ACCESSORY DRIVE SECTION SHOP VIS  FOR SATISFACTORY CONDITIONS, CRACKS, FREEDOM FROM  LEAKAGE (WITH PARTICULAR ATTENTION TO MOUNTING LUGS  AND BRACKETS).  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  726300-0802-1 450 TRANSFER GEARBOX ENG GVI I: 150 FC CESM AMM 726300/6 460 GE-CESM 76 R CHECK FLUID FITTING (ROZAN INSERTS) FOR LOOSENESS/ 9  LEAKAGE.  ACCESS: 435AL 436AR 451AL 455AL  445AL 446AR 461AL 465AL  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 731000-0802-1 430 ENGINE FUEL AND CONTROL ENG GVI I: SB 73-007 CN CN  440 FAA AD 1985-165-071 INSPECT ENGINE FUEL FLOWMETER INLET TUBE ASSEMBLY. FAA AD 85-16 ISB 73-0007  ACCESS: 435AL  445AL  731200-0801-1 430 FUEL FILTER (ENGINE) ENG RAR T: NOTE MRB AMM 731203/6 440 I: 1000 FH SIL SIL 73-011  DISCARD FUEL FILTER ELEMENT AND INSTALL A NEW ONE.  NOTE: REPLACE FILTER ELEMENT AT 150 FH AND 450 FH  AFTER A/C DELIVERY OR MAJOR TANK REPAIR  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  731200-0802-1 430 FUEL PUMP ENG CLN T: NOTE CESM AMM 731201/6 440 I: 1500 FC GE-CESM 76 R INSPECTION AND CLEANING OF FUEL PUMP CARTRIDGE 9  STRAINER ELEMENT  NOTE: AFTER FUEL TANK MAINTENANCE OR A/C DELIVERY  THE TASK SHOULD BE PERFORMED WITHIN 50 FC.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  731200-0811-1 430 FUEL FILTER (ENGINE) ENG RAR T: NOTE MPD SIL 73-007  440 I: 1 C SIL  REMOVE, INSPECT AND REPLACE FUEL PUMP FILTER ELEMENT  NOTE: REPLACE FILTER ELEMENT AT 150 FH AND 450 FH  AFTER A/C DELIVERY OR MAJOR TANK REPAIR  ACCESS: 435AL  445AL  731201-0802-1 430 ENGINE FUEL PUMP - QAD ENG FUC I: 1500 FC CESM AMM 731201/2 440 GE-CESM 76 R CHECK 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: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 731201-0802-1 * * * * * C O N T I N U E * * * * *  ATTACH (QAD) RING FOR PLAY AND LOCK BOLT FOR TORQUE  ACCESS: 435AL  445AL  731201-0812-1 430 ENGINE FUEL PUMP ENG FUC I: 4 A MPD AMM 731201/4 440  CHECK ENGINE FUEL PUMP QUICK DISCONNECT NUT  ASSEMBLY FOR PLAY AND LOCK BOLT FOR TORQUE  731301-0811-1 450 FUEL NOZZLE ENG CLN I: 3 A MPD AMM 731300/0 460  CLEAN FUEL NOZZLE  ACCESS: 451AL 452AR  461AL 462AR  731500-0812-1 436 FUEL HEATER ENG GVI I: PRE-ACPT MPD AMM 731500/0 446  CHECK FUEL HEATER AIR OVERBOARD FOR EVIDENCE  OF FUEL SPRAY  732100-0812-1 450 FUEL CONTROL SYSTEM ENG GVI I: DY-TERM MPD AMM 732100/0 460  GENERAL VISUAL INSPECTION OF TT-2 SENSORS FOR  CONDITION AND CLEANLINESS  733000-0802-1 430 FUEL INDICATING ENG GVI I: C MRB AMM 733000/6 440 OR  GENERAL VISUAL INSPECTION OF: SHOP VIS  - FUEL FLOW TRANSMITTER, CONNECTOR AND HARNESS;  - FUEL PRESSURE TRANSMITTER, CONNECTOR AND HARNESS;  - FUEL FILTER DIFFERENTIAL SWITCH, CONNECTOR AND  HARNESS;  FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,  CORROSION, OVERHEATING, DETERIORATION AND FREEDOM  FROM LEAKS  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE FUEL AND CONTROL REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 733000-0802-1 * * * * * C O N T I N U E * * * * *  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  733000-0812-1 450 FUEL INDICATING ENG GVI I: C MRB AMM 733300/0 460 OR AMM 733400/0 GENERAL VISUAL INSPECTION OF: SHOP VIS  - FUEL FLOW TRANSMITTER, CONNECTOR AND HARNESS;  - FUEL PRESSURE TRANSMITTER, CONNECTOR AND HARNESS;  - FUEL FILTER DIFFERENTIAL SWITCH, CONNECTOR AND  HARNESS;  FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,  CORROSION, OVERHEATING, DETERIORATION AND FREEDOM  FROM LEAKS  ACCESS: 436AR 452AR  446AR 462AR  733400-0801-1 435 FUEL INDICATING SYSTEM ENG FUC I: ENG. CHG MRB AMM 733411/4 445  FUNCTIONAL TEST OF FUEL FILTER DIFFERENTIAL  PRESSURE INDICATING SYSTEM.  733400-0811-1 435 FUEL INDICATING SYSTEM ENG FUC I: 2 C MRB AMM 733400/5 445  FUNCTIONAL TEST OF FUEL FILTER DIFFERENTIAL  PRESSURE INDICATING SYSTEM.  733600-0811-1 210 FUEL HEATING SYSTEM ENG OPC I: ENG. CHG MRB AMM 733500/0 OPERATIONAL TEST OF FUEL HEATING MANUAL CONTROL WITH  ENGINE RUNNING  733600-0811-2 210 FUEL HEATING SYSTEM ENG OPC I: 1 A MRB AMM 733600/0 OPERATIONAL TEST OF FUEL HEATING AUTOMATIC CONTROL  WARNING 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: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 740000-0802-1 430 IGNITION SYSTEM ENG GVI I: C MRB AMM 740000/2 440 OR  VISUAL INSPECTION OF IGNITION EXCITERS, LEADS AND SHOP VIS  COMPONENTS FOR SATISFACTORY CONDITION  ACCESS: 436AR 452AR 456AR  446AR 462AR 466AR  740000-0812-1 430 IGNITION SYSTEM ENG GVI I: C MRB AMM 741101/4 440 OR AMM 742101/4 VISUAL INSPECTION OF IGNITION EXCITERS, LEADS AND SHOP VIS  COMPONENTS FOR SATISFACTORY CONDITION  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  742102-0802-1 436 IGNITER PLUGS - ENGINE ENG DET I: 2 A MRB AMM 742102/4 446  01. DETAILED INSPECTION OF IGNITER PLUGS FOR  CLEANLINESS, BURNS AND EROSION  02. DEPENDING OF CONDITION OF PLUGS ROTATE PLUGS  ( TYPE 3 ONLY ) SO THAT PORTION OF PLUG WITH  MOST EROSION IS LOCATED IN ONE OF THE LOWER  QUADRANTS OF THE IGNITER PORT OR REPLACE.  03. AURAL CHECK OF CONTINUOUS IGNITION SYSTEM  (A AND B) AFTER IGNITER RE-INSTALLATION  ACCESS: 436AR 452AR 456AR  446AR 462AR 466AR  742102-0812-1 436 IGNITER PLUGS - ENGINE ENG DET I: 2 A MRB AMM 742102/4 446 AMM 742102/6 01. DETAILED INSPECTION OF IGNITER PLUGS  (OR REPLACEMENT AS NECESSARY)  02. AURAL CHECK OF CONTINUOUS IGNITION SYSTEM (A AND  B POSITION) AFTER RE-INSTALLATION  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : IGNITION REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 750000-0802-1 450 AIR - GENERAL MEC DET I: GE SB CESM AMM 752600/6 460 75-064 GE-CESM 76 R DETAILED INSPECTION OF STAGE 8 AND 14 9  MANIFOLDS FOR CRACKS SB GE 75-064  SB GE 75-070  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  751000-0802-1 450 ANTI-ICING TUBE ENG GVI I: 150 FC CESM AMM 752201/6 460 GE-CESM 76 R CHECK 10TH STAGE ANTI-ICING TUBE FOR CRACKING 9  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  752400-0813-1 450 ACCESSORY COOLING - TURBINE CASE COOLING ENG DET I: 1 A EMP PW JT9D EMP  460  DETAILED INSPECTION OF UPPER AND LOWER RIGHT  REAR TCA TUBES AND BRACKETS FOR CRACKING,  DEFORMATION, WEAR AND SECURITY OF ATTACHMENT.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  753100-0811-1 450 VSV FEEDBACK SYSTEM ENG FUC I: 2 A MPD AMM 753101/5 460  FRICTION TEST OF VARIABLE STATOR VANE  FEED BACK CABLE  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  753104-0812-1 450 CONTROL-ENG.VANE AND BLEED ENG DET I: 1400 FH MAN MAN  460 MAN-JT9-3-92  DETAILED INSPECTION OF THE ENGINE VANE AND  BLEED CONTROL (EVBC) WATER TRAP.  ACCESS: 435AL  445AL  SYSTEMS AND POWERPLANT PROGRAM : ENGINE - AIR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 EMP  460  CHECK EVC AND EVBC TRIMMING.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  753105-0811-1 450 FILTER ELEMENT-FUEL/EVBC ENG CLN T: NOTE MPD AMM 753105/5 460 I: 5 A  REMOVE AND INSPECT (PH) FILTER ELEMENT OF ENGINE VANE  AND BLEED CONTROL FOR FOREIGN MATTER AND/OR DAMAGE  SCREEN. INSTALL A NEW FILTER ELEMENT.  NOTE: FIRST INSPECTION AT 3 MO AFTER  ENGINE OR FUEL PUMP INSTALLATION.  ACCESS: 435AL  445AL  753400-0802-1 450 VBV SYSTEM FEED BACK CABLE ENG GVI I: 2 A MPD AMM 753401/2 460  VISUAL INSPECTION OF VARIABLE BLEED VALVES ACTUATING  SYSTEM AND FEEDBACK MECHANISM  ACCESS: 435AL 451AL  445AL 461AL  753400-0812-1 450 VBV SYSTEM FEEDBACK CABLE ENG GVI I: 2 A MPD AMM 753400/4 460  VISUAL INSPECTION OF 3.0 MODULATING BLEED VALVES  ACTUATING SYSTEM AND FEEDBACK MECHANISM  ACCESS: 435AL 451AL  445AL 461AL  754300-0802-2 450 LOW PRESSURE TURBINE COOLING AIR ENG DET I: 250 FC FAA AD CN  460 MANIFOLD 1986-003-IMP FAA AD 85-25 DETAILED INSPECTION OF RELATED STAGE 7 GE-CESM 76 R COOLING TUBES AND ATTACHING HARDWARE. 9  SB GE 75-005 * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE - AIR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 75-006 445AL 446AR 461AL 462AR  754300-0811-1 450 TURBINE CASE COOLING SYSTEM ENG FUC I: 5 A MRB AMM 752400/5 460  FUNCTIONAL CHECK OF TURBINE CASE COOLING SYSTEM. (TCC  INDICATING SYSTEM AND 13TH STAGE AIR SHUT OFF VALVE)  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE - AIR REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 760000-0503-1 510 ENGINE CONTROLS ENG FUC I: 3 C MRB AMM 761100/5 610 AMM 762100/5 CABLE TENSION CHECK OF THROTTLE, THRUST REVERSER AND AMM 783000/5 EMERGENCY SHUT DOWN SYSTEMS WITH TENSIOMETER  (INCLUDING ZONE 130)  ACCESS: 131AZ 131CZ 132AZ 132EZ  760000-0503-2 510 ENGINE CONTROLS ENG FUC I: 3 C MRB AMM 761100/5 610 AMM 783000/5 CABLE TENSION CHECK OF THROTTLE AND THRUST REVERSER  SYSTEMS WITH TENSIOMETER (INCLUDING ZONE 130)  ACCESS: 131AZ 131CZ 132AZ 132EZ  761000-0802-1 430 POWER CONTROLS ENG GVI I: C MRB AMM 761100/0 440 OR AMM 761200/0 VISUAL INSPECTION OF THROTTLE AND THRUST REVERSER SHOP VIS AMM 783100/2 CONTROLS (ENGINE PORTION) FOR SATISFACTORY CONDITION,  SECURITY OF ATTACHMENT, WEAR, CHAFING AND CORROSION.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  761000-0812-1 450 POWER CONTROLS ENG GVI I: C MRB AMM 761100/5 460 OR  VISUAL INSPECTION OF THROTTLE AND THRUST REVERSER SHOP VIS  CONTROLS (ENGINE PORTION) FOR SATISFACTORY CONDITION,  SECURITY OF ATTACHMENT, WEAR, CHAFING AND CORROSION.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  761131-0802-1 410 TRANSMISSION - SECONDARY MEC DET I: 1 C MPD AMM 761131/6 420 SIL SIL 76-015  01. DETAILED INSPECTION OF ADJUSTABLE  LEVER FOR SECURITY.  02. CHECK THE LOCKBOLT AND LOCKWASHER FOR  EVIDENCE OF LOOSENESS.  ACCESS: 415AL 416AR  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 761131-0802-1 * * * * * C O N T I N U E * * * * *  425AL 426AR  761131-0812-1 410 TRANSMISSION - SECONDARY MEC DET I: 1 C MPD AMM 761131/6 420  01. DETAILED INSPECTION OF ADJUSTABLE  LEVER FOR SECURITY.  02. CHECK THE LOCKBOLT AND LOCKWASHER FOR  EVIDENCE OF LOOSENESS.  ACCESS: 415AL 416AR  425AL 426AR  762000-0503-1 210 EMERGENCY SHUT DOWN SYSTEM ENG OPC I: ENG. CHG MRB ** AMM 762100/5 OPERATIONAL CHECK OF THE EMERGENCY SHUT DOWN SYSTEM  INCLUDING:  - FUEL LP FIRE SHUT-OFF VALVES CLOSING  - PACK SHUT OFF VALVES AUTOMATIC CLOSING  - HP BLEED VALVE AND X-BLEED VALVE AUTOMATIC  CLOSING  NOTE: HYDRAULIC FIRE SHUT-OFF VALVE CLOSING  IS COVERED BY TASK 291133-0503-1  762000-0503-2 210 EMERGENCY SHUT DOWN SYSTEM ENG OPC I: ENG. CHG MRB ** AMM 282100/5 AMM 762100/5 OPERATIONAL TEST OF THE EMERGENCY SHUT DOWN SYSTEM  (FIRE CONTROL HANDLES OPERATION) INCLUDING:  - FUEL LOW PRESSURE FIRE SHUT OFF VALVES ELECTRICAL  ACTUATORS USING EACH MOTOR IN TURN (MSI 28.21.18)  - PACK SHUT OFF VALVES AUTOMATIC CLOSING  -HP VALVE, BLEED VALVE AND X FEED VALVE AUTOMATIC  CLOSING  NOTE: HYDRAULIC FIRE SHUT OFF VALVES  CLOSING IS COVERED BY TASK 291133-0503-1  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE CONTROLS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 770000-0802-1 430 RPM INDICATING SYSTEM ENG GVI I: C MPD AMM 770000/6 440 OR  GENERAL 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  445AL 446AR 461AL 462AR  770000-0812-1 430 RPM INDICATING SYSTEM ENG GVI I: C MPD AMM 771100/0 440 OR AMM 771200/0 GENERAL VISUAL INSPECTION OF: SHOP VIS AMM 771500/0 - 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 CHAFING  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  771100-0801-1 210 N1 RPM INDICATING SYSTEM ENG OPC I: 1 C MRB ** AMM 771112/4 BITE CHECK OF THE N1 RPM INDICATING SYSTEM FOR THE  L/H AND R/H ENGINE  771500-0811-1 210 ENGINE PRESSURE RATIO ENG OPC I: 1 C MRB ** AMM 771500/0 BITE TEST OF EPR INDICATORS  771500-0812-1 450 ENGINE PRESSURE RATIO ENG GVI I: DY-TERM MPD AMM 771500/0 460  GENERAL VISUAL INSPECTION OF PT-2 AND PT-7 PROBES FOR  CONDITION AND CLEANLINESS  SYSTEMS AND POWERPLANT PROGRAM : ENGINE INDICATING REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 771500-0812-2 450 ENGINE PRESSURE RATIO ENG GVI I: 3 A MRB AMM 771500/0 460  VISUAL 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 771500/0 460  GENERAL VISUAL INSPECTION OF PT-7 PROBES FOR  CONDITION  772100-0802-1 430 EGT TEMPERATURE SYSTEM ENG GVI I: C MPD AMM 772101/2 440 OR  VISUAL INSPECTION OF THERMOCOUPLE HARNESSES AND LEADS SHOP VIS  FOR SATISFACTORY CONDITION AND SECURITY OF  ATTACHMENT.  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  772100-0812-1 450 EGT TEMPERATURE SYSTEM ENG GVI I: C MPD AMM 772100/0 460 OR  VISUAL INSPECTION OF THERMOCOUPLE HARNESSES AND LEADS SHOP VIS  FOR SATISFACTORY CONDITION AND SECURITY OF  ATTACHMENT.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  772100-0812-2 210 EGT INDICATING SYSTEM ENG CHK I: 1 C EMP PW JT9D EMP  EGT SYSTEM RESISTANCE CHECK FOR INSULATION GROUND  FAULTS.  773200-0802-1 430 ENGINE VIBRATION INDICATING ENG GVI I: C MPD AMM 773200/4 440 OR  GENERAL VISUAL INSPECTION OF: SHOP VIS  - AFT VIBRATION TRANSDUCER AND HARNESS  - INTERNAL FAN BEARING VIBRATION TRANSDUCER HARNESS  FOR 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 773200-0802-1 * * * * * C O N T I N U E * * * * *  CORROSION, CRACKS, DENTS AND BENDS  ACCESS: 435AL 436AR 451AL 455AL  445AL 446AR 461AL 465AL  773200-0812-1 450 ENGINE VIBRATION INDICATING ENG GVI I: C MPD AMM 773200/0 460 OR  GENERAL VISUAL INSPECTION OF: SHOP VIS  - AFT VIBRATION TRANSDUCER AND HARNESS  - FORWARD VIBRATION TRANSDUCER AND HARNESS  FOR SATSFACTORY CONDITION, SECURITY OF ATTACHMENT.  ACCESS: 436AR 452AR  446AR 462AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE INDICATING REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 781100-0802-1 450 CORE EXHAUST NOZZLE ASSEMBLY ENG DET I: 1500 FC CESM AMM 781100/6 460 GE-CESM 76  VISUAL CHECK FOR LOOSE OR MISSING BOLTS/NUTS/STUDS  AT FORWARD CENTERBODY TO TURBINE REAR FRAME  ATTACHMENT AND AT FORWARD TO AFT CENTERBODY JOINT.  CHECK FOR CORRODED OR DAMAGED NUTPLATES IN AFT  CENTERBODY. CHECK FOR SKIN CRACKS IN CENTERBODY,  OUTER COWLING AND INNER LINERS.  ACCESS: 455AL 456AR  465AL 466AR  781100-0802-2 450 LONG CORE EXHAUST NOZZLE ENG GVI I: 1500 FC CESM AMM 781100/6 460 GE-CESM 76 R GENERAL VISUAL INSPECTION OF LONG FIXED-CORE EXHAUST 9  NOZZLE FOR CRACKS IN THE "C" CHANNEL SUPPORT  ACCESS: 455AL 456AR  465AL 466AR  781100-0802-4 450 LONG CORE EXHAUST NOZZLE ENG GVI I: 1500 FC CESM AMM 781100/6 460 GE-CESM 76 R CHECK FOR MISSING BOLTS/NUTS/STUDS AT FWD 9  CENTERBODY TO TRF ATTACH POINTS  NOTE: DO NOT REMOVE AFT CENTERBODY FOR THIS CHECK.  ACCESS: 455AL 456AR  465AL 466AR  783100-0801-2 430 THRUST REVERSER SYSTEM CONTROL ENG FUC I: 1500 FC CESM AMM 783100/2 440 GE-CESM 76 R PARTIALLY DEPLOY AND STOW EACH REVERSER HALF 9  BY DRIVING THROUGH THE CENTER GEAR BOX REDUNDANT PAD  AND CHECK RUNNING TORQUE WHILE DEPLOYING AND STOWING  THRUST REVERSER  ACCESS: 435AL 436AR  445AL 446AR  SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 783100-0801-5 450 THRUST REVERSER SYSTEM CONTROL ENG RAR I: 7200 FC CESM AMM 783102/2 460 AMM 783103/2 REMOVE FAN REVERSER ACTUATOR GEARBOXES AND GE-CESM 76 R RETURN TO OVERHAUL FACILITY FOR GREASE PACKING 9  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783100-0801-6 210 THRUST REVERSER SYS. CONTR. ENG OPC I: 1500 FC CESM AMM 783100/2 GE-CESM 76 R OPERATIONAL CHECK OF THRUST REVERSER COCKPIT 9  INDICATING LIGHTS  783100-0801-7 450 THRUST REVERSER SYSTEM ENG CHK I: NOTE CN CN  460 EUAD 1999-422-IMP FAN REVERSER HEALTH CHECKS. FAA AD EUAD AD  2008-02-17  NOTE : INTERVAL IN ACCORDANCE WITH VENDOR FAA AD 99-18 RECOMMENDATIONS SB GE  SBA78-3001  ACCESS: 435AL 436AR 455AL 456AR  445AL 446AR 465AL 466AR  783100-0801-9 450 THRUST REVERSER SYSTEM CONTROL ENG DET I: 8000 FH CN CN F-2005-20 460 ISB ISB 78-0025  DETAILED INSPECTION OF THE THRUST REVERSER  DIRECTIONAL PILOTING VALVE (DPV) AND ITS ASSOCIATED  CONTROL MECHANISM.  ACCESS: 435AL 436AR 455AL 456AR  445AL 446AR 465AL 466AR  783100-0802-1 450 PNEUMATIC DRIVE MOTOR FILTER ENG RAR I: 1500 FC CESM AMM 783101/2 460 GE-CESM 76 R REMOVE AND REPLACE INLET FILTER SCREEN OF 9  PNEUMATIC DRIVE MOTOR  ACCESS: 436AR 452AR 456AR  446AR 462AR 466AR  SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 783100-0802-2 450 THRUST REVERSER STRUCTURE ENG DET I: 1500 FC CESM AMM 783100/2 460 GE-CESM 76 R DETAILED INSPECTION OF FAN REVERSER STRUCTURE 9  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  783100-0802-3 430 THRUST REVERSER SYS. CONTR. ENG GVI I: 1500 FC CESM GE-CESM 76 R 440 9  VISUAL INSPECTION OF PRESSURE REGULATOR FLANGE FOR  LOOSENED BOLTS  ACCESS: 436AR 452AR 456AR  446AR 462AR 466AR  783100-0802-4 450 PNEUM. DRIVE MOTOR MEC GVI I: 500 FC CESM AMM 783100/2 460 GE-CESM 76 R GENERAL VISUAL INSPECTION OF: 9  - REVERSER DRIVE CABLES FOR CONDITION.  - SHAFT SEALS FOR LEAKAGE.  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783100-0802-5 450 PNEUM. DRIVE MOTOR MEC GVI I: 500 FC CESM AMM 783101/2 460 GE-CESM 76 R CHECK DRIVE MOTOR TEMPERATURE DECAL FOR 9  OVERTEMPERATURE.  ACCESS: 436AR 452AR  446AR 462AR  783100-0802-6 430 THRUST REVERSER SYSTEM CONTROL ENG FUC I: 1500 FC CESM AMM 783100/2 440 GE-CESM 76 R GAP CHECK BETWEEN TRANSLATING COWL AND SUPPORT 9  ASSEMBLY (IF NOT WITHIN SPECIFIED LIMITS, ADJUST ROD  END BEARINGS ON BALL SCREW ACTUATOR TO OBTAIN CORRECT  GAP) SERVICE FLEXIBLE SHAFTS AND PERFORM RIGGING IF  REQUIRED  ACCESS: 435AL 436AR 455AL 456AR  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 783100-0802-6 * * * * * C O N T I N U E * * * * *  445AL 446AR 465AL 466AR  783100-0802-7 430 FAN REVERSER FEEDBACK MECHANISM ENG GVI I: 1500 FC MRB AMM 783100/2 440 GE-CESM 76 R VISUAL INSPECTION OF PNEUMATIC VALVES AND ELECTRICAL 9  SWITCHES CAM FOLLOWERS FOR WEAR AND FREE ROTATION BY  HAND  ACCESS: 435AL 436AR  445AL 446AR  783100-0802-8 430 THRUST REVERSER SYSTEM CONTROL ENG DET I: 1500 FC CESM AMM 783112/2 440 GE-CESM 76 R 01. REMOVE MAIN AND INTERCONNECTING DRIVE CABLES 9  02. PERFORM DRIVE CABLE CASING CHECK. PULL ALL CORES  AND INSPECT FOR BROKEN WIRES, DEFORMATION  LOCAL BOWING AND WEAR. LUBRICATE EXTERIOR OF  CORES AFTER WIPING WITH A LINT FREE CLOTH DAM-  PENED WITH SOLVENT  03. REINSTALL DRIVE CABLES AND PERFORM GAP CHECK  AND RIGGING  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783100-0802-9 450 THRUST REVERSER SYS. CONTR. ENG DET I: 1500 FC CESM AMM 783100/2 460 GE-CESM 76  CHECK TORQUE OF V-BAND CLAMPS IN THE REVERSER  AIR SYSTEM  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  783100-0803-1 450 THRUST REVERSER SYS. CONTR. ENG CLN I: 1 C MRB AMM 783105/2 460  REMOVE, INSPECT AND CLEAN PRESSURE REGULATOR  FILTER  ACCESS: 436AR 452AR  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 783100-0803-1 * * * * * C O N T I N U E * * * * *  446AR 462AR  783100-0805-2 450 FAN REVERSER BALL SCREW MEC LUB I: 1000 FC MRB AMM 122271/0 460 GE-CESM 76 R LUBRICATION OF FAN REVERSER BALL SCREW ACTUATORS. 9  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783100-0805-3 450 PNEUM. DRIVE MOTOR MEC RPL I: 500 FC CESM AMM 783101/2 460 GE-CESM 76 R CHECK PNEUM. DRIVE MOTOR OIL LEVEL, 9  REPLENISH IF NECESSARY.  ACCESS: 436AR 452AR  446AR 462AR  783100-0805-5 450 THRUST REVERSER SYSTEM CONTROL ENG RPL I: 1500 FC CESM AMM 783101/2 460 GE-CESM 76 R DRAIN AND FLUSH DRIVE MOTOR. REFILL WITH 9  110 CC OF OIL  ACCESS: 436AR 452AR  446AR 462AR  783100-0811-1 450 THRUST REVERSER SYS. CONTR. ENG OPC I: 3 C MRB ** AMM 783100/5 460  OPERATIONAL TEST OF THRUST REVERSER DEPLOYMENT  INHIBITION  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783100-0811-2 430 THRUST REVERSER SYS. CONTR. ENG GVI I: 5 A MPD AMM 783115/2 440  WITH THRUST REVERSER IN STOWED POSITION, CHECK THAT  TRANSLATING SLEEVES ARE RESTING ON THE RUBBER RING  AGAINST 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 783211/2 440  CHECK SMOOTH OPERATION OF THRUST REVERSER WHILE  DEPLOYING AND STOWING TRANSLATING SLEEVES BY  ACTUATING THE SYSTEM THROUGH DRIVE PAD ON EITHER  LOWER SLAVE ACTUATOR.  ACCESS: 435AL 436AR  445AL 446AR  783100-0811-6 450 THRUST REVERSER SYS. CONTR. ENG RAR I: 3 C MPD AMM 783100/4 460  REMOVE FAN REVERSER ACTUATOR GEARBOXES AND  RETURN TO OVERHAUL FACILITY FOR GREASE PACKING  ACCESS: 435AL 436AR  445AL 446AR  783100-0812-2 430 THRUST REVERSER SYS. CONTR. ENG CHK I: 1 C MPD AMM 783112/4 440  01. REMOVE MAIN AND INTERCONNECTING DRIVE CABLES  02. PERFORM DRIVE CABLE CASING CHECK. PULL ALL CORES  AND INSPECT FOR BROKEN WIRES, DEFORMATION  LOCAL BOWING AND WEAR. LUBRICATE EXTERIOR OF  CORES AFTER WIPING WITH A LINT FREE CLOTH DAM-  PENED WITH SOLVENT  03. REINSTALL DRIVE CABLES AND PERFORM GAP CHECK  AND RIGGING  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783100-0812-3 430 THRUST REVERSER SYS. CONTR. ENG GVI I: 1 C MRB AMM 783100/0 440  GENERAL VISUAL INSPECTION OF ELECTRICAL SWITCHES FOR  CONDITION 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  445AL 446AR 461AL 462AR  783100-0815-1 450 FAN REVERSER BALL SCREW ENG LUB I: 800 FC MRB AMM 122278/0 460  CLEAN AND LUBRICATE FAN REVERSER BALL SCREW  ACTUATOR BALL NUTS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783200-0802-1 450 FAN THRUST REVERSER BLOCKER DOORS ENG GVI I: 1500 FC CESM AMM 783200/6 460 GE-CESM 76 R CHECK HINGE LUG BEARINGS OF FAN THRUST REVERSER 9  BLOCKER DOORS FOR CONDITION  ACCESS: 436AR 452AR 456AR  446AR 462AR 466AR  783200-0805-1 450 FAN REVERSER FEEDBACK MECH. ENG LUB I: 800 FC MRB GE-CESM 76 R 460 9  LUBRICATE ALL MOVING PARTS OF FAN REVERSER  FEED BACK MECHANISM  ACCESS: 435AL 436AR  445AL 446AR  783200-0815-1 450 FAN REV. STOW LATCHES ENG LUB I: 5 A MRB AMM 122271/0 460  CLEAN AND LUBRICATE THRUST REVERSER STOW LATCHES  AND ROD END OF INTERLOCK PUSH-PULL CABLE  ACCESS: 435AL 436AR  445AL 446AR  783300-0802-1 450 FIXED CORE EXHAUST NOZZLE ENG DET I: 3 C MPD AMM 781200/6 460  DETAILED INSPECTION OF FIXED NOZZLE FOR  * * * * * C O N T I N U E D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AND  CRACKS  ACCESS: 435AL 436AR 452AR 455AL 456AR  445AL 446AR 462AR 465AL 466AR  783300-0812-1 450 FIXED CORE EXHAUST NOZZLE ENG DET I: 3 C MPD AMM 781000/0 460  DETAILED INSPECTION OF FIXED NOZZLE FOR  SATISFACTORY CONDITION, SECURITY OF ATTACHMENT AND  CRACKS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783600-0801-2 430 FAN REVERSER DOOR OPENING SYSTEM MEC OPC I: 1500 FC CESM AMM 783100/2 440 GE-CESM 76 R OPERATIONAL CHECK OF FAN REVERSER DOOR POWER-OPENING 9  SYSTEM.  783600-0802-1 450 FAN REVERSER COWL DOOR SYS. ENG GVI I: 1500 FC CESM AMM 783100/2 460 AMM 783600/2 01. VISUAL INSPECTION OF ACTUATOR MOUNT CUP AND GE-CESM 76 R BRACKET FOR CRACKS 9  02. CHECK ALL CONNECTIONS AND FITTINGS IN SYSTEM  FOR LEAKS  ACCESS: 435AL 436AR 451AL 452AR 455AL 456AR  445AL 446AR 461AL 462AR 465AL 466AR  783600-0812-1 430 FAN REV. DOORS OPEN. SYSTEM ENG OPC I: 3 A MPD AMM 711300/3 440 AMM 783100/5 01. VISUAL INSPECTION FOR CRACKS OF MOUNTING FLANGE  AND FORK OF THRUST REVERSER DOOR OPENING ACTU-  ATORS  02. CHECK SMOOTH OPERATION DURING CLOSING  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

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SAMPLE 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 122278/0 460  CLEAN AND LUBRICATE THRUST REVERSER DOOR JACK  SCREWS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  783605-0802-1 450 THRUST REVERSER HOLD OPEN RODS ENG DET I: 3000 FH MPD SB GE 78-228  460  DETAILED INSPECTION OF HOLD OPEN ROD ASSEMBLY  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : EXHAUST REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 790000-0805-2 430 ENGINE OIL SYSTEM ENG RPL I: 150 FC CESM AMM 121379/0 440 GE-CESM 76 R CHECK ENGINE OIL LEVEL BY DIPSTICK AND PERFORM 9  SNIFF SMELL CHECK  NOTE: OBSERVE COLOR OF OIL,VERY DARK OIL COULD  INDICATE CONTAMINATION OR BEARING DISTRESS  ACCESS: 436DR  446DR  790000-0805-3 430 OIL-GENERAL MEC DET I: 150 FC CESM AMM 123279/0 440 GE-CESM 111  TAKE OIL SAMPLE FROM ENGINE OIL TANK FOR GE-CESM 76 R SOAP-INSPECTION. 9  NOTE: OIL SAMPLE SHOULD BE TAKEN WITHIN 45 MIN  AFTER ENGINE SHUT-DOWN.  ACCESS: 435AL 436AR  445AL 446AR  790000-0815-1 430 ENGINE OIL SYSTEM ENG RPL I: DY-TERM MRB AMM 121379/0 440  CHECK ENGINE OIL LEVEL AT TANK FILLER NECK  NOTE:-WHEN SERVICING OIL TANK SMELL FOR PRESENCE OF  FUEL IN OIL  -OBSERVE COLOR OF OIL.VERY DARK OIL COULD  INDICATE CONTAMINATION OR BEARING DISTRESS  ACCESS: 436CR  446CR  791100-0815-1 430 LUBRICATION SYSTEM ENG RPL I: NOTE 5-2 MPD AMM 123279/0 440  OIL SAMPLE EVALUATION FOR S.O.A.P.  NOTE: SAMPLE SHALL BE TAKEN FROM THE MIDDLE  OF THE ENGINE OIL TANK WITHIN 30 MIN. AFTER  ENGINE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

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SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 791100-0815-1 * * * * * C O N T I N U E * * * * *  ACCESS: 436AR  446AR  792100-0812-1 435 MAIN (SUPPLY) OIL FILTER ENG RAR T: NOTE MPD AMM 792103/4 445 I: 5 A  REMOVE AND INSPECT (FOR PARTICLES) THE MAIN (SUPPLY)  OIL FILTER. INSTALL A NEW FILTER ELEMENT.  NOTE: FIRST INSPECTION 3 MO AFTER  ENGINE INSTALLATION.  ACCESS: 435AL 436AR  445AL 446AR  792101-0802-1 435 PUMP-LUBE AND SCAVENGE ENG CLN T: 150 CSN CESM AMM 792101/3 445 I: 1500 FC GE-CESM 76 R REMOVE AND INSPECT FOR PARTICLES BEFORE CLEANING 9  THE LUBE SUPPLY OIL FILTER ELEMENT ASSEMBLY AND LUBE  PUMP SUPPLY INLET SCREEN  ACCESS: 435AL 436AR  445AL 446AR  792101-0802-2 435 PUMP-LUBE AND SCAVENGE ENG CLN T: 150 CSN CESM AMM 792101/3 445 I: 600 FC GE-CESM 76 R REMOVE AND INSPECT FOR PARTICLES BEFORE CLEANING 9  THE LUBE SCAVENGE PUMP INLET SCREEN.  ACCESS: 435AL 436AR  445AL 446AR  792201-0802-1 435 SCAVENGE OIL FILTER ENG CLN T: 150 CSN CESM AMM 792201/3 445 I: 1500 FC CESM  REPLACE LUBE SCAVENGE FILTER CESM 76 REV  ACCESS: 435AL 436AR  445AL 446AR  SYSTEMS AND POWERPLANT PROGRAM : ENGINE - OIL REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

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SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 792203-0802-1 435 OIL MAGNETIC CHIP DETECTOR ENG GVI I: 150 FC MRB AMM 792203/3 445 GE-CESM 76 R REMOVE AND INSPECT BEFORE CLEANING MASTER 9  MAGNETIC CHIP DETECTOR FOR METAL PARTICLES  ACCESS: 435AL 436AR  445AL 446AR  792203-0812-1 435 OIL MAGNETIC CHIP DETECTOR ENG GVI I: 250 FH MRB AMM 792203/3 445 SB PW 5890  01. REMOVE THE FOLLOWING MAGNETIC PLUGS TO CHECK  FOR METAL DEPOSITS BEFORE CLEANING :  - NO. 1 & 2 BEARING SCAVENCE PLUG  - NO. 3 BEARING SCAVENGE PLUG  - NO. 4 SCAVENGE PLUG  02. REINSTALL  ACCESS: 435AL  445AL  792204-0802-1 435 LUBE SCAVENGE PUMP ENG CLN I: NOTE CESM AMM 792101/3 445 GE-CESM 76 R REMOVE AND INSPECT FOR PARTICLES BEFORE CLEANING 9  THE LUBE SCAVENGE PUMPS SCREEN (5 OFF) AND - IF  INSTALLED - INSPECT FOR CHIPS THE SCAVENGE ISOLATION-  MAGNETIC PLUGS (5 OFF)  NOTE: - SCAVENGE PUMP SCREENS : FIRST INSPECTION  500FH/150CY AFTER ENGINE INSTALLATION THERE-  AFTER EVERY 2000FH/600CY  - ISOLATION MAGNETIC PLUGS INSPECT EVERY  500FH/150CY  ACCESS: 435AL 436AR  445AL 446AR  793000-0802-1 430 OIL INDICATION SYSTEM ENG GVI I: C MRB AMM 793000/6 440 OR  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

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SAMPLE 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 HARNESS  FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,  CORROSION, DETERIORATION, CRACKS, DENTS AND FREEDOM  FROM LEAKS  ACCESS: 435AL 436AR 451AL 452AR  445AL 446AR 461AL 462AR  793000-0812-1 430 OIL INDICATION SYSTEM ENG GVI I: C MRB AMM 793000/0 440 OR  GENERAL 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 HARNESS  FOR SATISFACTORY CONDITION, SECURITY OF ATTACHMENT,  CORROSION, DETERIORATION, CRACKS, DENTS AND FREEDOM  FROM LEAKS  ACCESS: 436AR  446AR  793500-0801-1 435 OIL FILTER CLOGGING INDICATING ENG FUC I: ENG. CHG MRB AMM 793511/4 445  TEST OF MAIN OIL FILTER CLOGGING INDICATING SYSTEM  793500-0801-2 212 OIL FILTER CLOGGING INDICATING ENG OPC I: ENG. CHG MPD AMM 793500/0 BITE TEST OF SCAVENGE OIL FILTER MAGNETIC INDICATOR  793500-0811-1 435 OIL FILTER CLOGG. INDICAT. ENG FUC I: ENG. CHG MRB AMM 793511/4 445  TEST OF MAIN OIL FILTER CLOGGING INDICATING SYSTEM  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE - OIL REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

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SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 801300-0802-1 430 PNEUMATIC STARTER AND VALVE MEC DET I: 1500 FC CESM AMM 801302/2 440 GE-CESM 76 R REMOVE ENGINE STARTER VALVE FILTER, INSPECT, CLEAN 9  AND REINSTALL.  ACCESS: 436AR  446AR  801300-0811-1 430 AIR FILTER (ENGINE) ENG CLN I: 1 C MPD AMM 801307/4 440  CLEAN AIR FILTER OF PNEUMATIC STARTER VALVE  ACCESS: 436AR  446AR  801301-0805-1 430 PNEUMATIC STARTER ENG RPL I: 300 FC CESM AMM 121380/0 440 GE-CESM 76 R OIL CHANGE OF PNEUMATIC STARTER 9  ACCESS: 435AL 436AR  445AL 446AR  801301-0805-2 430 PNEUMATIC STARTER ENG RPL I: 150 FC CESM AMM 121380/0 440 MRB AMM 801301/2 CHECK AND TOP UP OIL LEVEL OF PNEUMATIC STARTER AND GE-CESM 76 R CHECK MAGNETIC PLUG FOR METAL PARTICLES 9  ACCESS: 435AL 436AR  445AL 446AR  801301-0815-1 430 PNEUMATIC STARTER ENG RPL I: 3 A MPD AMM 121380/0 440  OIL CHANGE OF PNEUMATIC STARTER  ACCESS: 435AL 436AR  445AL 446AR  801301-0815-2 430 PNEUMATIC STARTER ENG RPL I: 1 A MRB AMM 121380/0 440 AMM 801301/2 CHECK 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  445AL 446AR  * * * * * E N D * * * * *  SYSTEMS AND POWERPLANT PROGRAM : ENGINE - STARTING REV. DATE: APR 01/10 SECTION: 
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 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. 
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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. 
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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. 
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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 tasks 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 calling 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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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 510000-0603-1 000 STRUCTURES - GENERAL MEC GVI I: SEE ISB ISB ISB 20-0007  GENERAL VISUAL INSPECTION OF ALL EXPOSED UNPAINTED  CADMIUM PLATED PARTS FOR CORROSION.  * * * * * E N D * * * * *  STRUCTURE PROGRAM : STRUCTURES REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

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SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 521101-0602-1 831 FWD PASSENGER/CREW DOORS MEC GVI I: 5 YE CPCP MRB REFERENC 841 MRB S  GENERAL VISUAL INSPECTION OF FORWARD PASSENGER/CREW 521101-C602- DOOR EXTERNAL STRUCTURE  521110-0602-1 831 FWD PASSENGER/CREW DOORS MEC GVI I: 5 YE CPCP MRB REFERENC 841 MRB S  GENERAL VISUAL INSPECTION OF FORWARD PASSENGER/CREW 521110-C602- DOOR EXTERNAL STRUCTURE  521202-0602-1 831 FORWARD PASSENGER/CREW DOORS MEC DET I: 8500 FC MRB S AMM SSI 5212 841  DETAILED INSPECTION OF FWD PASSENGER/CREW  DOOR EXTERNAL STRUCTURE.  521202-0603-1 831 FORWARD PASSENGER/CREW DOORS MEC DET I: 5 YE CPCP AMM SSI 5212 841 MRB S  DETAILED INSPECTION OF FORWARD PASSENGER/CREW MRB REFERENC DOOR INTERNAL STRUCTURE.  521202-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 ,  G2 OR G3 AFTER INSPECTION  PREP.: ESCAPE SLIDE/RAFT, DOOR LINING AND INSULATION  REMOVED  521210-0602-1 832 MID PASSENGER/CREW DOORS MEC GVI I: 5 YE CPCP MRB REFERENC 842 MRB S  GENERAL VISUAL INSPECTION OF MID PASSENGER/CREW 521210-C602- DOOR EXTERNAL STRUCTURE  521403-0603-1 832 MID PASSENGER/CREW DOORS MEC DET I: 5 YE CPCP AMM SSI 5214 842 MRB S  DETAILED INSPECTION OF MID PASSENGER/CREW DOOR MRB REFERENC INTERNAL STRUCTURE.  521403-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2  OR G3 AFTER INSPECTION  PREP.: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 521403-0603-1 * * * * * C O N T I N U E * * * * *  REMOVED  521409-0602-1 832 SKIN OF MID PASS/CREW DOOR MEC DET I: 7000 FC MRB S AMM SSI 5214 842  DETAILED INSPECTION OF EXTERNAL  SKIN AND RIVETS OF MID PASSENGER/CREW DOOR.  521801-0602-1 833 AFT PASSENGER/CREW DOORS MEC GVI I: 5 YE SSI  843  GENERAL VISUAL INSPECTION OF AFT PASSENGER/CREW  DOOR EXTERNAL STRUCTURE  521803-0602-1 833 AFT PASSENGER/CREW DOORS MEC DET I: 8500 FC MRB S AMM SSI 5218 843  DETAILED INSPECTION OF EXTERNAL STRUCTURE  OF AFT PASSENGER/CREW DOOR.  521803-0603-1 833 AFT PASSENGER/CREW DOORS MEC DET I: 5 YE CPCP AMM SSI 5218 843 MRB S  DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR MRB REFERENC INTERNAL STRUCTURE.  521803-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2  OR G3 AFTER INSPECTION  PREP.: ESCAPE SLIDE/RAFT, DOOR LINING AND INSULATION  REMOVED  522201-0602-1 834 STRUCTURE OF EMERGENCY EXITS MEC GVI I: 5 YE CPCP MRB REFERENC 844 MRB S  GENERAL VISUAL INSPECTION OF EMERGENCY EXIT 522201-C602- EXTERNAL STRUCTURE  522601-0603-1 834 STRUCTURE OF EMERG.EXITS MEC DET I: 5 YE CPCP AMM SSI 5226 844 MRB S  DETAILED INSPECTION OF EMERGENCY EXITS  INTERNAL STRUCTURE.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 522601-0603-1 * * * * * C O N T I N U E * * * * *  522601-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2  OR G3 AFTER INSPECTION  PREP.: ESCAPE SLIDE/RAFT, DOOR LINING AND INSULATION  REMOVED  522605-0602-1 834 SKIN OF EMERGENCY EXITS MEC DET I: 7000 FC MRB S AMM SSI 5226 844  DETAILED INSPECTION OF EXTERNAL SKIN OF  EMERGENCY EXIT.  523301-0602-1 811 HINGE END OF FWD CARGO DOOR MEC DET T: 23300 FC ALI AMM SSI 5233 I: 3500 FC MRB S CN 2006-0071 DETAILED INSPECTION OF HINGE END OF FWD FAA AD 96-13 CARGO COMPARTMENT DOOR AT FRAMES 20B TO 24A  (9 PLACES) (AS FAR AS VISIBLE) ALI REFERENC 523301-01-1  ACCESS: 132AR  523301-0602-2 811 HINGE END OF FWD CARGO DOOR MEC DET T: 14000 FC ALI AMM SSI 5233 I: 3500 FC MRB S CN 2006-0071 DETAILED INSPECTION OF HINGE END OF FWD FAA AD 96-13 CARGO COMPARTMENT DOOR AT FRAMES 20B TO 25, AS  FAR AS VISIBLE. ALI REFERENC 523301-01-1  ACCESS: 132AR  523303-0603-1 811 LOCK MECHAN.ATTACH.FITTINGS MEC DET T: 12600 FC ALI AMM SSI 5233 I: 9500 FC MRB S CN 2006-0071 DETAILED INSPECTION OF INTERNAL LOCK MECHANISM FAA AD 96-13 ATTACH FITTINGS AND SUPPORT STRUCTURE OF FWD CARGO  COMPARTMENT DOOR AT ALL FRAMES LONGERON 4 TO 5 ALI REFERENC 523303-01-1  ACCESS: 811AR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 523204  PART 6  SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH NTM 523300  FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FRAME PART 6  22A. ISB 52-0136  NOTE: FORWARD CARGO COMPARTMENT DOOR  LINING TO BE REMOVED  523309-0602-1 811 SKIN OF FORWARD CARGO DOOR MEC DET T: 5 YE CPCP AMM SSI 5233 I: 7000 FC MRB S  DETAILED INSPECTION OF EXTERNAL FWD CARGO 30 MO MRB REFERENC COMPARTMENT DOOR SKIN AND RIVETS  523101-C602- 523315-0603-1 835 UDC-DOOR LOCKING-HOOKS MEC DET T: 12400 FC ALI AMM SSI 5233 I: 6200 FC MRB S AMM 523600/6 DETAILED INSPECTION OF INTERNAL UDC-DOOR CN 2006-0071 LOCKING-HOOKS AT FRAMES 20B TO 26A FAA AD 96-13 ( 8 PLACES )  ALI REFERENC ACCESS: 835 835BR 835CR 835DR 523315-01-1  523316-0603-1 835 UDC-DOOR LOCKING PLATES MEC DET I: 6000 FC MPD  DETAILED INSPECTION OF UDC-DOOR LOCKING  PLATES AT FRAMES 20B TO 26A (8 PLACES).  ACCESS: 835 835BR 835CR 835DR  523317-0603-1 835 ATTACH FITTING OF UDC-DOOR MEC DET T: 12200 FC ALI AMM SSI 5233 I: 6100 FC MRB S AMM 523600/6 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 MECHANISM ATTACH FITTINGS AND SUPPORT STRUCTURE OF FAA AD 96-13 UDC-DOOR AT ALL FRAMES, BETWEEN STRINGER 27 AND  STRINGER 30 AND BETWEEN LONGERON 8 AND 9. ALI REFERENC 523317-01-1  PREP.: DOOR LINING TO BE REMOVED.  ACCESS: 835 835BR 835CR 835DR  523317-0603-2 835 ATTACH FITTING OF UDC-DOOR MEC DET T: 12200 FC ALI AMM SSI 5233 I: 6100 FC MRB S CN 2006-0071 DETAILED INSPECTION OF INTERNAL LOCKING FAA AD 96-13 MECHANISM ATTACH FITTINGS AND SUPPORT STRUCTURE OF  UDC-DOOR AT ALL FRAMES, BETWEEN STRINGER 27 AND ALI REFERENC STRINGER 30 AND BETWEEN LONGERON 8 AND 9. 523317-01-1  PREP.: DOOR LINING TO BE REMOVED.  ACCESS: 835 835BR 835CR 835DR  523319-0603-1 835 ACTUATOR ATTACH FITTING, UDC DOOR MEC DET I: 6000 FC MRB S AMM SSI 5233 AMM 523600/6 DETAILED INSPECTION OF INTERNAL ACTUATOR  ATTACH FITTINGS OF UDC DOOR  PREP.: DOOR LININGS AND INSULATION REMOVED  ACCESS: 835  523321-0603-1 835 MECH. LINKAGE OF UDC DOOR ACTUATOR MEC DET I: 6000 FC MRB S AMM SSI 5233 AMM 523600/6 DETAILED INSPECTION OF INTERNAL MECHANICAL  LINKAGE OF UDC DOOR ACTUATOR UNIT CONSISTING OF  LEVER, BRACES, YOKE AND DOOR BOLTS.  PREP.: DOOR LININGS REMOVED  ACCESS: 835  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC MRB S  GENERAL VISUAL INSPECTION OF UPPER (MAIN) DECK CARGO 523601-C602- (UDC) DOOR EXTERNAL SURFACE.  523701-0602-1 812 HINGE END OF AFT CARGO DOOR MEC DET T: 12000 FC ALI AMM SSI 5237 I: 3000 FC MRB S NTM 523200  DETAILED INSPECTION OF EXTERNAL HINGE END PART 7  OF AFT CARGO COMPARTMENT DOOR AT FRAMES 60 TO 63 CN 2006-0071 7 PLACES) ESPECIALLY IN FLANGE RADII ADJACENT TO FAA AD 96-13 OUTER SKIN, CHECK WITH MAGNIFYING GLASS  ALI REFERENC ACCESS: 812AR 523701-01-1  523701-0602-2 812 HINGE END OF AFT CARGO DOOR MEC DET I: 1000 FC ALI NTM 523200  MRB S PART 7  DETAILED INSPECTION OF EXTERNAL HINGE END CN 2006-0071 OF AFT CARGO COMPARTMENT DOOR AT FRAMES 60 TO 63 FAA AD 96-13 7 PLACES) ESPECIALLY IN FLANGE RADII ADJACENT TO  OUTER SKIN, CHECK WITH MAGNIFYING GLASS ALI REFERENC 523701-01-2  ACCESS: 812AR  523707-0603-1 812 ACTUATOR ATTACH FITTING ON DOOR NDT SDI I: 6000 FC ISB NTM 523204  PART 6  SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH ISB 52-136  FITTING OF AFT CARGO COMPARTMENT DOOR AT FRAME 61A.  NOTE: AFT CARGO COMPARTMENT DOOR  LINING TO BE REMOVED  523715-0602-1 812 AFT CARGO COMPARTMENT DOOR MEC DET T: 5 YE SSI  I: 11200 FC  DETAILED INSPECTION OF EXTERNAL 30 MO  AFT CARGO COMPARTMENT DOOR SKIN AND RIVETS  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5237 I: 7000 FC MRB S  DETAILED INSPECTION OF EXTERNAL 30 MO MRB REFERENC BULK CARGO COMPARTMENT DOOR SKIN AND RIVETS  523401-C602- 523719-0602-1 813 BULK CARGO DOOR STOPS MEC DET T: 13300 FC ALI AMM SSI 5237 I: 6000 FC MRB S CN 2006-0071 DETAILED INSPECTION OF DOOR STOPS ON BULK FAA AD 96-13 CARGO COMPARTMENT DOOR AT FRAME 67 AND 69.  ALI REFERENC ACCESS: 813 523719-01-1  523719-0602-2 813 BULK CARGO DOOR STOPS MEC DET I: 1000 FC ALI ALI REFERENC MRB S 523719-01-1  DETAILED INSPECTION OF DOOR STOPS ON BULK  CARGO COMPARTMENT DOOR AT FRAME 67 AND 69.  ACCESS: 813  526101-0602-1 120 AVIONICS COMPARTMENT ACCESS DOOR MEC DET T: 40000 FC ALI CN 2006-0071 I: 24000 FC FAA AD 96-13 DETAILED INSPECTION OF AVIONICS COMPARTMENT  ACCESS DOOR INTERNAL STRUCTURE. ALI REFERENC 526101-01-1  PREP : FLOOR PANELS AND DOOR TO BE REMOVED.  ACCESS: 212BL  526101-0602-2 120 AVIONICS COMPARTMENT ACCESS DOOR MEC DET T: 40000 FC ALI CN 2006-0071 I: 24000 FC FAA AD 96-13 DETAILED INSPECTION OF AVIONICS COMPARTMENT  ACCESS DOOR INTERNAL STRUCTURE. ALI REFERENC 526101-01-1  PREP : FLOOR PANEL AND DOOR TO BE REMOVED  ACCESS: 212BL  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 533300  SI: 11200 FC PART 6  DETAILED INTERNAL AND EXTERNAL INSPECTION T: 12000 FC CN 2006-0071 OF HINGES OF UPPER DECK CARGO DOOR INCLUDING I: 11200 FC FAA AD 96-13 ADJACENT STRUCTURE BETWEEN DOOR STRS. 1 AND 3.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-01-1  526305-0606-3  PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOOR  LINING AND INSULATION TO BE REMOVED  PASSENGER CONFIGURATION : UPPER DECK CARGO  DOOR LINING, CEILING, INSULATION AND HATRACKS  TO BE REMOVED  ACCESS: 835  526305-0606-2 835 UPPER (MAIN) DECK CARGO DOOR HINGE MEC DET I: 11200 FC ALI NTM 533300  PART 6  DETAILED INTERNAL AND EXTERNAL INSPECTION CN 2006-0071 OF HINGES OF UPPER DECK CARGO DOOR INCLUDING FAA AD 96-13 ADJACENT STRUCTURE BETWEEN DOOR STRS. 1 AND 3.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-01-2  526305-0606-3  PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOOR  LINING AND INSULATION TO BE REMOVED  PASSENGER CONFIGURATION : UPPER DECK CARGO  DOOR LINING, CEILING, INSULATION AND HATRACKS  TO BE REMOVED  ACCESS: 835  526305-0606-3 835 UPPER (MAIN) DECK CARGO DOOR HINGE NDT SDI ST: 12000 FC ALI NTM 533300  SI: 11200 FC PART 6  SPECIAL DETAILED INSPECTION OF HINGES OF UPPER DECK CN 2006-0071 CARGO DOOR (UDC) INCLUDING ADJACENT STRUCTURE BETWEEN FAA AD 96-13 DOOR STRINGER 1 AND 3.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-02-1  526305-0606-1  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 526305-0606-3 * * * * * C O N T I N U E * * * * *  PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOOR  LINING AND INSULATION TO BE REMOVED  PASSENGER CONFIGURATION : UPPER DECK CARGO  DOOR LINING, CEILING, INSULATION AND HATRACKS  TO BE REMOVED  ACCESS: 835  526305-0606-4 835 UPPER (MAIN) DECK CARGO DOOR HINGE NDT SDI I: 11200 FC ALI NTM 533300  PART 6  SPECIAL DETAILED INSPECTION OF HINGES OF UPPER DECK CN 2006-0071 CARGO DOOR (UDC) INCLUDING ADJACENT STRUCTURE BETWEEN FAA AD 96-13 DOOR STRINGER 1 AND 3.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO THE TASK 526305-02-2  526305-0606-2  PREP.: CARGO CONFIGURATION : UPPER DECK CARGO DOOR  LINING AND INSULATION TO BE REMOVED  PASSENGER CONFIGURATION : UPPER DECK CARGO  DOOR LINING, CEILING, INSULATION AND HATRACKS  TO BE REMOVED  ACCESS: 835  528021-0603-1 811 CARGO COMPARTMENT DOORS MEC DET I: 5 YE CPCP AMM SSI 5237 812 MRB S AMM SSI 5237 813 DETAILED INSPECTION OF FORWARD, AFT AND REAR  CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE. MRB REFERENC NOTE: 01. DOOR LINING AND INSULATION TO BE REMOVED. 528021-C603- 02. APPLY TEMPORARY PROTECTION SYSTEM TYPE 1,  G2 OR G3 AFTER INSPECTION.  ACCESS: 811AR  812AR  528023-0603-1 835 UDC DOOR MEC DET I: 5 YE CPCP MRB REFERENC 528023-C603- 01. DETAILED INSPECTION OF INTERNAL STRUCTURE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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) DOOR  02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2  OR G3 AFTER INSPECTION.  PREP.: DOOR LINING AND INSULATION REMOVED.  ACCESS: 835AR 835BR 835CR 835DR 835ER 835FR  835GR  528203-0602-1 710 NOSE GEAR DOOR HINGES MEC SDI I: 8500 FC MRB S AMM SSI 5282 NTM 528211  DETAILED OR SPECIAL DETAILED INSPECTION OF EXTERNAL PART 4 AND 6  NOSE GEAR DOOR HINGES, ZONE 713,714,715,716  NOTE: FOR REARMOST HINGE, ONLY VISUAL INSPECTION OR  HF-EC INSPECTION IS REQUIRED IN ACCORDANCE WITH  ILLUSTRATION IN SECTION 13, OR IN ACCORDANCE  WITH NTM 52-82-11 PART 6, RESPECTIVELY  528503-0602-1 734 MAIN GEAR DOOR HINGES MEC SDI I: 8500 FC MRB S AMM SSI 5285 744 NTM 528112  DETAILED OR SPECIAL DETAILED INSPECTION OF EXTERNAL PART 6  MAIN GEAR DOOR HINGES  528505-0602-1 734 MLG-DOOR ACT.ATTACH.FITTING MEC SDI I: 8500 FC MRB S AMM SSI 5285 744 NTM 528112  DETAILED OR SPECIAL DETAILED INSPECTION OF EXTERNAL PART 4 AND 6  MAIN GEAR DOOR ACTUATING CYLINDER ATTACH FITTING  529003-0603-2 831 DOORS MEC DET T: 36 MO ISB CN  832 I: 36 MO 1999-410-294 833 DETAILED INSPECTION OF THE PAX DOOR EMERGENCY FAA AD  841 CYLINDER STRIKER MECHANISM. 2003-03-04  842 ISB 52-168  843 ACCESS : OPEN THE DOOR  * * * * * E N D * * * * *  STRUCTURE PROGRAM : DOORS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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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 132 I: 9000 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT FITTINGS FOR  FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENC TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-1  STRINGERS 40 AND 41, LH AND RH  PREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TO  TO BE REMOVED.  530407-0603-2 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET I: 4500 FC ALI CN 2006-0071 132 FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT FITTINGS FOR  FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENC TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-2  STRINGERS 40 AND 41, LH AND RH  PREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TO  TO BE REMOVED.  530407-0603-3 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET I: 4500 FC ALI CN 2006-0071 132 FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT FITTINGS FOR  FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENC TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-3  STRINGERS 40 AND 41, LH AND RH  PREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TO  TO BE REMOVED.  530407-0603-4 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET T: 17700 FC ALI CN 2006-0071 132 I: 9000 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT FITTINGS FOR  FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENC TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-5  STRINGERS 40 AND 41, LH AND RH  PREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TO  TO BE REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE 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 132 FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT FITTINGS FOR  FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENC TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-4  STRINGERS 40 AND 41, LH AND RH  PREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TO  TO BE REMOVED.  530407-0603-6 131 FLOOR BEAMS FROM FRAME 20 TO FRAME 38.2 MEC DET T: 17700 FC ALI CN 2006-0071 132 I: 9000 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT FITTINGS FOR  FORWARD CARGO COMPARTMENT FLOOR BEAMS FROM FRAMES 20 ALI REFERENC TO 38.2LH AND FR26 TO FR38.2RH INCLUDING SKIN BETWEEN 530407-01-6  STRINGERS 40 AND 41, LH AND RH  PREP.: LH, RH SIDE PANELS OF FWD CARGO COMPARTMENT TO  TO BE REMOVED.  530503-0603-1 147 KEEL BEAM INTERNAL STRUCT. MEC DET I: 9000 FH ISB CN  148 1979-125-018 DETAILED INSPECTION OF KEEL BEAM CENTER ISB 53-0096  AND SIDE WEBS AT FR. 47A AND FR. 53A (STRINGER 53LH,  RH AND STRG. 57) FOR CRACKS  ACCESS: 147AF 147SZ 147TZ  148AF 148SZ 148TZ  530505-0602-1 577 FLAP TRACK NO.1 ATT.FITTING MEC DET I: 5700 FC MRB S AMM SSI 5305 677  DETAILED INSPECTION OF ATTACHMENT FITTINGS AT  FLAP TRACK NO.1 TO FUSELAGE AT FRAME 51.  NOTE: AS ALTERNATE TO TASK 530505-0602-1  NDT INSPECTION OF FLAP TRACK NO.1  ATTACHMENT FITTINGS TO FUSELAGE AT  FRAME 51 INSIDE ZONE 577/677 CAN BE  PERFORMED ACCORDING TO NTM 531500 PART 6.  THIS INSPECTION REQUIRES REMOVAL OF FLAP  TRACK  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 530505-0604-1 147 FLAP TRACK NO.1 ATT.FITTING MEC DET I: 27300 FC MRB S AMM SSI 5305 148  DETAILED INSPECTION OF FLAP TRACK NO.1  ATTACHMENT FITTINGS TO FUSELAGE AT FRAME 51.  ACCESS: 147PZ 147QZ  148PZ 148QZ  530601-0604-1 577 SUPPORT STRUCTURE FRAM 54.1 MEC DET I: 8400 FC MRB S AMM SSI 5306 677  DETAILED INSPECTION OF SUPPORT STRUCTURE IN  AREA OF WING FLAP ATTACH FITTINGS ON FUSELAGE BETWEEN  FRAMES NO. 54.1 AND 54.2 AND BETWEEN STRINGERS 30 AND  35.  ACCESS: 577BB 677BB  530601-0604-2 577 SUPPORT STRUCTURE FRAM 54.1 MEC DET I: 8400 FC MRB S AMM SSI 5306 677  DETAILED INSPECTION OF SUPPORT STRUCTURE IN  AREA OF WING FLAP ATTACH FITTINGS ON FUSELAGE BETWEEN  FRAMES NO. 54.1 AND 54.2 AND BETWEEN STRINGERS 30 AND  35.  ACCESS: 577BB 677BB  530601-0604-3 577 SUPPORT STRUCTURE FRAM 54.1 MEC DET I: 8400 FC MRB S AMM SSI 5306 677  DETAILED INSPECTION OF SUPPORT STRUCTURE IN  AREA OF WING FLAP ATTACH FITTINGS ON FUSELAGE BETWEEN  FRAMES NO. 54.1 AND 54.2 AND BETWEEN STRINGERS 30 AND  35.  ACCESS: 577BB 677BB  531000-0602-2 100 FUSELAGE SKIN - SCUFF PLATE AREA MEC DET I: 30 MO MPD  200  DETAILED INSPECTION OF FUSELAGE SKIN AT EDGES  OF PAX CREW DOOR SCUFF PLATES (AND CARGO DOOR SCUFF  PLATES IF INSTALLED) FOR CORROSION AND SCUFF PLATE  EXTERNAL SURFACES FOR BULGING.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531000-0602-3 100 FUSELAGE JOINTS MEC DET I: ISB ISB ISB 53-0154  200 53-154  DETAILED INSPECTION OF LONGITUDINAL AND  CIRCUMFERENTIAL SKIN JOINTS FOR SEALING CONDITION AND  EXTERNAL SURFACE CORROSION.  NOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0154  531000-0602-4 100 FUSELAGE JOINTS MEC DET I: ISB ISB CN  200 53-178 1984-140-064 DETAILED EXTERNAL INSPECTION OF BONDED FAA AD  LONGITUDINAL AND CIRCUMFERENTIAL JOINTS FOR CORROSION 2000-16-07  ISB 53-0178  NOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0178  531000-0603-1 100 FUSELAGE JOINTS NDT SDI I: ISB ISB NTM 533010  200 53-148 PART 4 AND 6  SPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP NTM 533020  JOINTS AND CIRCUMFERENCIAL JOINTS FOR BONDING PART 4 AND 6  DELAMINATION. NTM 533030  PART 5  NOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0148 CN  1984-140-064 FAA AD  2000-16-07  ISB 53-0148  531000-0603-2 100 FUSELAGE STRINGERS/DOUBLERS NDT SDI I: ISB ISB NTM 531010  200 53-149 PART 4, 5  SPECIAL DETAILED INSPECTION OF BONDED STRINGERS AND NTM 533050  DOUBLERS FOR BONDING DELAMINATION. PART 5  CN  NOTE: FOR AFFECTED AREAS PER MSN REFER TO ISB 53-0149 1984-140-064 FAA AD  2000-16-07  ISB 53-0149  531000-0603-5 100 FUSELAGE LAP JOINTS NDT SDI T: 24000 FC ISB NTM 533010  200 NOTE NTM 533010  SPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP I: 6000 FC PART 4  JOINTS IN SECTION 14, 16 AND 17 AT SPECIAL AREAS NOTE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531000-0603-5 * * * * * C O N T I N U E * * * * *  NTM 533010  NOTE: FOR THRESHOLD AND FOLLOW UP INTERVALS OF PART 6  REPAIRED AREAS REFER TO ISB 53-0211 CATEGORY 3. CN  1989-061-092 FAA AD 90-01 ISB 53-0211  531000-0603-6 100 FUSELAGE LAP JOINTS NDT SDI T: 32000 FC ISB NTM 533010  200 NOTE PART 4 CONFI SPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP I: 6000 FC PART 6  JOINTS IN SECTION 13 THRU 18 AT STANDARD AREAS NOTE CONFIG 1 TO  CN  NOTE: 01. FOLLOW-UP INTERVAL FOR LAP JOINTS WITH 1989-061-092 BONDED DOUBLERS 6000 FC FAA AD 90-01 ISB 53-211  02. FOLLOW-UP INTERVAL FOR LAP JOINTS WITHOUT  BONDED DOUBLERS 8000 FC.  03. FOR THRESHOLD AND FOLLOW-UP INTERVALS OF  REPAIRED AREAS REFER TO ISB 53-0211 CATE-  GORY 3.  ACCESS: 577AB 577AT 577BB 577BT 577CT 577DT  577ET 577GT 677AB 677AT 677BB 677BT  677CT 677DT 677ET 677GT  531000-0603-7 100 FUSELAGE LAP JOINTS NDT SDI T: NOTE ISB NTM 533010  200 I: 5000 FC PART 4 CONFI SPECIAL DETAILED INSPECTION MODIFIED LONGITUDINAL LAP PART 6  JOINTS IN SECTION 13/14 AND 18 CONFIG 1 TO  CN  NOTE: 01. THRESHOLD 32000 FC FOR LAP JOINTS WITH 1989-061-092 CUT OUT, SB 53-206 OR SB 53-209 FAA AD 90-01 02. THRESHOLD 32000 FC FOR LOWER SHELL (4 PANEL ISB 53-0211  SOLUTION), SB 53-215  03. THRESHOLD 32000 FC FOR LOWER SHELL (3 PANEL  SOLUTION), SB 52-216  04. THRESHOLD 42000 FC FOR LAP JOINTS WITHOUT  CUT OUT, SB 53-209  05. THRESHOLD 42000 FC FOR LAP JOINTS SB 53-223  06. 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531000-0603-7 * * * * * C O N T I N U E * * * * *  JOINTS, SB 53-306  531001-0603-1 230 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 533010  240 OR PART 6  SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 15 YE NTM 533040  OF LONGITUDINAL LAP JOINTS, IN SECTION 13 AND 14, I: 12000 FC PART 5  ABOVE AND INCLUDING STR 22 LH/RH EXCEPT STR 22 RH IN OR CN  SECTION 13. 7 YE 1989-061-092 FAA AD 90-01 NOTE: 01. MSN 102, 103 ONLY SECTION 14 EFFECTED ISB 53-0229  02. LINING, HATRACKS AND INSULATION TO BE  REMOVED AS REQUIRED.  531001-0603-2 130 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 533010  140 OR PART 6  240 SPECIAL DETAILED INSPECTION BONDED INNER DOUBLERS OF 15 YE NTM 533040  250 LONGITUDINAL LAP JOINTS, IN SECTION 15 THRU 18 EXCEPT I: 12000 FC PART 5  260 STR 31 LH/RH AND SECTION 13 AND 14, BELOW STR 22, OR CN  (INCLUDING ZONE 140, 240, 250 AND 260). 102 MO 1989-061-092 FAA AD 90-01 NOTE: LININGS, HATRACKS AND INSULATION TO BE ISB 53-0229  REMOVED AS REQUIRED.  531001-0603-3 150 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 533010  160 OR PART 6  SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 12 YE NTM 533040  OF LONGITUDINAL LAP JOINTS, IN SECTION 16 AND 17, STR I: 12000 FC PART 5  31 (INCLUDING ZONE 160). OR CN  7 YE 1989-061-092 NOTE: INSULATION TO BE REMOVED AS REQUIRED FAA AD 90-01 ISB 53-0229  531001-0603-5 130 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 533010  OR PART 6  SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 15 YE NTM 533040  LONGITUDINAL LAP JOINTS, IN SECTION 14 AT STR. 47 LH I: 12000 FC PART 5  AND STR. 49 RH BETWEE FR. 26 AND FR. 38.1. OR CN  7 YE 1989-061-092 NOTE: INSULATION TO BE REMOVED AS REQUIRED FAA AD 90-01 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531001-0603-5 * * * * * C O N T I N U E * * * * *  ISB 53-0229  531001-0603-6 130 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 533010  240 OR PART 6  SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLERS 15 YE NTM 533040  LONGITUDINAL LAP JOINTS, IN SECTION 14 I: 12000 FC PART 5  - AT STR. 22 LH AND AT STR. 31 LH, BETWEEN FRAME 16 OR CN  AND FRAME 39 7 YE 1989-061-092 - AT STR. 47 LH AND AT STR. 49 RH BETWEEN FRAME 26 FAA AD 90-01 AND FRAME 38.1 ISB 53-0229  PREP.: LININGS AND INSULATION TO BE REMOVED  AS REQUIRED.  531001-0603-7 230 INNER DOUBLER NDT SDI T: 24000 FC ISB NTM 533010  240 OR PART 6  SPECIAL DETAILED INSPECTION OF BONDED INNER DOUBLER 15 YE NTM 533040  OF LONGITUDINAL LAP JOINTS, IN SECTION 14 AT STR. 5 I: 12000 FC PART 5  LH BETWEEN FR. 26 AND FR 38.1 (INCLUDING ZONE 240). OR CN  7 YE 1989-061-092 PREP.: INSULATION TO BE REMOVED FAA AD 90-01 ISB 53-0229  531101-0602-1 211 SECTION OF FRAMES 2 TO 6 MEC DET I: 7000 FC MRB S AMM SSI 5311 212  DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS IN AREA OF FRAMES 2 TO 6 EXTENDING FROM WIND-  SHIELD TO FLIGHT COMPARTMENT FLOOR  531105-0602-1 121 FRAMES 2 TO 9 MEC DET I: 8500 FC MRB S AMM SSI 5311 122  DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS 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 FAA AD 96-13 DETAILED INSPECTION OF FWD PRESSURE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 531107-0602-1 * * * * * C O N T I N U E * * * * *  BULKHEAD FRONT FACE SURROUNDING FRAME 1 AND FUSELAGE ALI REFERENC SKIN AT ATTACHMENT WITH FRAME 1. 531107-01-1  ACCESS: 110AL  531107-0602-2 110 FWD PRESSURE BULKHEAD MEC DET I: 9200 FC ALI CN 2006-0071 FAA AD 96-13 DETAILED INSPECTION OF FWD PRESSURE  BULKHEAD FRONT FACE SURROUNDING FRAME 1 AND FUSELAGE ALI REFERENC SKIN AT ATTACHMENT WITH FRAME 1. 531107-01-2  ACCESS: 110AL  531107-0602-3 110 FWD PRESSURE BULKHEAD MEC DET I: 9200 FC ALI CN 2006-0071 FAA AD 96-13 DETAILED INSPECTION OF FWD PRESSURE  BULKHEAD FRONT FACE SURROUNDING FRAME 1 AND FUSELAGE ALI REFERENC SKIN AT ATTACHMENT WITH FRAME 1. 531107-01-3  ACCESS: 110AL  531115-0602-1 211 FRAME 7 ABOVE WINDSHIELD MEC DET I: 8500 FC MRB S AMM SSI 5311 212  DETAILED INSPECTION OF EXTERNAL STRUCTURE IN  AREA OF FRAME 7 ABOVE WINDSHIELD.  531120-0602-1 211 WINDSHIELD CENTER POST MEC DET I: 7000 FC MRB S AMM SSI 5311 212  DETAILED INSPECTION OF EXTERNAL WINDSHIELD  CENTER POST.  531120-0604-1 211 WINDSHIELD CENTER POST MEC DET I: 27300 FC MRB S AMM SSI 5311 NTM 531100  DETAILED INSPECTION OF INTERNAL WINDSHIELD PART 2  CENTER POST  -NDT INSPECTION, CAN BE CARRIED OUT AS ALTERNATE TO  VISUAL INSPECTION WITHOUT LINING REMOVAL ACCORDING  TO NTM 531100 PART 2 -  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 531120-0604-1 * * * * * C O N T I N U E * * * * *  NOTE: LINING REMOVED  531121-0602-1 211 WINDSHIELD SIDE POST FRAME 7 MEC DET I: 5700 FC ALI CN 2006-0071 212 FAA AD 96-13 DETAILED INSPECTION OF EXTERNAL WINDSHIELD  SIDE POST AT FRAME 7. ALI REFERENC 531121-01-1  531121-0604-1 211 WINDSHIELD SIDE POST FR. 7 MEC DET I: 27300 FC MRB S AMM SSI 5311 NTM 531100  DETAILED INSPECTION OF INTERNAL WINDSHIELD PART 6  SIDE POST AT FRAME 7  -NDT INSPECTION CAN BE CARRIED OUT AS ALTERNATE TO  VISUAL INSPECTION, WITHOUT LINING REMOVAL ACCORDING  TO NTM 531100 PART 6  NOTE: LINING REMOVED  531125-0602-1 211 SIDE WINDOWS STRUCTURE MEC DET I: 7500 FC ALI CN 2006-0071 212 FAA AD 96-13 DETAILED INSPECTION OF EXTERNAL  STRUCTURE IN AREA OF SIDE WINDOWS UPPER ALI REFERENC AND LOWER SECTIONS BETWEEN FRAMES 2 AND 10, 531125-01-1  ESPECIALLY THE LOWER CORNER ADJOINING FRAME 10  531125-0604-1 211 SIDE WINDOWS STRUCTURE MEC DET I: 27300 FC MRB S AMM SSI 5311 NTM 531100  DETAILED INSPECTION OF INTERNAL SIDE WINDOWS, PART 2  UPPER AND LOWER STRUCTURE BETWEEN FRAME 2 AND 10, NTM 531100  ESPECIALLY THE LOWER CORNER ADJOINING FRAME 10 PART 6  -NDT INSPECTION CAN BE CARRIED OUT AS ALTERNATE OF  VISUAL INSPECTION OF LOWER CORNER AT FRAME 10  NOTE: LINING REMOVED  531129-0602-1 211 WINDSHIELD CENTER POST MEC DET I: 7000 FC MRB S AMM SSI 5311 212  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 531129-0602-1 * * * * * C O N T I N U E * * * * *  DETAILED INSPECTION OF EXTERNAL WINDSHIELD  CENTER POST LOWER ATTACHMENT.  531129-0604-1 211 WINDSHIELD CENTER POST NDT SDI I: 27300 FC MRB S AMM SSI 5311 212 NTM 531100  DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 4  WINDSHIELD CENTER POST LOWER ATTACHMENT,  (INCLUDING ZONE 212).  NOTE: LH 3VU, RH 5VU, LINING BELOW 13VU INSULATION  REMOVED  531131-0602-1 211 WINDSHIELD CENTER POST MEC DET I: 7000 FC MRB S AMM SSI 5311 212  DETAILED INSPECTION OF EXTERNAL WINDSHIELD  CENTER POST UPPER ATTACHMENT.  531131-0604-1 211 WINDSHIELD CENTER POST NDT SDI I: 27300 FC MRB S AMM SSI 5311 212 NTM 531100  DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 2  WINDSHIELD CENTER POST UPPER ATTACHMENT.  NOTE: LINING BELOW 20VU AND INSULATION REMOVED  531133-0604-1 211 JUNCTION AT FRAMES 6 AND 7 NDT SDI I: 27300 FC MRB S AMM SSI 5311 212 NTM 531100  DETAILED AND SPECIAL DETAILED INSPECTION OF JUNCTIONS PART 6  BETWEEN FRAMES 6 ́AND 7 AND WINDSHIELD FRAME LOWER  SECTION.  NOTE: 1VU, 7VU, LINING AND INSULATION REMOVED  531135-0604-1 211 WINDSHIELD SIDE POST NDT SDI I: 27300 FC MRB S AMM SSI 5311 212 NTM 531100  DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 6  WINDSHIELD SIDE POST UPPER ATTACHMENT AT FRAME 7.  NOTE: LINING REMOVED  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 531137-0602-1 211 CLOSING PANEL AT FRAME 4 MEC DET I: 7500 FC ALI CN 2006-0071 212 FAA AD 96-13 DETAILED INSPECTION OF JUNCTION OF CLOSING  PANEL TO FRAME 4, JUNCTION OF WINDSHIELD FRAME LOWER ALI REFERENC SECTION WITH FRAMES 2, 3 AND 4 AND JUNCTION AREA 531137-01-1  BETWEEN TRIM PANEL, FRAMES 4 AND 2 AND WINDSHIELD  FRAME LOWER SECTION. JUNCTION OF FRAME 4 WITH  WINDSHIELD SIDE POST AND TWO RIVETS FOR ATTACHMENT OF  FRAME 2 TO SKIN.  531137-0604-1 211 CLOSING PANEL AT FRAME 4 NDT SDI I: 27300 FC MRB S AMM SSI 5311 212 NTM 531100  DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 2  JUNCTION OF CLOSING PANEL TO FRAME 4, JUNCTION OF NTM 531100  WINDSHIELD FRAME LOWER SECTION WITH FRAMES 2, 3 AND PART 6  JUNCTION AREA BETWEEN TRIM PANEL, FRAMES 4 AND 2 AND  WINDSHIELD FRAME LOWER SECTION JUNCTION OF FRAME 4  WITH WINDSHIELD SIDE POST AND TWO RIVETS FOR  ATTACHMENT OF FRAME 2 TO SKIN.  NOTE: 2VU, 6VU, 13VU, LINING REMOVED  531150-0603-1 121 FUSELAGE STRUCTURE FROM FRAME 1 TO FRAME MEC GVI T: 15 YE CPCP MRB REFERENC 122 20 I: 9 YE MRB S  531150-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL  STRUCTURE FROM FRAME 1 TO FRAME 20 BELOW CABIN  FLOOR LEVEL INCLUDING REAR FACE OF FORWARD  PRESSURE BULKHEAD.  PREP.: INSULATION TO BE LIFTED ENOUGH TO INSPECT THE  STRUCTURE WITHOUT REMOVAL OF ELECTRICAL  DEVICES.  ACCESS: 131AZ  132AZ 811  531200-0603-1 200 FUSELAGE FWD DOOR FRAME MEC DET I: 5 YE SIL SIL 53-030  DETAILED INSPECTION OF FUSELAGE FWD PASS/CREW  DOOR FRAMES IN AREA OF FITTINGS  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 531200-0603-1 * * * * * C O N T I N U E * * * * *  NOTE: LININGS TO BE REMOVED  531208-0602-1 221 INSPECTION OF FRAME 12A STIFFENERS NDT SDI T: 20400 FC ALI NTM 513000  222 I: 13300 FC PART 1  SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERS  AT UPPER HORIZONTAL FLANGE (LH/RH). ALI REFERENC 531208-01-1  PREP : FLOOR PANELS, INSULATION AND IF INSTALLED  CABIN ATTENDANT SEAT, LAVATORY AND GALLEY  TO BE REMOVED  531208-0602-2 221 INSPECTION OF FRAME 12A STIFFENERS NDT SDI T: 16100 FC ALI NTM 513000  222 I: 10700 FC PART 1  SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERS  AT UPPER HORIZONTAL FLANGE (LH/RH). ALI REFERENC 531208-01-2  PREP : FLOOR PANELS, INSULATION AND IF INSTALLED  CABIN ATTENDANT SEAT, LAVATORY AND GALLEY  TO BE REMOVED  531208-0603-1 121 MAIN FRAME - FUSELAGE NOSE SECTION NDT SDI T: 19300 FC CN NTM 513105  122 I: 11450 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERS ISB CN F-2005-08 AT UPPER HORIZONTAL FLANGE LH AND RH. FAA AD  2005-25-19  NOTE: FLOOR PANELS, INSULATION AND IF INSTALLED ISB 53-0365  CABIN ATTENDENT SEAT, LAVATORY AND GALLEY.  ACCESS: 831  841  531208-0603-2 121 MAIN FRAME - FUSELAGE NOSE SECTION NDT SDI T: 15500 FC CN NTM 513105  122 I: 9200 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF FRAME 12A STIFFENERS ISB CN F-2005-08 AT UPPER HORIZONTAL FLANGE LH AND RH. FAA AD  2005-25-19  NOTE: 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: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 531208-0603-2 * * * * * C O N T I N U E * * * * *  CABIN ATTENDENT SEAT, LAVATORY AND GALLEY.  ACCESS: 831  841  531214-0602-1 211 INSPECTION OF FRAME 10 TO 12 MEC DET T: 27800 FC ALI EASA AD  212 I: 8700 FC FAA AD 2006-0071  221 DETAILED INSPECTION OF FRAME 10 TO 12 AT EACH FAA AD  222 INTERSECTION OF STRINGER FROM CABIN FLOOR TO STR 9. 2007-04-11  PREP : LINING, INSULATION, 15VU, 50VU, LH TOILET ALI REFERENC TO BE REMOVED. 531214-01-1  531215-0602-1 223 SKIN PANELS FRAMES 10 TO 18 MEC DET T: 11400 FC ALI CN 2006-0071 224 I: 5700 FC FAA AD 96-13 DETAILED INSPECTION OF EXTERNAL SKIN  PANELS BETWEEN FRAMES 10 AND 18 AND BETWEEN ALI REFERENC SRINGERS 9 RH AND 9 LH. 531215-01-1  531216-0602-1 121 FRAMES 10 TO 18 MEC DET I: 7000 FC MRB S AMM SSI 5312 122 NOTE 6-1  DETAILED INSPECTION OF EXTERNAL SKIN  AND RIVETS FROM FRAME 10 TO 18 AND FROM CABIN FLOOR  AREA TO 30 CM DOWN.  531216-0604-1 121 FRAMES 10 TO 18 MEC DET I: 27300 FC MRB S AMM SSI 5312 122  DETAILED INSPECTION OF FRAMES 10 TO 18  INCLUSIVE EXCEPT FRAMES 14 AND 16A FROM CABIN FLOOR  30 CM DOWN, PARTICULARY AT ATTACHMENTS OF FLOOR BEAMS  TO FRAMES.  NOTE: LINING AND INSULATION REMOVED  ACCESS: 221DF 221EF 221KF 222DF 222EF 222JF  531219-0604-1 121 FRAMES 14 AND 16A MEC DET I: 27300 FC MRB S AMM SSI 5312 122  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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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 REMOVED  531220-0603-1 221 STRUCTURE AROUND FORWARD PAX DOOR MEC DET T: 9 YE CPCP AMM SSI 5312 222 I: 5 YE MRB S  DETAILED INSPECTION OF INTERNAL STRUCTURE MRB REFERENC AROUND FORWARD PASSENGER/CREW DOOR ABOVE CABIN FLOOR  BETWEEN FRAMES 13A AND 17 AND BETWEEN STRINGER 9 AND 531220-C603- 26. 531220-C603- NOTE: 01. FURNISHINGS, LINING AND INSULATION IN  FLOOR AREA REMOVED  02. 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 5312 122  DETAILED INSPECTION OF NOSE GEAR BAY ARCHES  BETWEEN FRAMES 11A AND 16A, UPPER CORNERS, INCLUDING  BRACE STRUT ATTACH FITTING LUGS.  ACCESS: 131AZ 132AZ  531223-0604-1 121 NOSE GEAR BAY ARCHES MEC DET I: 27300 FC MRB S AMM SSI 5312 122  DETAILED INSPECTION OF NOSE GEAR BAY ARCHES  BETWEEN FRAMES 11 AND 16A LOWER CORNERS.  ACCESS: 121KF 121MF 121NF 121PF 121QF 122EF  122GF 122HF 122JF 122KF  531225-0604-1 121 NOSE GEAR BAY ARCHES MEC DET I: 27300 FC MRB S AMM SSI 5312 122  DETAILED INSPECTION OF NOSE GEAR BAY ARCHES  ATTACHMENTS TO FRAMES AT STRINGER 44, BETWEEN FRAMES  11A AND 16A INCLUSIVE.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 531225-0604-1 * * * * * C O N T I N U E * * * * *  ACCESS: 121LF 121MF 121NF 121PF 121QF 122FF  122GF 122HF 122JF 122KF  531227-0602-1 123 NOSE GEAR BAY TOP PANEL MEC DET I: 5 YE MRB S AMM SSI 5312 124  DETAILED INSPECTION OF TOP PANEL IN  NOSE GEAR BAY.  531237-0604-1 121 FRAME 17 MEC DET I: 27300 FC MRB S AMM SSI 5312 122  DETAILED INSPECTION OF FRAME 17 AT STRINGERS  43, 48 AND 51.  ACCESS: 121TF 121UF 121VF 122LF 122MF 131AZ  531249-0603-1 120 NLG DOOR ACTUATOR ATTACHMENT FITTING NDT SDI T: 7500 FC ISB NTM 513010  I: 2400 FC PART 1  SPECIAL DETAILED INSPECTION OF FASTENER HOLES OF LH ISB 53-0248  FITTING, NOSE GEAR WELL ROOF AND CROSSBEAM FRAME 14  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  531249-0603-2 120 NLG DOOR ATTACHMENT FITTING MEC SDI T: 7000 FC ISB NTM 531252  I: 1500 FC PART 4  SPECIAL DETAILED INSPECTION OF NLG DOOR ACTUATOR ISB 53-0248  UPPER SUPPORT ATTACHMENT FITTING, AND DETAILED  INSPECTION OF FITTING FASTENERS AND CROSSBEAM AT FR  14,RH.  ACCESS: 132AZ  531249-0603-3 120 NLG DOOR ACTUATOR UPPER SUPPORT FITTING NDT SDI T: 16000 FC ISB NTM 531252  I: 2200 FC PART 4  SPECIAL DETAILED INSPECTION OF RH FITTING LUGS, FRAME ISB 53-0248  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 531249-0603-3 * * * * * C O N T I N U E * * * * *  14.  ACCESS: 132AZ  531249-0603-4 120 NLG DOOR ACTUATOR UPPER SUPPORT FITTING MEC DET T: 7000 FC ISB ISB 53-0248  I: 1500 FC  DETAILED INSPECTION OF CROSSBEAM, FRAME 14.  ACCESS: 132AZ  531251-0604-1 121 NOSE GEAR BAY SIDE LONGERON MEC DET I: 27300 FC MRB S AMM SSI 5312 122  DETAILED INSPECTION OF INTERNAL NOSE GEAR BAY  SIDE LONGERON AT STRINGER 49 BETWEEN FRAMES 10 AND 11  AND BETWEEN FRAMES 17 AND 19.  ACCESS: 121JF 121TF 122CF 122DF 131AZ N 531253-0604-1 121 FUSELAGE NOSE SECTION MEC DET T: 6600 FC EASA AD EASA AD  122 I: NOTE ISB 2009-0165  DETAILED INSPECTION OF THE CROSSBEAM ON NLG FR 15A ISB 53-0327  WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FITTING  NOTE: REFER TO ISB 53-0388 FOR INTERVAL  ACCESS: 121BL  531303-0604-1 232 LONGERON CAB.FLOOR SUPPORT MEC DET I: 27300 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF LONGERON FOR CABIN  FLOOR PANEL SUPPORT FROM FRAME 20B TO 24A RH.  PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTING  PANELS REMOVED.  531303-0604-2 232 LONGERON CAB. FLOOR SUPPORT MEC DET I: 27300 FC MRB S AMM SSI 5313 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 CABIN  FLOOR PANEL SUPPORT FROM FRAME 20B TO 25 RH.  PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTING  PANELS REMOVED.  531303-0604-3 232 LONGERON CAB.FLOOR SUPPORT MEC DET I: 22600 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF LONGERON FOR CABIN  FLOOR PANEL SUPPORT FROM FRAME 20B TO 24A RH.  PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTING  PANELS REMOVED.  531303-0604-4 232 LONGERON CAB. FLOOR SUPPORT MEC DET I: 22600 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF LONGERON FOR CABIN  FLOOR PANEL SUPPORT FROM FRAME 20B TO 25 RH.  PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTING  PANELS REMOVED.  531303-0604-5 232 LONGERON CAB.FLOOR SUPPORT MEC DET I: 19200 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF LONGERON FOR CABIN  FLOOR PANEL SUPPORT FROM FRAME 20B TO 24A RH.  PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTING  PANELS REMOVED.  531303-0604-6 232 LONGERON CAB. FLOOR SUPPORT MEC DET I: 19200 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF LONGERON FOR CABIN  FLOOR PANEL SUPPORT FROM FRAME 20B TO 25 RH.  PREP.: LOWER SIDE WALL PANELS AND BASE CONNECTING  PANELS REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5313 DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS AT ATTACHMENT AREA OF STRINGER 24R TO FRAME 20  AT UPPER FORWARD CORNER OF FWD CARGO COMPARTMENT DOOR  FRAME  531309-0604-1 232 CARGO COMPARTM. DOOR FRAME MEC DET I: 27300 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF ATTACHMENT AREA OF  STRINGER 24R TO FRAME 20 AT UPPER FORWARD CORNER OF  FWD CARGO COMPARTMENT DOOR FRAME.  PREP.: CABIN SIDE LINING AND INSULATION REMOVED  531309-0604-2 232 CARGO COMPARTM. DOOR FRAME MEC DET I: 22600 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF ATTACHMENT AREA OF  STRINGER 24R TO FRAME 20 AT UPPER FORWARD CORNER OF  FWD CARGO COMPARTMENT DOOR FRAME.  PREP.: CABIN SIDE LINING AND INSULATION REMOVED  531309-0604-3 232 CARGO COMPARTM. DOOR FRAME MEC DET I: 19200 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF ATTACHMENT AREA OF  STRINGER 24R TO FRAME 20 AT UPPER FORWARD CORNER OF  FWD CARGO COMPARTMENT DOOR FRAME.  PREP.: CABIN SIDE LINING AND INSULATION REMOVED  531313-0603-1 134 FWD CARGO DOOR SILL BEAM MEC DET I: 5 YE CPCP AMM SSI 5313 MRB S AMM SSI 5313 DETAILED INSPECTION OF FWD CARGO COMPARTMENT  DOOR SILL BEAM FROM FRAME 19 TO FRAME 26, INCLUDING MRB REFERENC TORSION BOX AND ATTACHMENT AREAS.  531313-C603- NOTE: 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.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 51-70-00  I: SEE SB PART 1  SPECIAL DETAILED INSPECTION OF BONDED DOUBLERS IN THE NTM 53-30-00  AREA OF LON LONGITUDINAL LAP JOINTS BETWEEN FR18 AND PART 5  FR 40 NTM 53-30-50  PART 5  NOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 ISB 53-0378  FOR APPLICABILITY DETAILS REFER TO SB 53-0378  531314-0604-2 100 FRAME BETWEEN 26 AND 40 NDT SDI T: SEE SB ISB NTM 51-70-00  I: SEE SB PART 1  SPECIAL DETAILED INSPECTION OF BONDED DOUBLERS IN THE NTM 53-30-00  CIRCUMFERENTIAL JOINT AREA BETWEEN FR 26 AND FR 40 PART 5  NTM 53-30-10  NOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 PART 4 OR  FOR APPLICABILITY DETAILS REFER TO SB 53-0378 PART 6  NTM 53-30-16  PART 6  NTM 53-30-20  PART 4 OR  PART 6  NTM 53-30-50  PART 5  ISB 53-0378  531314-0604-3 100 FRAME BETWEEN 34 AND 39 LH/RH NDT SDI T: SEE SB ISB NTM 51-70-00  I: SEE SB PART 1  SPECIAL DETAILED INSPECTION OF BONDED WING DOUBLERS NTM 53-30-00  BETWEEN FR.34 AND FR.39, STGR 22 AND STGR 43 LH/RH PART 5  NTM 53-30-10  NOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 PART 4 OR  FOR APPLICABILITY DETAILS REFER TO SB 53-0378 PART 6  NTM 53-30-16  PART 6  NTM 53-30-20  PART 4 OR  PART 6  NTM 53-30-50  PART 5  ISB 53-0378  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 51-70-00  AND BETWEEN FR 38.1 AND FR 38.2 I: SEE SB PART 1  NTM 53-30-00  SPECIAL DETAILED INSPECTION OF BONDED DOUBLERS IN PART 5  THE MANHOLE AREA BETWEEN FR 23 RH AND 24 RH AND NTM 53-30-10  BETWEEN FR 38.1 AND FR 38.2 PART 4 OR  PART 6  NOTE:FOR DETAILS OF THE THRESHOLD REFER TO SB 53-0378 NTM 53-30-16  FOR APPLICABILITY DETAILS REFER TO SB 53-0378 PART 6  NTM 53-30-20  PART 4 OR  PART 6  NTM 53-30-50  PART 5  ISB 53-0378  531315-0604-1 132 FRAME 25 MEC DET I: 27300 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF FRAME 25, BETWEEN  STRINGERS 35R AND 37R.  PREP.: SIDE LINING AND INSULATION REMOVED.  531315-0604-2 132 FRAME 26 MEC DET I: 27300 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF FRAME 26 BETWEEN  STRINGERS 35R AND 37R.  PREP.: SIDE LINING AND INSULATION REMOVED.  531315-0604-3 132 FRAME 25 MEC DET I: 22600 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF FRAME 25, BETWEEN  STRINGERS 35R AND 37R.  PREP.: SIDE LINING AND INSULATION REMOVED.  531315-0604-4 132 FRAME 26 MEC DET I: 22600 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF FRAME 26 BETWEEN  STRINGERS 35R AND 37R.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5313 DETAILED INSPECTION OF FRAME 25, BETWEEN  STRINGERS 35R AND 37R.  PREP.: SIDE LINING AND INSULATION REMOVED.  531315-0604-6 132 FRAME 26 MEC DET I: 19200 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF FRAME 26 BETWEEN  STRINGERS 35R AND 37R.  PREP.: SIDE LINING AND INSULATION REMOVED.  531317-0604-1 132 FRAME 20 MEC DET I: 27300 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF FRAME 20, BETWEEN EFERENC 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 5313 DETAILED INSPECTION OF FRAME 20, BETWEEN  STRINGERS 35R AND 37R.  PREP.: SIDE LINING AND INSULATION REMOVED.  531317-0604-3 132 FRAME 20 MEC DET I: 19200 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF FRAME 20, BETWEEN  STRINGERS 35R AND 37R.  PREP.: SIDE LINING AND INSULATION REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5313 DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS IN AREA OF FRAMES 21 TO 24 (4 PLACES) BETWEEN  STRINGERS 21R AND 22R.  531319-0602-2 232 FORMED FRAMES 21 TO 25 MEC DET I: 3500 FC MRB S AMM SSI 5313 DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS IN AREA OF FRAME 21 TO 25 BETWEEN STRINGERS  21RH AND 22RH.  531319-0604-1 232 FORMED FRAMES 21 TO 24 MEC DET I: 27300 FC MRB S AMM SSI 5313 DETAILED INTERNAL INSPECTION OF HINGE FITTINGS  FITTINGS OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE AT  ATTACHMENT AREAS OF FORMED FRAMES 21 TO 24 (4 PLACES)  TO HINGE FITTINGS BETWEEN STRINGERS 21R AND 22R.  PREP.: SIDE LINING AND INSULATION REMOVED  531319-0604-2 232 FORMED FRAMES 21 TO 25 MEC DET I: 27300 FC MRB S AMM SSI 5313 DETAILED INTERNAL INSPECTION OF HINGE FITTINGS  OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE AT  ATTACHMENT AREAS OF FORMED FRAMES 21 TO 25 BETWEEN  STRINGERS 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 5313 DETAILED INTERNAL INSPECTION OF HINGE FITTINGS  FITTINGS OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE AT  ATTACHMENT AREAS OF FORMED FRAMES 21 TO 24 (4 PLACES)  TO HINGE FITTINGS BETWEEN STRINGERS 21R AND 22R.  PREP.: SIDE LINING AND INSULATION REMOVED  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5313 DETAILED INTERNAL INSPECTION OF HINGE FITTINGS  OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE AT  ATTACHMENT AREAS OF FORMED FRAMES 21 TO 25 BETWEEN  STRINGERS 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 5313 DETAILED INTERNAL INSPECTION OF HINGE FITTINGS  FITTINGS OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE AT  ATTACHMENT AREAS OF FORMED FRAMES 21 TO 24 (4 PLACES)  TO HINGE FITTINGS BETWEEN STRINGERS 21R AND 22R.  PREP.: SIDE LINING AND INSULATION REMOVED  531319-0604-6 232 FORMED FRAMES 21 TO 25 MEC DET I: 19200 FC MRB S AMM SSI 5313 DETAILED INTERNAL INSPECTION OF HINGE FITTINGS  OF FWD CARGO COMPARTMENT DOOR IN FUSELAGE AT  ATTACHMENT AREAS OF FORMED FRAMES 21 TO 25 BETWEEN  STRINGERS 21RH AND 22RH.  PREP.: SIDE LINING AND INSULATION REMOVED.  531321-0602-1 100 INSPECTION AT CIRCUMFERENTIAL SKIN NDT SDI T: 30000 FC ALI NTM 531321  200 SPLICE AT FR 26 OR PART 6  34200 FH  SPECIAL DETAILED INSPECTION AT SPLICE PLATE AT I: 3700 FC ALI REFERENC CIRCUMFERENTIAL SKIN SPLICE AT FR26, FROM STR13 TO OR 531321-01-1  CROWN CENTERLINE, LH/RH AREA 1. 4200 FH  531321-0602-2 100 INSPECTION AT CIRCUMFERENTIAL SKIN NDT SDI T: 30000 FC ALI NTM 531321  200 SPLICE AT FR 26 OR PART 6  41700 FH  SPECIAL DETAILED INSPECTION AT SPLICE PLATE AT I: 3100 FC ALI REFERENC CIRCUMFERENTIAL SKIN SPLICE AT FR26, FROM STR13 TO OR 531321-01-2  CROWN CENTERLINE, LH/RH. 4300 FH  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531321-0602-3 100 INSPECTION AT CIRCUMFERENTIAL SKIN NDT SDI T: 30000 FC ALI NTM 531321  200 SPLICE AT FR 26 OR PART 6  69600 FH EASA AD  SPECIAL DETAILED INSPECTION AT SPLICE PLATE AT I: 4100 FC 2006-0071  CIRCUMFERENTIAL SKIN SPLICE AT FR26, FROM STR13 TO OR FAA AD  CROWN CENTERLINE, LH/RH. 9500 FH 2007-04-11  ALI REFERENC 531321-01-3  531400-0602-1 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 7400 FC ISB ISB 53-0162  I: 2400 FC  DETAILED INSPECTION OF THE FRONT LOWER  REINFORCEMENT AT FR.40.  531400-0602-2 231 MID.PASS/CREW DOOR FRAME MEC DET T: 30000 FC ISB CN  232 I: 2000 FC 1983-102-053 DETAILED INSPECTION OF WEB- PLATE BETWEEN NOTE FAA AD 98-20 FR.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 53-0162  I: 2000 FC  DETAILED INSPECTION OF THE FRONT LOWER  REINFORCEMENT AT FR.40.  531400-0602-4 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 4500 FC ISB ISB 53-0162  I: 1400 FC  DETAILED INSPECTION OF THE FRONT LOWER  REINFORCEMENT AT FR.40.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 53-0162  NOTE  DETAILED INSPECTION OF THE FRONT LOWER I: 4800 FC  REINFORCEMENT AT FR.40.  NOTE : THRESHOLD IS APPLICABLE STARTING FROM LAST  EMBODYMENT OF SB 53-0161.  531400-0602-6 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 8100 FC ISB ISB 53-0162  NOTE  DETAILED INSPECTION OF THE FRONT LOWER I: 3900 FC  REINFORCEMENT AT FR.40.  NOTE : THRESHOLD IS APPLICABLE STARTING FROM LAST  EMBODYMENT OF SB 53-0161.  531400-0602-7 140 FUS. DOUBLER ANGLE FR.40 MEC DET T: 6200 FC ISB ISB 53-0162  NOTE  DETAILED INSPECTION OF THE FRONT LOWER I: 3000 FC  REINFORCEMENT AT FR.40.  NOTE : THRESHOLD IS APPLICABLE STARTING FROM LAST  EMBODYMENT OF SB53-0161.  531409-0603-1 231 FUSELAGE FRAME 28A AND 30A NDT SDI T: 10 YE ISB NTM 531402  232 I: 5 YE PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 28A AND ISB 53-0274  30A, DOOR FRAME AREA.  PREP.: MID DOOR FRAME LINING TO BE REMOVED.  UPPER CARGO COMPARTMENT SIDEWALL PANELS  TO BE REMOVED.  531411-0603-1 230 STRUCTURE AROUND MID PAX/CREW DOOR MEC DET I: 5 YE AD AD 2007-04-1 240 ALI EUAD 2006-00 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND CPCP  MID PASSENGER/CREW DOOR ABOVE CABIN FLOOR BETWEEN EUAD ALI REFERENC 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC AND FURNISHING, LINING AND INSULATION IN SSI 531411  DOOR REMOVED 531411-C603- 531411-C603- - 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 531400  232 PART 2,6  DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL EASA AD  STRUCTURE AROUND MID PASSENGER/CREW DOOR ABOVE CABIN 2006-0071  FLOOR BETWEEN FR27 AND FR32 AND BETWEEN STR9 AND FAA AD  STR26. 2007-04-11  PREP : FURNISHING, LINING AND INSULATION IN DOOR ALI REFERENC AREA TO BE REMOVED 531411-01-1  531411-02-1  531501-0604-1 130 FRAME NO. 39 MEC DET I: 27300 FC MRB S AMM SSI 5315 240  DETAILED INSPECTION OF FRAME 39 BETWEEN  STRINGERS 20 AND 30.  PREP.: LOWER SIDE WALL PANEL AND DECOMPRESSION PANEL,  CABIN AND CARGO SIDE LINING AND INSULATION  REMOVED.  ACCESS: 241TF 241YF 242QF 242UF  531503-0604-1 143 WING CENTER BOX ATTACHMENT MEC DET I: 27300 FC MRB S AMM SSI 5315 144  DETAILED INSPECTION OF LOWER ATTACHMENTS OF  CENTER WING BOX FRONT SPAR TO FRAME FITTINGS AT  FRAME 40.  ACCESS: 147GZ 148GZ  531503-0604-2 143 WING CENTER BOX ATTACHMENT MEC DET I: 22600 FC MRB S AMM SSI 5315 144  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 OF  CENTER WING BOX FRONT SPAR TO FRAME FITTINGS AT  FRAME 40.  ACCESS: 147GZ 148GZ  531503-0604-3 143 WING CENTER BOX ATTACHMENT MEC DET I: 19200 FC MRB S AMM SSI 5315 144  DETAILED INSPECTION OF LOWER ATTACHMENTS OF  CENTER WING BOX FRONT SPAR TO FRAME FITTINGS AT  FRAME 40.  ACCESS: 147GZ 148GZ  531505-0604-1 145 WING CENTER BOX ATTACHMENTS MEC DET I: 27300 FC MRB S AMM SSI 5315 146  DETAILED INSPECTION OF UPPER ATTACHMENTS OF  CENTER WING BOX FRONT SPAR TO FRAME FITTINGS AT  FRAME 40.  ACCESS: 241VF  531505-0604-2 145 WING CENTER BOX ATTACHMENTS MEC DET I: 22600 FC MRB S AMM SSI 5315 146  DETAILED INSPECTION OF UPPER ATTACHMENTS OF  CENTER WING BOX FRONT SPAR TO FRAME FITTINGS AT  FRAME 40.  ACCESS: 241VF  531505-0604-3 145 WING CENTER BOX ATTACHMENTS MEC DET I: 19200 FC MRB S AMM SSI 5315 146  DETAILED INSPECTION OF UPPER ATTACHMENTS OF  CENTER WING BOX FRONT SPAR TO FRAME FITTINGS AT  FRAME 40.  ACCESS: 241VF  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5315 240  DETAILED INSPECTION OF FRAMES 40 TO 53,BETWEEN  PRESSURIZED FLOOR AND STRINGERS 18 ́LH,RH.  PREP.: SIDE LININGS AND INSULATION REMOVED.  ACCESS: 241AC 241AD 241AH 241AJ 241AN 241AP  241AT 241AU 241AV 242AB 242AC 242AF  242AG 242AK 242AL 242AM 242XF 242YF  531508-0604-2 140 FRAMES 40 TO 53 MEC DET I: 22600 FC MRB S AMM SSI 5315 240  DETAILED INSPECTION OF FRAMES 40 TO 53,BETWEEN  PRESSURIZED FLOOR AND STRINGERS 18 ́LH,RH.  PREP.: SIDE LININGS AND INSULATION REMOVED.  ACCESS: 241AC 241AD 241AH 241AJ 241AN 241AP  241AT 241AU 241AV 242AB 242AC 242AF  242AG 242AK 242AL 242AM 242XF 242YF  531508-0604-3 140 FRAMES 40 TO 53 MEC DET I: 19200 FC MRB S AMM SSI 5315 240  DETAILED INSPECTION OF FRAMES 40 TO 53,BETWEEN  PRESSURIZED FLOOR AND STRINGERS 18 ́LH,RH.  PREP.: SIDE LININGS AND INSULATION REMOVED.  ACCESS: 241AC 241AD 241AH 241AJ 241AN 241AP  241AT 241AU 241AV 242AB 242AC 242AF  242AG 242AK 242AL 242AM 242XF 242YF  531513-0602-1 240 FRAME 47 MEC DET T: 12000 FC MRB S  I: 4300 FC  DETAILED INSPECTION AT FR47 FROM STR 13 TO STR 22,  LH/RH, EXTERNAL SURFACE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531513-0602-1 * * * * * C O N T I N U E * * * * *  531514-0602-1 140 SPLICE AT FRAME 54 MEC DET I: 5500 FC MRB S AMM SSI 5315 150  DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS AT STRINGER TO SKIN PICK UP SPLICE AT FRAME 54  BETWEEN STRINGERS 42, L/H AND R/H.  531514-0602-2 140 SPLICE AT FRAME 54 MEC DET I: 4500 FC MRB S AMM SSI 5315 150  DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS AT STRINGER TO SKIN PICK UP SPLICE AT FRAME 54  BETWEEN STRINGERS 42, L/H AND R/H.  531514-0602-3 140 SPLICE AT FRAME 54 MEC DET I: 3800 FC MRB S AMM SSI 5315 150  DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS AT STRINGER TO SKIN PICK UP SPLICE AT FRAME 54  BETWEEN STRINGERS 42, L/H AND R/H.  531514-0604-1 140 SPLICE AT FRAME 54 MEC DET I: 27300 FC MRB S AMM SSI 5315 150  DETAILED INSPECTION OF INTERNAL STRINGER TO  SKIN PICK-UP SPLICE AT FRAME 54 BETWEEN STRINGERS 42,  LH AND RH.  ACCESS: 147SZ 147TZ 148SZ 148TZ  151AF 151BF 151CF 152AF 152BF  531514-0604-2 140 SPLICE AT FRAME 54 MEC DET I: 22600 FC MRB S AMM SSI 5315 150  DETAILED INSPECTION OF INTERNAL STRINGER TO  SKIN PICK-UP SPLICE AT FRAME 54 BETWEEN STRINGERS 42,  LH AND RH.  ACCESS: 147SZ 147TZ 148SZ 148TZ  151AF 151BF 151CF 152AF 152BF  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5315 150  DETAILED INSPECTION OF INTERNAL STRINGER TO  SKIN PICK-UP SPLICE AT FRAME 54 BETWEEN STRINGERS 42,  LH AND RH.  ACCESS: 147SZ 147TZ 148SZ 148TZ  151AF 151BF 151CF 152AF 152BF  531518-0604-1 143 WING CENTER BOX LOWER PANEL MEC DET I: 27300 FC MRB S AMM SSI 5315 144  DETAILED INSPECTION OF WING CENTER BOX LOWER  PANEL OUTER SURFACE FROM FRAME NO.45 TO FRAME NO.47.  ACCESS: 147FZ 147GZ  531518-0604-2 143 WING CENTER BOX LOWER PANEL MEC DET I: 22600 FC MRB S AMM SSI 5315 144  DETAILED INSPECTION OF WING CENTER BOX LOWER  PANEL OUTER SURFACE FROM FRAME NO.45 TO FRAME NO.47.  PREP.: VAPOR SEAL REMOVED  ACCESS: 147FZ 147GZ  531518-0604-3 143 WING CENTER BOX LOWER PANEL MEC DET I: 19200 FC MRB S AMM SSI 5315 144  DETAILED INSPECTION OF WING CENTER BOX LOWER  PANEL OUTER SURFACE FROM FRAME NO.45 TO FRAME NO.47.  PREP.: VAPOR SEAL REMOVED  ACCESS: 147FZ 147GZ  531525-0604-1 150 FRAME 54 MEC DET I: 27300 FC MRB S AMM SSI 5315 240  DETAILED INSPECTION OF FRAME NO.54 BETWEEN  STRINGERS 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  242AQ 242AR  531531-0602-1 147 BRACE STRUT HINGE FITTING MEC DET T: 18800 FC ALI CN 2006-0071 148 OR FAA AD 96-13 DETAILED INSPECTION OF BRACE STRUT 21200 FH  HINGE FITTING IN MAIN GEAR BAY AND ATTACHMENTS TO I: 8500 FC ALI REFERENC CANTED FRAMES. OR 531531-01-1  9600 FH  ACCESS: 734  744  531531-0602-2 147 BRACE STRUT HINGE FITTING MEC DET T: 18800 FC ALI CN 2006-0071 148 OR FAA AD 96-13 DETAILED INSPECTION OF BRACE STRUT 25700 FH  HINGE FITTING IN MAIN GEAR BAY AND ATTACHMENTS TO I: 8500 FC ALI REFERENC CANTED FRAMES. OR 531531-01-2  11600 FH  ACCESS: 734  744  531531-0602-3 147 BRACE STRUT HINGE FITTING MEC DET T: 18800 FC ALI CN 2006-0071 148 OR FAA AD 96-13 DETAILED INSPECTION OF BRACE STRUT 42700 FH  HINGE FITTING IN MAIN GEAR BAY AND ATTACHMENTS TO I: 8500 FC ALI REFERENC CANTED FRAMES. OR 531531-01-3  19300 FH  ACCESS: 734  744  531533-0604-1 143 WING CENTER BOX FRONT SPAR MEC DET I: 27300 FC MRB S AMM SSI 5315 144  DETAILED INSPECTION OF ATTACHMENT OF WING  CENTER BOX FRONT SPAR TO LOWER SKIN PANEL IN AREA OF  AIRCRAFT CENTER LINE.  ACCESS: 147GZ  148GZ  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5315 144  DETAILED INSPECTION OF ATTACHMENT OF WING  CENTER BOX FRONT SPAR TO LOWER SKIN PANEL IN AREA OF  AIRCRAFT CENTER LINE.  PREP.: REMOVE/INSTALL VAPOR SEAL.  ACCESS: 147GZ  148GZ  531533-0604-3 143 WING CENTER BOX FRONT SPAR MEC DET I: 19200 FC MRB S AMM SSI 5315 144  DETAILED INSPECTION OF ATTACHMENT OF WING  CENTER BOX FRONT SPAR TO LOWER SKIN PANEL IN AREA OF  AIRCRAFT CENTER LINE.  PREP.: REMOVE/INSTALL VAPOR SEAL.  ACCESS: 147GZ  148GZ  531537-0604-1 141 WING CENTER SPAR MEC DET I: 27300 FC MRB S AMM SSI 5315 142 NTM 531500  DETAILED OR NDT INSPECTION OF CORNERS OF PART 6  TRIANGULAR CUTOUTS IN WING CENTER SPAR.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531537-0604-2 141 WING CENTER SPAR MEC SDI I: 22600 FC MRB S AMM SSI 5315 142 NTM 531500  DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6  TRIANGULAR CUTOUTS IN WING CENTER SPAR.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531537-0604-3 141 WING CENTER SPAR MEC DET I: 19200 FC MRB S AMM SSI 5315 142 NTM 531500  DETAILED NDT INSPECTION OF CORNERS OF PART 6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  148AZ 148DZ  531539-0604-1 147 WING REAR SPAR MEC SDI I: 27300 FC MRB S AMM SSI 5315 148 NTM 531500  DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6  TRIANGULAR CUTOUTS IN WING REAR SPAR.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531539-0604-2 147 WING REAR SPAR MEC SDI I: 22600 FC MRB S AMM SSI 5315 148 NTM 531500  DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6  TRIANGULAR CUTOUTS IN WING REAR SPAR.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531539-0604-3 147 WING REAR SPAR MEC SDI I: 19200 FC MRB S AMM SSI 5315 148 NTM 531500  DETAILED OR SPECIAL DETAILED INSPECTION OF CORNERS OF PART 6  TRIANGULAR CUTOUTS IN WING REAR SPAR.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531540-0603-1 145 FRAME 47 NDT SDI I: 6000 FC ISB ISB 53-0195  146  SPECIAL DETAILED INSPECTION OF FLANGES OF FRAME 47  LH/RH BETWEEN STRINGERS 23 AND 26  NOTE: 1. TASK NOT APPLICABLE AFTER SHOT PEENING  2. LINING AND INSULATION TO BE REMOVED  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531540-0603-2 241 FUSELAGE FRAME 47 NDT SDI T: 6000 FC ISB CN  242 I: 6000 FC 1984-117-062 SPECIAL DETAILED INSPECTION OF TWO FASTENER HOLES ON CN  FR 47 IN ACCORDANCE WITH ISB 53-0194 FOR FIRST 1990-222-116 INSPECTION AND WITH ISB 53-0196 FOR SUBSEQUENT FAA AD  INSPECTION. 2000-10-01  FAA AD 87-04 NOTE : LINING AND INSULATION TO BE REMOVED FAA AD 96-08 ISB 53-0194  ISB 53-0196  531540-0604-1 145 FRAME 47 NDT SDI I: 27300 FC MRB S AMM SSI 5315 146 NTM 531500  147 DETAILED AND SPECIAL DETAILED INSPECTION OF FRAME 47 PART 2  148 MACHINED AREAS AND ATTACHMENT TO ADJOINING PARTS  241 (INCLUDING ZONES 146, 147/148, 241/242).  242  PREP.: LINING AND INSULATION REMOVED.  ACCESS: 241AKF 241ALF 241AMF 241ANF  242ADF 242AEF 242AFF  531540-0604-2 145 FRAME 47 NDT SDI I: 22600 FC MRB S AMM SSI 5315 146 NTM 531500  147 DETAILED AND SPECIAL DETAILED INSPECTION OF FRAME 47 PART 2  148 MACHINED AREAS AND ATTACHMENT TO ADJOINING PARTS.  241  242 PREP.: LINING AND INSULATION REMOVED.  ACCESS: 241AKF 241ALF 241AMF 241ANF  242ADF 242AEF 242AFF  531540-0604-3 145 FRAME 47 NDT SDI I: 19200 FC MRB S AMM SSI 5315 146 NTM 531500  147 DETAILED AND SPECIAL DETAILED INSPECTION OF FRAME 47 PART 2  148 MACHINED AREAS AND ATTACHMENT TO ADJOINING PARTS.  241  242 PREP.: LINING AND INSULATION REMOVED.  ACCESS: 241AKF 241ALF 241AMF 241ANF  242ADF 242AEF 242AFF  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5315 142  DETAILED INSPECTION OF INNER FACE OF LOWER  SKIN PANEL OF CENTER WING BOX BETWEEN FRAMES NO.44  AND 46 AT AIRCRAFT CENTER LINE.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531543-0604-2 141 CENTER WING BOX MEC DET I: 22600 FC MRB S AMM SSI 5315 142  DETAILED INSPECTION OF INNER FACE OF LOWER  SKIN PANEL OF CENTER WING BOX BETWEEN FRAMES NO.44  AND 46 AT AIRCRAFT CENTER LINE.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531543-0604-3 141 CENTER WING BOX MEC DET I: 19200 FC MRB S AMM SSI 5315 142  DETAILED INSPECTION OF INNER FACE OF LOWER  SKIN PANEL OF CENTER WING BOX BETWEEN FRAMES NO.44  AND 46 AT AIRCRAFT CENTER LINE.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531547-0604-1 141 WING CENTER BOX - INBOARD NDT SDI I: 27300 FC MRB S AMM SSI 5315 142 NTM 531500  DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2  CENTER BOX LOWER SKIN SPLICE WITH RIB 1 INBOARD.  ACCESS: 147AZ 147DZ 541AB 542CB  148AZ 148DZ 641AB 642CB  531547-0604-2 141 WING CENTER BOX - INBOARD NDT SDI I: 22600 FC MRB S AMM SSI 5315 142 NTM 531500  DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2  CENTER BOX LOWER SKIN SPLICE WITH RIB 1 INBOARD,  ACCESS: 147AZ 147DZ 541AB 542CB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531547-0604-2 * * * * * C O N T I N U E * * * * *  148AZ 148DZ 641AB 642CB  531547-0604-3 141 WING CENTER BOX - INBOARD NDT SDI I: 19200 FC MRB S AMM SSI 5315 142 NTM 531500  DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2  CENTER BOX LOWER SKIN SPLICE WITH RIB 1 INBOARD.  ACCESS: 147AZ 147DZ 541AB 542CB  148AZ 148DZ 641AB 642CB  531548-0603-1 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 26300 FC ALI NTM 531548  542 OR PART 4  641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 28400 FH EASA AD  642 ATTACHMENT (WING SIDE). I: 3800 FC 2006-0071  OR FAA AD  4100 FH 2007-04-11  ALI REFERENC 531548-01-1  531548-0603-2 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 30300 FC ALI NTM 531548  542 OR PART 4  641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 40300 FH EASA AD  642 ATTACHMENT (WING SIDE). I: 4500 FC 2006-0071  OR FAA AD  9400 FH 2007-04-11  ALI REFERENC 531548-01-2  531548-0603-3 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 31100 FC ALI NTM 531548  542 OR PART 4  641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 64700 FH EASA AD  642 ATTACHMENT (WING SIDE). I: 4500 FC 2006-0071  OR FAA AD  9400 FH 2007-04-11  ALI REFERENC 531548-01-3  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531548-0603-4 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 31100 FC ALI NTM 531548  542 OR PART 2  641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 64700 FH EASA AD  642 ATTACHMENT (WING SIDE). I: 4500 FC 2006-0071  OR FAA AD  ACCESS: 541AB 9400 FH 2007-04-11  542CB  641AB ALI REFERENC 642CB 531548-02-1  531548-0603-5 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 35100 FC ALI NTM 531548  542 OR PART 2  641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 46700 FH EASA AD  642 ATTACHMENT (WING SIDE). I: 2300 FC 2006-0071  OR FAA AD  ACCESS: 541AB 3100 FH 2007-04-11  542CB  641AB ALI REFERENC 642CB 531548-02-2  531548-0603-6 541 WING FUSELAGE LOWER ATTACHMENT NDT SDI T: 31100 FC ALI NTM 531548  542 OR PART 2  641 SPECIAL DETAILED INSPECTION OF WING FUSELAGE LOWER 64700 FH EASA AD  642 ATTACHMENT (WING SIDE). I: 2200 FC 2006-0071  OR FAA AD  ACCESS: 541AB 4500 FH 2007-04-11  542CB  641AB ALI REFERENC 642CB 531548-02-3  531548-0604-1 540 LOWER SKIN SPLICE RIB 1 NDT SDI I: 27300 FC MRB S AMM SSI 5315 640 NTM 531500  DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2  CENTER BOX LOWER SKIN SPLICE WITH RIB 1 (IN SITU AS  FAR AS VISIBLE).  ACCESS: 541AB 542CB  641AB 642CB  531548-0604-2 540 LOWER SKIN SPLICE RIB 1 NDT SDI I: 22600 FC MRB S AMM SSI 5315 640  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531500  CENTER BOX LOWER SKIN SPLICE WITH RIB 1 (IN SITU AS PART 2  FAR AS VISIBLE).  ACCESS: 541AB 542CB  641AB 642CB  531548-0604-3 540 LOWER SKIN SPLICE RIB 1 NDT SDI I: 19200 FC MRB S AMM SSI 5315 640 NTM 531500  DETAILED AND SPECIAL DETAILED INSPECTION OF WING PART 2  CENTER BOX LOWER SKIN SPLICE WITH RIB 1 (IN SITU AS  FAR AS VISIBLE).  ACCESS: 541AB 542CB  641AB 642CB  531549-0602-1 140 WING SPAR BOX MEC DET I: 3800 FC MRB S AMM SSI 5315 DETAILED INSPECTION OF EXTERNAL  WING SPAR BOX LOWER SKIN PANEL AREA BETWEEN  FRAME 43 AND 46 AT THE END OF THE REINFORCING  MEMBERS (3 LAST BOLTS).  531549-0602-2 140 WING SPAR BOX MEC DET I: 6000 FH MRB S AMM SSI 5315 DETAILED INSPECTION OF EXTERNAL  WING SPAR BOX LOWER SKIN PANEL AREA BETWEEN  FRAME 43 AND 46 AT THE END OF THE REINFORCING  MEMBERS (3 LAST BOLTS).  531549-0604-1 140 WING SPAR BOX NDT SDI I: 19200 FC MRB S AMM SSI 5315 NTM 531500  SPECIAL DETAILED INSPECTION OF WING CENTER BOX LOWER PART 2  SKIN PANEL AREA BETWEEN FRAME 43 AND 46 AT THE END OF  THE REINFORCING MEMBERS (3 LAST BOLTS).  ACCESS: 147AZ 148AZ  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5315 NTM 531500  SPECIAL DETAILED INSPECTION OF WING CENTER BOX LOWER PART 2  SKIN PANEL AREA BETWEEN FRAME 43 AND 46 AT THE END OF  THE REINFORCING MEMBERS (3 LAST BOLTS).  ACCESS: 147AZ 147DZ 148AZ 148DZ  531553-0604-1 141 WEB PLATE MEC DET I: 27300 FC MRB S AMM SSI 5315 142  DETAILED INSPECTION OF WEB PLATE AROUND FUEL  PIPE CUTOUT IN RIB 1.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531553-0604-2 141 WEB PLATE MEC DET I: 22600 FC MRB S AMM SSI 5315 142  DETAILED INSPECTION OF WEB PLATE AROUND FUEL  PIPE CUTOUT IN RIB 1.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531553-0604-3 141 WEB PLATE MEC DET I: 19200 FC MRB S AMM SSI 5315 142  DETAILED INSPECTION OF WEB PLATE AROUND FUEL  PIPE CUTOUT IN RIB 1.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531555-0604-1 147 MACHINED PART OF PRESSURE FLOOR MEC DET I: 27300 FC MRB S AMM SSI 5315 148  DETAILED INSPECTION OF MACHINED PART OF  PRESSURE FLOOR LH AND RH BETWEEN FRAMES 51 AND 52.  ACCESS: 147PZ  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531557-0602-1 147 PRESSURIZED FLOOR MEC DET I: 5700 FC MRB S AMM SSI 5315 DETAILED INSPECTION OF PRESSURIZED  FLOOR SEALED WEB L/H SIDE BETWEEN FRAMES 48 AND 49 -  CUTOUT IN MACHINED SECTION  NOTE: QUICK RELEASE BOOT REMOVED  ACCESS: 147KZ  531557-0602-2 147 PRESSURIZED FLOOR MEC DET I: 5700 FC MRB S AMM SSI 5315 DETAILED INSPECTION OF PRESSURIZED FLOOR  SEALED WEB LH SIDE BETWEEN FRAMES 48 AND 49 CUTOUT  IN MACHINED SECTION  531559-0604-1 147 VERTICAL STIFFENERS MEC DET I: 27300 FC MRB S AMM SSI 5315 148  DETAILED INSPECTION OF VERTICAL STIFFENERS AT  Y = 420 (LH,RH) AND UPPER SECTIONS OF THE 7 OTHER  VERTICAL STIFFENERS AT MAIN GEAR BAY REAR BULKHEAD.  ACCESS: 147LZ 147MZ  148LZ 148MZ  531561-0604-1 147 PRESSURIZED FLOOR MEC DET I: 27300 FC MRB S AMM SSI 5315 148  DETAILED INSPECTION OF ATTACHMENT OF WEB TO  HORIZONTAL BEAMS LH AND RH BETWEEN FRAMES NO.47  AND 54.  ACCESS: 147LZ 147MZ 147NZ  148LZ 148MZ 148NZ  531563-0602-1 147 FRAMES 48 TO 53A MEC DET I: 8500 FC MRB S AMM SSI 5315 148  DETAILED INSPECTION OF FRAMES 48 TO 53A BELOW  PRESSURIZED FLOOR SEALED WEB, INCLUDING Y-FITTING  CONNECTING THE REAR OBLIQUE FRAME TO FRAME 53A.  FRAME 50 EXCEPTED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531563-0602-2 147 FRAME 53A MEC GVI I: 5700 FC ISB ISB 53-0129  148  GENERAL VISUAL INSPECTION OF Y-FITTING  CONNECTING THE REAR OBLIQUE FRAME TO FRAME 53A FOR  DAMAGE.  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 5315 146  DETAILED INSPECTION OF HINGE SEAT RAILS NO. 1,  2, 3, 4 LH AND RH AT FRAMES 40 AND 54.  PREP.: FLOOR PANELS REMOVED  531568-0604-2 145 HINGE SEAT RAILS MEC DET I: 22600 FC MRB S AMM SSI 5315 146  DETAILED INSPECTION OF HINGE SEAT RAILS NO. 1,  2, 3, 4 LH AND RH AT FRAMES 40 AND 54.  PREP.: FLOOR PANELS REMOVED  531569-0604-1 145 FLOOR CROSS MEMBERS MEC DET I: 19200 FC MRB S AMM SSI 5315 146  DETAILED INSPECTION OF FLOOR CROSS MEMBERS  BETWEEN SEAT RAILS NO.2 AND 3 LH AND RH BETWEEN  FRAMES 40 AND 54.  PREP.: FLOOR PANELS REMOVED.  531569-0604-2 145 FLOOR CROSS MEMBERS MEC DET I: 22600 FC MRB S AMM SSI 5315 146  DETAILED INSPECTION OF FLOOR CROSS MEMBERS  BETWEEN SEAT RAILS NO.2 AND 3 LH AND RH BETWEEN  FRAMES 40 AND 54.  PREP.: FLOOR PANELS REMOVED.  531570-0603-1 141 MAIN FRAME - FUSELAGE CENTER SECTION MEC DET T: 9750 FC SB SB 53-0337  142 I: 8100 FC  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FITTINGS  BETWEEN FRAME 41 AND FRAME 46.  ACCESS: 147FZ 734  744  531570-0603-2 141 MAIN FRAME - FUSELAGE CENTER SECTION MEC DET T: 8200 FC SB SB 53-0337  142 I: 6800 FC  DETAILED INSPECTION OF THE FRAME BASE FITTINGS  BETWEEN FRAME 41 AND FRAME 46.  ACCESS: 147FZ 734  744  531570-0603-3 141 MAIN FRAME - FUSELAGE CENTER SECTION MEC DET T: 6400 FC SB SB 53-0337  142 I: 5300 FC  DETAILED INSPECTION OF THE FRAME BASE FITTINGS  BETWEEN FRAME 41 AND FRAME 46.  ACCESS: 147FZ 734  744  531571-0604-1 141 PUMP APERTURES MEC DET I: 19200 FC MRB S AMM SSI 5315 142 AMM 281311/4 DETAILED INSPECTION OF INTERNAL PUMP APERTURES AMM 282137/4 IN CENTER WING BOX LOWER SKIN AND REINFORCINGS.  PREP.: VAPOR SEAL, PUMP AND CANISTER REMOVED.  ACCESS: 147AZ 147DZ  148AZ 148DZ  531571-0604-2 141 PUMP APERTURES MEC DET I: 22600 FC MRB S AMM SSI 5315 142 AMM 281311/4 DETAILED INSPECTION OF INTERNAL PUMP APERTURES AMM 282137/4 IN 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531571-0604-2 * * * * * C O N T I N U E * * * * *  ACCESS: 147AZ 147DZ  148AZ 148DZ  531572-0602-1 240 SKIN AROUND VHF 3 ANTENNA MEC DET T: 40000 FC ALI EASA AD  I: 9000 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN AROUND FAA AD  VHF 3 ANTENNA FR47-FR48. 2007-04-11  PREP : ANTENNA TO BE REMOVED ALI REFERENC 531572-01-1  531573-0602-1 240 SKIN AROUND ANTI-COLLISION LIGHT MEC DET T: 24000 FC ALI EASA AD  I: 5500 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN AROUND ANTI- FAA AD  COLLISION LIGHT BETWEEN FR 43 AND FR 44. 2007-04-11  PREP : ANTI-COLLISION LIGHT TO BE REMOVED ALI REFERENC 531573-01-4  531603-0604-1 151 STRUCTURE - FRAMES 55 TO 58 MEC DET I: 27300 FC MRB S AMM SSI 5316 152  DETAILED INSPECTION OF INTERNAL STRUCTURE  AROUND EMERGENCY EXIT BELOW CABIN FLOOR BETWEEN  FRAMES 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 5316 152  DETAILED INSPECTION OF INTERNAL STRUCTURE  AROUND EMERGENCY EXIT BELOW CABIN FLOOR BETWEEN  FRAMES 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 5316 152  DETAILED INSPECTION OF INTERNAL STRUCTURE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 BETWEEN  FRAMES 55 AND 58 AND BETWEEN STRINGERS 26 AND 29.  PREP.: LINING AND INSULATION REMOVED  531605-0603-1 241 EMERG. EXIT DOOR CUTOUT NDT SDI T: ISB ISB NTM 533052  242 53-0204 PART 4,6,7  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053  AREAS BEHIND SCUFF PLATES AT EMERGENCY EXITS CUTOUT. PART 6  CN  NOTE: SCUFF PLATES TO BE REMOVED. 1991-132-124 FAA AD 97-11 ISB 53-0204  ISB 53-0233  531605-0604-1 240 STRUCTURE - FRAMES 55 TO 58 MEC DET T: 9 YE CPCP AMM SSI 5316 250 I: 5 YE MRB S  DETAILED INSPECTION OF INTERNAL STRUCTURE MRB REFERENC AROUND EMERGENCY EXITS ABOVE CABIN FLOOR UP TO  STRINGER 12 BETWEEN FRAME 55 AND 58. 531605-C604- 531605-C604- APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2 OR G3  AFTER INSPECTION.  PREP.: LININGS AND FURNISHINGS IN DOOR AREAS AND  INSULATION REMOVED  531605-0604-4 241 STRUCTURE AROUND EMERGENCY EXIT MEC DET T: 16000 FC ALI EASA AD  242 OR 2006-0071  DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND 18000 FH FAA AD  EMERGENCY EXIT ABOVE CABIN FLOOR BETWEEN FR 55 AND I: 7500 FC 2007-04-11  FR 59 AND BETWEEN STR 12 AND STR 26. OR  8400 FH ALI REFERENC ACCESS: 844 531605-01-1  531605-0604-5 241 STRUCTURE AROUND EMERGENCY EXIT MEC DET T: 16000 FC ALI EASA AD  242 OR 2006-0071  DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND 21700 FH FAA AD  EMERGENCY 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 10200 FH 531605-01-2  ACCESS: 844  531605-0604-6 241 STRUCTURE AROUND EMERGENCY EXIT MEC DET T: 16000 FC ALI EASA AD  242 OR 2006-0071  DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND 35300 FH FAA AD  EMERGENCY EXIT ABOVE CABIN FLOOR BETWEEN FR 55 AND I: 7500 FC 2007-04-11  FR 59 AND BETWEEN STR 12 AND STR 26. OR  16500 FH ALI REFERENC ACCESS: 844 531605-01-3  531700-0602-1 251 FRAME 57A AND FRAME 65 MEC GVI T: 20000 FH CN CN  252 OR FAA AD 1983-102-053 VISUAL INSPECTION OF STRINGER 5 CONNECTION AT FRAME 20000 FC ISB FAA AD 98-20 65, LH AND RH, AND REINFORCING CROSS STRAP BETWEEN I: 3000 FH ISB 53-0143  STRINGER 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 5317 MRB S  DETAILED INSPECTION OF AFT CARGO COMPARTMENT MRB REFERENC DOOR SILL BEAM FROM FRAME 59 TO FRAME 64, INCLUDING  TORSION BOX AND ATTACHMENT AREAS OF FRAMES 60 TO 63 531701-C603- (7 PLACES) BETWEEN STRINGERS 44 RH AND 46 RH  NOTE: 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  531703-0602-1 252 FRAME 59 MEC DET I: 7000 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS IN AREA OF FRAME 59 BETWEEN STRINGERS  21R AND 22R  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531703-0604-1 252 FRAME 59 MEC DET I: 27300 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 59 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 21R AND 22R.  PREP.: LINING AND INSULATION REMOVED.  531703-0604-2 252 FRAME 59 MEC DET I: 22600 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 59 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 21R AND 22R.  PREP.: LINING AND INSULATION REMOVED.  531703-0604-3 252 FRAME 59 MEC DET I: 19200 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 59 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 21R AND 22R.  PREP.: LINING AND INSULATION REMOVED.  531704-0602-1 154 FRAME 59 MEC DET I: 7000 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS IN AREA OF FRAME 59 BETWEEN STRINGERS  46R AND 47R  531704-0604-1 154 FRAME 59 MEC DET I: 27300 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 59 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 46R AND 47R.  PREP.: INSULATION REMOVED.  ACCESS: 152FF  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531704-0604-2 154 FRAME 59 MEC DET I: 22600 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 59 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 46R AND 47R.  PREP.: INSULATION REMOVED.  ACCESS: 152FF  531704-0604-3 154 FRAME 59 MEC DET I: 19200 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 59 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 46R AND 47R.  PREP.: INSULATION REMOVED.  ACCESS: 152FF  531705-0602-1 252 FRAME 64 MEC DET I: 7000 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS IN AREA OF FRAME 64 BETWEEN STRINGERS  21R AND 22R  531705-0604-1 252 FRAME 64 MEC DET I: 27300 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 64 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 21R AND 22R.  PREP.: LINING AND INSULATION REMOVED.  531705-0604-2 252 FRAME 64 MEC DET I: 22600 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 64 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 21R AND 22R.  PREP.: LINING AND INSULATION REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531705-0604-3 252 FRAME 64 MEC DET I: 19200 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 64 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 21R AND 22R.  PREP.: LINING AND INSULATION REMOVED.  531706-0602-1 154 FRAME 64 MEC DET I: 7000 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF EXTERNAL SKIN AND  RIVETS IN AREA OF FRAME 64 BETWEEN STRINGERS  46R AND 47R  531706-0604-1 154 FRAME 64 MEC DET I: 27300 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 64 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 46R AND 47R.  PREP.: LINING AND FLOOR PANELS REMOVED.  531706-0604-2 154 FRAME 64 MEC DET I: 22600 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 64 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 46R AND 47R.  PREP.: LINING AND FLOOR PANELS REMOVED.  531706-0604-3 154 FRAME 64 MEC DET I: 19200 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF FRAME 64 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME BETWEEN  STRINGERS 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 FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC ATTACHMENT AREA OF FORMED FRAMES 60 TO 63 (4 PLACES) 531711-01-1  BETWEEN STRINGERS 21RH AND 22RH.  531711-0604-1 252 FRAMES 60 TO 63 MEC DET I: 27300 FC MRB S AMM SSI 5317 DETAILED INSPECTION OF HINGE FITTINGS OF AFT  CARGO COMPARTMENT DOOR AT ATTACHMENT AREAS OF FORMED  FRAMES 60 TO 63 (4 PLACES) TO HINGE FITTINGS BETWEEN  STRINGERS 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 5317 DETAILED INSPECTION OF HINGE FITTINGS OF AFT  CARGO COMPARTMENT DOOR AT ATTACHMENT AREAS OF FORMED  FRAMES 60 TO 63 (4 PLACES) TO HINGE FITTINGS BETWEEN  STRINGERS 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 5317 DETAILED INSPECTION OF HINGE FITTINGS OF AFT  CARGO COMPARTMENT DOOR AT ATTACHMENT AREAS OF FORMED  FRAMES 60 TO 63 (4 PLACES) TO HINGE FITTINGS BETWEEN  STRINGERS 21R AND 22R.  PREP.: CABIN LINING AND INSULATION REMOVED.  531715-0603-1 162 FRAME 67 MEC DET I: 27300 FC MRB S AMM SSI 5317 164  DETAILED INSPECTION OF FRAME 67 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME AND MACHINED  FRAME BETWEEN STRINGERS 32RH AND 47RH.  PREP.: LINING AND INSULATION REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531715-0603-2 162 FRAME 67 MEC DET I: 22600 FC MRB S AMM SSI 5317 164  DETAILED INSPECTION OF FRAME 67 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME AND MACHINED  FRAME 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 5317 164  DETAILED INSPECTION OF FRAME 67 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME AND MACHINED  FRAME 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 53-0187  I: 2000 FH  SPECIAL DETAILED INSPECTION ON THE EXTERNAL FLANGES  OF REAR CARGO COMPARTMENT DOOR FRAME UPPER AND LOWER  BEAMS FOR CRACKS  531717-0603-1 162 FRAME 69 MEC DET I: 11200 FC MRB S AMM SSI 5317 164  DETAILED INSPECTION OF FRAME 69 AT ATTACHMENT  AREA OF MACHINED FRAME TO FORMED FRAME AND MACHINED  FRAME BETWEEN STRINGERS 32RH AND 47RH.  PREP.: LINING AND INSULATION REMOVED.  531719-0603-2 162 BULK CARGO DOOR CUTOUT MEC SDI T: ISB ISB NTM 533052  53-0204 PART 4,6,7  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053  AREAS BEHIND SCUFF PLATES AT BULK CARGO DOOR CUTOUT. PART 6  CN  NOTE: SCUFF PLATES TO BE REMOVED 1991-132-124 FAA AD 97-11 ISB 53-0204  ISB 53-0233  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC BOX I: 30 MO 531720-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL  STRUCTURE AROUND WASTE WATER CONNECTION BOX  BETWEEN FRAME 78 AND FRAME 79 FROM STRINGER 45 LH  TO STRINGER 51 LH.  NOTE: APPLY TEMPORARY PROTECTION SYSTEM TYPE 1 AND  TYPE 2 AFTER INSPECTION.  ACCESS : INSULATION REMOVED  ACCESS: 162AZ 813  531813-0603-1 171 REAR PRESSURE BULKHEAD MEC DET I: 7000 FC MRB S AMM SSI 5318 172  DETAILED INSPECTION OF INTERNAL REAR PRESSURE  BULKHEAD FORWARD FACE LOWER PORTION BELOW CABIN FLOOR  LINE.  PREP.: INSULATION TO BE REMOVED.  ACCESS: 162AZ  531814-0604-1 261 TORSION BOX FRAMES 72 TO 73 MEC DET I: 27300 FC MRB S AMM SSI 5318 262  DETAILED INSPECTION OF INTERNAL TORSION BOX  RUN-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 5318 262  DETAILED INSPECTION OF INTERNAL TORSION BOX  RUN-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 5318 262  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 BOX  RUN-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 REFERENC 260 I: 30 MO MRB S  DETAILED INSPECTION OF EXTERNAL SKIN 531815-C602- AND RIVETS AROUND AFT PASSENGER/CREW DOOR ABOVE CABIN  FLOOR BETWEEN FRAMES 72 AND 76 AND STRINGERS 9 AND 26  AND 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 SB  53-0233, CPCP TASK IS NOT TO BE APPLIED.  PREPARATION: PAX DOORS OPENED  531815-0603-1 250 STRUCTURE AROUND AFT PAX DOOR MEC DET T: 9 YE CPCP AMM SSI 5318 260 I: 5 YE MRB S  DETAILED INSPECTION OF INTERNAL STRUCTURE MRB REFERENC AROUND AFT PASSENGER/CREW DOORS ABOVE CABIN FLOOR  BETWEEN FRAMES 72 AND 76 BETWEEN STRINGER 9 531815-C603- AND STRINGER 26 LH/RH. 531815-C603- NOTE: 01. LININGS AND FURNISHINGS IN DOOR AREAS AND  INSULATION 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 AD  252 DOOR I: 10000 FC 2006-0071  FAA AD  DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT 2007-04-11  PASSENGER/CREW DOORS ABOVE CABIN FLOOR BETWEEN FR 72  AND FR 76 BETWEEN STR 9 AND STR 26, TORSION BOX RUN- ALI REFERENC OUT BETWEEN FR 72/73 AND 76/77, STR 9 AND 11. 531815-01-1  PREP : LINING AND INSULATION TO BE REMOVED  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531815-0604-4 * * * * * C O N T I N U E * * * * *  ACCESS: 843  531816-0603-1 261 FRAME 73A MEC DET T: 20000 FC ALI EASA AD  262 I: 9000 FC 2006-0071  DETAILED INSPECTION OF INTERNAL FRAME 73A FAA AD  BETWEEN STRINGER 11 AND 13 IN THE RADII BETWEEN FRAME 2007-04-11  OUTER STRAP AND WEB.  ALI REFERENC PREP.: PANELS AND INSULATION TO BE REMOVED. 531816-01-1  531817-0604-1 171 FRAME 73 TO 76 NDT SDI I: 17700 FC MRB S AMM SSI 5318 172 NTM 531800  DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 6 AND 7  STRUCTURE BELOW CABIN FLOOR AT AFT PASSENGER/CREW  DOORS BETWEEN FRAME NO.73 AND 76 AND BETWEEN  STRINGERS 24 AND 28.  PREP.: INSULATION REMOVED.  ACCESS: 162AZ  531817-0604-3 171 FRAME 73 TO 76 NDT SDI I: 15100 FC MRB S AMM SSI 5318 172 NTM 531800  DETAILED AND SPECIAL DETAILED INSPECTION OF INTERNAL PART 6 AND 7  STRUCTURE BELOW CABIN FLOOR AT AFT PASSENGER/CREW  DOORS BETWEEN FRAME NO.73 AND 76 AND BETWEEN  STRINGERS 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 5318 262  DETAILED INSPECTION OF INTERNAL TORSION BOX  RUN OUT BETWEEN FRAMES 76 AND 77 STRINGERS 9 AND 11.  PREP.: LINING AND INSULATION REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5318 262  DETAILED INSPECTION OF INTERNAL TORSION BOX  RUN OUT BETWEEN FRAMES 76 AND 77 STRINGERS 9 AND 11  PREP.: LINING AND INSULATION REMOVED.  531818-0604-3 261 TORSION BOX, FRAME 76 TO 77 MEC DET I: 19200 FC MRB S AMM SSI 5318 262  DETAILED INSPECTION OF INTERNAL TORSION BOX  RUN 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 5318 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD  FORWARD 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 5318 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD  FORWARD 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 5318 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD  FORWARD 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 531800  262 I: 4000 FC FAA AD PART 6  SPECIAL DETAILED INSPECTION OF THE INNER FLANGE OF ISB CN  FRAME 73A RH AND LH BETWEEN BEAMS 5 AND 7 1988-061-083 FAA AD 89-03 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 53-0220  FRAME LININGS AND INSULATION  531820-0603-2 171 FUSELAGE NDT SDI T: 24100 FC CN NTM 531802  172 I: 3400 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW ISB CN F-2002-63 STRINGER 28 BETWEEN FRAME 72 AND FRAME 76 LH AND RH. FAA AD  2004-08-05  ISB 53-0357  531820-0603-3 171 FUSELAGE NDT SDI T: 29500 FC CN NTM 531802  172 I: 5400 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW ISB CN F-2002-63 STRINGER 28 BETWEEN FRAME 72 AND FRAME 76 LH AND RH. FAA AD  2004-08-05  ISB 53-0357  531912-0603-1 310 PRESSURE BULKHEAD NDT SDI T: 12000 FC CN NTM 531911  I: 6000 FC FAA AD PART 2, 4 AN SPECIAL DETAILED INSPECTION OF REAR PRESSURE BULKHEAD ISB CN  AT INNER RIVET ROW OF CIRCUMFERENTIAL SPLICE IN AREAS 1980-218-028 1 AND 2 FAA AD 94-09 ISB 53-0152  ACCESS: 312AR  531912-0603-2 310 PRESSURE BULKHEAD NDT SDI T: 32000 FC CN NTM 531911  I: 9000 FC FAA AD PART 2, 4 AN SPECIAL DETAILED INSPECTION OF PRESSURE BULKHEAD AT ISB CN  INNER RIVET ROW OF RADIAL STIFFENER ATTACHMENT 1980-218-028 FITTINGS IN AREAS 3 AND 4. FAA AD 94-09 ISB 53-0152  ACCESS: 312AR  531921-0603-1 311 PRESSURE BULKHEAD NDT SDI T: 20000 FC ALI NTM 531911  I: 7200 FC PART 4 AND 6  SPECIAL DETAILED INSPECTION OF PRESSURE BULKHEAD AT CN 2006-0071 INNER RIVET ROW OF CIRCUMFERENTIAL SPLICE IN AREAS 1 FAA AD 96-13 AND 2.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531921-0603-1 * * * * * C O N T I N U E * * * * *  ACCESS: 312AR ALI REFERENC 531921-01-1  531921-0603-2 311 PRESSURE BULKHEAD NDT SDI T: 32000 FC ALI NTM 531911  I: 7200 FC PART 4 AND 6  SPECIAL DETAILED INSPECTION OF PRESSURE BULKHEAD AT CN 2006-0071 INNER RIVET ROW OF RADIAL STIFFENER ATTACHMENT FAA AD 96-13 FITTINGS 1, 5LH, 5RH, 9RH, 9LH AND 13 (AREAS 3 AND 4  AS DEFINED BY NTM 531911) ALI REFERENC 531921-02-1  ACCESS: 312AR  531925-0603-1 313 FRAME NO. 91 COMPLETE MEC DET T: 11200 FC ALI CN 2006-0071 314 OR CN FAA AD 96-13 DETAILED INSPECTION OF FRAME NO.91 COMPLETE, 12800 FH FAA AD  INCLUDING CENTER FITTINGS DIAGONAL SUPPORTS, HINGE I: 8400 FC ALI REFERENC SUPPORT MEMBERS AND LUGS OF HINGE SUPPORT MEMBERS AND OR 531925-01-1  FRAME. 9600 FH  ACCESS: 313AL  531925-0603-2 313 FRAME NO. 91 COMPLETE MEC DET T: 11000 FC ALI CN 2006-0071 314 OR CN FAA AD 96-13 DETAILED INSPECTION OF FRAME NO.91 COMPLETE, 15300 FH FAA AD  INCLUDING CENTER FITTINGS DIAGONAL SUPPORTS, HINGE I: 8300 FC ALI REFERENC SUPPORT MEMBERS AND LUGS OF HINGE SUPPORT MEMBERS AND OR 531925-01-2  FRAME. 11500 FH  ACCESS: 313AL  531925-0603-3 313 FRAME NO.91 COMPLETE MEC DET T: 10000 FC ALI CN 2006-0071 314 OR CN FAA AD 96-13 DETAILED INSPECTION OF FRAME NO.91 COMPLETE, 23000 FH FAA AD  INCLUDING CENTER FITTINGS DIAGONAL SUPPORTS, HINGE I: 7500 FC ALI REFERENC SUPPORT MEMBERS AND LUGS OF HINGE SUPPORT MEMBERS AND OR 531925-01-3  FRAME. 17000 FH  ACCESS: 313AL  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 531926-0603-1 313 FRAME 91 NDT SDI T: 24000 FC ISB AMM SSI 5319 314 I: 12000 FC MRB S NTM 531900  SPECIAL DETAILED INSPECTION OF FRAME 91, UPPER AND PART 4  LOWER LUGS AND HINGE SUPPORT MEMBERS. ISB 53-258  PREP: REMOVE HORIZONTAL STABILIZER ATTACH.FITTINGS  531929-0603-1 311 REAR PRESSURE BULKHEAD MEC DET I: 8400 FC MRB S AMM SSI 5319 312  DETAILED INSPECTION OF REAR PRESSURE BULKHEAD  AFT FACE RIVETING OF ALL JOINTS.  ACCESS: 312AR  531931-0603-1 311 REAR PRESSURE BULKHEAD MEC DET I: 30 MO CPCP AMM SSI 5319 312 MRB S  DETAILED INSPECTION OF REAR PRESSURE BULKHEAD MRB REFERENC LOWER AREA (BELOW STRINGER 26 LEVEL) AND STRUCTURE  AROUND DRAINAGE HOLE BETWEEN FRAME 80 AND FRAME 81. 531931-C603- NOTE:01.APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION.  NOTE:02.ENSURE DRAIN HOLES FREE OF ANY OBSTRUCTIONS.  ACCESS: 312AR R 531933-0603-1 170 REAR PRESSURE BULKHEAD NDT SDI T: 90 MO AD NTM 513010  310 I: 8000 FC ISB PART 1  SPECIAL DETAILED INSPECTION OF LOWER ATTACHMENT NTM 531911  ANGLES OF REAR PRESSURE BULKHEAD, FWD AND REAR FACES, CONFIG-1  BELOW STRINGER 27 LEVEL. PART 2, 6  AD F-2004-19 NOTE: INSULATION TO BE REMOVED ISB 53-0363  ACCESS: 162AZ 312AR R 531933-0603-2 170 REAR PRESSURE BULKHEAD MEC DET T: 90 MO AD AD F-2004-19 310 I: 3 YE ISB ISB 53-0363  DETAILED INSPECTION OF LOWER ATTACHMENT ANGLES  OF 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REMOVED  ACCESS: 162AZ 312AR  531933-0603-3 170 REAR PRESSURE BULKHEAD NDT SDI T: 90 MO AD NTM 513010  310 I: 8000 FC EUAD PART 1  SPECIAL DETAILED INSPECTION OF LOWER ATTACHMENT ISB NTM 531911  ANGLES OF REAR PRESSURE BULKHEAD, FWD AND REAR FACES, CONFIG-1  BELOW STRINGER 27 LEVEL. PART 2, 6  AD 2005-26-1 NOTE: INSULATION TO BE REMOVED CN  F-1989-068-0 ACCESS: 162AZ 312AR EUAD F-2004- FAA AD 90-03 ISB 53-0363  531933-0603-4 170 REAR PRESSURE BULKHEAD MEC DET T: 90 MO AD AD 2005-26-1 310 I: 5 YE EUAD CN  DETAILED INSPECTION OF LOWER ATTACHMENT ANGLES ISB F-1989-068-0 OF REAR PRESSURE BULKHEAD, FWD AND REAR FACES, BELOW EUAD F-2004- STRINGER 27 LEVEL. FAA AD 90-03 ISB 53-0363  NOTE: INSULATION TO BE REMOVED  ACCESS: 162AZ 312AR  532100-0603-1 130 SEAT TRACKS MEC DET I: 1500 FH ISB CN  240 1990-222-116 DETAILED INSPECTION OF ALL DUMMY FAA AD  SWIVELLING SEAT TRACKS BETWEEN FR. 38.2 AND FR. 40 2000-10-01  AND BETWEEN FR. 54 AND FR. 54.2 FOR CRACKS, RUPTURE ISB 53-0103  AND DISTORTION.  ACCESS: 131BZ  532100-0603-3 130 SEAT TRACKS MEC DET I: 3000 FH ISB ISB 53-0179  240  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 SWIVELLING  SEAT TRACKS BETWEEN FR.38.2 AND FR.40 AND BETWEEN  FR.54 AND FR.54.2 FOR WEAR IN SIDE FITTINGS  RECTANGULAR HOLES.  ACCESS: 131BZ 131CZ 132EZ  533101-0602-1 211 UPPER SKIN PANEL, FRAME 10 MEC DET I: 8500 FC MRB S AMM SSI 5331 212  DETAILED INSPECTION OF EXTERNAL UPPER SKIN  SPLICE AT FRAME 10.  533103-0602-1 211 SKIN PANEL SPLICES MEC DET I: 8500 FC MRB S AMM SSI 5331 212  DETAILED INSPECTION OF EXTERNAL SKIN  SPLICES AT WINDSHIELD LOWER SECTION BETWEEN FRAMES 0  AND 10.  533105-0602-1 211 SKIN PANEL AT FRAME 7 MEC DET I: 8500 FC MRB S AMM SSI 5331 212  DETAILED INSPECTION OF EXTERNAL UPPER SIDE  SKIN 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 5331 122  DETAILED INSPECTION OF EXTERNAL UPPER SIDE  SKIN PANEL AT LOWER LONGITUDINAL SKIN SPLICE BETWEEN  FRAMES 0 AND 10.  533107-0602-1 121 SIDE SKIN PANEL MEC DET I: 11400 FC MRB S AMM SSI 5331 122  DETAILED INSPECTION OF EXTERNAL SIDE SKIN PANEL  ATTACHMENT TO LOWER SKIN PANEL BETWEEN FRAMES 0 AND  10.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5331 122  DETAILED INSPECTION OF EXTERNAL LOWER SKIN  PANEL AT TRANSVERSE SPLICE TO ACCESS DOOR SURROUND  PANEL.  533201-0602-1 210 SKIN PANEL, FRAMES 10 TO 18 MEC DET I: 8500 FC MRB S AMM SSI 5332 220  DETAILED INSPECTION OF EXTERNAL SKIN PANEL  SPLICES AT STRINGERS 9 L/H AND 9 R/H BETWEEN FRAMES  10 AND 18.  533209-0602-1 121 SKIN PANEL, FRAME 12 TO FRAME 13 MEC DET T: 19000 FC ALI EASA AD  122 I: 11400 FC 2006-0071  DETAILED INSPECTION OF EXTERNAL SKIN FAA AD  PANELS BETWEEN FRAMES 12 AND 13 AND BETWEEN 2007-04-11  STRINGERS 30 AND 40.  ALI REFERENC 533209-01-1  533211-0602-1 121 SKIN PANEL SPLICES MEC DET I: 8500 FC MRB S AMM SSI 5332 122  DETAILED INSPECTION OF EXTERNAL SKIN PANEL  SPLICES BETWEEN FRAMES 16A AND 18 AND STRINGERS 29 TO  45 L/H AND R/H SIDES.  533214-0602-1 121 NLG BAY SURROUND PANEL MEC DET I: 5700 FC MRB S AMM SSI 5332 122  DETAILED INSPECTION OF EXTERNAL NOSE LANDING  GEAR BAY SURROUND PANEL AND DOUBLER AT REAR LH AND RH  CORNER.  ACCESS: 713  714  533214-0604-1 123 NLG BAY SURROUND PANEL NDT SDI I: 27300 FC MRB S AMM SSI 5332 124 NTM 533200  SPECIAL DETAILED INSPECTION OF NOSE GEAR SURROUND PART 2  PANEL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 533214-0604-1 * * * * * C O N T I N U E * * * * *  ACCESS: 713  714  533215-0602-1 121 NOSE GEAR BAY FRONT SECTION MEC DET I: 11400 FC MRB S AMM SSI 5332 122  DETAILED INSPECTION OF EXTERNAL NOSE  GEAR 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 5332 122  DETAILED INSPECTION OF EXTERNAL NOSE  GEAR 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 5332 122  DETAILED INSPECTION OF EXTERNAL NOSE LANDING  GEAR BAY SURROUND PANEL LONGITUDINAL SPLICING AT  STRINGER 43 BETWEEN FRAMES 17 AND 19.  533218-0602-1 221 SKIN AROUND FWD PAX DOOR MEC DET I: 30 MO CPCP MRB REFERENC 222 OR MRB S  DETAILED INSPECTION OF EXTERNAL SKIN 2800 FC 533218-C602- AROUND FORWARD PASSENGER/CREW DOOR CUT-OUTS (25 CM/  10 INCHES AROUND CUT-OUT EDGES), INCLUDING FAIL SAFE  RING, AND CUT-OUT EDGES BETWEEN FRAMES 13A AND 17 AND  FROM STRINGER 9 DOWN TO FLOOR.  NOTE: 01. PAX DOORS TO BE OPENED  02. WHERE AREAS ARE COVERED BY SB 53-0204 AND  SB 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 53-0075  222  DETAILED INSPECTION OF EXTERNAL DOUBLERS  AROUND FWD PASS/CREW DOOR CUT-OUT BETWEEN FR.14 AND  16A AND STRG.9 TO 28 FOR CRACKS  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5332 122  DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  PANEL BETWEEN FRAMES 17 AND 19 AND STRINGER 43 L/H  AND 43 R/H.  533220-0603-1 220 FWD PAX/CREW DOOR CUTOUT MEC DET I: 6000 FH ISB ISB 53-0076  DETAILED INSPECTION OF FWD. PAX/CREW DOOR  CUT-OUT AT FR. 14 AND 16A FOR CRACKS  PREP: REMOVE LINING AND INSULATION  533220-0603-2 121 FWD PAX/CREW DOOR CUTOUT NDT SDI T: ISB ISB NTM 533052  122 53-0204 PART 4, 6, 7  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053  AREAS BEHIND SCUFF PLATES AT FORWARD PASSENGER/CREW PART 6  DOOR CUTOUT. CN  1991-132-124 PREP.: SCUFF PLATES TO BE REMOVED FAA AD 97-11 ISB 53-0204  ISB 53-0233  533220-0603-3 121 FWD PAX/CREW DOOR CUTOUT NDT SDI T: 20000 FC ISB NTM 533053  122 I: ISB PART 6  DETAILED AND SPECIAL DETAILED INSPECTION OF FWD 53-0227 CN  PAX/CREW DOOR CUTOUT AT HOLES OF CORNER DOUBLERS, 1991-132-124 FAIL SAFE RING AND DOOR FRAMES. FAA AD 97-11 ISB 53-0227  533302-0602-1 121 FUS.SKIN, FRAMES 18 TO 19 MEC DET I: 7000 FC MRB S AMM SSI 5333 DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  AROUND CUT-OUTS BETWEEN FRAMES 18 AND 19 AND BETWEEN  STRINGERS 28L AND 34L.  533304-0602-1 122 FUS.SKIN, FRAMES 18 TO 19 MEC DET I: 7000 FC MRB S AMM SSI 5333 DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  AROUND 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5333 240  DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  AND VISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAMES  18 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 5333 240  DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  AND VISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAMES  18 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 5333 240  DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  AND VISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAMES  18 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 5333 234  DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  AROUND ANTENNA CUT-OUT BETWEEN FRAMES 19 AND 21 FROM  STRINGER 1 TO CROWN CENTERLINE.  533315-0602-1 133 FUS.SKIN, FRAMES 25 TO 26 MEC DET I: 9000 FC MRB S AMM SSI 5333 134  DETAILED INSPECTION OF EXTERNAL FUSELAGE SKIN  AROUND 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 5333 DETAILED INSPECTION OF EXTERNAL FUSELAGE BUTT  JOINT BETWEEN UDC-DOOR AND MID PASSENGER/CREW DOOR,  BETWEEN FRAMES 27 AND 28 AT STRINGER 25L, EXTERNAL  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 231 I: 7900 FC FAA AD 96-13 233 DETAILED INSPECTION OF (EXTERNAL) SKIN IN  CORNERS OF UDC-DOOR CUT-OUT. ALI REFERENC 533331-01-1  ACCESS: 835  533331-0603-1 131 SKIN, UDC-DOOR CUT-OUT MEC DET T: 31600 FC ALI CN 2006-0071 231 I: 7900 FC FAA AD 96-13 233 DETAILED INSPECTION OF FUSELAGE SKIN IN  CORNERS OF UPPER (MAIN) DECK CARGO DOOR CUT-OUT. ALI REFERENC 533331-01-1  ACCESS: 835  533335-0603-1 233 STRUCTURE, FRAMES 20 TO 27 MEC DET I: 6000 FC MRB S AMM SSI 5333 DETAILED INSPECTION OF INTERNAL SUPPORT  STRUCTURE OF HINGE FITTINGS OF UDC DOOR INCLUDING  LONGERON BETWEEN FRAMES 20 AND 27 AND BETWEEN  STRINGERS 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 5333 DETAILED INSPECTION OF INTERNAL SUPPORT  STRUCTURE OF HINGE FITTINGS OF UDC-DOOR INCLUDING  LONGERON BETWEEN FRAMES 20 AND 27 AND BETWEEN  STRINGER 4 AND 5.  PREP: HATRACKS, FUSELAGE LINING AND INSULATION  REMOVED.  ACCESS: 835  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 I: 4200 FC FAA AD 96-13 DETAILED INSPECTION OF (INTERNAL) ATTACHMENT  AREAS OF LOCK FITTING AND LOWER UDC-DOOR LONGERON ALI REFERENC BETWEEN FRAMES 20 AND 27 AND BETWEEN STRINGER 26 AND 533339-01-1  34.  PREP.: LINING AND INSULATION TO BE REMOVED.  ACCESS: 811  533341-0603-1 130 FUSELAGE, FRAMES 20 AND 27 MEC DET I: 6000 FC MRB S AMM SSI 5333 230  DETAILED INSPECTION OF INTERNAL FUSELAGE  FRAMES 20 AND 27 BETWEEN CROWN AND BOTTOM CENTER LINE  LH AND RH.  PREP.: LINING AND INSULATION TO BE REMOVED  ACCESS: 132BF 132CF 811  533343-0603-1 232 FUSELAGE, FRAMES 21 TO 26 MEC DET T: 8400 FC ALI CN 2006-0071 234 I: 4200 FC FAA AD 96-13 DETAILED INSPECTION OF (INTERNAL) ATTACHMENT  AREA OF TRUSS FRAMES WITH NORMAL FRAMES FROM FRAMES ALI REFERENC 21 TO 26 BETWEEN STRINGERS 5 AND 10 (6 PLACES). 533343-01-1  PREP.: LINING AND INSULATION TO BE REMOVED.  533345-0602-1 231 SKIN IN CUT-OUT CORNERS MEC DET T: 12000 FC MRB S AMM SSI 5333 241 I: 3000 FC  DETAILED INSPECTION OF EXTERNAL SKIN IN CUT-  OUT CORNERS OF MID PASSENGER/CREW DOOR, L/H.  533401-0602-1 131 FUS.SKIN AROUND SPOTLIGHT MEC DET I: 7000 FC MRB S AMM SSI 5334 132  DETAILED INSPECTION OF EXTERNAL SKIN AROUND  SPOTLIGHT CUT-OUTS BETWEEN FRAMES 26 AND 27 AND  BETWEEN STRINGER 32 AND 34.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5334 132  DETAILED INSPECTION OF EXTERNAL SKIN AROUND  STATIC PRESSURE PORT CUT-OUTS BETWEEN FRAMES 27 AND  29 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 I: 9000 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE (EXTERNAL)  SKIN AROUND AIR CONDITIONING GROUND CONNECTION ALI REFERENC PANEL CUT-OUT BETWEEN FRAMES 36 AND 38 AND BETWEEN 533407-01-1  STRINGERS 47LH AND 50LH  533409-0604-1 130 FUS. SKIN, SLOT FLAP CUT-OUT NDT SDI I: 17700 FC MRB S AMM SSI 5334 NTM 533400  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AROUND PART 6  SLOT FLAP CUT-OUT, BETWEEN FRAMES 37 AND 38.1  STRINGERS 28 TO 34, ESPECIALLY IN CUT-OUT CORNERS IN  ZONES 137/138.  PREP.: FORWARD WING ROOT AND SLOT FAIRING OR BLANKING  PANEL REMOVED.  533409-0604-2 130 FUS. SKIN, SLOT FLAP CUT-OUT NDT SDI I: 15100 FC MRB S AMM SSI 5334 NTM 533400  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AROUND PART 6  SLOT FLAP CUT-OUT, BETWEEN FRAMES 37 AND 38.1  STRINGERS 28 TO 34, ESPECIALLY IN CUT-OUT CORNERS IN  ZONES 137/138.  PREP.: FORWARD WING ROOT AND SLOT FAIRING OR BLANKING  PANEL REMOVED.  533415-0602-1 231 FUS. SKIN, FRAMES 26 TO 27 MEC DET T: 14200 FC ALI CN 2006-0071 232 OR CN FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 26300 FC FAA AD  SKIN AROUND SPOTLIGHT CUT-OUTS BETWEEN FRAMES I: 7100 FC ALI REFERENC 26 AND 27 AND BETWEEN STRINGERS 24 AND 26. 533415-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 232 OR CN FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 23300 FC FAA AD  SKIN AROUND POTLIGHT CUT-OUTS BETWEEN FRAMES I: 7000 FC ALI REFERENC 26 AND 27 AND BETWEEN STRINGERS 24 AND 26. 533415-01-2  533415-0602-3 231 FUS.SKIN FRAMES 26 TO 27 MEC DET T: 13800 FC ALI CN 2006-0071 232 OR CN FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 23000 FC FAA AD  SKIN AROUND SPOTLIGHT CUT-OUTS BETWEEN FRAMES 26 I: 6900 FC ALI REFERENC AND 27 AND BETWEEN STRINGERS 24 AND 26, RH SIDE ONLY. 533415-01-3  NOTE: FOR C4, F4 AND B4-2C POST 6208, INSPECTION IS  APPLICABLE ONLY ON RH SIDE  533417-0602-1 230 FUS. SKIN, FRAMES 32 TO 33 MEC DET I: 7200 FC MRB S AMM SSI 5334 DETAILED INSPECTION OF EXTERNAL SKIN  AROUND CUT-OUT FOR ESCAPE SLIDE SPOTLIGHT BETWEEN  FRAMES 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 5334 DETAILED INSPECTION OF EXTERNAL SKIN  AROUND CUT-OUT FOR ESCAPE SLIDE SPOTLIGHT BETWEEN  FRAMES 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 5334 DETAILED INSPECTION OF EXTERNAL SKIN  AROUND DRAIN VALVE BETWEEN FRAMES 27 AND 28 FROM  STRINGER 54 TO CENTERLINE.  533425-0602-1 230 FUS. SKIN SPLICE, FRAME 26 MEC DET I: 7200 FC MRB S AMM SSI 5334 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  AT FRAME 26 FROM STRINGER 5 TO CROWN CENTER-LINE.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5334 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  AT 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 5334 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  AT 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 5334 DETAILED INSPECTION OF EXTERNAL SKIN  FROM FRAME 38.2 TO 40 FROM STRINGER 5 TO CROWN  CENTERLINE.  533427-0602-2 240 FUS.SKIN,FRAMES 38.2 TO 40 MEC DET I: 6500 FC MRB S AMM SSI 5334 DETAILED INSPECTION OF EXTERNAL SKIN  FROM FRAME 38.2 TO 40 FROM STRINGER 5 TO CROWN  CENTERLINE.  533427-0602-3 240 FUS.SKIN,FRAMES 38.2 TO 40 MEC DET I: 6400 FC MRB S AMM SSI 5334 DETAILED INSPECTION OF EXTERNAL SKIN  FROM FRAME 38.2 TO 40 FROM STRINGER 5 TO CROWN  CENTERLINE.  533429-0604-1 137 FUS. SKIN, FRAMES 37 TO 39 MEC DET I: 9300 FC MRB S AMM SSI 5334 138  DETAILED INSPECTION OF INTERNAL FUSELAGE SKIN  AROUND CUT-OUTS FOR WIRE BUNDLES BETWEEN FRAMES 37  AND 39 AND BETWEEN STRINGERS 27 AND 30.  PREP.: INSULATION REMOVED.  ACCESS: 131CZ  132EZ  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5334 138  DETAILED INSPECTION OF INTERNAL FUSELAGE SKIN  AROUND CUT-OUTS FOR WIRE BUNDLES BETWEEN FRAMES 37  AND 39 AND BETWEEN STRINGERS 27 AND 30.  PREP.: INSULATION REMOVED.  ACCESS: 131CZ  132EZ  533430-0602-1 130 FUSELAGE SKIN AT FR.28A & 30A NDT SDI T: 18000 FC ISB NTM 531403  OR PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME 24000 FH CN F-2004-18 28A AND FRAME 30A ABOVE STRINGER 30 LH/RH. I: 3000 FC FAA AD 96-17 ISB 53-0283  533435-0602-1 243 FUS.SKIN AT FRAME 34 MEC DET T: 17600 FC ALI EASA AD  244 I: 8800 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE (EXTERNAL)SKIN FAA AD  AT FRAME 34 FROM STRINGER 5 TO CROWN CENTERLINE. 2007-04-11  ALI REFERENC 533435-01-1  533435-0602-2 243 FUS.SKIN AT FRAME 34 MEC DET T: 17800 FC ALI EASA AD  244 I: 8900 FC 2006-0071  DETAILED INSPECTION OF FUESELAGE (EXTERNAL) FAA AD  SKIN AT FRAME 34 FROM STRINGER 5 TO CROWN CENTERLINE. 2007-04-11  ALI REFERENC 533435-01-2  533435-0602-3 243 FUS.SKIN AT FRAME 34 MEC DET T: 16000 FC ALI EASA AD  244 I: 8000 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA AD  SKIN AT FRAME 34 FROM STRINGER 5 TO CROWN CENTERLINE. 2007-04-11  ALI REFERENC 533435-01-3  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 230 I: 3500 FC 533437-C602- 240 DETAILED INSPECTION OF SURROUNDING OF MID  PASSENGER/CREW DOOR CUT-OUTS (25 CM/10 INCHES AROUNDS  CUT-OUT EDGES), INCLUDING FAIL SAFE RING, AND CUT-OUT  EDGES.  NOTE : WHERE AREAS ARE COVERED BY SB 53-0204 AND  SB 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 CN  132 I: NOTE 1983-102-053 DETAILED INSPECTION OF FUSELAGE AREA FAA AD 98-20 FROM FR.28 TO FR.31 BETWEEN STRINGER 29 AND 31 FOR ISB 53-0112  EVIDENCE OF CRACKING AT RIVET HOLES.  NOTE: REPET INSPECTION AT 30000 FC, 36000 FC AND  SUBSEQUENTLY EVERY 3000 FC.  533437-0602-4 130 SKIN AROUND MID PAX DOOR MEC DET T: 14000 FC ALI EASA AD  230 OR EASA AD 2006-0071  240 DETAILED INSPECTION OF FUSELAGE SKIN AROUND 23300 FC FAA AD FAA AD  MID PASSENGER/CREW DOOR CUT-OUT BETWEEN FRAME 27 AND I: 3500 FC 2007-04-11  FRAME 32 AND BETWEEN STRINGER 9 AND STRINGER 30  INCLUDING SCUFF PLATE. ALI REFERENC 533437-01-1  533439-0603-1 130 MID PAX/CREW DOOR CUTOUT NDT SDI T: ISB ISB AMM SSI 5334 53-0204 MRB S NTM 533052  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE PART 4, 6, 7  AREAS BEHIND SCUFF PLATES AT MID PASSENGER/CREW DOOR NTM 533053  CUTOUT PART 6  CN  PREP.: SCUFF PLATE TO BE REMOVED. 1991-132-124 FAA AD 97-11 ISB 53-0204  ISB 53-0233  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531400  I: ISB PART 2  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE 53-0227 NTM 533053  MID DOOR CUTOUT AT HOLES, OF CORNER DOUBLERS, FAIL PART 6  SAFE RING AND DOOR FRAMES. NTM 533400  PART 2  CN  1991-132-124 FAA AD 97-11 ISB 53-0227  533439-0603-3 131 FUSELAGE NDT SDI T: 30300 FC CN NTM 531406  132 I: 4100 FC ISB PART 4  SPECIAL DETAILED INSPECTION OF LAP JOINT BELOW CN F-2002-63 STRINGER 27 BETWEEN FRAME 28A AND FRAME 30A LH AND FAA AD  RH. 2004-08-05  ISB 53-0356  PREP.: INSULATION TO BE REMOVED  533507-0602-1 140 SKIN SPLICE, FR. 47 TO 48 MEC DET I: 8200 FC MRB S AMM SSI 5335 DETAILED INSPECTION OF SKIN SPLICE BETWEEN  FRAMES 47 AND 48 AT STRINGER 36 FROM INSIDE OF MLG  BAY.  533507-0602-2 140 SKIN SPLICE, FR. 47 TO 48 MEC DET I: 7000 FC MRB S AMM SSI 5335 DETAILED INSPECTION OF SKIN SPLICE BETWEEN  FRAMES 47 AND 48 AT STRINGER 36 FROM INSIDE OF MLG  BAY.  533507-0602-3 140 SKIN SPLICE, FR. 47 TO 48 MEC DET I: 5800 FC MRB S AMM SSI 5335 DETAILED INSPECTION OF SKIN SPLICE BETWEEN  FRAMES 47 AND 48 AT STRINGER 36 FROM INSIDE OF MLG  BAY.  533511-0604-1 147 SKIN PANEL ATTACHMENT MEC DET I: 27300 FC MRB S AMM SSI 5335 148  DETAILED INSPECTION OF ATTACHMENT OF SKIN  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  148KZ  533511-0604-2 147 SKIN PANEL ATTACHMENT MEC DET I: 22600 FC MRB S AMM SSI 5335 148  DETAILED INSPECTION OF ATTACHMENT OF SKIN  PANEL TO FRAME 47 BETWEEN STRINGERS 30 AND 36.  ACCESS: 147KZ  148KZ  533511-0604-3 147 SKIN PANEL ATTACHMENT MEC DET I: 19200 FC MRB S AMM SSI 5335 148  DETAILED INSPECTION OF ATTACHMENT OF SKIN  PANEL TO FRAME 47 BETWEEN STRINGERS 30 AND 36.  ACCESS: 147KZ  148KZ  533513-0602-1 240 SKIN SPLICES, FR.46 TO 48 MEC DET I: 8300 FC MRB S AMM SSI 5335 DETAILED INSPECTION OF EXTERNAL SKIN SPLICES  AT STRINGER 5 AND STRINGER 13 BETWEEN FRAME 46 AND  FRAME 48.  533513-0602-2 240 SKIN SPLICES, FR.46 TO 48 MEC DET I: 6800 FC MRB S AMM SSI 5335 DETAILED INSPECTION OF EXTERNAL SKIN SPLICES  AT STRINGER 5 AND STRINGER 13 BETWEEN FRAME 46 AND  FRAME 48.  533513-0602-3 240 SKIN SPLICES, FR.46 TO 48 MEC DET I: 6500 FC MRB S AMM SSI 5335 DETAILED INSPECTION OF EXTERNAL SKIN SPLICES  AT STRINGER 5 AND STRINGER 13 BETWEEN FRAME 46 AND  FRAME 48.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5335 DETAILED INSPECTION OF EXTERNAL SKIN SPLICES  AT 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 5335 DETAILED INSPECTION OF EXTERNAL SKIN SPLICES  AT 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 5335 DETAILED INSPECTION OF EXTERNAL SKIN SPLICES  AT STRINGER 5 BETWEEN FRAME 53 AND FRAME 54A.  533517-0602-1 241 CABIN WINDOW FRAMES MEC DET T: 11000 FC ALI EASA AD  242 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE (EXTERNAL)SKIN 12400 FH FAA AD  AND VISIBLE SECTIONS OF WINDOW FRAME FORGED COMPO- I: 5500 FC 2007-04-11  NENTS BETWEEN FRAMES 40 AND 54 AND STRINGERS 18 TO 28 OR  6200 FH ALI REFERENC NOTE THRESHOLD: 11000 FC 18300 FC 533517-01-1  12400 FH 20700 FH  533517-0602-2 240 CABIN WINDOW FRAMES MEC DET T: 2 YE MRB S AMM SSI 5335 I: 1 YE  DETAILED INSPECTION OF EXTERNAL SKIN  AND VISIBLE SECTIONS OF WINDOW FRAME FORGED COMPO-  NENTS BETWEEN FRAMES 40 AND 54 AND STRINGERS 18 TO 22  NOTE: IN CASE OF FINDINGS INSPECT REMAINING CABIN  WINDOW FRAMES I.A.W. TASK 533311-0602-1 AND  TASK 533725-0602-1  533517-0602-4 241 CABIN WINDOW FRAMES MEC DET T: 9200 FC ALI EASA AD  242 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 12500 FH FAA AD  SKIN AND VISIBLE SECTIONS OF WINDOW FRAME FORGED I: 4600 FC 2007-04-11  COMPONENTS BETWEEN FRAMES 40 AND 54 AND OR  STRINGERS 18 TO 28. 6200 FH ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 533517-0602-4 * * * * * C O N T I N U E * * * * *  533517-01-2  NOTE THRESHOLD: 9200 FC 15300 FC  12500 FH 20800 FH  533517-0602-5 241 CABIN WINDOW FRAMES MEC DET T: 8600 FC ALI EASA AD  242 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 19000 FH FAA AD  SKIN AND VISIBLE SECTIONS OF WINDOW FRAME I: 4300 FC 2007-04-11  FORGED COMPONENTS AND BETWEEN FRAMES 40 AND 54 AND OR  STRINGERS 18 TO 28. 9500 FH ALI REFERENC 533517-01-3  NOTE THRESHOLD: 8600 FC 14300 FC  19000 FH 31600 FH  533521-0602-1 145 CUT-OUT IN SKIN AT FRAME 40 MEC DET I: 11000 FC MRB S AMM SSI 5335 146  DETAILED INSPECTION OF UPPER CUT-OUT FOR WING  CENTER 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 5335 146  DETAILED INSPECTION OF UPPER CUT-OUT FOR WING  CENTER 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 5335 146  DETAILED INSPECTION OF UPPER CUT-OUT FOR WING  CENTER 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 5336 152  DETAILED INSPECTION OF EXTERNAL SKIN AT SHEAR  TIE ATTACHMENTS AND LONGITUDINAL SKIN SPLICES BETWEEN  FRAMES 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 5336 152  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 SHEAR  TIE ATTACHMENTS AND LONGITUDINAL SKIN SPLICES BETWEEN  FRAMES 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 5336 152  DETAILED INSPECTION OF EXTERNAL SKIN AT SHEAR  TIE ATTACHMENTS AND LONGITUDINAL SKIN SPLICES BETWEEN  FRAMES 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 AD  244 OR 2006-0071  253 DETAILED INSPECTION OF EXTERNAL SURFACE (SKIN) 21000 FH FAA AD  254 AROUND ANTENNA CUT-OUTS AT CROWN CENTERLINE BETWEEN I: 8000 FC 2007-04-11  FRAME 56 AND 57 AND BETWEEN FRAME 60 AND 61 AND OR  WIRE HOLES AT FR 57/58. 9000 FH ALI REFERENC 533605-01-1  PREP.: 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 AD  244 OR 2006-0071  253 DETAILED INSPECTION OF EXTERNAL SURFACE (SKIN) 18000 FH FAA AD  254 AROUND ANTENNA CUT-OUTS AT CROWN CENTERLINE BETWEEN I: 8000 FC 2007-04-11  FRAME 56 AND 57 AND BETWEEN FRAME 60 AND 61 AND WIRE OR  HOLES AT FR 57/58. 10800 FH ALI REFERENC 533605-01-2  PREP.: 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 AD  244 OR 2006-0071  253 DETAILED INSPECTION OF EXTERNAL SKIN AROUND 25400 FH FAA AD  254 ANTENNA CUT-OUTS AT CROWN CENTERLINE BETWEEN FRAME 56 I: 6200 FC 2007-04-11  AND 57 AND BETWEEN FRAME 60 AND 61 AND WIRE OR  HOLES AT FR 57/58. 13700 FH ALI REFERENC 533605-01-3  PREP.: ADF SENSE AND LOOP ANTENNAE TO BE REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5336 DETAILED INSPECTION OF EXTERNAL FUSELAGE JOINT  STRAP AT FRAME 54 FROM STRINGER 12 TO CROWN CENTER-  LINE  533607-0602-2 240 JOINT AT FRAME 54 MEC DET I: 6300 FC MRB S AMM SSI 5336 DETAILED INSPECTION OF EXTERNAL FUSELAGE JOINT  STRAP AT FRAME 54 FROM STRINGER 12 TO CROWN CENTER-  LINE  533607-0602-3 240 JOINT AT FRAME 54 MEC DET I: 5400 FC MRB S AMM SSI 5336 DETAILED INSPECTION OF EXTERNAL FUSELAGE JOINT  STRAP AT FRAME 54 FROM STRINGER 12 TO CROWN CENTER-  LINE  533607-0604-1 243 JOINT AT FRAME 54 NDT SDI I: 27300 FC MRB S AMM SSI 5336 244 NTM 533600  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 2 AND 7  JOINT STRAP AT FRAME 54 FROM STRINGER 12 TO CROWN  CENTER LINE.  PREP.: LINING AND INSULATION REMOVED.  533607-0604-2 240 JOINT AT FRAME 54 NDT SDI I: 22600 FC MRB S AMM SSI 5336 NTM 533600  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 2 AND 7  JOINT STRAP AT FRAME 54 FROM STRINGER 12 TO CROWN  CENTER LINE.  PREP.: LINING AND INSULATION REMOVED.  533607-0604-3 240 JOINT AT FRAME 54 NDT SDI I: 19200 FC MRB S AMM SSI 5336 NTM 533600  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 2 AND 7  JOINT STRAP AT FRAME 54 FROM STRINGER 12 TO CROWN  CENTER LINE.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 OR FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 26300 FH  SURFACE (SKIN) AROUND EMERGENCY EXITS BETWEEN I: 7000 FC ALI REFERENC FRAMES 54.1 - FR 58 AND BETWEEN CROWN CENTER LINE OR 533614-01-1  AND STR 30. 7900 FH  533614-0602-2 250 SKIN AROUND EMERGENCY EXIT MEC DET I: 30 MO CPCP MRB REFERENC 533614-C602- DETAILED INSPECTION OF SURROUNDING OF  EMERGENCY EXIT CUT-OUTS (25 CM/10 INCHES AROUND CUT-O  EDGES), INCLUDING FAIL SAFE RING, AND CUT-OUT EDGES.  NOTE : WHERE AREAS ARE COVERED BY SB 53-0204 AND  SB 53-0233 CPCP TASK IS NOT TO BE APPLIED.  PREP.: PAX DOORS OPENED  533614-0602-3 250 SKIN AROUND EMERG. EXIT MEC DET T: 16600 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 22500 FH  SURFACE (SKIN) AROUND EMERGENCY EXITS BETWEEN I: 5000 FC ALI REFERENC FRAMES 54.1 - FR 58 AND BETWEEN CROWN CENTER LINE OR 533614-01-2  AND STR 30. 6800 FH  533614-0602-4 250 SKIN AROUND EMERG. EXIT MEC DET T: 14300 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 31600 FH  SURFACE (SKIN) AROUND EMERGENCY EXITS BETWEEN I: 4300 FC ALI REFERENC FRAMES 54.1 - FR 58 AND BETWEEN CROWN CENTER LINE OR 533614-01-3  AND BETWEEN STRINGER 1 AND STRINGER 30. 9500 FH  533615-0603-1 251 EMERGENCY DOOR CUTOUT NDT SDI T: 18600 FC ALI NTM 533600  261 OR PART 4  VISUAL AND SPECIAL DETAILED INSPECTION OF FUSELAGE 21000 FH CN 2006-0071 SKIN UNDER UPPER DOUBLER BETWEEN FRAME 57A AND AFT I: 8400 FC FAA AD 96-13 END 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 533615-0603-1 * * * * * C O N T I N U E * * * * *  9500 FH ALI REFERENC PREP.: LINING AND INSULATION REMOVED. 533615-01-1  533615-0603-2 251 EMERGENCY DOOR CUTOUT NDT SDI T: 13300 FC ALI NTM 533600  261 OR PART 4  VISUAL AND SPECIAL DETAILED INSPECTION FUSELAGE SKIN 18100 FH CN 2006-0071 UNDER UPPER DOUBLER BETWEEN FRAME 57A AND AFT END OF I: 6000 FC FAA AD 96-13 DOUBLER FROM STRINGER 14 TO 17. OR  8100 FH ALI REFERENC PREP.: LINING AND INSULATION REMOVED. 533615-01-2  533615-0603-3 251 EMERGENCY DOOR CUTOUT NDT SDI T: 11500 FC ALI NTM 533600  261 OR PART 4  VISUAL AND SPECIAL DETAILED INSPECTION OF FUSELAGE 25400 FH CN 2006-0071 SKIN UNDER UPPER DOUBLER BETWEEN FRAME 57A AND AFT I: 5200 FC FAA AD 96-13 END OF DOUBLER FROM STRINGER 14 TO 17. OR  11500 FH ALI REFERENC PREP.: LINING AND INSULATION REMOVED. 533615-01-3  533616-0603-1 151 EMERGENCY DOOR CUTOUT NDT SDI T: 18600 FC ALI NTM 533600  152 OR PART 4  251 01. DETAILED INSPECTION OF FUSELAGE SKIN UNDER 21000 FH CN 2006-0071 261 LOWER DOUBLER BETWEEN FRAME 56A AND FRONT END I: 8400 FC FAA AD 96-13 OF DOUBLER FROM STRINGER 25 TO 27. OR  02. SPECIAL DETAILED INSPECTION OF PARTIAL AREAS. 9500 FH ALI REFERENC 533616-01-1  PREP.: CABIN AND CARGO COMPARTMENT LININGS TO BE  REMOVED.  533616-0603-2 151 EMERGENCY DOOR CUTOUT NDT SDI T: 13300 FC ALI NTM 533600  152 OR PART 4  251 01. DETAILED INSPECTION OF FUSELAGE SKIN 18100 FH CN 2006-0071 261 UNDER LOWER DOUBLER BETWEEN FRAME 56A AND I: 6000 FC FAA AD 96-13 FRONT END OF DOUBLER FROM STRINGER 25 TO 27. OR  02. SPECIAL DETAILED INSPECTION OF PARTIAL AREAS. 8100 FH ALI REFERENC 533616-01-2  PREP.: CABIN AND CARGO COMPARTMENT LININGS TO BE  REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 533616-0603-3 151 EMERGENCY DOOR CUTOUT NDT SDI T: 11500 FC ALI NTM 533600  152 OR PART 4  251 01. DETAILED INSPECTION OF FUSELAGE SKIN 25400 FH CN 2006-0071 261 UNDER LOWER DOUBLER BETWEEN FRAME 56A AND I: 5200 FC FAA AD 96-13 FRONT END OF DOUBLER FROM STRINGER 25 TO 27. OR  02. SPECIAL DETAILED INSPECTION OF PARTIAL AREAS. 11500 FH ALI REFERENC 533616-01-3  PREP.: CABIN AND CARGO COMPARTMENT LININGS TO BE  REMOVED.  533616-0603-4 153 FUSELAGE NDT SDI T: 30300 FC CN NTM 531601  154 I: 4100 FC ISB PART 4  SPECIAL DETAILED INSPECTION OF LAP JOINT AT STRINGER CN F-2002-63 52 BETWEEN FRAME 56 AND FRAME 58 LH AND RH. FAA AD  2004-08-05  ISB 53-0356  533617-0603-1 241 FUSELAGE SKIN FR. 55 TO 58 NDT SDI I: 6500 FC MRB S AMM SSI 5336 242 NTM 533600  251 VISUAL AND SPECIAL DETAILED INSPECTION OF FUSELAGE PART 4  252 SKIN UNDER OUTER DOUBLER BETWEEN FRAME 55 AND 58 FROM  STRINGER 10 TO 13, ESPECIALLY THE FIRST RIVET ROW.  NOTE: 01. CABIN LININGS AND INSULATION REMOVED  02. 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, 179  533711-0602-1 250 FUSELAGE SKIN FR. 58 TO 65 MEC DET I: 6800 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT SHEAR  TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEEN  FRAME 58 AND 65 FROM STRINGER 5 TO 13  FATIGUE RATE = 0.18  533711-0602-2 250 FUSELAGE SKIN FR. 58 TO 65 MEC DET I: 6500 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT SHEAR  TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEEN  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 13  FATIGUE RATE = 0.18  533711-0602-3 250 FUSELAGE SKIN FR. 58 TO 65 MEC DET I: 5800 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT SHEAR  TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEEN  FRAME 58 AND 65 FROM STRINGER 5 TO 13  FATIGUE RATE = 0.18  533715-0602-1 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 6900 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT  SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES  BETWEEN FRAMES 65 AND 72 FROM STRINGER 5 TO 13  533715-0602-2 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 5900 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT  SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES  BETWEEN FRAMES 65 AND 72 FROM STRINGER 5 TO 13  533715-0602-3 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 5700 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT  SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES  BETWEEN FRAMES 65 AND 72 FROM STRINGER 5 TO 13  533717-0602-1 250 FUSELAGE SKIN FR. 65 TO 72 MEC DET I: 6900 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT  SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES  BETWEEN FRAME 65 AND 72 FROM STRINGER 13 TO 31.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT  SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES  BETWEEN 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 5337 DETAILED INSPECTION OF EXTERNAL SKIN AT  SHEAR TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES  BETWEEN 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 5337 DETAILED INSPECTION OF EXTERNAL SKIN AND  VISIBLE PORTION OF WINDOW FORGINGS BETWEEN FRAME  54 AND 77 FROM STRINGER 18 TO 22.  533727-0602-1 152 SKIN AROUND AFT CARGO DOOR MEC DET T: 18600 FC ALI CN  154 I: 8400 FC 1989-019-097 162 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA AD 96-13 164 SKIN AROUND AFT CARGO COMPARTMENT DOOR CUTOUT BETWEEN  252 FRAME 58 AND 65 FROM STRINGER 22RH TO 47RH ALI REFERENC 533727-01-1  533727-0602-3 152 SKIN AROUND AFT CARGO DOOR MEC DET T: 16600 FC ALI CN  154 I: 7500 FC 1989-019-097 162 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA AD 96-13 164 SKIN AROUND AFT CARGO COMPARTMENT DOOR CUTOUT BETWEEN  252 FRAME 58 AND 65 FROM STRINGER 22RH TO 47RH ALI REFERENC 533727-01-2  533727-0602-4 152 SKIN AROUND AFT CARGO DOOR MEC DET T: 18600 FC ALI CN  154 I: 8400 FC 1989-019-097 162 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) FAA AD 96-13 164 SKIN AROUND AFT CARGO COMPARTMENT DOOR CUTOUT BETWEEN  252 FRAME 58 AND 65 FROM STRINGER 22RH TO 47RH ALI REFERENC 533727-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 533727-0603-2 171 AFT PASSENGER DOOR CUTOUT NDT SDI T: 20000 FC ISB NTM 533053  172 I: ISB PART 6  DETAILED AND SPECIAL DETAILED INSPECTION OF AFT 53-0227 NTM 533800  PAX/CREW DOOR CUTOUT AT HOLES OF CORNER DOUBLERS, PART 2, 7  FAIL SAFE RING AND DOOR FRAMES. NTM 533810  PART 2  CN  1991-132-124 FAA AD 97-11 ISB 53-0227  533727-0603-3 162 AFT PASSENGER DOOR CUTOUT NDT SDI T: ISB ISB NTM 533052  53-0204 PART 4, 6, 7  DETAILED AND SPECIAL DETAILED INSPECTION OF FUSELAGE I: 5 YE NTM 533053  AREAS BEHIND SCUFF PLATES AT AFT PASSENGER/CREW DOOR PART 6  CUTOUT CN  1991-132-124 PREP.: SCUFF PLATES TO BE REMOVED. FAA AD 97-11 ISB 53-0204  ISB 53-0233  533729-0602-1 162 SKIN AROUND BULK CARGO DOOR MEC DET T: 23300 FC ALI EASA AD  164 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN AROUND 26500 FH FAA AD  BULK CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR.66 AND I: 7000 FC 2007-04-11  70 FROM STRINGER 31RH TO 48RH ESPECIALLY CUTOUT OR  CORNERS 8000 FH ALI REFERENC 533729-01-1  533729-0602-3 162 SKIN AROUND BULK CARGO DOOR MEC DET T: 22300 FC ALI EASA AD  164 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 31000 FH FAA AD  SKIN AROUND BULK CARGO DOOR CUTOUT BETWEEN FRAMES 66 I: 6700 FC 2007-04-11  AND 70 AND STRINGER 31RH TO 48RH ESPECIALLY CUTOUT OR  CORNERS. 9300 FH ALI REFERENC 533729-01-2  533729-0602-4 162 SKIN AROUND BULK CARGO DOOR MEC DET T: 21600 FC ALI EASA AD  164 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 50100 FH FAA AD  SKIN AROUND BULK CARGO DOOR CUTOUT BETWEEN FRAMES 66 I: 6500 FC 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC CORNERS. 15100 FH 533729-01-3  533730-0603-1 160 LONGITUDINAL LAP JOINT NDT SDI I: 7.5 MO ISB NTM 513105  OR PART 1  SPECIAL DETAILED INSPECTION OF LONGITUDINAL LAP JOINT 1250 FC NTM 533005  BETWEEN FRAMES 65 AND 72 AT STRINGER 57. PART 6  CN  NOTE: TASK TO BE PERFORMED ALTERNATING EXTERNAL 1998-150-246 FUSELAGE INSPECTION (NO ACCESS) AND INTERNAL FAA AD 99-26 FUSELAGE INSPECTION (FLOOR PANELS AND ISB 53-0305  INSULATION REMOVED)  533731-0602-1 250 FUSELAGE SKIN SPLICE FR.58 MEC DET I: 6800 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGS  AT FRAME 58 FROM STRINGER 12 TO CROWN CENTER LINE  NOTE: FOR PRE MOD 02526 AND 02147 THIS TASK CAN  BE COMBINED WITH TASK REF:533731-0602-2  PREP.: ANTENNA COVER TO BE REMOVED.  533731-0602-2 250 FUSELAGE SKIN SPLICE FR.58 MEC DET T: 18000 FH CN CN  OR FAA AD 1983-102-053 DETAILED INSPECTION OF EXTERNAL SKIN OF 18000 FC ISB FAA AD 98-20 FUSELAGE AT FRAME 58 IN AREA BETWEEN STRINGER 5 LH I: 3000 FH ISB 53-0127  AND STRINGER 5 RH FOR CRACKS  PREP.: ANTENNA COVER TO BE REMOVED  533731-0602-3 250 FUSELAGE SKIN SPLICE FR. 58 MEC DET I: 5400 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGS  AT FRAME 58 FROM STRINGER 12 TO CROWN CENTER LINE  NOTE: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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:533731-0602-2  PREP.: ANTENNA COVER TO BE REMOVED.  533731-0602-4 250 FUSELAGE SKIN SPLICE FR. 58 MEC DET I: 6300 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGS  AT FRAME 58 FROM STRINGER 12 TO CROWN CENTER LINE  NOTE: FOR PRE MOD 02526 AND 02147 THIS TASK CAN  BE COMBINED WITH TASK REF:533731-0602-2  PREP.: ANTENNA COVER TO BE REMOVED  533733-0602-1 250 FUSELAGE SKIN SPLICE FR.65 NDT DET I: 6900 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGS  AT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE  533733-0602-2 250 FUSELAGE SKIN SPLICE FR.65 NDT DET I: 6800 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGS  AT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE  533733-0602-3 250 FUSELAGE SKIN SPLICE FR.65 NDT DET I: 6400 FC MRB S AMM SSI 5337 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  INCLUDING FWD AND AFT RIVET ROW OF STRINGER COUPLINGS  AT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE  533803-0602-1 172 SKIN, WASTE DRAIN MAST AREA MEC DET I: 8400 FC MRB S AMM SSI 5338 DETAILED INSPECTION OF SKIN AROUND AFT WASTE  WATER DRAIN MAST  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5338 DETAILED INSPECTION OF EXTERNAL SKIN AT SHEAR  TIE ATTACHMENT AND LONGITUDINAL SKIN SPLICES BETWEEN  FRAME 72 AND 80 FROM STRINGER 6 TO CROWN CENTERLINE  533815-0602-1 250 FUSELAGE SKIN SPLICE.FR.72 NDT DET I: 7000 FC MRB S AMM SSI 5338 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  AT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE  533815-0602-3 253 FUSELAGE SKIN SPLICE FR.72 NDT SDI I: 3000 FC ISB NTM 512104  254 PART 1  SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL SPLICE NTM 513106  AT FR.72 FROM STRINGER 12 TO CROWN CENTER LINE. PART 1  NTM 533809  PART 4  CN  1983-102-053 FAA AD 98-20 ISB 53-0101  533821-0602-1 251 FUSELAGE SKIN FR. 73 TO 76 MEC DET T: 24600 FC ALI EASA AD  252 OR 2006-0071  261 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 28000 FH FAA AD  262 SKIN IN UPPER CORNERS ON AFT PASSENGER/CREW DOOR, I: 3700 FC 2007-04-11  BETWEEN FRAMES 73/74 AND 75/76 FROM STRINGER 10 TO 12 OR  4200 FH ALI REFERENC PREP.: DOORS TO BE OPENED 533821-01-1  533821-0602-2 251 FUSELAGE SKIN FR 73 TO 76 MEC DET T: 23300 FC ALI EASA AD  252 OR 2006-0071  261 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 32400 FH FAA AD  262 SKIN IN UPPER CORNERS ON AFT PASSENGER/CREW DOOR, I: 3500 FC 2007-04-11  BETWEEN FRAMES 73/74 AND 75/76 FROM STRINGER 10 TO 12 OR  4800 FH ALI REFERENC PREP.: DOORS TO BE OPENED 533821-01-2  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  252 OR 2006-0071  261 DETAILED INSPECTION OF FUSELAGE (EXTERNAL) 54000 FH FAA AD  262 SKIN IN UPPER CORNERS ON AFT PASSENGER/CREW DOOR, I: 3500 FC 2007-04-11  BETWEEN FRAMES 73/74 AND 75/76 FROM STRINGER 10 TO 12 OR  8100 FH ALI REFERENC PREP.: DOORS TO BE OPENED 533821-01-3  533822-0602-1 250 FUSELAGE SKIN FR. 73 TO 76 MEC DET I: 2700 FC MRB S AMM SSI 5338 DETAILED INSPECTION OF EXTERNAL SKIN AND SCUFF  PLATE AT LOWER CORNERS OF AFT PAX/CREW DOORS, BETWEEN  FRAMES 73/74 AND 75/76 AND BETWEEN STRINGERS 24  AND 27  533822-0602-2 250 FUSELAGE SKIN FR. 73 TO 76 MEC DET I: 2600 FC MRB S AMM SSI 5338 DETAILED INSPECTION OF EXTERNAL SKIN AND SCUFF  PLATE AT LOWER CORNERS OF AFT PAX/CREW DOORS, BETWEEN  FRAMES 73/74 AND 75/76 AND BETWEEN STRINGERS 24  AND 27  533822-0602-3 250 FUSELAGE SKIN FR. 73 TO 76 MEC DET I: 2400 FC MRB S AMM SSI 5338 DETAILED INSPECTION OF EXTERNAL SKIN AND SCUFF  PLATE AT LOWER CORNERS OF AFT PAX/CREW DOORS, BETWEEN  FRAMES 73/74 AND 75/76 AND BETWEEN STRINGERS 24  AND 27  533822-0604-1 251 AFT PAX/CREW DOOR CUTOUT - LOWER CORNERS MEC DET I: 17700 FC MRB S AMM SSI 5338 252  261 DETAILED INSPECTION OF INTERNAL STRUCTURE AT  262 LOWER CORNERS OF AFT PASSENGER/CREW DOOR CUTOUT  BETWEEN FRAME 73 AND 74 AND BETWEEN FRAME 75 AND 76  FROM 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 5338 252  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AT  262 LOWER CORNERS OF AFT PASSENGER/CREW DOOR CUTOUT  BETWEEN FRAME 73 AND 74 AND BETWEEN FRAME 75 AND 76  FROM 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 5338 MRB S NTM 533800  SPECIAL DETAILED INSPECTION OF LAP JOINTS AT STRINGER PART 4,6 AND  51 LH AND RH BETWEEN FRAME 72 AND FRAME 80. ISB 53-0225  533909-0602-1 312 SKIN CUT OUT FR. 82 TO 84 MEC DET I: 11200 FC MRB S AMM SSI 5339 DETAILED INSPECTION OF INTERNAL SKIN CUT OUT  BETWEEN FRAME 82 AND 84, FROM STRINGER 28R TO 33R  ACCESS: 312AR  533909-0602-2 312 SKIN CUT OUT FR. 82 TO 84 MEC DET I: 7300 FC MRB S AMM SSI 5339 DETAILED INSPECTION OF INTERNAL SKIN CUT OUT  BETWEEN FRAME 82 AND 84, FROM STRINGER 28R TO 33R  ACCESS: 312AR  533909-0602-3 312 SKIN CUT OUT FR. 82 TO 84 MEC DET I: 6200 FC MRB S AMM SSI 5339 DETAILED INSPECTION OF INTERNAL SKIN CUT OUT  BETWEEN FRAME 82 AND 84, FROM STRINGER 28R TO 33R  ACCESS: 312AR  533911-0602-1 310 FUSELAGE SKIN AT FRAME 80 MEC DET I: 8400 FC MRB S AMM SSI 5339 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 533911-0602-1 * * * * * C O N T I N U E * * * * *  DETAILED INSPECTION OF EXTERNAL SKIN  AT FRAME 80 FROM CROWN TO BOTTOM CENTER LINE  533911-0602-2 310 FUSELAGE SKIN AT FRAME 80 MEC DET I: 7500 FC MRB S AMM SSI 5339 DETAILED INSPECTION OF EXTERNAL SKIN  AT FRAME 80 FROM CROWN TO BOTTOM CENTER LINE  533911-0602-3 310 FUSELAGE SKIN AT FRAME 80 MEC DET I: 7900 FC MRB S AMM SSI 5339 DETAILED INSPECTION OF EXTERNAL SKIN  AT FRAME 80 FROM CROWN TO BOTTOM CENTER LINE  533915-0603-1 310 FUSELAGE SKIN AT FRAME 80 NDT SDI I: 8400 FC MRB S AMM SSI 5339 NTM 533900  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AND PART 4 AND 7  EXTERNAL DOUBLER AT FRAME 80 FROM STRINGER 24 TO  BOTTOM CENTER LINE, LH/RH.  533935-0603-1 260 REAR PRESSURE BULKHEAD NDT SDI T: 24000 FC EASA AD NTM 531911  310 I: 8000 FC FAA AD PART 2  01.DETAILED INSPECTION OF UPPER AREA (STRINGER ISB NTM 531911  26LH/RH TO CROWN CENTER LINE ) OF REAR PRESSURE PART 6  BULKHEAD FROM AFT FACE, EASA AD  02.SPECIAL DETAILED INSPECTION FROM OUTBOARD. F-2005-093  FAA AD  NOTE: INSULATION TO BE REMOVED 2006-25-04  ISB 53-0218  ACCESS: 162AZ  312AR  533935-0603-2 260 REAR PRESSURE BULKHEAD NDT SDI T: 24000 FC EASA AD NTM 531911  310 I: 6000 FC FAA AD PART 6  01.DETAILED INSPECTION OF ALL SERVICE ISB EASA AD  APERTURES IN REAR PRESSURE BULKHEAD. F-2005-093  02.SPECIAL DETAILED INSPECTION OF APU FUEL APERTURES. FAA AD  2006-25-04  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 53-0218  ACCESS: 162AZ  312AR  533935-0603-3 260 REAR PRESSURE BULKHEAD NDT SDI T: 24000 FC EASA AD NTM 531911  310 I: 6000 FC FAA AD PART 6  SPECIAL DETAILED INSPECTION OF APU BLEED AIR ISB EASA AD  APERTURE. F-2005-093  FAA AD  NOTE: INSULATION TO BE REMOVED 2006-25-04  ISB 53-0218  ACCESS: 162AZ  312AR  534100-0603-1 131 SEAT AND DUMMY TRACK ATTACHMENTS MEC DET I: 6000 FC CN CN  132 FAA AD 1999-511-297 151 DETAILED INSPECTION OF SEAT AND DUMMY TRACK ISB FAA AD 98-21 152 ATTACHMENTS LOCATED BETWEEN FRAME 38.2 AND FRAME 40 SB ISB 53-0329  AND BETWEEN FRAME 54 AND FRAME 54.2.  PREP.: AFT CARGO COMPARTMENT: REMOVE CEILING PANELS  BETWEEN FRAME 54 AND FRAME 54.2  ACCESS: 131BZ 131CZ  132EZ  241AXF 241AYF 241UF 241VF 241WF  242ANF 242APF 242AQF 242ASF  534100-0603-2 131 SEAT AND DUMMY TRACK ATTACHMENTS NDT SDI T: 9000 FC MPD AMM 531544/6 132 I: 9000 FC  151 SPECIAL DETAILED INSPECTION OF SEAT AND DUMMY TRACK  152 ATTACHMENTS LOCATED BETWEEN FRAME 38.2 AND FRAME 40  AND BETWEEN FRAME 54 AND FRAME 54.2.  PREP.: FWD AND AFT CARGO COMPARTMENT PARTITION AND  CEILING PANELS BETWEEN FRAME 38/38.2 AND  FRAME 54/54.2 REMOVAL  ACCESS: 131BZ 131CZ  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 534100-0603-2 * * * * * C O N T I N U E * * * * *  132EZ  534205-0602-1 120 NOSE GEAR ATTACH FITTING MEC DET I: 8500 FC MRB S AMM SSI 5342 DETAILED INSPECTION OF NOSE GEAR ACTUATING  CYLINDER ATTACH FITTING  534205-0604-1 120 NOSE GEAR ATTACH FITTING MEC SDI I: 27300 FC MRB S AMM SSI 5342 NTM 531200  SPECIAL DETAILED INSPECTION OF NOSE GEAR ACTUATING PART 4  CYLINDER ATTACH FITTING NTM 531200  PART 6  534206-0602-1 120 NOSE GEAR ATTACH FITTING MEC DET I: 8500 FC MRB S AMM SSI 5342 DETAILED INSPECTION OF NOSE GEAR TELESCOPIC  DRAG STRUT ATTACH FITTING  534213-0602-1 120 NLG DOOR HINGE FITTINGS MEC SDI I: 8500 FC MRB S AMM SSI 5342 NTM 531200  DETAILED OR SPECIAL DETAILED INSPECTION OF NOSE GEAR PART 6  DOOR HINGE FITTINGS ON FUSELAGE  534213-0603-1 120 AFT HINGE BOLT-AFT NLG DOOR NDT SDI I: 2000 LG ISB NTM 515000  ISB 53-0190  SPECIAL DETAILED INSPECTION OF AFT NLG DOOR AFT HINGE  BOLT FOR CRACKS  ACCESS: 121QF  534215-0602-1 120 NOSE GEAR HINGE FITTING MEC DET I: 7000 FC MRB S AMM SSI 5342 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FITTING  534215-0604-1 123 NOSE GEAR HINGE FITTING NDT SDI I: 27300 FC MRB S AMM SSI 5342 124 NTM 534300  SPECIAL DETAILED INSPECTION OF NOSE GEAR HINGE PART 6  FITTING.  534217-0604-1 121 NOSE GEAR HINGE FITTING NDT SDI I: 27300 FC MRB S AMM SSI 5342 122 NTM 534300  SPECIAL DETAILED INSPECTION OF NOSE GEAR HINGE PART 6  FITTING.  ACCESS: 121QF  122KF  534301-0604-1 132 CARGO DOOR JACK ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5343 DETAILED INSPECTION OF FWD CARGO COMPARTMENT  DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOOR  BEAMS 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 5343 DETAILED INSPECTION OF FWD CARGO COMPARTMENT  DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOOR  BEAMS 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 5343 DETAILED INSPECTION OF FWD CARGO COMPARTMENT  DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOOR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5343 DETAILED INSPECTION OF HINGE FITTINGS OF FWD  CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO  24A BETWEEN STRINGER 26R TO 27R  ACCESS: 132AR  534303-0604-2 132 HINGE FITTINGS CARGO DOOR MEC DET I: 27300 FC MRB S AMM SSI 5343 DETAILED INSPECTION OF HINGE FITTINGS OF FWD  CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO  25 BETWEEN STRINGER 26R TO 27R.  ACCESS: 132AR  534303-0604-3 132 HINGE FITTINGS CARGO DOOR MEC DET I: 22600 FC MRB S AMM SSI 5343 DETAILED INSPECTION OF HINGE FITTINGS OF FWD  CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO  25 BETWEEN STRINGER 26R TO 27R.  ACCESS: 132AR  534303-0604-4 132 HINGE FITTINGS CARGO DOOR MEC DET I: 22600 FC MRB S AMM SSI 5343 DETAILED INSPECTION OF HINGE FITTINGS OF FWD  CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO  25 BETWEEN STRINGER 26R TO 27R.  ACCESS: 132AR  534303-0604-5 132 HINGE FITTINGS. CARGO DOOR MEC DET I: 19200 FC MRB S AMM SSI 5343 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FWD  CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO  24A BETWEEN STRINGER 26R TO 27R  534303-0604-6 132 HINGE FITTINGS CARGO DOOR MEC DET I: 19200 FC MRB S AMM SSI 5343 DETAILED INSPECTION OF HINGE FITTINGS OF FWD  CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 20B TO  25 BETWEEN STRINGER 26R TO 27R.  534407-0602-1 231 HOOK ATTACHMENT FITTING MEC DET I: 8500 FC MRB S AMM SSI 5344 232  DETAILED 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 5345 142  DETAILED INSPECTION OF BRACE STRUTS AT FRAMES  41 TO 43, 45 AND 46 LOWER AND UPPER END FITTINGS AND  ATTACH LUGS.  ACCESS: 147AZ 147DZ  148AZ 148DZ  534507-0604-2 141 BRACE STRUTS , FR. 41 TO 46 MEC DET I: 22600 FC MRB S AMM SSI 5345 142  DETAILED INSPECTION OF BRACE STRUTS AT FRAMES  41 TO 43, 45 AND 46 LOWER AND UPPER END FITTINGS AND  ATTACH LUGS.  ACCESS: 147AZ 147DZ  148AZ 148DZ  534507-0604-3 141 BRACE STRUTS , FR. 41 TO 46 MEC DET I: 19200 FC MRB S AMM SSI 5345 142  DETAILED INSPECTION OF BRACE STRUTS AT FRAMES  41 TO 43, 45 AND 46 LOWER AND UPPER END FITTINGS AND  ATTACH LUGS.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 534507-0604-3 * * * * * C O N T I N U E * * * * *  ACCESS: 147AZ 147DZ  148AZ 148DZ  534509-0604-1 147 BRACE STRUTS, FR. 47 TO 54 MEC SDI I: 27300 FC MRB S AMM SSI 5345 148 NTM 531500  DETAILED OR SPECIAL DETAILED INSPECTION OF BRACE PART 6  STRUTS BETWEEN FRAMES 47 AND 54 AT LOWER AND UPPER  END, INCLUDING FITTING AND ATTACHMENT LUGS.  PREP.: REMOVE BOLTS AND BRACE STRUTS.  ACCESS: 147KZ  148KZ  534511-0604-1 147 BRACE STRUT FORK-END FITTING MEC DET I: 27300 FC MRB S AMM SSI 5345 148  DETAILED INSPECTION OF STRUCTURAL BRACE STRUT  FORK-END FITTING AND KEEL PICK-UP FITTING.  ACCESS: 147CF  534511-0604-2 147 BRACE STRUT FORK-END FITTING MEC DET I: 22600 FC MRB S AMM SSI 5345 148  DETAILED INSPECTION OF STRUCTURAL BRACE STRUT  FORK-END FITTING AND KEEL PICK-UP FITTING.  ACCESS: 147CF  534511-0604-3 147 BRACE STRUT FORK-END FITTING MEC DET I: 19200 FC MRB S AMM SSI 5345 148  DETAILED INSPECTION OF STRUCTURAL BRACE STRUT  FORK-END FITTING AND KEEL PICK-UP FITTING.  ACCESS: 147CF  534513-0604-1 140 BRACE STRUT FITTINGS MEC SDI I: 27300 FC MRB S AMM SSI 5345 NTM 531500  DETAILED 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AT  REAR SPAR AND PRESSURE WEB BEAMS.  PREP.: REMOVE BOLTS AND BRACE STRUTS.  ACCESS: 147BZ 147DZ 147KZ 148DZ 148KZ  534513-0604-2 140 BRACE STRUT FITTINGS MEC SDI I: 22600 FC MRB S AMM SSI 5345 NTM 531500  DETAILED OR SPECIAL DETAILED INSPECTION OF STRUCTURAL PART 6  BRACE STRUT FORK-END FITTINGS AND ATTACH FITTINGS AT  REAR SPAR AND PRESSURE WEB BEAMS.  PREP.: REMOVE BOLTS AND BRACE STRUTS.  ACCESS: 147BZ 147DZ 147KZ 148DZ 148KZ  534513-0604-3 140 BRACE STRUT FITTINGS MEC SDI I: 19200 FC MRB S AMM SSI 5345 NTM 531500  DETAILED OR SPECIAL DETAILED INSPECTION OF STRUCTURAL PART 6  BRACE STRUT FORK-END FITTINGS AND ATTACH FITTINGS AT  REAR SPAR AND PRESSURE WEB BEAMS.  PREP.: REMOVE BOLTS AND BRACE STRUTS.  ACCESS: 147BZ 147DZ 147KZ 148DZ 148KZ  534515-0602-1 147 MLG DOOR HINGE FITTINGS MEC DET I: 11400 FC MRB S AMM SSI 5345 148  DETAILED INSPECTION OF MAIN GEAR DOOR FWD AND  AFT HINGE FITTINGS.  534517-0602-1 147 MLG DOOR SUPPORT FITTING MEC DET I: 11400 FC MRB S AMM SSI 5345 148  DETAILED INSPECTION OF MAIN GEAR DOOR ACTU-  ATING CYLINDER SUPPORT FITTING AND CENTER HINGE.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5346 252  DETAILED 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 5347 DETAILED INSPECTION OF DOOR STOPS ON FRAMES OF  BULK CARGO COMPARTMENT CUT-OUT  534703-0604-1 152 CARGO DOOR JACK ATTACH. MEC DET I: 11200 FC MRB S AMM SSI 5347 DETAILED INSPECTION OF AFT CARGO COMPARTMENT  DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOOR  BEAMS 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 5347 DETAILED INSPECTION OF AFT CARGO COMPARTMENT  DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOOR  BEAMS 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 5347 DETAILED INSPECTION OF AFT CARGO COMPARTMENT  DOOR ACTUATING CYLINDER ATTACH BRACKET BETWEEN FLOOR  BEAMS AT FRAMES 61 AND 62.  PREP.: CEILING PANELS REMOVED.  534705-0604-4 152 HINGE FITTINGS, CARGO DOOR MEC DET T: 20000 FC ALI ALI REFERENC I: 8000 FC 534705-01-1  DETAILED INSPECTION OF HINGE FITTINGS OF AFT  CARGO COMPARTMENT DOOR IN FUSELAGE FROM FRAME 60 TO  FRAME 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 534705-0604-4 * * * * * C O N T I N U E * * * * *  ACCESS: 152BR  534803-0602-1 261 HOOK ATTACHMENT FITTINGS MEC DET I: 8400 FC MRB S AMM SSI 5348 262  DETAILED INSPECTION OF HOOK ATTACHMENT FIT  TINGS ON AFT PASSENGER DOOR CUTOUT UPPER FRAMES.  534805-0603-1 260 FUSELAGE - DOOR AREA NDT SDI T: 10 YE ISB NTM 531801  I: 5 YE PART 6  SPECIAL DETAILED INSPECTION OF FRAME 73A AND FRAME CN  75A, AT DOOR FRAME AREA. 1996-135-199 FAA AD 98-06 ACCESS: 162AZ ISB 53-0303  534901-0603-1 310 ATT.FITTINGS AT FR.86 - 87 MEC DET I: 11200 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF ATTACH FITTINGS 12700 FH  FOR HORIZONTAL STABILIZER TRIM ACTUATOR AND RIVETING ALI REFERENC AREA BETWEEN FRAMES 86 AND 87. 534901-01-1  ACCESS: 312AR  534901-0603-2 310 ATT. FITTING AT FR 86 FR 87 MEC DET I: 10700 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF ATTACH FITTINGS FOR 14800 FH  HORIZONTAL STABILIZER TRIM ACTUATOR AND RIVETING AREA ALI REFERENC BETWEEN FRAME 86 AND 87. 534901-01-2  ACCESS: 312AR  534901-0603-3 310 ATT. FITTING AT FR 86 FR 87 MEC DET I: 10100 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF ATTACH FITTINGS FOR 23400 FH  HORIZONTAL STABILIZER TRIM ACTUATOR AND RIVETING AREA ALI REFERENC BETWEEN FRAMES 86 AND 87. 534901-01-3  ACCESS: 312AR  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536101-0606-1 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI ST: 33000 FC ALI NTM 531102  212 SI: 8600 FC PART 6  SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071 BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13 AND CLOSING PANEL.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-2 536101-02-1  PREP.: 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 212 SI: 4700 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE BETWEEN FRAME 2 AND 4, WINDSHIELD ALI REFERENC FRAME LOWER SECTION AND CLOSING PANEL. 536101-01-1  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-1  PREP.: 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 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE  BETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENC AND CLOSING PANEL. 536101-01-2  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-1  PREP.: 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 212 SI: 4700 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE  BETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENC AND CLOSING PANEL. 536101-01-3  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-2  PREP.: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 212 SI: 4700 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE  BETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENC AND CLOSING PANEL. 536101-01-4  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-3  PREP.: 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 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE  BETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENC AND CLOSING PANEL. 536101-01-5  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-4  PREP.: 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 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE  BETWEEN FRAME 2 AND 4, WINDSHIELD FRAME LOWER SECTION ALI REFERENC AND CLOSING PANEL. 536101-01-6  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0607-5  PREP.: 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 531102  212 PART 6  SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071 BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536101-0607-1 * * * * * C O N T I N U E * * * * *  AND CLOSING PANEL. ALI REFERENC 536101-02-2  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-3  PREP.: 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 531102  212 SI: 8600 FC PART 6  SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071 BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13 AND CLOSING PANEL.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-4 536101-02-3  PREP.: 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 531102  212 SI: 8600 FC PART 6  SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071 BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13 AND CLOSING PANEL.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-5 536101-02-4  PREP.: 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 531102  212 PART 6  SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071 BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13 AND CLOSING PANEL.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-6 536101-02-5  PREP.: OPEN/CLOSE PANEL 2VU, 6VU AND 13VU.  (8.0 M/H)  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536101-0607-5 211 WINDSHIELD FRAME OF FUSELAGE NDT SDI I: 7000 FC ALI NTM 531102  212 PART 6  SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE, CN 2006-0071 BETWEEN FRAME 2 AND 4,WINDSHIELD FRAME LOWER SECTION FAA AD 96-13 AND CLOSING PANEL.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536101-0606-7 536101-02-6  PREP.: 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 212 SI: 9400 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENC AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-1  JUNCTION, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-2  PREP.: 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 212 SI: 11900 FC FAA AD 96-13 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT ALI REFERENC FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-02-1  JUNCTION, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-1  PREP.: 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 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENC AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-2  JUNCTION, LH/RH.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 536110-0607-1  PREP.: 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 212 SI: 9400 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENC AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-3  JUNCTION, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-2  PREP.: 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 212 SI: 9400 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENC AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-4  JUNCTION, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-3  PREP.: 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 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENC AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-5  JUNCTION, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-4  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION ALI REFERENC AT FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9 536110-01-6  JUNCTION, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0607-5  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  536110-0607-1 211 COCKPIT INTERNAL STRUCTURE NDT SDI I: 11900 FC ALI NTM 531104  212 PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071 STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13 FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9  JUNCTION, LH/RH. ALI REFERENC 536110-02-2  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-3  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  536110-0607-2 211 COCKPIT INTERNAL STRUCTURE NDT SDI ST: 25000 FC ALI NTM 531104  212 SI: 11900 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071 STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13 FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9  JUNCTION, LH/RH. ALI REFERENC 536110-02-3  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-4  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  536110-0607-3 211 COCKPIT INTERNAL STRUCTURE NDT SDI ST: 25000 FC ALI NTM 531104  212 SI: 11900 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071 STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13 FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9  JUNCTION, LH/RH. ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536110-0607-3 * * * * * C O N T I N U E * * * * *  536110-02-4  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-5  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  536110-0607-4 211 COCKPIT INTERNAL STRUCTURE NDT SDI I: 11900 FC ALI NTM 531104  212 PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071 STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13 FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9  JUNCTION, LH/RH. ALI REFERENC 536110-02-5  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-6  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  536110-0607-5 211 COCKPIT INTERNAL STRUCTURE NDT SDI I: 11900 FC ALI NTM 531104  212 PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071 STRUCTURE, LATERAL WINDSHIELD FRAME UPPER SECTION AT FAA AD 96-13 FRONT WINDSHIELD SIDE POST, FRAME 8 AND FRAME 9  JUNCTION, LH/RH. ALI REFERENC 536110-02-6  NOTE : THIS TASK IS AN ALTERNATIVE TO 536110-0606-7  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  536111-0606-1 211 STRUCTURE LATERAL WINDOWS MEC DET T: SEE ISB ALI EASA AD  212 I: SEE ISB FAA AD 2006-0071  DETAILED INSPECTION OF UPPER FRAME SECTION OF ISB FAA AD  LATERAL WINDOW FWD TO FR7 SPLICE JUNCTION. 2007-04-11  ISB 53-0348  PREP.: REMOVE/INSTALL LININGS AND INSULATION.  ALI REFERENC 536111-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  232 I: SEE ISB CN 2006-0071  DETAILED INSPECTION OF STRINGER 12, BETWEEN ISB FAA AD  FRAME 17 AND FRAME 19, LH AND RH SIDE. 2007-04-11  ISB 53-0359  PREP.: LININGS AND INSULATION REMOVED.  ALI REFERENC 536112-01-1  536112-0606-2 231 FUSELAGE FRAME 17 AND 19 MEC DET T: 29000 FC ALI EASA AD  232 I: 24900 FC CN 2006-0071  DETAILED INSPECTION OF STRINGER 12, BETWEEN ISB FAA AD  FRAME 17 AND FRAME 19, LH AND RH SIDE. 2007-04-11  ISB 53-0359  PREP.: LININGS AND INSULATION REMOVED.  ALI REFERENC 536112-01-1  536113-0606-1 210 AFT FACE OF FORWARD PRESSURE BULKHEAD MEC DET T: 45000 FC ALI EASA AD  I: 9200 FC 2006-0071  DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE FAA AD  BULKHEAD, ABOVE FLOOR LEVEL INCLUDING FR1, STRINGERS, 2007-04-11  CONNECTION, SKIN AND VERTICAL BEAM.  ALI REFERENC ACCESS: 121BL 536112-01-1  536114-0606-1 211 FIXATION BOLT AT FRAME 2, LOWER SURFACE MEC DET T: 40000 FC ALI EASA AD  212 I: 40000 FC 2006-0071  DETAILED INSPECTION OF FIXATION BOLT AT FRAME 2, FAA AD  LOWER SURFACE OF CLOSING PANEL AND LOWER POST OF 2007-04-11  FRONT WINDSHIELD.  ALI REFERENC PREP.: 3 VU,4 VU, 5 VU TO BE DISPLACED , FRONT 536114-01-1  WINDSHIELD TO BE REMOVED R 536114-0606-2 211 FIXATION BOLT AT FRAME 2, LOWER SURFACE MEC DET T: 40000 FC ALI EASA AD  212 I: 40000 FC 2006-0071  DETAILED INSPECTION OF FIXATION BOLT AT FRAME 2, FAA AD  LOWER SURFACE OF CLOSING PANEL AND LOWER POST OF 2007-04-11  FRONT WINDSHIELD.  ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 536114-01-2  WINDSHIELD TO BE REMOVED  536202-0606-1 221 FUSELAGE FRAME 14 AND 16A MEC DET T: 21000 FC ALI EASA AD  222 I: 1200 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF 2007-04-11  CROSS BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-8 536202-01-1  PREP.: 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 AD  222 SI: 1600 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF 2007-04-11  CROSS BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-9 536202-01-5  PREP.: 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 AD  222 SI: 9300 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536203-0606-1 536202-01-9  PREP.: 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 AD  222 SI: 1300 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  BEAMS 1 AND 8, LH/RH. 2007-04-11  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-2 ALI REFERENC 536202-01-2  PREP.: 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 AD  222 SI: 2000 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-3 536202-01-6  PREP.: 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 AD  222 SI: 4000 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-4 536202-01-11  PREP.: 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 AD  222 SI: 1700 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536203-0606-5 536202-01-3  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (2.0 M/H).  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531201  222 SI: 6000 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-1  ALI REFERENC 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 531201  222 SI: 9100 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME T: 29000 FC EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS I: 9100 FC 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-2  ALI REFERENC 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-2 536202-01-4  PREP.: 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 AD  222 SI: 5000 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE 1: THIS TASK IS AN ALTERNATIVE TO 536202-0608-3 536202-01-7  NOTE 2: GENERAL ALLOWANCE NOT APPLICABLE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-4 536202-01-8  PREP.: 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-5 536202-01-10  PREP.: 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-6 536202-01-12  PREP.: 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 AD  222 I: 4000 FC 2006-0071  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-7 536202-01-13  PREP.: 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-8 536202-01-14  PREP.: 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-9 536202-01-15  PREP.: 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0609-1 536202-01-16  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2007-04-11  BEAMS 1 AND 8, LH/RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0609-2 536202-01-17  PREP.: 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 531201  222 PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-1  ALI REFERENC 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 531201  222 SI: 8300 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE 1: THIS TASK IS AN ALTERNATIVE TO 536202-0607-2  ALI REFERENC NOTE 2: GENERAL ALLOWANCE NOT APPLICABLE 536202-02-7  PREP.: 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 531201  222 PART 6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-3  ALI REFERENC 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 531201  222 PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-4  ALI REFERENC 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 531201  222 PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-5  ALI REFERENC 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 531201  222 I: 13800 FC PART 6  SPECIAL DETAILED INSPECTION (ROT)OF FUSELAGE FRAME 14 EASA AD  AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-6  ALI REFERENC 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531201  222 PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-7  ALI REFERENC 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 531201  222 PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-8  ALI REFERENC 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 531201  222 PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0607-9  ALI REFERENC 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 531201  222 PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0608-1  ALI REFERENC 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 531201  222 SI: 13800 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME T: 36000 FC EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS I: 13800 FC 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-3  ALI REFERENC 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 531201  222 SI: 6200 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-4  ALI REFERENC 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 531201  222 SI: 10200 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-5  ALI REFERENC PREP.: REMOVE/INSTALL LININGS, INSULATION AND BOLTS 536202-02-6  (2.0 M/H).  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531201  222 SI: 13800 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536202-0606-6  ALI REFERENC 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 531202  222 SI: 6700 FC PART 6  SPECIAL DETAILED INSPECTION (ROT) OF FUSELAGE FRAME EASA AD  14 AND 16A, FORWARD AND REAR FACES, IN AREAS OF CROSS 2006-0071  BEAMS 1 AND 8, LH/RH. FAA AD  2007-04-11  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536202-0606-7  ALI REFERENC 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 AD  222 I: 2600 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AT FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-01-1  536204-0606-2 221 FUSELAGE FRAME 14 MEC DET T: 38000 FC ALI EASA AD  222 I: 10000 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 FAA AD  AT FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-01-5  536204-0606-3 221 FUSELAGE FRAME 14 MEC DET T: 30000 FC ALI CN 2006-0071 222 I: 3200 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE FRAME 14 AT  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 536204-01-2  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (1.6 M/H).  536204-0606-4 221 FUSELAGE FRAME 14 MEC DET T: 38000 FC ALI EASA AD  222 I: 8500 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-01-6  536204-0606-5 221 FUSELAGE FRAME 14 MEC DET T: 30000 FC ALI EASA AD  222 I: 4000 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  NOTE: THIS TASK IS AN ALTERNATIVE TO 536214-0606-1 ALI REFERENC 536204-01-3  PREP.: REMOVE/INSTALL LININGS AND INSULATION,  (1.6 M/H).  536204-0606-6 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 531205  222 I: 4700 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11  (1.6 M/H).  ALI REFERENC 536204-02-1  536204-0606-7 221 FUSELAGE FRAME 14 NDT SDI T: 38000 FC ALI NTM 531205  222 I: 10600 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  PREP.: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 536204-02-5  536204-0606-8 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 531205  222 I: 5900 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11  (1.6 M/H).  ALI REFERENC 536204-02-2  536204-0606-9 221 FUSELAGE FRAME 14 NDT SDI T: 38000 FC ALI NTM 531205  222 I: 10000 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11  (1.6 M/H).  ALI REFERENC 536204-02-6  536204-0607-2 221 FUSELAGE FRAME 14 MEC DET T: 38000 FC ALI EASA AD  222 I: 8500 FC 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-01-7  536204-0607-4 221 FUSELAGE FRAME 14 MEC DET I: 8500 FC ALI EASA AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-01-9  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536204-0607-5 221 FUSELAGE FRAME 14 MEC DET I: 2600 FC ALI EASA AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-01-10  536204-0607-6 221 FUSELAGE FRAME 14 MEC DET I: 2600 FC ALI EASA AD  222 2006-0071  DETAILED INSPECTION OF FUSELAGE FRAME 14 AT FAA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-01-11  536204-0607-7 221 FUSELAGE FRAME 14 NDT SDI I: 4000 FC ALI NTM 531205  222 PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11  (1.6 M/H).  ALI REFERENC 536204-02-4  536204-0607-8 221 FUSELAGE FRAME 14 NDT SDI T: 38000 FC ALI NTM 531205  222 I: 10600 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536204-0607-2 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-02-7  536204-0607-9 221 FUSELAGE FRAME 14 NDT SDI I: 10600 FC ALI NTM 531205  222 PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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). 2007-04-11  ALI REFERENC 536204-02-8  536204-0608-2 221 FUSELAGE FRAME 14 MEC DET I: 4000 FC ALI NTM 531205  222 PART 4  NDT INSPECTION OF FUSELAGE FRAME 14 AT FLOOR BEAM EASA AD  ATTACHMENT, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11  (1.6 M/H).  ALI REFERENC 536204-02-10  536204-0608-4 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 531205  222 I: 4000 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL LININGS AND INSULATION, 2007-04-11  (1.6 M/H).  ALI REFERENC 536204-02-3  536205-0606-1 211 FUSELAGE FRAME 10 MEC DET ST: 24000 FC ALI CN 2006-0071 212 SI: 3100 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE FRAME 10 INNER  FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENC LEVEL, LH/RH. 536205-01-1  NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-6  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536205-0606-1 * * * * * C O N T I N U E * * * * *  ACCESS: 221DF  222DF  536205-0606-2 211 FUSELAGE FRAME 10 MEC DET ST: 20000 FC ALI CN 2006-0071 212 SI: 2800 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE FRAME 10 INNER  FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENC LEVEL, LH/RH. 536205-01-2  NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-7  PREP.: 15 VU TO BE OPENED (REMOVAL NOT NECESSARY)  LINING AND INSULATION.  (EXTENDED AREA FOR AIRPLANE POST 726).  ACCESS: 221DF  222DF  536205-0606-3 211 FUSELAGE FRAME 10 MEC DET I: 2800 FC ALI CN 2006-0071 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE FRAME 10 INNER  FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENC LEVEL, LH/RH. 536205-01-3  NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-8  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  ACCESS: 221DF  222DF  536205-0606-4 211 FUSELAGE FRAME 10 MEC DET ST: 20000 FC ALI CN 2006-0071 212 SI: 3100 FC FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR 536205-01-4  LEVEL, LH/RH.  NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-9  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  ACCESS: 221DF  222DF  536205-0606-5 211 FUSELAGE FRAME 10 MEC DET I: 3400 FC ALI CN 2006-0071 212 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE FRAME 10 INNER  FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FLOOR ALI REFERENC LEVEL, LH/RH. 536205-01-5  NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0607-1  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  ACCESS: 221DF  222DF  536205-0606-6 211 FUSELAGE FRAME 10 NDT SDI ST: 24000 FC ALI NTM 531101  212 SI: 10000 FC PART 6 PROC  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071 INNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13 FLOOR LEVEL, LH/RH.  ALI REFERENC NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-1  LOWER END OF REINFORCEMENT  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 536205-0606-1  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  ACCESS: 221DF 222DF  536205-0606-7 211 FUSELAGE FRAME 10 NDT SDI ST: 20000 FC ALI NTM 531101  212 SI: 8700 FC PART 6 PROC  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071 INNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13 FLOOR LEVEL, LH/RH.  ALI REFERENC NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-2  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-2  PREP.: 15 VU TO BE OPENED (REMOVAL NOT NECESSARY)  LINING AND INSULATION.  (EXTENDED AREA FOR AIRPLANE POST 726).  ACCESS: 221DF  222DF  536205-0606-8 211 FUSELAGE FRAME 10 NDT SDI I: 8700 FC ALI NTM 531101  212 PART 6 PROC  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071 INNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13 FLOOR LEVEL, LH/RH.  ALI REFERENC NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-3  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-3  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  ACCESS: 221DF 222DF  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536205-0606-9 211 FUSELAGE FRAME 10 NDT SDI ST: 20000 FC ALI NTM 531101  212 SI: 6800 FC PART 6 PROC  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071 INNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13 FLOOR LEVEL, LH/RH.  ALI REFERENC NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-4  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-4  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  ACCESS: 221DF  222DF  536205-0607-1 211 FUSELAGE FRAME 10 NDT SDI I: 9000 FC ALI NTM 531101  212 PART 6 PROC  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 10 CN 2006-0071 INNER FLANGE FROM SIDE WINDOW LOWER SECTION TO CABIN FAA AD 96-13 FLOOR LEVEL, LH/RH.  ALI REFERENC NOTE 01: FOR A/C POST MOD 00726 AREA EXTENDED TO 536205-02-5  LOWER END OF REINFORCEMENT  NOTE 02: THIS TASK IS AN ALTERNATIVE TO 536205-0606-5  PREP.: OPEN/CLOSE 15VU, REMOVE/INSTALL LININGS  AND INSULATION, (10.0 M/H).  ACCESS: 221DF  222DF  536207-0606-1 123 FUSELAGE FRAME 17 NDT SDI ST: 30000 FC ALI NTM 531203  124 SI: 4200 FC CN 2006-0071 SPECIAL DETAILED INSPECTION (X-RAY) OF NLG BAY, T: 30000 FC FAA AD 96-13 FUSELAGE INTERNAL SKIN, DOUBLERS AND CORNER FLANGE AT I: 4200 FC  FR17, LH/RH. ALI REFERENC 536207-01-1  NOTE: GRACE PERIOD = 2400 FC  PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536207-0606-2 123 FUSELAGE FRAME 17 NDT SDI ST: 31000 FC ALI NTM 531203  124 SI: 4800 FC CN 2006-0071 SPECIAL DETAILED INSPECTION (X-RAY) OF NLG BAY, T: 31000 FC FAA AD 96-13 FUSELAGE INTERNAL SKIN, DOUBLERS AND CORNER FLANGE AT I: 4800 FC  FR17, LH/RH. ALI REFERENC 536207-01-2  NOTE: GRACE PERIOD = 2400 FC  PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.  536207-0606-3 123 FUSELAGE FRAME 17 NDT SDI ST: 31000 FC ALI NTM 531203  124 SI: 6700 FC PART 2  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 31000 FC CN 2006-0071 DOUBLER AND LOWER FLANGE OF FRAME 17, FORWARD PART I: 6700 FC FAA AD 96-13 FROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOM  CENTER LINE LH/RH. ALI REFERENC 536207-01-3  PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.  536207-0606-4 123 FUSELAGE FRAME 17 NDT SDI ST: 31000 FC ALI NTM 531203  124 SI: 3000 FC PART 2  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 31000 FC CN 2006-0071 DOUBLER AND LOWER FLANGE OF FRAME 17, FORWARD PART I: 3000 FC FAA AD 96-13 FROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOM  CENTER LINE LH/RH. ALI REFERENC 536207-01-4  PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.  536207-0606-5 123 FUSELAGE FRAME 17 NDT SDI I: 3000 FC ALI NTM 531203  124 PART 2  SPECIAL DETAILED INSPECTION (X-RAY) OF NLG BAY, CN 2006-0071 FUSELAGE INTERNAL SKIN, DOUBLERS AND CORNER FLANGE AT FAA AD 96-13 FR17, LH/RH.  ALI REFERENC NOTE: GRACE PERIOD = 2400 FC (FOR B2 ONLY) 536207-01-5  PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.  536207-0606-6 123 FUSELAGE FRAME 17 NDT SDI I: 3000 FC ALI NTM 531203  124 PART 2  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOM  CENTER LINE LH/RH. ALI REFERENC 536207-01-6  PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.  536207-0606-7 123 FUSELAGE FRAME 17 NDT SDI I: 3000 FC ALI NTM 531203  124 PART 2  SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL CN 2006-0071 DOUBLER AND LOWER FLANGE OF FRAME 17, FORWARD PART FAA AD 96-13 FROM NOSE LANDING GEAR BAY AFT CORNER TO A/C BOTTOM  CENTER LINE LH/RH. ALI REFERENC 536207-01-7  PREP.: NOSE LANDING GEAR DOORS TO BE OPENED.  536208-0605-1 211 FUSELAGE SKIN FRAME 10 MEC DET T: 18300 FC ISB NTM 513010  212 I: 3600 FC PART 1  DETAILED INSPECTION OF REAR LOWER CORNER OF NTM 531202  THE FLIGHT COMPARTMENT AFT WINDOW AND ADJACENT PART 2  FUSELAGE SKIN. AD 2000-10-0 CN  NOTE: EFFECTIVITY IS POST PARTIAL MOD 00793 90-222-116(B EMBOBIMENT, AS DEFINED PER ISB 53-278. ISB 53-0278  536208-0605-2 211 FUSELAGE SKIN FRAME 10 MEC DET T: 22000 FC ISB NTM 513010  212 I: 3600 FC PART 1  DETAILED INSPECTION OF REAR LOWER CORNER OF NTM 531202  THE FLIGHT COMPARTMENT AFT WINDOW AND ADJACENT PART 2  FUSELAGE SKIN. AD 2000-10-0 CN  90-222-116(B ISB 53-0278  536208-0605-3 211 FUSELAGE SKIN FRAME 10 MEC DET T: 26000 FC ISB NTM 513010  212 I: 5000 FC PART 1  DETAILED INSPECTION OF REAR LOWER CORNER OF NTM 531202  THE FLIGHT COMPARTMENT AFT WINDOW AND ADJACENT PART 2  FUSELAGE SKIN. AD 2000-10-0 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536208-0605-3 * * * * * C O N T I N U E * * * * *  CN  90-222-116(B ISB 53-0278  536210-0606-1 223 FR 13 BETWEEN STR 1 AND 2, LH/RH MEC DET ST: 32000 FC ALI CN 2006-0071 224 SI: 10000 FC FAA AD 96-13 DETAILED INSPECTION OF FRAME 13 BETWEEN T: 32000 FC  STRINGER 1 AND 2, LH/RH I: 10000 FC ALI REFERENC 536210-01-1  PREP.: 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 224 FAA AD 96-13 DETAILED INSPECTION OF FRAME 13 BETWEEN  STRINGER 1 AND 2, LH/RH ALI REFERENC 536210-01-2  PREP.: 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 224 SI: 10000 FC FAA AD 96-13 DETAILED INSPECTION OF FRAME 13 BETWEEN T: 32000 FC  STRINGER 1 AND 2, LH/RH I: 10000 FC ALI REFERENC 536210-01-3  PREP.: 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 224 SI: 10000 FC FAA AD 96-13 DETAILED INSPECTION OF FRAME 13 BETWEEN T: 32000 FC  STRINGER 1 AND 2, LH/RH I: 10000 FC ALI REFERENC 536210-01-4  PREP.: 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 224 FAA AD 96-13 DETAILED INSPECTION OF FRAME 13 BETWEEN  STRINGER 1 AND 2, LH/RH ALI REFERENC 536210-01-5  PREP.: CEILING PANELS AND INSULATION TO BE REMOVED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 224 FAA AD 96-13 DETAILED INSPECTION OF FRAME 13 BETWEEN  STRINGER 1 AND 2, LH/RH ALI REFERENC 536210-01-6  PREP.: CEILING PANELS AND INSULATION TO BE REMOVED.  536214-0606-1 221 FUSELAGE FRAME 14 NDT SDI T: 30000 FC ALI NTM 531205  222 I: 4000 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE FRAME 14 AT EASA AD  FLOOR BEAM ATTACHMENT, LH/RH. 2006-0071  FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536204-0606-5 2007-04-11  PREP.: REMOVE/INSTALL LININGS AND INSULATION, ALI REFERENC (1.6 M/H). 536204-02-3  536215-0603-1 121 FUSELAGE NOSE SECTION MEC DET T: 6600 FC ISB ISB 53-0388  122 I: SEE ISB  DETAILED INSPECTION OF THE CROSSBEAM ON NLG FR 15A  WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FITTING.  ACCESS: 121BL  536225-0606-1 223 FUSELAGE SKIN AT FRAME 13 NDT SDI ST: 32000 FC ALI NTM 531204  224 SI: 14000 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.B.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-X  ALI REFERENC PREP.:INSULATION AND BOLTS. 536225-01-1  536225-0606-2 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 531204  224 I: 8300 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.B.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  TASK 536225-0606-X 2007-04-11  PREP.:INSULATION AND BOLTS. ALI REFERENC 536225-01-2  536225-0606-3 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 531204  224 I: 14000 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.B.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-X  ALI REFERENC PREP.:INSULATION AND BOLTS. 536225-01-3  536225-0606-4 223 FUSELAGE SKIN AT FRAME 13 NDT SDI ST: 32000 FC ALI NTM 531204  224 SI: 7100 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-1  ALI REFERENC PREP.:INSULATION 536225-02-1  536225-0606-5 223 FUSELAGE SKIN AT FRAME 13 NDT SDI ST: 32000 FC ALI NTM 531204  224 SI: 8000 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-1  ALI REFERENC PREP.:INSULATION. 536225-02-2  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531204  224 SI: 5600 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-1  ALI REFERENC PREP.:INSULATION. 536225-02-3  536225-0606-7 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 531204  224 I: 3300 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-2  ALI REFERENC PREP.:INSULATION. 536225-02-4  536225-0606-8 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 531204  224 I: 6200 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-3  ALI REFERENC PREP.:INSULATION. 536225-02-5  536225-0606-9 223 FUSELAGE SKIN AT FRAME 13 NDT SDI T: 40000 FC ALI NTM 531204  224 I: 5600 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT FRAME (PROC.A.)  13 CIRCUMFERENTIAL JOINT, FROM STRINGER 9 TO STRINGER EASA AD  25 LH/RH. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 536225-0606-3  ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536225-0606-9 * * * * * C O N T I N U E * * * * *  PREP.:INSULATION. 536225-02-8  536230-0606-1 221 INTERNAL STRUCTURE AT CABIN FLOOR NDT SDI T: 22000 FC ALI NTM 536230  222 I: 3300 FC PART 4  SPECIAL DETAILED INSPECTION OF FUSELAGE AT FRAME 16A EASA AD  INTERNAL STRUCTURE AT CABIN FLOOR LEVEL, IN AREA OF 2006-0071  PASSENGER/CREW DOOR LOWER KEEL JUNCTION, LH/RH FAA AD  2007-04-11  ALI REFERENC 536230-01-1  536231-0606-1 221 INTERNAL STRUCTURE NDT SDI T: 18500 FC ALI NTM 536231  222 I: 13000 FC PART 6  SPECIAL DETAILED INSPECTION OF FUSELAGE AT FRAME 16A EASA AD  JOINT BETWEEN STRINGER 28 AND STRINGER 30, LH/RH 2006-0071  FAA AD  PREP: REMOVE LINING AND INSULATION 2007-04-11  ALI REFERENC 536231-01-1  536231-02-1  536232-0606-1 121 INTERNAL STRUCTURE MEC DET T: 45000 FC ALI EASA AD  122 I: 40000 FC 2006-0071  DETAILED INSPECTION OF FRAME 19 WEB AT LEVEL OF FAA AD  STR 43LH AND RH. 2007-04-11  ACCESS: 121BL ALI REFERENC 536232-01-1  536233-0606-1 211 INTERNAL STRUCTURE MEC SDI T: 48000 FC ALI NTM 536233  212 I: 24000 FC EASA AD PART 6  221 SPECIAL DETAILED INSPECTION OF ROD UNDER PASSENGERS FAA AD EASA AD  222 FLOOR AT FR 10LH AND RH. 2006-0071  FAA AD  PREP.: LINING AND INSULATION, 15VU, 50VU LH TOILET 2007-04-11  TO BE REMOVED.  ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536233-0606-1 * * * * * C O N T I N U E * * * * *  536233-01-1  536234-0606-1 123 INTERNAL STRUCTURE MEC DET T: 45000 FC ALI EASA AD  124 I: 3800 FC 2006-0071  DETAILED INSPECTION OF NLG BAY ROOF PANEL BETWEEN FAA AD  FR 15 AND FR 17. 2007-04-11  ACCESS: 713 ALI REFERENC 714 536234-01-1  536234-0606-2 123 INTERNAL STRUCTURE MEC DET T: 45000 FC ALI EASA AD  124 I: 6000 FC 2006-0071  DETAILED INSPECTION OF NLG BAY ROOF PANEL BETWEEN FAA AD  FR 15 AND FR 17. 2007-04-11  ACCESS: 713 ALI REFERENC 714 536234-01-2  536235-0606-1 121 NOSE GEAR BAY ARCHES UPPER AND LOWER MEC DET T: 48000 FC ALI EASA AD  122 CORNERS I: 8500 FC 2006-0071  FAA AD  DETAILED INSPECTION OF NOSE GEAR BAY ARCHES UPPER AND 2007-04-11  LOWER CORNERS,BETWEEN FR 11A AND FR 16A INCLUDED,  INCLUDING STRUTS ATTACHMENT LUGS, FRAMES ATTACHMENTS ALI REFERENC AT STG 44LH AND RH. 536235-01-1  ACCESS: 121KF 121MF 121NF 121PF 121QF  122EF 122GF 122HF 122JF 122KF  536235-0606-2 121 NOSE GEAR BAY ARCHES UPPER AND LOWER MEC DET T: 40000 FC ALI EASA AD  122 CORNERS I: 8500 FC 2006-0071  FAA AD  DETAILED INSPECTION OF NOSE GEAR BAY ARCHES UPPER AND 2007-04-11  LOWER CORNERS,BETWEEN FR 11A AND FR 16A INCLUDED,  INCLUDING STRUTS ATTACHMENT LUGS, FRAMES ATTACHMENTS ALI REFERENC AT STG 44LH AND RH. 536235-01-2  ACCESS: 121KF 121MF 121NF 121PF 121QF  122EF 122GF 122HF 122JF 122KF  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  122 CORNERS I: 8500 FC 2006-0071  FAA AD  DETAILED INSPECTION OF NOSE GEAR BAY ARCHES UPPER AND 2007-04-11  LOWER CORNERS,BETWEEN FR 11A AND FR 16A INCLUDED,  INCLUDING STRUTS ATTACHMENT LUGS, FRAMES ATTACHMENTS ALI REFERENC AT STG 44LH AND RH. 536235-01-3  ACCESS: 121KF 121MF 121NF 121PF 121QF  122EF 122GF 122HF 122JF 122KF  536301-0606-1 100 LONGITUDINAL LAP JOINTS MEC GVI T: 33000 FC ALI EASA AD  200 I: 3900 FC CN 2006-0071  GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0607-1 AND 536301-0608-1 536301-02-1  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0606-2 100 LONGITUDINAL LAP JOINTS MEC GVI T: 33000 FC ALI EASA AD  200 I: 6400 FC CN 2006-0071  GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0607-2 AND 536301-0608-2 536301-01-2  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0606-3 100 LONGITUDINAL LAP JOINTS MEC GVI T: 33000 FC ALI EASA AD  200 I: 2000 FC CN 2006-0071  GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 536301-0607-3 AND 536301-0608-3 536301-01-3  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0606-4 100 LONGITUDINAL LAP JOINTS MEC GVI I: 2000 FC ALI EASA AD  200 CN 2006-0071  GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0607-4 AND 536301-0608-4 536301-01-4  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0606-5 100 LONGITUDINAL LAP JOINTS MEC GVI I: 2000 FC ALI EASA AD  200 CN 2006-0071  GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0607-5 AND 536301-0608-5 536301-01-5  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0606-6 100 LONGITUDINAL LAP JOINTS MEC GVI I: 2000 FC ALI EASA AD  200 CN 2006-0071  GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. 2007-04-11  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 536301-01-6  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39  ACCESS: 513AB 613AB  536301-0607-1 100 LONGITUDINAL LAP JOINTS MEC DET T: 33000 FC ALI CN 2006-0071 200 I: 4700 FC CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENC 536301-02-1  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS  536301-0606-1 AND 536301-0608-1  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0607-2 100 LONGITUDINAL LAP JOINTS MEC DET T: 33000 FC ALI CN 2006-0071 200 I: 7000 FC CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENC 536301-02-2  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS  536301-0606-2 AND 536301-0608-2  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0607-3 100 LONGITUDINAL LAP JOINTS MEC DET T: 33000 FC ALI CN 2006-0071 200 I: 2900 FC CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENC 536301-02-3  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS  536301-0606-3 AND 536301-0608-3  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39  ACCESS: 513AB 613AB  536301-0607-4 100 LONGITUDINAL LAP JOINTS MEC DET I: 2900 FC ALI CN 2006-0071 200 CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENC 536301-02-4  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS  536301-0606-4 AND 536301-0608-4  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0607-5 100 LONGITUDINAL LAP JOINTS MEC DET I: 2900 FC ALI CN 2006-0071 200 CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENC 536301-02-5  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS  536301-0606-5 AND 536301-0608-5  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0607-6 100 LONGITUDINAL LAP JOINTS MEC DET I: 2900 FC ALI CN 2006-0071 200 CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. ALI REFERENC 536301-02-6  NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS  536301-0606-6 AND 536301-0608-6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39  ACCESS: 513AB 613AB  536301-0608-1 100 LONGITUDINAL LAP JOINTS MEC SDI T: 33000 FC ALI NTM 533002  200 I: 12900 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13 NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0606-1 AND 536301-0607-1 536301-03-1  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0608-2 100 LONGITUDINAL LAP JOINTS MEC SDI T: 33000 FC ALI NTM 533002  200 I: 8900 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13 NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0606-2 AND 536301-0607-2 536301-03-2  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0608-3 100 LONGITUDINAL LAP JOINTS MEC SDI T: 33000 FC ALI NTM 533002  200 I: 8900 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13 NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0606-3 AND 536301-0607-3 536301-03-3  NOTE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 39  ACCESS: 513AB 613AB  536301-0608-4 100 LONGITUDINAL LAP JOINTS MEC SDI I: 8900 FC ALI NTM 533002  200 CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13 NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0606-4 AND 536301-0607-4 536301-03-4  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0608-5 100 LONGITUDINAL LAP JOINTS MEC SDI I: 8900 FC ALI NTM 533002  200 CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13 NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0606-5 AND 536301-0607-5 536301-03-5  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; LH/RH BETWEEN FRAMES 38.1 AND 39:  ACCESS: 513AB 613AB  536301-0608-6 100 LONGITUDINAL LAP JOINTS MEC SDI I: 8900 FC ALI NTM 533002  200 CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 18 AND 40. FAA AD 96-13 NOTE 01:THIS TASK IS AN ALTERNATIVE TO THE TASKS ALI REFERENC 536301-0606-6 AND 536301-0607-6 536301-03-6  NOTE 02:N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31; 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536301-0608-6 * * * * * C O N T I N U E * * * * *  ACCESS: 513AB 613AB  536311-0606-1 134 FWD CARGO DOOR LOCK FITTING MEC DET T: 32000 FC ALI CN 2006-0071 I: 4200 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA OF LOCK  FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR POST ALI REFERENC 02295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL AND 536311-01-1  STRINGER 45 RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-4  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  (0,6 M/H)  ACCESS: 132BF 132CF 811  536311-0606-2 134 FWD CARGO DOOR LOCK FITTING MEC DET T: 32000 FC ALI CN 2006-0071 I: 5600 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA OF LOCK  FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR POST ALI REFERENC 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL AND 536311-01-2  STRINGER 45 RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-5  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  (0,6 M/H)  ACCESS: 132BF 132CF 811  536311-0606-3 134 FWD CARGO DOOR LOCK FITTING MEC DET T: 32000 FC ALI CN 2006-0071 I: 3500 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA OF LOCK  FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR POST ALI REFERENC 02295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL AND 536311-01-3  STRINGER 45 RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-6  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  536311-0606-4 134 FWD CARGO DOOR LOCK FITTING NDT SDI T: 32000 FC ALI NTM 531300  I: 8400 FC PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13 POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL  AND STRINGER 45 RH. ALI REFERENC 536311-02-1  NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-1  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  (0,6 M/H)  ACCESS: 132BF 132CF 811  536311-0606-5 134 FWD CARGO DOOR LOCK FITTING NDT SDI T: 32000 FC ALI NTM 531300  I: 8000 FC PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13 POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL  AND STRINGER 45 RH. ALI REFERENC 536311-02-2  NOTE : THIS TASK IS AN ALTERNATIVE TO 536311-0606-2  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  (0,6 M/H)  ACCESS: 132BF 132CF 811  536311-0606-6 134 FWD CARGO DOOR LOCK FITTING NDT SDI T: 32000 FC ALI NTM 531300  I: 7500 FC PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13 POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL  AND STRINGER 45 RH. ALI REFERENC 536311-02-3  NOTE : 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  536311-0606-7 134 FWD CARGO DOOR LOCK FITTING NDT SDI I: 4800 FC ALI NTM 531300  PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13 POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL  AND STRINGER 45 RH. ALI REFERENC 536311-02-4  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  (0,6 M/H)  ACCESS: 132BF 132CF 811  536311-0606-8 134 FWD CARGO DOOR LOCK FITTING NDT SDI I: 4800 FC ALI NTM 531300  PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13 POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL  AND STRINGER 45 RH. ALI REFERENC 536311-02-5  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  (0,6 M/H)  ACCESS: 132BF 132CF 811  536311-0606-9 134 FWD CARGO DOOR LOCK FITTING NDT SDI I: 4800 FC ALI NTM 531300  PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 LOCK FITTINGS FROM FRAME 20B TO 24A (20B TO 25 FOR FAA AD 96-13 POST 2295, DOOR EXTENSION) BETWEEN CARGO DOOR SILL  AND STRINGER 45 RH. ALI REFERENC 536311-02-6  PREP.: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536311-0606-9 * * * * * C O N T I N U E * * * * *  ACCESS: 132BF 132CF 811  536355-0606-1 233 UDC CARGO DOOR HINGE FTG NDT SDI T: 12000 FC ALI NTM 533300  NOTE 01 PART 6  01. DETAILED (INTERNAL AND EXTERNAL) I: 11200 FC CN 2006-0071 INSPECTION OF HINGE FITTINGS FOR UPPER (MAIN) FAA AD 96-13 DECK CARGO DOOR, FROM FUSELAGE FRAME 20 TO 27,  INCLUDING SURROUNDING SKIN BETWEEN STR 4 AND 5 LH ALI REFERENC 536355-01-1  02. SPECIAL DETAILED INSPECTION OF UPPER BOLT ROW OF 536355-02-1  HINGE FITTINGS FOR UDC DOOR  NOTE: ON A/C RETROFITTED TO C4 SERIES THE VALUE  FOR INSPECTION THRESHOLD APPLIES FROM THE  TIME OF THE RETROFIT.  PREP.: REMOVE/INSTALL LININGS AND INSULATION.  REMOVE FASTENER (UPPER ROW) FROM UPPER HINGE  FITTING.  (6.0 M/H)  ACCESS: 835  536355-0606-2 233 UDC CARGO DOOR HINGE FTG NDT SDI T: 12000 FC ALI NTM 533300  NOTE 02. PART 6  01. DETAILED INTERNAL AND EXTERNAL I: 11200 FC CN 2006-0071 INSPECTION OF HINGE FITTINGS FOR UPPER (MAIN) FAA AD 96-13 DECK CARGO DOOR, FROM FUSELAGE FRAME 20 TO 27,  INCLUDING SURROUNDING SKIN BETWEEN STR 4 AND 5 LH ALI REFERENC 536355-01-1  02. SPECIAL DETAILED INSPECTION OF UPPER BOLT ROW OF 536355-02-1  HINGE FITTINGS FOR UDC DOOR  NOTE: ON A/C RETROFITTED TO C4 SERIES THE QUOTED  VALUE FOR INSPECTION THRESHOLD APPLIES  FROM THE TIME OF THE RETROFIT.  PREP.: REMOVE/INSTALL FUSELAGE CEILING,  LININGS, HATRACK AND INSULATION.  REMOVE/INSTALL FASTENER (UPPER ROW) FROM  UPPER HINGE FITTING.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 I: 11200 FC FAA AD 96-13 DETAILED INSPECTION OF UPPER (MAIN) DECK CARGO  DOOR LOCK FITTING LUGS AND ECCENTRIC BOLTS AT ALI REFERENC FUSELAGE FRAMES 20B TO 26A (8 PLACES), LH. 536359-01-1  PREP.: LINING REMOVED, ECCENTRIC BOLTS TO BE REMOVED.  (4.0 M/H)  ACCESS: 835  536359-0606-2 231 UDC DOOR LOCK FITTING MEC DET T: 13200 FC ALI CN 2006-0071 I: 11200 FC FAA AD 96-13 DETAILED INSPECTION OF UPPER (MAIN) DECK CARGO  DOOR LOCK FITTING LUGS AND ECCENTRIC BOLTS AT ALI REFERENC FUSELAGE FRAME 20B TO 26A,(8 PLACES), LH. 536359-01-1  PREP.: 01. PASSENGER CONFIGURATION:  REMOVE/INSTALL HATRACKS, FUSELAGE  LINING, CEILING AND INSULATION.  02. ECCENTRIC BOLTS TO BE REMOVED.  (4.0 M/H)  ACCESS: 835  536365-0606-1 121 LONGITUDINAL BUTT JOINTS NDT SDI T: 22000 FC ALI NTM 533001  131 I: 6100 FC PART 6  230 SPECIAL DETAILED INSPECTION OF LONGITUDINAL BUTT CN 2006-0071 232 JOINTS BETWEEN FRAMES 18 AND 33 (IN THE FOLLOWING FAA AD 96-13 233 AREAS:) 01. BUTT JOINT BETWEEN STR 3 AND 4 FROM FRAME  29 TO 33, LH ALI REFERENC 02. BUTT JOINT BETWEEN STR 8 AND 10 FROM FRAME 536365-01-1  18 TO 29, RH  03. BUTT JOINT BETWEEN STR 34 AND 35 FROM FRAME  18 TO 30, LH  NOTE: REMOVE/INSTALL UPPER DECK CARGO COMPARTMENT  SEALING PANELS, FORWARD COMPARTMENT SIDEWALL  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 533001  131 PART 6  230 SPECIAL DETAILED INSPECTION OF LONGITUDINAL BUTT CN 2006-0071 232 JOINTS BETWEEN FRAMES 18 AND 33 (IN THE FOLLOWING FAA AD 96-13 233 AREAS:) 01. BUTT JOINT BETWEEN STR 3 AND 4 FROM FRAME  29 TO 33, LH ALI REFERENC 02. BUTT JOINT BETWEEN STR 8 AND 10 FROM FRAME 536365-01-2  18 TO 29, RH  03. BUTT JOINT BETWEEN STR 34 AND 35 FROM FRAME  18 TO 30, LH  NOTE: REMOVE/INSTALL UPPER DECK CARGO COMPARTMENT  SEALING PANELS, FORWARD COMPARTMENT SIDEWALL  PANELS, INSULATION.  536367-0606-1 121 LONGITUDINAL BUTT JOINT MEC GVI T: 33000 FC ALI CN 2006-0071 131 I: 2400 FC FAA AD 96-13 GENERAL VISUAL INSPECTION OF SKIN AT LONGITUDINAL  BUTT JOINT AREA AT STR 35 FROM FRAME 18 TO 30, LH ALI REFERENC 536367-01-1  NOTE : THIS TASK HAS TO BE DONE AS THE SAME TIME AS  TASK 536367-0606-2  536367-0606-2 121 LONGITUDINAL BUTT JOINT MEC DET T: 33000 FC ALI CN 2006-0071 131 I: 11000 FC FAA AD 96-13 DETAILED INSPECTION OF LONGITUDINAL BUTT  JOINT (AREA) AT STR 35 BETWEEN (FROM) FRAME 18 TO ALI REFERENC 30 LH 536367-02-1  NOTE : THIS TASK HAS TO BE DONE AS THE SAME TIME AS  TASK 536367-0606-1  536369-0606-1 200 UPPER HALF OF FUSELAGE MEC GVI T: 20000 FC ALI CN 2006-0071 I: 5000 FC FAA AD 96-13 GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL  SURFACE - UPPER HALF OF FUSELAGE - SECTION 13 TO 18 ALI REFERENC (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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536369-0606-1 * * * * * C O N T I N U E * * * * *  LINE  536403-0606-1 231 FUSELAGE FRAME 28A AND 30A MEC DET T: 28000 FC ALI CN 2006-0071 232 I: 9300 FC FAA AD 96-13 233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A  234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENC 241 SUPPORT 536403-01-1  242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE  EACH 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 232 I: 10100 FC FAA AD 96-13 233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A  234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENC 241 SUPPORT 536403-01-2  242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE  EACH 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 232 I: 9200 FC FAA AD 96-13 233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A  234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENC 241 SUPPORT 536403-01-3  242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE  EACH 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 232 FAA AD 96-13 233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A  234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536403-0606-4 * * * * * C O N T I N U E * * * * *  241 SUPPORT 536403-01-4  242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE  EACH 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 232 FAA AD 96-13 233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A  234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENC 241 SUPPORT 536403-01-5  242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE  EACH 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 232 FAA AD 96-13 233 DETAILED INSPECTION OF (FUSELAGE) FRAME 28A  234 AND 30A, BETWEEN STRNGERS 9 AND 26 AND DOOR STOP ALI REFERENC 241 SUPPORT 536403-01-6  242 FITTINGS ON FRAMES 28/28A AND 30A/31, (8 PLACES ONE  EACH 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 AD  234 I: 9300 FC FAA AD 2006-0071  243 DETAILED INSPECTION OF PASSENGER DOOR FRAME FAA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-4 ALI REFERENC 536405-01-1  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND  INSULATION. (2.5 M/H)  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536405-0606-2 233 PASSENGER DOOR FRAME MEC DET T: 28000 FC ALI EASA AD  234 I: 10100 FC FAA AD 2006-0071  243 DETAILED INSPECTION OF PASSENGER DOOR FRAME FAA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-5 ALI REFERENC 536405-01-2  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND  INSULATION. (2.5 M/H)  536405-0606-3 233 PASSENGER DOOR FRAME MEC DET I: 10100 FC ALI EASA AD  234 EASA AD 2006-0071  243 DETAILED INSPECTION OF PASSENGER DOOR FRAME FAA AD FAA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-6 ALI REFERENC 536405-01-2  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND  INSULATION.  536405-0606-4 233 PASSENGER DOOR FRAME NDT SDI T: 28000 FC ALI NTM 531413  234 I: 10200 FC FAA AD PART 6  243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-0071  FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-1 2007-04-11  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND ALI REFERENC INSULATION. (2.5 M/H) 536405-02-1  536405-0606-5 233 PASSENGER DOOR FRAME NDT SDI T: 28000 FC ALI NTM 531413  234 I: 11100 FC FAA AD PART 6  243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-0071  FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-2 2007-04-11  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND ALI REFERENC INSULATION. (2.5 M/H) 536405-02-6  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536405-0606-6 233 PASSENGER DOOR FRAME NDT SDI T: 28000 FC ALI NTM 531413  234 I: 11100 FC FAA AD PART 6  243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-0071  FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536405-0606-3 2007-04-11  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND ALI REFERENC INSULATION. (2.5 M/H) 536405-02-2  536405-0606-7 233 PASSENGER DOOR FRAME NDT SDI I: 7000 FC ALI NTM 531413  234 FAA AD PART 6  243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND 2007-04-11  INSULATION. (2.5 M/H)  ALI REFERENC 536405-02-3  536405-0606-8 233 PASSENGER DOOR FRAME NDT SDI I: 7000 FC ALI NTM 531413  234 FAA AD PART 6  243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND 2007-04-11  INSULATION. (2.5 M/H)  ALI REFERENC 536405-02-4  536405-0606-9 233 PASSENGER DOOR FRAME NDT SDI I: 7000 FC ALI NTM 531413  234 FAA AD PART 6  243 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR FRAME EASA AD  244 PROFIL SPLICE AT FRAME 28A AND 30A AT STR 14, LH/RH. 2006-0071  FAA AD  PREP.: REMOVE/INSTALL CABIN SIDE LINING AND 2007-04-11  INSULATION. (2.5 M/H)  ALI REFERENC 536405-02-5  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 132 I: 2000 FC FAA AD 96-13 233 DETAILED (INTERNAL AND EXTERNAL) INSPECTION  234 OF PASSENGER DOOR CUT OUT REINFORCEMENT BETWEEN ALI REFERENC 243 FRAMES 30 AND 30A AND BETWEEN STRINGERS 27 AND 536407-01-1  244 28, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-3  PREP.: 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 132 I: 2400 FC FAA AD 96-13 233 DETAILED (INTERNAL AND EXTERNAL) INSPECTION  234 OF PASSENGER DOOR CUT OUT REINFORCEMENT BETWEEN ALI REFERENC 243 FRAMES 30 AND 30A AND BETWEEN STRINGERS 27 AND 536407-01-2  244 28, LH/RH.  NOTE 01: THIS TASK IS AN ALTERNATIVE TO 536407-0606-4  PREP.: 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 531401  132 I: 4100 FC PART 6  233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071 234 REINFORCEMENT BETWEEN FRAMES 30 AND 30A AND BETWEEN FAA AD 96-13 243 STRINGERS 27 AND 28, LH/RH.  244 ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-1 536407-02-1  PREP.: 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 531401  132 I: 4800 FC PART 6  233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071 234 REINFORCEMENT BETWEEN FRAMES 30 AND 30A AND BETWEEN FAA AD 96-13 243 STRINGERS 27 AND 28, LH/RH.  244 ALI REFERENC NOTE : 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 132 I: 3000 FC FAA AD 96-13 233 DETAILED INTERNAL AND EXTERNAL INSPECTION OF  234 PASSENGER DOOR CUT OUT REINFORCEMENT BETWEEN FRAME ALI REFERENC 243 30 AND FRAME 30A AND BETWEEN STRINGER 27 AND 536407-01-3  244 STRINGER 28, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-6  PREP.: 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 531401  132 I: 3100 FC PART 6  233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071 234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13 243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.  244 ALI REFERENC 536407-02-3  NOTE : THIS TASK IS AN ALTERNATIVE TO 536407-0606-5  PREP.: 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 531401  132 PART 6  233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071 234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13 243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.  244 ALI REFERENC PREP.: 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 531401  132 PART 6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13 243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.  244 ALI REFERENC PREP.: 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 531401  132 PART 6  233 SPECIAL DETAILED INSPECTION OF PASSENGER DOOR CUT OUT CN 2006-0071 234 REINFORCEMENT BETWEEN FRAME 30 AND FRAME 30A AND FAA AD 96-13 243 BETWEEN STRINGER 27 AND STRINGER 28, LH/RH.  244 ALI REFERENC PREP.: 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 132 I: 9300 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENC FRAMES 27 AND 32 AND BETWEEN STRINGERS 26 AND 31, 536415-01-1  LH/RH.  PREP.: REMOVE/INSTALL CARGO COMPARTMENT LINING AND  INSULATION. (1.3 M/H)  536415-0606-2 131 FUSELAGE INTERNAL STRUCTURE MEC DET T: 28000 FC ALI CN 2006-0071 132 I: 10100 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENC FRAMES 27 AND 32 AND BETWEEN STRINGERS 26 AND 31, 536415-01-2  LH/RH.  PREP.: REMOVE/INSTALL CARGO COMPARTMENT LINING AND  INSULATION. (1.3 M/H)  536415-0606-3 131 FUSELAGE INTERNAL STRUCTURE MEC DET T: 28000 FC ALI CN 2006-0071 132 I: 9500 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC FRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-3  STRINGER 31, LH/RH.  PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING AND  INSULATION. (1.3 M/H)  536415-0606-4 131 FUSELAGE INTERNAL STRUCTURE MEC DET I: 6000 FC ALI CN 2006-0071 132 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUKTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENC FRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-4  STRINGER 31, LH/RH.  PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING AND  INSULATION. (1.3 M/H)  536415-0606-5 131 FUSELAGE INTERNAL STRUCTURE MEC DET I: 6000 FC ALI CN 2006-0071 132 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUKTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENC FRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-5  STRINGER 31, LH/RH.  PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING AND  INSULATION. (1.3 M/H)  536415-0606-6 131 FUSELAGE INTERNAL STRUCTURE MEC DET I: 6000 FC ALI CN 2006-0071 132 FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUKTURE BELOW MID PASSENGER/CREW DOOR BETWEEN ALI REFERENC FRAME 27 AND FRAME 32 AND BETWEEN STRINGER 26 AND 536415-01-6  STRINGER 31, LH/RH.  PREP.: REMOVA/INSTALL CARGO COMPARTMENT LINING AND  INSULATION. (1.3 M/H)  536421-0606-1 230 MID PASSENGER DOOR PANEL MEC DET T: 40000 FC ALI CN 2006-0071 I: 12000 FC CN FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC PASSENGER DOOR PANEL AT RUN-OUT OF FRAME PROFILE AT 536421-01-1  STRINGER 12, FRAME 29 AND FRAME 30, LH/RH.  PREP.: REMOVE LININGS, CEILING, HATRACKS AND  INSULATION.  536421-0606-2 230 MID PASSENGER DOOR PANEL MEC DET T: 34000 FC ALI CN 2006-0071 I: 12000 FC CN FAA AD 96-13 DETAILED INSPECTION OF SECTION 14, MID FAA AD  PASSENGER DOOR PANEL AT RUN-OUT OF FRAME PROFILE AT ALI REFERENC STRINGER 12, FRAME 29 AND FRAME 30, LH/RH. 536421-01-2  PREP.: FOR CARGO CONFIGURATION REMOVE LINING AND  INSULATION.  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 200 I: 2500 FC CN FAA AD 96-13 GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENC EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-1  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0604-1 AND 536502-0605-1  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0603-2 100 LONGITUDINAL LAP JOINTS MEC GVI T: 32000 FC ALI CN 2006-0071 200 I: 4300 FC CN FAA AD 96-13 GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENC EXCEPT 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 TASKS  536502-0604-2 AND 536502-0605-2  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0603-3 100 LONGITUDINAL LAP JOINTS MEC GVI T: 32000 FC ALI CN 2006-0071 200 I: 2000 FC CN FAA AD 96-13 GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENC EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-3  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0604-3 AND 536502-0605-3  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0603-4 100 LONGITUDINAL LAP JOINTS MEC GVI I: 1900 FC ALI CN 2006-0071 200 CN FAA AD 96-13 GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENC EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-4  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0604-4 AND 536502-0605-4  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  536502-0603-5 100 LONGITUDINAL LAP JOINTS MEC GVI I: 1900 FC ALI CN 2006-0071 200 CN FAA AD 96-13 GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENC EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-5  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0604-5 AND 536502-0605-5  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0603-6 100 LONGITUDINAL LAP JOINTS MEC GVI I: 1900 FC ALI CN 2006-0071 200 CN FAA AD 96-13 GENERAL VISUAL INSPECTION OF LOWER SKIN OF ALL FAA AD  LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 ALI REFERENC EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-01-6  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0604-6 AND 536502-0605-6  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0604-1 100 LONGITUDINAL LAP JOINTS MEC DET T: 32000 FC ALI CN 2006-0071 200 I: 3400 FC CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA AD  LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENC LAP 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 TASKS  536502-0603-1 AND 536502-0605-1  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0604-2 100 LONGITUDINAL LAP JOINTS MEC DET T: 32000 FC ALI CN 2006-0071 200 I: 5400 FC CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA AD  LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENC LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-2  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0603-2 AND 536502-0605-2  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0604-3 100 LONGITUDINAL LAP JOINTS MEC DET T: 32000 FC ALI CN 2006-0071 200 I: 2300 FC CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA AD  LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENC LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-3  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0603-3 AND 536502-0605-3  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 200 CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA AD  LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENC LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-4  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0603-4 AND 536502-0605-4  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0604-5 100 LONGITUDINAL LAP JOINTS MEC DET I: 2300 FC ALI CN 2006-0071 200 CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA AD  LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENC LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-5  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0603-5 AND 536502-0605-5  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0604-6 100 LONGITUDINAL LAP JOINTS MEC DET I: 2300 FC ALI CN 2006-0071 200 CN FAA AD 96-13 DETAILED INSPECTION OF LOWER SKIN OF ALL LONGITUDINAL FAA AD  LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 EXEPT ALI REFERENC LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH. 536502-02-6  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS  536502-0603-6 AND 536502-0605-6  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0605-1 100 LONGITUDINAL LAP JOINTS NDT SDI T: 32000 FC ALI NTM 533004  200 I: 12800 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13 EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.  ALI REFERENC NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-1  536502-0603-1 AND 536502-0604-1  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0605-2 100 LONGITUDINAL LAP JOINTS NDT SDI T: 32000 FC ALI NTM 533004  200 I: 8900 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13 EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.  ALI REFERENC NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-2  536502-0603-2 AND 536502-0604-2  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0605-3 100 LONGITUDINAL LAP JOINTS NDT SDI T: 32000 FC ALI NTM 533004  200 I: 8900 FC CN PART 6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13 EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.  ALI REFERENC NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-3  536502-0603-3 AND 536502-0604-3  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0605-4 100 LONGITUDINAL LAP JOINTS NDT SDI I: 8900 FC ALI NTM 533004  200 CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13 EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.  ALI REFERENC NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-4  536502-0603-4 AND 536502-0604-4  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0605-5 100 LONGITUDINAL LAP JOINTS NDT SDI I: 8900 FC ALI NTM 533004  200 CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13 EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.  ALI REFERENC NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-5  536502-0603-5 AND 536502-0604-5  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0605-6 100 LONGITUDINAL LAP JOINTS NDT SDI I: 8900 FC ALI NTM 533004  200 CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF ALL FAA AD CN 2006-0071 LONGITUDINAL LAP JOINTS BETWEEN FRAME 40 AND FRAME 80 FAA AD 96-13 EXCEPT LAP JOINT IN SECTION 16 AT STRINGER 52 LH/RH.  ALI REFERENC NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASKS 536502-03-6  536502-0603-6 AND 536502-0604-6  N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  PREP.:REMOVE LININGS AND INSULATION AT STRINGER 31  LH/RH BETWEEN FRAME 54 AND FRAME 55.  ACCESS: 577ET 577GT 677ET 677GT  536502-0606-1 100 LONGITUDINAL LAP JOINTS NDT SDI T: 28000 FC ALI NTM 533004  I: 9000 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071 LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13 LH/RH.  ALI REFERENC PREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-1  NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  ACCESS: 577ET 577GT 677ET 677GT  536502-0606-2 100 LAP JOINT AT STRINGER 52 NDT SDI T: 28000 FC ALI NTM 533004  I: 10200 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071 LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536502-0606-2 * * * * * C O N T I N U E * * * * *  LH/RH. ALI REFERENC 536502-04-2  PREP.: REMOVE FLOOR PANELS AND INSULATION.  NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  536502-0606-3 100 LONGITUDINAL LAP JOINTS NDT SDI T: 28000 FC ALI NTM 533004  I: 6500 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071 LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13 LH/RH.  ALI REFERENC PREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-3  NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  ACCESS: 577ET 577GT 677ET 677GT  536502-0606-4 100 LONGITUDINAL LAP JOINTS NDT SDI I: 6500 FC ALI NTM 533004  CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071 LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13 LH/RH.  ALI REFERENC PREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-4  NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  ACCESS: 577ET 577GT 677ET 677GT  536502-0606-5 100 LONGITUDINAL LAP JOINTS NDT SDI I: 6500 FC ALI NTM 533004  CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071 LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13 LH/RH.  ALI REFERENC 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  ACCESS: 577ET 577GT 677ET 677GT  536502-0606-6 100 LONGITUDINAL LAP JOINTS NDT SDI I: 6500 FC ALI NTM 533004  CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER SKIN OF FAA AD CN 2006-0071 LONGITUDINAL LAP JOINT IN SECTION 16 AT STRINGER 52 FAA AD 96-13 LH/RH.  ALI REFERENC PREP.: REMOVE FLOOR PANELS AND INSULATION. 536502-04-6  NOTE.: N/A WITH EXCEPTION OF LAP JOINTS AT STRINGER  31, LH/RH BETWEEN FRAMES 54 AND 55  ACCESS: 577ET 577GT 677ET 677GT  536503-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI ST: 25000 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 27700 FH FAA AD CN 2006-0071 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 3300 FC FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH. OR  3700 FH ALI REFERENC NOTE:THRESHOLD SARTS COUNTING FROM ENTRY INTO SERVICE 536503-01-1  ACCESS: 147AZ  148AZ  536503-0606-2 141 CENTER WING BOX REAR SPAR NDT SDI ST: 25000 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 27700 FH FAA AD CN 2006-0071 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 3300 FC FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH. OR  3900 FH ALI REFERENC ACCESS: 147AZ 536503-01-2  148AZ  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 39100 FH FAA AD CN 2006-0071 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 6400 FC FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH. OR  8600 FH ALI REFERENC NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-4  SERVICE  ACCESS: 147AZ  148AZ  536503-0606-4 141 CENTER WING BOX REAR SPAR NDT SDI ST: 30000 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 40500 FH FAA AD CN 2006-0071 SPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS SI: 6800 FC FAA AD 96-13 NO. 1, 2 AND 4, LH/RH. OR  9200 FH ALI REFERENC ACCESS: 147AZ 536503-01-5  148AZ  536503-0606-5 141 CENTER WING BOX REAR SPAR NDT SDI ST: 24000 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 49200 FH FAA AD CN 2006-0071 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH SI: 4200 FC FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH. OR  8600 FH ALI REFERENC NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-9  SEVICE  ACCESS: 147AZ  148AZ  536503-0606-6 141 CENTER WING BOX REAR SPAR NDT SDI ST: 25000 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 51200 FH FAA AD CN 2006-0071 SPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS SI: 4800 FC FAA AD 96-13 NO. 1, 2 AND 4, LH/RH. OR  9800 FH ALI REFERENC ACCESS: 147AZ 536503-01-10  148AZ  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 3000 FH FAA AD CN 2006-0071 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH.  ALI REFERENC ACCESS: 147AZ 536503-01-3  148AZ  536503-0606-8 141 CENTER WING BOX REAR SPAR NDT SDI I: 2900 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 3900 FH FAA AD CN 2006-0071 SPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS FAA AD 96-13 NO. 1, 2 AND 4, LH/RH.  ALI REFERENC ACCESS: 147AZ 536503-01-6  148AZ  536503-0606-9 141 CENTER WING BOX REAR SPAR NDT SDI I: 3300 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 4450 FH FAA AD CN 2006-0071 SPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS FAA AD 96-13 NO. 1, 2 AND 4, LH/RH.  ALI REFERENC ACCESS: 147AZ 536503-01-7  148AZ  536503-0607-1 141 CENTER WING BOX REAR SPAR NDT SDI I: 3300 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 4450 FH FAA AD CN 2006-0071 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH.  ALI REFERENC NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-8  SERVICE  ACCESS: 147AZ  148AZ  536503-0607-2 141 CENTER WING BOX REAR SPAR NDT SDI I: 2400 FC ALI NTM 531513  142 OR CN PART 4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH.  ALI REFERENC NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-11  SERVICE  ACCESS: 147AZ  148AZ  536503-0607-3 141 CENTER WING BOX REAR SPAR NDT SDI I: 2400 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX 4900 FH FAA AD CN 2006-0071 REAR SPAR LOWER FLANGE AT CROSSING AREAS WITH FAA AD 96-13 STIFFENERS NO. 1, 2 AND 4, LH/RH.  ALI REFERENC NOTE: THRESHOLD STARTS COUNTING FROM ENTRY INTO 536503-01-12  SERVICE  ACCESS: 147AZ  148AZ  536503-0607-4 141 CENTER WING BOX REAR SPAR NDT SDI I: 2100 FC ALI NTM 531513  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 4300 FH FAA AD CN 2006-0071 SPAR LOWER FLANGE AT CROSSING AREAS WITH STIFFENERS FAA AD 96-13 NO. 1, 2 AND 4, LH/RH.  ALI REFERENC ACCESS: 147AZ 536503-01-13  148AZ  536505-0606-1 141 CENTER WING BOX STRINGERS NDT SDI T: SEE SB ALI NTM 531501  142 I: SEE SB CN PART 4  SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD CN 2006-0071 CENTER WING BOX FORWARD AND REAR LOWER PANEL MAIN FAA AD  STRINGERS AT CROSSING AREA. 96-13-11-01- SB 53-0243  ACCESS: 147AZ 147DZ 147FZ 734  148AZ 148DZ 744 ALI REFERENC 536505-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536506-0606-2 141 CENTER WING BOX NDT SDI ST: 26000 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 28900 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 6200 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  6900 FH ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-1  148AZ 641AB 642CB  536506-0606-3 141 CENTER WING BOX NDT SDI ST: 35000 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 38800 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 9600 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  10600 FH ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-4  148AZ 641AB 642CB  536506-0606-4 141 CENTER WING BOX NDT SDI ST: 32000 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 43200 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 8000 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  10800 FH ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-6  148AZ 641AB 642CB  536506-0606-5 141 CENTER WING BOX NDT SDI ST: 24000 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 49200 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 6300 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  12900 FH ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-8  148AZ 641AB 642CB  536506-0606-6 141 CENTER WING BOX NDT SDI ST: 31000 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 63500 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT SI: 6500 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 148AZ 641AB 642CB 536506-01-11  536506-0606-7 141 CENTER WING BOX NDT SDI I: 6000 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 6700 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13 TO REAR SPARS LH/RH.  ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-2  148AZ 641AB 642CB  536506-0606-8 141 CENTER WING BOX NDT SDI I: 1200 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 1300 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13 TO REAR SPARS LH/RH.  ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-3  148AZ 641AB 642CB  536506-0606-9 141 CENTER WING BOX NDT SDI ST: 31000 FC ALI NTM 531518  142 SI: 6500 FC CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO T: 31000 FC FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 6500 FC FAA AD 96-13 TO REAR SPARS LH/RH.  ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-5  148AZ 641AB 642CB  536506-0607-1 141 CENTER WING BOX NDT SDI I: 6300 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 8300 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13 TO REAR SPARS LH/RH.  ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-7  148AZ 641AB 642CB  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536506-0607-2 141 CENTER WING BOX NDT SDI I: 5300 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 10900 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13 TO REAR SPARS LH/RH.  ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-9  148AZ 641AB 642CB  536506-0607-3 141 CENTER WING BOX NDT SDI I: 5600 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 11600 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13 TO REAR SPARS LH/RH.  ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-10  148AZ 641AB 642CB  536506-0607-4 141 CENTER WING BOX NDT SDI I: 5600 FC ALI NTM 531518  142 OR CN PART 2  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 11600 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT FAA AD 96-13 TO REAR SPARS LH/RH.  ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-01-12  148AZ 641AB 642CB  536506-0607-5 141 CENTER WING BOX NDT SDI T: 29200 FC ALI NTM 531518  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 31500 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 3100 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  3300 FH ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-02-1  148AZ 641AB 642CB  536506-0607-6 141 CENTER WING BOX NDT SDI T: 33900 FC ALI NTM 531518  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 45100 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 4200 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 148AZ 641AB 642CB 536506-02-2  536506-0607-7 141 CENTER WING BOX NDT SDI T: 29700 FC ALI NTM 531518  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX TO 61800 FH FAA AD CN 2006-0071 WING LOWER JUNCTION INTERNAL INBOARD SIDE FROM FRONT I: 4000 FC FAA AD 96-13 TO REAR SPARS LH/RH. OR  8300 FH ALI REFERENC ACCESS: 147AZ 541AB 542CB 536506-02-3  148AZ 641AB 642CB  536509-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI T: SEE ISB ALI CN 2006-0071 142 I: SEE ISB CN FAA AD 96-13 SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD ISB 53-0275  CENTER WING BOX REAR SPAR AROUND ACCESS DOOR CUT-OUTS ISB  LH/RH. ALI REFERENC 536509-01-1  ACCESS: 147AZ  148AZ  536510-0606-1 141 CENTER WING BOX REAR SPAR MEC DET T: 34000 FC ALI EASA AD  142 OR CN 2006-0071  DETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 45900 FH FAA AD FAA AD  REINFORCING PLATES AT CROSSING AREA WITH STRINGERS I: 6000 FC 2007-04-11  FROM RIB 1 LH TO RIB 1 RH. OR  8100 FH ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-01-1  536510-0606-5  PREP.: REMOVE/INSTALL INSULATION AND SEALANT.  ACCESS: 147AZ  148AZ  536510-0606-2 141 CENTER WING BOX REAR SPAR MEC DET I: 3200 FC ALI EASA AD  142 OR CN 2006-0071  DETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 4300 FH FAA AD FAA AD  REINFORCING 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 536510-01-2  NOTE : THIS TASK IS AN ALTERNATIVE TO TASK  536510-0606-5  PREP.: REMOVE/INSTALL INSULATION AND SEALANT.  ACCESS: 147AZ  148AZ  536510-0606-3 141 CENTER WING BOX REAR SPAR MEC DET T: 27000 FC ALI EASA AD  142 OR CN 2006-0071  DETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 55300 FH FAA AD FAA AD  REINFORCING PLATES AT CROSSING AREA WITH STRINGERS I: 3500 FC 2007-04-11  FROM RIB 1 LH TO RIB 1 RH. OR  7200 FH ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-01-3  536510-0606-6  PREP.: REMOVE/INSTALL INSULATION AND SEALANT.  ACCESS: 147AZ  148AZ  536510-0606-4 141 CENTER WING BOX REAR SPAR MEC DET I: 2400 FC ALI EASA AD  142 OR CN 2006-0071  DETAILED INSPECTION OF CENTER WING BOX, PUMP HOLES 4900 FH FAA AD FAA AD  REINFORCING PLATES AT CROSSING AREA WITH STRINGERS 2007-04-11  FROM RIB 1 LH TO RIB 1 RH.  ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-01-4  536510-0606-6  PREP.: REMOVE/INSTALL INSULATION AND SEALANT.  ACCESS: 147AZ  148AZ  536510-0606-5 141 CENTER WING BOX REAR SPAR NDT SDI T: 34000 FC ALI NTM 531520  142 OR CN PART 4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 HOLES REINFORCING PLATES AT CROSSING AREA WITH I: 9500 FC FAA AD 96-13 STRINGERS FROM RIB 1 LH TO RIB 1 RH. OR  12800 FH ALI REFERENC NOTE : THIS TASK IS AN ALTERNATIVE TO TASK 536510-02-1  536510-0606-1 AND TASK 536510-0606-2  PREP.: REMOVE/INSTALL INSULATION AND SEALANT.  ACCESS: 147AZ  148AZ  536510-0606-6 141 CENTER WING BOX REAR SPAR NDT SDI T: 27000 FC ALI NTM 531520  142 OR CN PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX, PUMP 55300 FH FAA AD CN 2006-0071 HOLES REINFORCING PLATES AT CROSSING AREA WITH I: 7300 FC FAA AD 96-13 STRINGERS FROM RIB 1 LH TO RIB 1 RH. OR  14900 FH ALI REFERENC PREP.: REMOVE/INSTALL INSULATION AND SEALANT. 536510-02-2  ACCESS: 147AZ  148AZ  536511-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI T: SEE ISB ALI NTM 531502  142 I: SEE ISB CN PART 4  SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD EASA AD  CENTER WING BOX REAR SPAR AT RIB 1 INTERNAL ANGLE ISB 2006-0071  RUNOUT LH/RH. FAA AD  2007-04-11  ACCESS: 147AZ  148AZ ALI REFERENC 536511-01-1  536512-0606-1 141 CENTER WING BOX REAR SPAR NDT SDI T: SEE SB ALI NTM 531504  142 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR FAA AD CN 2006-0071 SPAR AND BOTTOM PANEL UNDERNEATH INTERNAL ANGLE AT FAA AD 96-13 RIB 1 AREA, LH/RH. SB 53-0265  ACCESS: 147AZ ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536512-0606-1 * * * * * C O N T I N U E * * * * *  148AZ 536512-01-1  536513-0606-1 141 FRAME 47 - LOWER JUNCTION NDT SDI T: SEE SB ALI NTM 531504  142 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF FRAME 47 AT AREA OF FAA AD CN 2006-0071 LOWER JUNCTION WITH OUTER WING. ISB FAA AD 96-13 (HOLES H,I,K,L,M AND N ) ISB 53-0299  ACCESS: 147AZ ALI REFERENC 148AZ 536513-01-1  536515-0606-1 141 FRAME 47 LOWER RADIUS NDT SDI T: SEE SB ALI NTM 531503  142 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF FAA AD CN 2006-0071 FRAME 47 LOWER RADIUS LH/RH. ISB FAA AD 96-13 ISB 53-0259  ACCESS: 571AB  671AB ALI REFERENC 536515-01-1  536516-0606-1 140 FRAME 47 UPPER RADIUS NDT SDI T: SEE SB AD NTM 531529 P I: SEE SB CN 4 AND 6  SPECIAL DETAILED INSPECTION OF THE FRAME 47, UPPER ISB AD 2007-26-1 RADIUS. SB CN F-2006-01 FAA AD  ACCESS: 577BT 677BT 2003-06-04  ISB 53-0246  536516  536516-0606-4 140 FRAME 47 UPPER RADIUS NDT SDI T: SEE SB AD NTM 531529 P I: SEE SB CN 4 AND 6  SPECIAL DETAILED INSPECTION OF THE FRAME 47, UPPER ISB AD 2007-26-1 RADIUS. SB CN F-2006-01 FAA AD  ACCESS: 577BT 677BT 2003-06-04  ISB 53-0246  536516  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536516-0606-6 140 FRAME 47 UPPER RADIUS NDT SDI T: SEE SB AD NTM 531529  I: SEE SB CN PART 4 AND 6  SPECIAL DETAILED INSPECTION OF THE FRAME 47, UPPER ISB AD 2007-26-1 RADIUS. CN F-2006-01 FAA AD  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS TASK 2003-06-04  536523-0606-X ISB 53-0246  ACCESS: 577BT 677BT  536521-0606-2 243 FUSELAGE AT FRAME 40 MEC DET ST: 21000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 23700 FH FAA AD  AREAS AT FRAME 40, LH/RH. SI: 11900 FC ALI REFERENC OR 536521-01-1  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 13400 FH  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0606-3 243 FUSELAGE AT FRAME 40 MEC DET ST: 26000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 29400 FH FAA AD  AREAS AT FRAME 40, LH/RH. SI: 13200 FC ALI REFERENC OR 536521-01-3  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 14900 FH  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0606-4 243 FUSELAGE AT FRAME 40 MEC DET ST: 19000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 25800 FH FAA AD  AREAS AT FRAME 40, LH/RH. SI: 11000 FC ALI REFERENC OR 536521-01-5  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 14900 FH  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0606-5 243 FUSELAGE AT FRAME 40 MEC DET ST: 25000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 34000 FH FAA AD  AREAS AT FRAME 40, LH/RH. SI: 12700 FC ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536521-0606-5 * * * * * C O N T I N U E * * * * *  OR 536521-01-7  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 17300 FH  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0606-6 243 FUSELAGE AT FRAME 40 MEC DET ST: 19000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 42000 FH FAA AD  AREAS AT FRAME 40, LH/RH. SI: 9600 FC ALI REFERENC OR 536521-01-9  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 21200 FH  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0606-7 243 FUSELAGE AT FRAME 40 MEC DET ST: 24000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 53000 FH FAA AD  AREAS AT FRAME 40, LH/RH. SI: 10000 FC ALI REFERENC OR 536521-01-11  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR 22100 FH  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0607-1 243 FUSELAGE AT FRAME 40 MEC DET I: 8200 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 9200 FH FAA AD  COUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENC 536521-01-2  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0607-2 243 FUSELAGE AT FRAME 40 MEC DET I: 10000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 11300 FH FAA AD  COUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENC 536521-01-4  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR  CONDITIONING PIPE. REMOVE SEALANT IF  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 10300 FH FAA AD  COUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENC 536521-01-6  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0607-4 243 FUSELAGE AT FRAME 40 MEC DET I: 10000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 22100 FH FAA AD  COUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENC 536521-01-8  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0607-5 243 FUSELAGE AT FRAME 40 MEC DET I: 7300 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO 13 COUPLING 16100 FH FAA AD  AREAS AT FRAME 40, LH/RH. ALI REFERENC 536521-01-10  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  536521-0607-6 243 FUSELAGE AT FRAME 40 MEC DET I: 10000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 22100 FH FAA AD  COUPLING AREAS AT FRAME 40, LH/RH. ALI REFERENC 536521-01-12  PREP.: REMOVE/INSTALL LINING, INSULATION AND AIR  CONDITIONING PIPE. REMOVE SEALANT IF  INSTALLED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF SPLICE 47500 FH FAA AD EASA AD  244 PLATE AT FRAME 40 CIRCUMFERENTIAL SKIN SPLICE FROM SI: 6000 FC 2006-0071  STRINGER 13 LH/RH TO CROWN CENTER LINE. OR FAA AD  6800 FH 2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-7 ALI REFERENC 536523-01-1  536523-0606-3 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 6000 FC ALI NTM 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF SPLICE 6800 FH FAA AD EASA AD  244 PLATE AT THE CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 2006-0071  FROM STRINGER 13 LH/RH TO CROWN CENTER LINE. FAA AD  2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-8 ALI REFERENC 536523-01-2  536523-0606-4 241 SPLICE PLATE AT FRAME 40 NDT SDI ST: 39000 FC ALI NTM 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 53000 FH FAA AD EASA AD  244 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 FROM SI: 5800 FC 2006-0071  STRINGER 13 LH/RH TO CROWN CENTER LINE. OR FAA AD  7900 FH 2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-9 ALI REFERENC 536523-01-3  536523-0606-5 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 5800 FC ALI NTM 531523 P 242 OR CN 6  243 SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 7900 FH FAA AD EASA AD  244 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 FROM 2006-0071  STRINGER 13 LH/RH TO CROWN CENTER LINE. FAA AD  2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0607-1 ALI REFERENC 536523-01-4  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 83500 FH FAA AD EASA AD  244 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 40 FROM I: 5600 FC 2006-0071  STRINGER 13 LH/RH TO CROWN CENTER LINE. OR FAA AD  12400 FH 2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS TASK  536523-0607-2 ALI REFERENC 536523-01-5  536523-0606-7 241 SPLICE PLATE AT FRAME 40 NDT SDI ST: 42000 FC ALI NTM 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 47500 FH FAA AD EASA AD  244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO SI: 15500 FC 2006-0071  CROWN CENTER LINE LH/RH. OR FAA AD  17500 FH 2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-2 ALI REFERENC 536523-02-1  PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BE  REMOVED.  536523-0606-8 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 15500 FC ALI NTM 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 17500 FH FAA AD EASA AD  244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO 2006-0071  CROWN CENTER LINE LH/RH. FAA AD  2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-3 ALI REFERENC 536523-02-2  PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BE  REMOVED.  536523-0606-9 241 SPLICE PLATE AT FRAME 40 NDT SDI ST: 39000 FC ALI NTM 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 53000 FH FAA AD EASA AD  244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO SI: 14400 FC 2006-0071  CROWN CENTER LINE LH/RH. OR FAA AD  19600 FH 2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-4 ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536523-0606-9 * * * * * C O N T I N U E * * * * *  536523-02-3  PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BE  REMOVED.  536523-0607-1 241 SPLICE PLATE AT FRAME 40 NDT SDI I: 14400 FC ALI NTM 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 19600 FH FAA AD EASA AD  244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO 2006-0071  CROWN CENTER LINE LH/RH. FAA AD  2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-5 ALI REFERENC 536523-02-4  PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BE  REMOVED.  536523-0607-2 241 SPLICE PLATE AT FRAME 40 NDT SDI T: 37800 FC ALI NTM 531523  242 OR CN PART 6  243 SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 83500 FH FAA AD EASA AD  244 FRAME 40 CIRCUMFERENTIAL JOINT FROM STRINGERS 13 TO I: 13900 FC 2006-0071  CROWN CENTER LINE LH/RH. OR FAA AD  30700 FH 2007-04-11  NOTE: THIS TASK CAN BE DONE AT THE SAME TIME AS  TASK 536523-0606-6 ALI REFERENC 536523-02-5  PREP.:HATRACKS, LININGS INSULATION AND BOLTS TO BE  REMOVED.  536529-0606-1 141 CENTER WING BOX DOUBLER RUNOUT NDT SDI T: SEE ISB ALI NTM 531505  142 I: SEE ISB FAA AD PART 6  SPECIAL DETAILED OR GENERAL VISUAL INSPECTION OF ISB EASA AD  THE CENTER WING BOX CENTER SPAR AT CUTOUT DOUBLER 2006-0071(B)  RUN OUT. FAA AD 96-13 ISB 53-0242  ACCESS: 147AZ 147DZ 734  148AZ 148DZ 744 ALI REFERENC 536529-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531506  142 I: SEE ISB CN PART 6  SPECIAL DETAILED OR GENERAL VISUAL INSPECTION OF THE FAA AD CN 2006-0071 CENTER WING BOX FORWARD AND REAR LOWER PANEL MAIN ISB FAA AD 96-13 STRINGERS AT DRAINAGE HOLES. ISB 53-0244  ACCESS: 147AZ 147DZ 734 ALI REFERENC 148AZ 148DZ 744 536535-01-1  536541-0606-1 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 531522  641 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 23300 FH FAA AD CN 2006-0071 CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 7100 FC FAA AD 96-13 FRONT TO REAR SPAR, EXTERNAL SIDE. OR  7900 FH ALI REFERENC ACCESS: 577AT 577BT 536541-01-1  677AT 677BT  536541-0606-2 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 531522  641 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING TO CENTER 23300 FH FAA AD CN 2006-0071 WING BOX UPPER SPLICE AND PANEL AT RIB 1 FROM I: 5500 FC FAA AD 96-13 FRONT TO REAR SPAR, EXTERNAL SIDE. OR  6100 FH ALI REFERENC NOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE 536541-02-1  ACCESS: 577AT 577BT  677AT 677BT  536541-0606-3 541 OUTER WING TO CENTER WING NDT SDI T: 25000 FC ALI NTM 531522  641 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 27700 FH FAA AD CN 2006-0071 CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 9300 FC FAA AD 96-13 FRONT TO REAR SPAR, EXTERNAL SIDE. OR  10300 FH ALI REFERENC ACCESS: 577AT 577BT 536541-01-2  677AT 677BT  536541-0606-4 541 OUTER WING TO CENTER WING NDT SDI T: 25000 FC ALI NTM 531522  641 OR CN PART 4  SPECIAL DETAILED INSPECTION (US AND EDDY CURRENT) OF 27700 FH FAA AD  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  AT RIB 1, FROM FRONT TO REAR SPAR, EXTERNAL SIDE. OR PART 6  8000 FH CN 2006-0071 NOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE FAA AD 96-13 ACCESS: 577AT 577BT ALI REFERENC 677AT 677BT 536541-02-3  536541-0606-5 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 531522  641 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 28300 FH FAA AD CN 2006-0071 CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 8300 FC FAA AD 96-13 FRONT TO REAR SPAR, EXTERNAL SIDE. OR  11200 FH ALI REFERENC ACCESS: 577AT 577BT 536541-01-3  677AT 677BT  536541-0606-6 541 OUTER WING TO CENTER WING NDT SDI T: 21000 FC ALI NTM 531522  641 OR CN PART 4  SPECIAL DETAILED INSPECTION (US AND EDDY CURRENT) OF 28300 FH FAA AD NTM 531522  OUTER WING TO CENTER WING BOX UPPER SPLICE AND PANEL I: 6400 FC PART 6  AT RIB 1, FROM FRONT TO REAR SPAR, EXTERNAL SIDE. OR CN 2006-0071 8600 FH FAA AD 96-13 NOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE  ALI REFERENC ACCESS: 577AT 577BT 536541-02-5  677AT 677BT  536541-0606-7 541 OUTER WING TO CENTER WING NDT SDI T: 14000 FC ALI NTM 531522  641 OR CN PART 4  SPECIAL DETAILED INSPECTION (US) OF OUTER WING TO 28700 FC FAA AD CN 2006-0071 CENTER WING BOX UPPER SPLICE AND PANEL AT RIB 1, FROM I: 5700 FC FAA AD 96-13 FRONT TO REAR SPAR, EXTERNAL SIDE. OR  11700 FH ALI REFERENC ACCESS: 577AT 577BT 536541-01-4  677AT 677BT  536541-0606-8 541 OUTER WING TO CENTER WING NDT SDI T: 14000 FC ALI NTM 531522  641 OR FAA AD PART 4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531522  OUTER WING TO CENTER WING BOX UPPER SPLICE AND PANEL I: 4400 FC PART 6  AT RIB 1, FROM FRONT TO REAR SPAR, EXTERNAL SIDE. OR FAA AD 96-13 9000 FH  NOTE: THRESHOLD STARTS FROM ENTRY INTO SERVICE ALI REFERENC 536541-02-7  ACCESS: 577AT 577BT  677AT 677BT  536543-0606-1 541 FRAME 40 OUTBOARD LOWER RADIUS NDT SDI T: SEE SB ALI NTM 531517  641 I: SEE SB FAA AD PART 6  SPECIAL DETAILED INSPECTION OR DETAILED INSPECTION OF ISB EASA AD  FRAME 40 OUTBOARD LOWER RADIUS IN AREA OF CENTER WING 2006-0071  BOX TO FUSELAGE CONNECTION FORWARD FACE LH/RH. FAA AD  2007-04-11  ACCESS: 513AB ISB 53-0268  613AB  ALI REFERENC 536543-01-1  536544-0606-1 141 CENTER WING BOX LOWER PANEL NDT SDI T: SEE SB ALI NTM 531507  142 I: SEE SB FAA AD PART 4  143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER ISB EASA AD  144 PANEL AT FUSELAGE TO CENTER WING BOX JUNCTION FITTING 2006-0071  LH/RH. FAA AD  2007-04-11  ACCESS: 147AZ 734 ISB 53-0252  148AZ 744  ALI REFERENC 536544-01-2  536545-0606-1 141 CENTER WING BOX LOWER PANEL STRINGER NDT SDI T: SEE ISB ALI NTM 531508  142 I: SEE ISB FAA AD PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER ISB AND PART 6  PANEL STRINGERS REINFORCEMENT STRAP JUNCTIONS. CN 2006-0071 FAA AD 96-13 PREP.: VAPOR SEAL PARTLY REMOVED ISB 53-0245  ACCESS: 147AZ 147DZ 734 ALI REFERENC 148AZ 148DZ 744 536545-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536546-0606-1 542 CENTER WING SPAR NDT SDI T: 26000 FC ALI NTM 531519  642 OR FAA AD PART 4  SPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 28800 FH CN 2006-0071 RIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, I: 7200 FC FAA AD 96-13 LH/RH. OR  8000 FH ALI REFERENC NOTE: REMOVE SEALANT AND NUTS. 536546-01-1  ACCESS: 541AB 542CB  641AB 642CB  536546-0606-2 542 CENTER WING SPAR NDT SDI I: 7100 FC ALI NTM 531519  642 OR FAA AD PART 4  SPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 7900 FH CN 2006-0071 RIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, FAA AD 96-13 LH/RH.  ALI REFERENC NOTE: REMOVE SEALANT AND NUTS. 536546-01-2  ACCESS: 541AB 542CB  641AB 642CB  536546-0606-3 542 CENTER WING SPAR NDT SDI T: 22000 FC ALI NTM 531519  642 OR FAA AD PART 4  SPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 29700 FH CN 2006-0071 RIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, I: 5800 FC FAA AD 96-13 LH/RH. OR  7800 FH ALI REFERENC NOTE: REMOVE SEALANT AND NUTS. 536546-01-3  ACCESS: 541AB 542CB  641AB 642CB  536546-0606-4 542 CENTER WING SPAR NDT SDI T: 16000 FC ALI NTM 531519  642 OR FAA AD PART 4  SPECIAL DETAILED INSPECTION OF WING CENTER SPAR TO 32800 FH CN 2006-0071 RIB 1 SPLICE OUTBOARD LOWER AND VERTICAL FLANGE, I: 3700 FC FAA AD 96-13 LH/RH. OR  7600 FH ALI REFERENC NOTE: REMOVE SEALANT AND NUTS. 536546-01-4  ACCESS: 541AB 542CB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536546-0606-4 * * * * * C O N T I N U E * * * * *  641AB 642CB  536547-0606-1 141 CENTER WING BOX - RIB 1 NDT SDI T: 25000 FC ALI NTM 531515  142 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF CENTER WING BOX, 27700 FH CN 2006-0071 CENTER SPAR TO RIB 1 JUNCTION, INBOARD SIDE, LH/RH. I: 12000 FC FAA AD 96-13 OR  ACCESS: 147AZ 13300 FH ALI REFERENC 148AZ 536547-01-1  536548-0606-1 141 FUSELAGE/CENTER WING BOX NDT SDI T: SEE ISB ALI NTM SEE SB  142 I: ISE ISB FAA AD CN 2006-0071 SPECIAL DETAILED INSPECTION OF FRAME 40 FORWARD ISB FAA AD 96-13 FITTING RADIUS AT TENSION BOLT JUNCTION. ISB 53-0310  ACCESS: 512AB 513AB 513BB ALI REFERENC 612AB 613AB 613BB 536548-01-1  536549-0606-1 141 TENSION BOLT HOLES - FRAME 40 TO CENTER NDT SDI T: SEE SB ALI NTM 531528  142 WING BOX JUNCTION I: SEE SB FAA AD PART 6  241 ISB CN 2006-0071 242 SPECIAL DETAILED INSPECTION OF FRAME 40 TO CENTER FAA AD 96-13 WING CONNECTION AT UPPER SKIN LEVEL TENSION BOLTS ISB 53-0304  JUNCTION.  ALI REFERENC PREP.: REMOVE PASSENGER SEATS AND FLOOR COVERING IN 536549-01-1  CABIN, BETWEEN FR 39 AND FR 40, LH AND RH.  ACCESS: 811  241SF 241TF 241WF 241XF 513AB 841  242SF 242TF 242WF 242XF 613AB 841  536551-0604-1 145 UPPER FLANGE OF TRANSVERSAL FLOOR BEAM MEC DET T: 48000 FC ALI EASA AD  146 I: 13200 FC FAA AD 2006-0071  DETAILED INSPECTION OF TRANSVERSAL FLOOR BEAM UPPER FAA AD  FLANGE FROM BEAM 5 TO FRAME 50, LH/RH. 2007-04-11  PREP.: DUCTS TO BE REMOVED ALI REFERENC 536551-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  146 I: 13200 FC FAA AD 2006-0071  DETAILED INSPECTION OF TRANSVERSAL FLOOR BEAM UPPER FAA AD  FLANGE FROM BEAM 5 TO FRAME 50, LH/RH. 2007-04-11  PREP.: DUCTS TO BE REMOVED ALI REFERENC 536551-01-1  536551-0604-3 145 UPPER FLANGE OF TRANSVERSAL FLOOR BEAM MEC DET T: 34000 FC ALI EASA AD  146 I: 13200 FC FAA AD 2006-0071  DETAILED INSPECTION OF TRANSVERSAL FLOOR BEAM UPPER FAA AD  FLANGE FROM BEAM 5 TO FRAME 50, LH/RH. 2007-04-11  PREP.: DUCTS TO BE REMOVED ALI REFERENC 536551-01-1  536553-0604-1 143 CENTER WING BOX LOWER PANELS NDT SDI T: 48000 FC ALI NTM 536553  144 I: 8100 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX BOTTOM EASA AD  SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR FROM 2006-0071  RIB 1 LH TO RIB 1 RH. FAA AD  2007-04-11  PREP.: VAPOUR SEAL TO BE DISPLACED  ALI REFERENC ACCESS: 147FZ 734 536553-01-1  744  536553-0604-2 143 CENTER WING BOX LOWER PANELS NDT SDI T: 40000 FC ALI NTM 536553  144 I: 10100 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX BOTTOM EASA AD  SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR FROM 2006-0071  RIB 1 LH TO RIB 1 RH. FAA AD  2007-04-11  PREP.: VAPOUR SEAL TO BE DISPLACED  ALI REFERENC ACCESS: 147FZ 734 536553-01-2  744  536553-0604-3 143 CENTER WING BOX LOWER PANELS NDT SDI T: 34000 FC ALI NTM 536553  144 I: 10500 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF CENTER WING BOX BOTTOM  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  RIB 1 LH TO RIB 1 RH. 2006-0071  FAA AD  PREP.: VAPOUR SEAL TO BE DISPLACED 2007-04-11  ACCESS: 147FZ 734 ALI REFERENC 744 536553-01-3  536554-0606-1 145 FRAME FOOT RUNOUTS FRAME 48 TO FRAME 54 NDT SDI T: SEE SB ALI NTM 531509  146 I: SEE SB FAA AD PART 6  SPECIAL DETAILED INSPECTION OF FRAME FOOT RUNOUTS ISB EASA AD  FROM FRAME 48 TO FRAME 54 BETWEEN STRINGER 24 AND 2006-0071  STRINGER 28 AND FILLETS OF FRAME 48 TO FRAME 54 ON LH FAA AD  AND RH SIDES. 2007-04-11  ISB 53-0238  PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION,  MAIN DECK FLOOR PANELS TO BE REMOVED ALI REFERENC 536554-01-1  ACCESS: 832  842  536555-0606-1 145 FRAME FOOT RUNOUTS FRAME 41 TO FRAME 46 NDT SDI T: SEE SB ALI NTM 531509  146 I: SEE SB FAA AD PART 6  SPECIAL DETAILED INSPECTION OF FRAME FOOT RUNOUTS ISB EASA AD  FROM FRAME 41 TO FRAME 46 BETWEEN STRINGER 24 AND 2006-0071  STRINGER 28 LH/RH. FAA AD  2007-04-11  PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, ISB 53-0345  MAIN DECK FLOOR PANELS TO BE REMOVED  ALI REFERENC ACCESS: 832 536555-01-1  536556-0606-1 145 GANTRIES AND CENTER WING BOX AT FRAME 46 MEC DET T: 48000 FC ALI EASA AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF JUNCTION BETWEEN GANTRIES 53300 FH FAA AD  AND CENTER WING BOX UPPER PANEL AT FRAME 46, FROM I: 22000 FC 2007-04-11  GANTRY 1 TO GANTRY 5 LH/RH. OR  25000 FH ALI REFERENC PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R 536556-01-1  MAIN DECK FLOOR PANELS TO BE REMOVED  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF JUNCTION BETWEEN GANTRIES 55600 FH FAA AD  AND CENTER WING BOX UPPER PANEL AT FRAME 46, FROM I: 22000 FC 2007-04-11  GANTRY 1 TO GANTRY 5 LH/RH. OR  30300 FH ALI REFERENC PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R 536556-01-2  MAIN DECK FLOOR PANELS TO BE REMOVED  536556-0606-3 145 GANTRIES AND CENTER WING BOX AT FRAME 46 MEC DET T: 34000 FC ALI EASA AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF JUNCTION BETWEEN GANTRIES 74800 FH FAA AD  AND CENTER WING BOX UPPER PANEL AT FRAME 46, FROM I: 22000 FC 2007-04-11  GANTRY 1 TO GANTRY 5 LH/RH. OR  48400 FH ALI REFERENC PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R 536556-01-3  MAIN DECK FLOOR PANELS TO BE REMOVED  536557-0606-1 241 CENTER WING BOX FRONT SPAR MEC DET T: 48000 FC ALI EASA AD  242 I: 8100 FC FAA AD 2006-0071  DETAILED INSPECTION OF SEAT TRACK FITTINGS BETWEEN FAA AD  FRAME 48 AND FRAME 53 LH/RH 2007-04-11  PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R ALI REFERENC MAIN DECK FLOOR PANELS TO BE REMOVED 536557-01-1  536557-0606-2 241 CENTER WING BOX FRONT SPAR MEC DET T: 40000 FC ALI EASA AD  242 I: 8100 FC FAA AD 2006-0071  DETAILED INSPECTION OF SEAT TRACK FITTINGS BETWEEN FAA AD  FRAME 48 AND FRAME 53 LH/RH 2007-04-11  PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R ALI REFERENC MAIN DECK FLOOR PANELS TO BE REMOVED 536557-01-2  536557-0606-3 241 CENTER WING BOX FRONT SPAR MEC DET T: 34000 FC ALI EASA AD  242 I: 8100 FC FAA AD 2006-0071  DETAILED INSPECTION OF SEAT TRACK FITTINGS BETWEEN FAA AD  FRAME 48 AND FRAME 53 LH/RH 2007-04-11  PREP.: PASSENGER SEATS,(IF INSTALLED) INSULATION, R ALI REFERENC MAIN DECK FLOOR PANELS TO BE REMOVED 536557-01-3  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536560-0606-1 141 CENTER WING BOX MEC DET T: 24000 FC ALI EASA AD  142 I: 10000 FC FAA AD 2006-0071  DETAILED INSPECTION OF CENTER WING BOX FRONT SPAR FAA AD  VERTICAL STIFFENER. 2007-04-11  ACCESS: 147FZ 147GZ 147MZ ALI REFERENC 148GZ 148HZ 536560-01-1 R 536561-0606-1 141 CENTER WING BOX NDT SDI T: NOTE AD NTM 513010  142 I: NOTE FAA PART 1  SPECIAL DETAILED INSPECTION OF THE LOWER CORNER ANGLE ISB NTM 531504  FITTING AT FRAME 47. PART 2,4 AND  AD EU 2007-1 NOTE: FOR INTERVAL AND THRESHOLD SEE ISB. FAA AD  2008-14-09  ACCESS: 147AZ ISB 53-0381  148AZ R 536561-0606-2 141 CENTER WING BOX NDT SDI T: NOTE AD NTM 513010  142 I: NOTE FAA PART 1  SPECIAL DETAILED INSPECTION OF THE LOWER CORNER ANGLE ISB NTM 531504  FITTING AT FRAME 47. PART 2,4 AND  AD EU 2007-1 NOTE: FOR INTERVAL AND THRESHOLD SEE ISB. FAA AD  2008-14-09  ACCESS: 147AZ ISB 53-0383  148AZ  536578-0604-1 147 INSPECTION OF MAIN LANDING GEAR CUTOUT MEC DET T: 21000 FC ALI EASA AD  148 LOWER SKIN I: 6150 FC FAA AD 2006-0071  151 FAA AD  152 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL 2007-04-11  153 LAP JOINT AT STRINGER 36 AND STRINGER 44 LH/RH FROM  154 FRAME 54 TO MAIN LANDING GEAR CUT OUT INTERNAL ALI REFERENC SURFACE AND FRAME 54 TEE FITTING. 536578-01-1  NOTE: THRESHOLD AFTER EMBODIMENT OF 07301 (53-0239)  ACCESS: 147RZ  148RZ  577AB 577BB  677AB 677BB  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 536590  146 FRAME 49 I: 7500 FC FAA AD PART 6  EASA AD  SPECIAL DETAILED INSPECTION OF CENTER FUSELAGE 2006-0071  LONGITUDINAL BEAM (GANTRY) VERTICAL STIFFENER AT FAA AD  FRAME 49. 2007-04-11  PREP.: PASSENGER SEATS, INSULATION, MAIN DECK FLOOR ALI REFERENC PANELS TO BE REMOVED 536590-01-1  536596-0603-1 147 FUSELAGE - FUSELAGE CENTER SECTION NDT SDI T: SEE SB FAA AD NTM 53-15-11  148 I: SEE SB PART 4 AND 6  SPECIAL DETAILED INSPECTION OF THE LEFT AND RIGHT EASA AD  GANTRIES 1,2,3,4 AND 5 LOWER FLANGE BETWEEN 2006-177  FRAME 47 AND FRAME 54. FAA AD  2004-18-13  PREP.: FLOOR PANEL TO BE REMOVED ISB 53-0379  ACCESS: 734 831  744  536597-0602-1 241 FUSELAGE CENTER SECTION MEC DET T: 48000 FC ALI EASA AD  242 I: 5100 FC FAA AD 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA AD  TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11  EXTERNAL.  ALI REFERENC 536597-02-7  536597-0602-2 241 FUSELAGE CENTER SECTION MEC DET T: 48000 FC ALI EASA AD  242 I: 8000 FC FAA AD 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA AD  TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11  EXTERNAL.  ALI REFERENC 536597-02-8  536597-0602-3 241 FUSELAGE CENTER SECTION MEC DET T: 40000 FC ALI EASA AD  242 I: 5100 FC FAA AD 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA AD  TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536597-0602-3 * * * * * C O N T I N U E * * * * *  EXTERNAL. ALI REFERENC 536597-02-9  536597-0602-4 241 FUSELAGE CENTER SECTION MEC DET T: 40000 FC ALI EASA AD  242 I: 8000 FC FAA AD 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA AD  TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11  EXTERNAL.  ALI REFERENC 536597-02-10  536597-0602-5 241 FUSELAGE CENTER SECTION MEC DET T: 34000 FC ALI EASA AD  242 I: 5100 FC FAA AD 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA AD  TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11  EXTERNAL.  ALI REFERENC 536597-02-11  536597-0602-6 241 FUSELAGE CENTER SECTION MEC DET T: 34000 FC ALI EASA AD  242 I: 8000 FC FAA AD 2006-0071  DETAILED INSPECTION OF FUSELAGE SKIN FROM FRAME 40 FAA AD  TO FRAME 47 FROM STRINGER 22 TO STRINGER 28 LH/RH 2007-04-11  EXTERNAL.  ALI REFERENC 536597-02-12  536597-0606-1 241 FUSELAGE CENTER SECTION NDT SDI T: SEE ISB ALI NTM 531510  242 I: SEE ISB FAA AD PART 6  SPECIAL DETAILED OR DETAILED INSPECTION OF STRINGER ISB EASA AD  RUN OUTS AT FRAME 47 FORWARD AND REAR INTERNAL SIDE 2006-0071  FROM STRINGER 22 TO STRINGER 28. FAA AD  2007-04-11  PREP.: PASSENGER SEATS, INSULATION, MAIN DECK ISB 53-0237  FLOOR PANELS TO BE REMOVED  ALI REFERENC ACCESS: 831 536597-01-1  841  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536597-0606-2 241 FUSELAGE CENTER SECTION NDT SDI T: SEE ISB ALI NTM 531510  242 I: SEE ISB FAA AD PART 6  SPECIAL DETAILED OR DETAILED INSPECTION OF STRINGER ISB EASA AD  RUN OUTS AT FRAME 47 FORWARD AND REAR INTERNAL SIDE 2006-0071  FROM STRINGER 22 TO STRINGER 28. FAA AD  2007-04-11  PREP.: PASSENGER SEATS, INSULATION, MAIN DECK ISB 53-0237  FLOOR PANELS TO BE REMOVED  ALI REFERENC ACCESS: 831 536597-01-1  841  536597-0606-3 241 FUSELAGE CENTER SECTION NDT SDI T: SEE ISB ALI NTM 531510  242 I: SEE ISB CN PART 6  SPECIAL DETAILED OR DETAILED INSPECTION OF STRINGER FAA AD EASA AD  RUN OUTS AT FRAME 47 FORWARD AND REAR INTERNAL SIDE ISB 2006-0071  FROM STRINGER 22 TO STRINGER 28. FAA AD  2007-04-11  PREP.: PASSENGER SEATS, INSULATION, MAIN DECK ISB 53-0237  FLOOR PANELS TO BE REMOVED  ALI REFERENC ACCESS: 831 536597-01-1  841  536598-0606-1 145 GANTRIES 1 TO 5 MEC DET T: 21000 FC ALI EASA AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF GANTRIES 1 TO 5, 23900 FH FAA AD  LH/RH, AT FRAME 46. I: 1100 FC 2007-04-11  OR  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-1 1200 FH ALI REFERENC 536598-01-1  ACCESS: 241AEF 241AFF 241AGF 241AHF  242AAF 242ABF 242ZF  536598-0606-2 145 GANTRIES 1 TO 5 MEC DET T: 21000 FC ALI EASA AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF GANTRIES 1 TO 5, 29200 FH FAA AD  LH/RH, AT FRAME 46. I: 1100 FC 2007-04-11  OR  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-2 1500 FH ALI REFERENC AND 536598-0607-3 536598-01-2  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  242AAF 242ABF 242ZF  536598-0606-3 145 GANTRIES 1 TO 5 MEC DET T: 21000 FC ALI EASA AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF GANTRIES 1 TO 5, 48700 FH FAA AD  LH/RH, AT FRAME 46. I: 1200 FC 2007-04-11  OR  NOTE : THIS TASK IS AN ALTRNATIVE TO 536598-0607-4 2800 FH ALI REFERENC 536598-01-3  ACCESS: 241AEF 241AFF 241AGF 241AHF  242AAF 242ABF 242ZF  536598-0606-5 145 GANTRIES 1 TO 5 MEC DET T: 26000 FC ALI EASA AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF GANTRIES 1 TO 5, 60300 FH FAA AD  LH/RH, AT FRAME 46. I: 2500 FC 2007-04-11  OR  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-5 5800 FH ALI REFERENC 536598-01-4  ACCESS: 241DF 241EF 241FF 241HF  242AF 242BF 242ZF  536598-0606-6 145 GANTRIES 1 TO 5 MEC DET I: 2100 FC ALI EASA AD  146 OR FAA AD 2006-0071  DETAILED INSPECTION OF GANTRIES 1 TO 5, 4800 FH FAA AD  LH/RH, AT FRAME 46. 2007-04-11  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0607-5 ALI REFERENC 536598-01-5  ACCESS: 241DF 241EF 241FF 241HF  242AF 242BF 242ZF  536598-0607-1 145 GANTRIES 1 TO 5 NDT SDI T: 21000 FC ALI NTM 531521  146 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 23900 FH EASA AD  AT FRAME 46. I: 6600 FC 2006-0071  OR FAA AD  NOTE : 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 242AAF 242ABF 242ZF 536598-02-1  536598-0607-2 145 GANTRIES 1 TO 5 NDT SDI T: 21000 FC ALI NTM 531521  146 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 29200 FH EASA AD  AT FRAME 46. I: 7000 FC 2006-0071  OR FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-2 9700 FH 2007-04-11  ACCESS: 241AEF 241AFF 241AGF 241AHF ALI REFERENC 242AAF 242ABF 242ZF 536598-02-2  536598-0607-3 145 GANTRIES 1 TO 5 NDT SDI I: 6600 FC ALI NTM 531521  146 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 9200 FH EASA AD  AT FRAME 46. 2006-0071  FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-2 2007-04-11  ACCESS: 241AEF 241AFF 241AGF 241AHF ALI REFERENC 242AAF 242ABF 242ZF 536598-02-3  536598-0607-4 145 GANTRIES 1 TO 5 NDT SDI T: 21000 FC ALI NTM 531521  146 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 48700 FH EASA AD  LH/RH AT FRAME 46. I: 7000 FC 2006-0071  OR FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-3 16200 FH 2007-04-11  ACCESS: 241AEF 241AFF 241AGF 241AHF ALI REFERENC 242AAF 242ABF 242ZF 536598-02-4  536598-0607-5 145 OANTRIES 1 TO 5 MEC SDI T: 26000 FC ALI NTM 531521  146 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF GANTRIES 1 TO 5 LH/RH 60300 FH EASA AD  AT FRAME 46. I: 8000 FC 2006-0071  OR FAA AD  NOTE : THIS TASK IS AN ALTERNATIVE TO 536598-0606-5 18500 FH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 536598-02-5  ACCESS: 241AEF 241AFF 241AGF 241AHF  242AAF 242ABF 242ZF  536599-0606-1 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET T: 32000 FC ALI EASA AD  148 OR FAA AD 2006-0071  DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 36100 FH FAA AD  CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS AND I: 5600 FC 2007-04-11  TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN OR  FRAME 47 AND FRAME 48 LH/RH. 6300 FH ALI REFERENC 536599-01-1  NOTE: THIS TASK IS AN ALTERNATIVE TO 53699-0606-4  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0606-2 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET T: 30000 FC ALI EASA AD  148 OR FAA AD 2006-0071  DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 41100 FH FAA AD  CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS AND I: 6500 FC 2007-04-11  TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN OR  FRAME 47 AND FRAME 48 LH/RH. 8900 FH ALI REFERENC 536599-01-3  NOTE: THIS TASK IS AN ALTERNATIVE TO 53699-0606-5  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0606-3 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET T: 28000 FC ALI EASA AD  148 OR FAA AD 2006-0071  DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 63500 FH FAA AD  CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS AND I: 6000 FC 2007-04-11  TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN OR  FRAME 47 AND FRAME 48 LH/RH. 13600 FH ALI REFERENC 536599-01-5  NOTE: THIS TASK IS AN ALTERNATIVE TO 53699-0606-6  PREP.: MAIN LANDING GEAR DOORS OPENED.  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531527  148 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 36100 FH EASA AD  PANELS TO CENTER WING BOX REAR SPAR ATTACHMENT I: 13200 FC 2006-0071  FITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS OR FAA AD  BETWEEN FRAME 47 AND FRAME 48 LH/RH. 14900 FH 2007-04-11  NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0606-1 ALI REFERENC 536599-02-1  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0606-5 147 PRESSURIZED FLOOR AT FRAME 47 NDT SDI T: 30000 FC ALI NTM 531527  148 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 41100 FH EASA AD  PANELS TO CENTER WING BOX REAR SPAR ATTACHMENT I: 9900 FC 2006-0071  FITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS OR FAA AD  BETWEEN FRAME 47 AND FRAME 48 LH/RH. 13500 FH 2007-04-11  NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0606-2 ALI REFERENC AND 536599-0607-2 536599-02-3  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0606-6 147 PRESSURIZED FLOOR AT FRAME 47 NDT SDI T: 28000 FC ALI NTM 531527  148 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 63500 FH EASA AD  PANELS TO CENTER WING BOX REAR SPAR ATTACHMENT I: 8300 FC 2006-0071  FITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS OR FAA AD  BETWEEN FRAME 47 AND FRAME 48 LH/RH. 18800 FH 2007-04-11  NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0606-3 ALI REFERENC AND 536599-0607-3 536599-02-4  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0607-1 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET I: 3000 FC ALI EASA AD  148 OR FAA AD 2006-0071  DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 3400 FH FAA AD  CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS 2007-04-11  AND TO HORIZONTAL BEAM ATTACHMENT FITTING BETWEEN  FRAME 47 AND FRAME 48 LH/RH. ALI REFERENC 536599-01-2  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 536599-0607-4  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0607-2 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET I: 2700 FC ALI EASA AD  148 OR FAA AD 2006-0071  DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 3700 FH FAA AD  CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS 2007-04-11  AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN  FRAME 47 AND FRAME 48 LH/RH. ALI REFERENC 536599-01-4  NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0607-5  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0607-3 147 PRESSURIZED FLOOR AT FRAME 47 MEC DET I: 2300 FC ALI EASA AD  148 OR FAA AD 2006-0071  DETAILED INSPECTION OF PESSURIZED FLOOR PANEL TO 5200 FH FAA AD  CENTER WING BOX REAR SPAR ATTACHMENT FITTINGS 2007-04-11  AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS BETWEEN  FRAME 47 AND FRAME 48 LH/RH. ALI REFERENC 536599-01-6  NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0607-6  PREP.: MAIN LANDING GEAR DOORS OPENED.  536599-0607-4 147 PRESSURIZED FLOOR AT FRAME 47 NDT SDI I: 10000 FC ALI NTM 531527  148 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION OF PESSURIZED FLOOR 11300 FH EASA AD  PANELS TO CENTER WING BOX REAR SPAR ATTACHMENT 2006-0071  FITTINGS AND TO HORIZONTAL BEAM ATTACHMENT FITTINGS FAA AD  BETWEEN FRAME 47 AND FRAME 48 LH/RH. 2007-04-11  NOTE: THIS TASK IS AN ALTERNATIVE TO 536599-0607-1 ALI REFERENC 536599-02-2  PREP.: MAIN LANDING GEAR DOORS OPENED.  536601-0606-1 251 EMERGENCY EXIT TORSION BOX BEAM NDT NDT T: SEE SB ALI NTM 531600  252 I: SEE SB CN PART 6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 254 TORSION BOX BEAM BETWEEN FRAME 57 A AND FRAME 58 ISB FAA AD 96-13 FROM STRINGER 14 TO STRINGER 15 LH/RH. ISB 53-0254  PREP.: OVERHEAD STOWAGE COMPARTMENT, UPPER SIDEWALL ALI REFERENC PANELS BETWEEN FRAME 57 A AND FRAME 58 TO 536601-01-1  BE REMOVED.  BE REMOVED.  ACCESS: 833  843  536602-0606-1 243 SPLICE PLATE AT FRAME 54.3 NDT SDI T: SEE SB ALI NTM 533021  244 I: SEE SB CN PART 4  SPECIAL DETAILED INSPECTION (US AND EDDY CURRENT) OF FAA AD NTM 533021  SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FRAME ISB PART 6  54.3 FROM STRINGER 12 TO CROWN CENTER LINE LH/RH. CN 2006-0071 FAA AD 96-13 ISB 53-0257  ALI REFERENC 536602-01-1  536603-0606-1 243 SPLICE PLATE AT FRAME 55 NDT SDI T: SEE SB ALI NTM 533021  244 I: SEE SB CN PART 4  SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD AND PART 6  CIRCUMFERENTIAL SKIN SPLICE AT FRAME 55 FROM STRINGER ISB CN 2006-0071 12 TO STRINGER 5 LH/RH. FAA AD 96-13 ISB 53-0257  PREP.: HATRACKS, LININGS, INSULATION TO BE REMOVED.  ALI REFERENC 536603-01-1  536651-0606-2 243 FUSELAGE AT FRAME 54 MEC DET T: 19000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 21500 FH FAA AD  COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 7000 FC ALI REFERENC LH/RH. OR 536651-01-1  7900 FH  PREP.: LINING, INSULATION AND SEALANT REMOVED  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 TO  TASK 536651-0607-2  536651-0606-3 243 FUSELAGE AT FRAME 54 MEC DET T: 25000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 28200 FH FAA AD  COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 8500 FC ALI REFERENC LH/RH. OR 536651-01-2  9600 FH  PREP.: LINING, INSULATION AND SEALANT REMOVED  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0607-3  536651-0606-4 243 FUSELAGE AT FRAME 54 MEC DET T: 18000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 24500 FH FAA AD  COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 6400 FC ALI REFERENC LH/RH. OR 536651-01-3  8700 FH  PREP.: LINING, INSULATION AND SEALANT REMOVED  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0607-4  536651-0606-5 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 32600 FC FAA AD  COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 8300 FC ALI REFERENC LH/RH. OR 536651-01-4  11300 FH  PREP.: LINING, INSULATION AND SEALANT REMOVED  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0607-5  536651-0606-6 243 FUSELAGE AT FRAME 54 MEC DET T: 18000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 6400 FC 536651-01-5  LH/RH. OR  14100 FH  PREP.: LINING, INSULATION AND SEALANT REMOVED  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0607-6  536651-0606-7 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI CN 2006-0071 244 OR CN FAA AD 96-13 DETAILED INSPECTION OF STRINGER 1 TO STRINGER 13 53000 FH FAA AD  COUPLING AREAS AT FRAME 54 CIRCUMFERENTIAL JOINT, I: 8300 FC ALI REFERENC LH/RH. OR 536651-01-6  18300 FH  PREP.: LINING, INSULATION AND SEALANT REMOVED  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0607-7  536651-0607-2 243 FUSELAGE AT FRAME 54 MEC DET T: 19000 FC ALI NTM 531525  244 OR CN PART 6  SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 21500 FH FAA AD CN 2006-0071 STRINGER 13 COUPLING AREAS AT FRAME 54 I: 9200 FC FAA AD 96-13 CIRCUMFERENTIAL JOINT LH/RH. OR  10400 FH ALI REFERENC PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-1  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0606-2  536651-0607-3 243 FUSELAGE AT FRAME 54 MEC DET T: 25000 FC ALI NTM 531525  244 OR CN PART 6  SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 28200 FH FAA AD CN 2006-0071 STRINGER 13 COUPLING AREAS AT FRAME 54 I: 9700 FC FAA AD 96-13 CIRCUMFERENTIAL JOINT LH/RH. OR  10900 FH ALI REFERENC PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-2  NOTE: THIS TASK IS AN ALTERNATIVE TO  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536651-0607-3 * * * * * C O N T I N U E * * * * *  TASK 536651-0606-3  536651-0607-4 243 FUSELAGE AT FRAME 54 MEC DET T: 18000 FC ALI NTM 531525  244 OR CN PART 6  SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 24500 FH FAA AD CN 2006-0071 STRINGER 13 COUPLING AREAS AT FRAME 54 I: 8200 FC FAA AD 96-13 CIRCUMFERENTIAL JOINT LH/RH. OR  11100 FH ALI REFERENC PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-3  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0606-4  536651-0607-5 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI NTM 531525  244 OR CN PART 6  SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 32600 FC FAA AD CN 2006-0071 STRINGER 13 COUPLING AREAS AT FRAME 54 I: 9400 FC FAA AD 96-13 CIRCUMFERENTIAL JOINT LH/RH. OR  12800 FH ALI REFERENC PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-4  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0606-5  536651-0607-6 243 FUSELAGE AT FRAME 54 MEC SDI T: 18000 FC ALI NTM 531525  244 OR CN PART 6  SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 39800 FH FAA AD CN 2006-0071 STRINGER 13 COUPLING AREAS AT FRAME 54 I: 8200 FC FAA AD 96-13 CIRCUMFERENTIAL JOINT LH/RH. OR  18100 FH ALI REFERENC PREP.: LINING, INSULATION AND SEALANT REMOVED 536651-02-5  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0606-6  536651-0607-7 243 FUSELAGE AT FRAME 54 MEC DET T: 24000 FC ALI NTM 531525  244 OR CN PART 6  SPECIAL DETAIELD INSPECTION OF STRINGER 1 TO 53000 FH FAA AD CN 2006-0071 STRINGER 13 COUPLING AREAS AT FRAME 54 I: 9400 FC FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 20800 FH 536651-02-6  PREP.: LINING, INSULATION AND SEALANT REMOVED  NOTE: THIS TASK IS AN ALTERNATIVE TO  TASK 536651-0606-7  536652-0606-2 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 533021  244 OR FAA AD PART 4  SPECIAL DETAILED INSPECTION (LF-EC) OF SPLICE PLATE 59700 FH EASA AD  AT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO I: 6100 FC 2006-0071  CROWN CENTERLINE RH/LH. OR FAA AD  6900 FH 2007-04-11  ALI REFERENC 536652-01-1  536652-0606-3 243 SPLICE PLATE AT FRAME 54 NDT SDI I: 6100 FC ALI NTM 531526  244 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION (LF-EC) OF SPLICE PLATE 6900 FH EASA AD  AT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO 2006-0071  CROWN CENTERLINE RH/LH. FAA AD  2007-04-11  ALI REFERENC 536652-01-2  536652-0606-4 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 531526  244 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION (LF-EC) OF SPLICE PLATE 59700 FH EASA AD  AT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO I: 5700 FC 2006-0071  CROWN CENTERLINE RH/LH. OR FAA AD  7700 FH 2007-04-11  ALI REFERENC 536652-01-3  536652-0606-5 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 531526  244 OR FAA AD PART 6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  AT FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO I: 5700 FC 2006-0071  CROWN CENTERLINE RH/LH. OR FAA AD  12600 FH 2007-04-11  ALI REFERENC 536652-01-4  536652-0606-6 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 47000 FC ALI NTM 531526  244 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 53100 FH EASA AD  FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN I: 18400 FC 2006-0071  CENTERLINE RH/LH. OR FAA AD  20800 FH 2007-04-11  ALI REFERENC 536652-02-1  536652-0606-7 243 SPLICE PLATE AT FRAME 54 NDT SDI I: 18400 FC ALI NTM 531526  244 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 20800 FH EASA AD  FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN 2006-0071  CENTERLINE RH/LH. FAA AD  2007-04-11  ALI REFERENC 536652-02-2  536652-0606-8 243 SPLICE PLATE AT FRAME 54 NDT SDI T: 43900 FC ALI NTM 531526  244 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 59700 FH EASA AD  FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN I: 10300 FC 2006-0071  CENTERLINE RH/LH. OR FAA AD  14000 FH 2007-04-11  ALI REFERENC 536652-02-3  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531526  244 OR FAA AD PART 6  SPECIAL DETAILED INSPECTION (ROT) OF SPLICE PLATE AT 97000 FH EASA AD  FRAME 54 CIRCUMFERENTIAL JOINT STRINGER 13 TO CROWN I: 10300 FC 2006-0071  CENTERLINE RH/LH. OR FAA AD  22800 FH 2007-04-11  ALI REFERENC 536652-02-4  536653-0602-1 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENC 242 FRAME 55 OR 536653-01-1  243 45600 FH  244 DETAILED INSPECTION OF SECTION 16 IN AREA OF I: 12000 FC  STRINGER COUPLING RUN OUT AT CIRCUMFERENTIAL JOINT OR  FRAME 55 FROM STRINGER 5 TO STRINGER 12 LH/RH 13600 FH  EXTERNAL SURFACE.  536653-0602-2 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENC 242 FRAME 55 OR 536653-01-2  243 55600 FH  244 DETAILED INSPECTION OF SECTION 16 IN AREA OF I: 12000 FC  STRINGER COUPLING RUN OUT AT CIRCUMFERENTIAL JOINT OR  FRAME 55 FROM STRINGER 5 TO STRINGER 12 LH/RH 16600 FH  EXTERNAL SURFACE.  536653-0602-3 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 34000 FC ALI EASA AD  242 FRAME 55 OR 2006-0071  243 78800 FH FAA AD  244 DETAILED INSPECTION OF SECTION 16 IN AREA OF I: 10500 FC 2007-04-11  STRINGER COUPLING RUN OUT AT CIRCUMFERENTIAL JOINT OR  FRAME 55 FROM STRINGER 5 TO STRINGER 12 LH/RH 24300 FH ALI REFERENC EXTERNAL SURFACE. 536653-01-3  536654-0604-1 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENC 242 FRAME 55 OR 536654-01-1  243 45600 FH  244 DETAILED INSPECTION OF STRINGER COUPLING AT I: 12000 FC  CIRCUMFERENTIAL JOINT FRAME 55 STRINGER 5 TO OR  STRINGER 12 LH/RH INTERNAL. 13600 FH  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REMOVED  536654-0604-2 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 40000 FC ALI ALI REFERENC 242 FRAME 55 OR 536654-01-2  243 55600 FH  244 DETAILED INSPECTION OF STRINGER COUPLING AT I: 12000 FC  CIRCUMFERENTIAL JOINT FRAME 55 STRINGER 5 TO OR  STRINGER 12 LH/RH INTERNAL. 16600 FH  PREP:. LININGS AND INSULATION TO BE REMOVED  536654-0604-3 241 STRINGER 5 TO STRINGER 12 COUPLINGS AT MEC DET T: 34000 FC ALI EASA AD  242 FRAME 55 OR 2006-0071  243 78800 FH FAA AD  244 DETAILED INSPECTION OF STRINGER COUPLING AT I: 10500 FC 2007-04-11  CIRCUMFERENTIAL JOINT FRAME 55 STRINGER 5 TO OR  STRINGER 12 LH/RH INTERNAL. 24300 FH ALI REFERENC 536654-01-3  PREP:. LININGS AND INSULATION TO BE REMOVED  536701-0606-1 162 FUSELAGE BETWEEN FRAME 66 AND FRAME 67 MEC DET T: SEE SB ALI CN 2006-0071 164 I: SEE SB CN FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE FAA AD ISB 53-0255  BETWEEN AND INCLUDING FRAME 66 AND FRAME 67 FROM ISB  STRINGER 42 TO STRINGER 46, RH. ALI REFERENC 536701-01-1  PREP.: FLOOR PANELS, LININGS AND INSULATION  TO BE REMOVED.  ACCESS: 813  536702-0606-1 253 SPLICE PLATE AT FRAME 58 NDT SDI T: SEE SB ALI NTM 533021  254 I: SEE SB CN PART 4 AND 6  SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 58, FROM ISB FAA AD 96-13 STRINGER 13 TO CROWN CENTER LINE LH/RH. ISB 53-0260  PREP.: HATRACKS LININGS INSULATION TO BE REMOVED. ALI REFERENC 536702-01-1  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 533021  254 I: SEE SB CN PART 4 AND 6  SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 65 FROM STRINGER ISB FAA AD 96-13 13 TO CROWN CENTERLINE LH/RH ISB 53-0261  PREP.: LININGS, HATRACKS, INSULATION ALI REFERENC TO BE REMOVED. 536703-01-1  536703-0606-2 253 SPLICE PLATE AT FRAME 65 NDT SDI T: SEE SB ALI NTM 533021  254 I: SEE SB CN PART 4 AND 6  SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 65 FROM STRINGER ISB FAA AD 96-13 13 TO CROWN CENTERLINE LH/RH ISB 53-0261  PREP.: LININGS, HATRACKS, INSULATION ALI REFERENC TO BE REMOVED. 536703-01-2  536703-0606-3 253 SPLICE PLATE AT FRAME 65 NDT SDI T: SEE SB ALI NTM 533021  254 I: SEE SB CN PART 4 AND 6  SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT FAA AD CN 2006-0071 CIRCUMFERENTIAL SKIN SPLICE AT FRAME 65 FROM STRINGER ISB FAA AD 96-13 13 TO CROWN CENTERLINE LH/RH ISB 53-0261  PREP.: LININGS, HATRACKS, INSULATION ALI REFERENC TO BE REMOVED. 536703-01-3  536704-0606-1 154 FUSELAGE FRAME 60 TO 63 MEC DET ST: 30000 FC ALI CN 2006-0071 SI: 7000 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA OF  FRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN ALI REFERENC STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE. 536704-01-1  NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-4  PREP.: 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 SI: 5600 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC STRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-3  NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-5  PREP.: 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 SI: 8400 FC FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA  OF FRAMES 60 TO 63, TO LOCK FITTINGS BETWEEN ALI REFERENC STRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-2  NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-6  PREP.: 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 531700  SI: 11600 FC PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 FRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13 STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.  ALI REFERENC NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-1 536704-02-1  PREP.: 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 531700  SI: 9100 FC PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 FRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13 STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.  ALI REFERENC NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-2 536704-02-3  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  (12.0 M/H)  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531700  SI: 10000 FC PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 FRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13 STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.  ALI REFERENC NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0606-3 536704-02-2  PREP.: 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 FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA OF  FRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN ALI REFERENC STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE. 536704-01-4  NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0607-4  PREP.: 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 FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA  OF FRAMES 60 TO 63, TO LOCK FITTINGS BETWEEN ALI REFERENC STRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-5  NOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-5  PREP.: 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 FAA AD 96-13 DETAILED INSPECTION OF ATTACHMENT AREA  OF FRAMES 60 TO 63, TO LOCK FITTINGS BETWEEN ALI REFERENC STRINGERS 44 AND 48, RH, INTERNAL STRUCTURE. 536704-01-6  NOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-6  PREP.: REMOVE/INSTALL BALLMATS AND INSULATION.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 531700  PART 6  SPECIAL DETAILED INSPECTION OF ATTACHMENT AREA OF CN 2006-0071 FRAME 60 TO FRAME 63, TO LOCK FITTINGS BETWEEN FAA AD 96-13 STRINGER 44 AND STRINGER 48 RH, INTERNAL STRUCTURE.  ALI REFERENC NOTE: 01.THIS TASK IS AN ALTERNATIVE TO 536704-0607-1 536704-02-4  PREP.: 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 531700  PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF CN 2006-0071 ATTACHMENT AREA OF FRAME 60 TO FRAME 63, TO LOCK FAA AD 96-13 FITTINGS BETWEEN STRINGER 44 AND STRINGER 48 RH,  INTERNAL STRUCTURE. ALI REFERENC 536704-02-5  NOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-2  PREP.: 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 531700  PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF CN 2006-0071 ATTACHMENT AREA OF FRAME 60 TO FRAME 63, TO LOCK FAA AD 96-13 FITTINGS BETWEEN STRINGER 44 AND STRINGER 48 RH,  INTERNAL STRUCTURE. ALI REFERENC 536704-02-6  NOTE: THIS TASK IS AN ALTERNATIVE TO 536704-0607-3  PREP.: 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 I: 6000 FC FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC STRUCTURE FROM FRAME 59 TO FRAME 64, AND FROM 536705-01-1  STRINGER 18 TO STRINGER 23, LH/RH, IN FRAME  COUPLING AREAS.  ACCESS: REMOVE LINING AND INSULATION  536705-0606-2 240 FUSELAGE INTERNAL STRUCTURE MEC DET T: 34000 FC ALI CN 2006-0071 I: 6000 FC FAA AD 96-13 DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE FROM FRAME 59 TO FRAME 64, AND FROM ALI REFERENC STRINGER 18 TO STRINGER 23, LH/RH, IN FRAME 536705-01-2  COUPLING AREAS.  ACCESS: REMOVE LINING AND INSULATION  536706-0606-1 253 STRINGER COUPLINGS NDT SDI T: 46000 FC ALI NTM 513105  254 I: 8200 FC PART 1  SPECIAL DETAILED INSPECTION OF STRINGER COUPLINGS CN 2006-0071 FROM STRINGER 5LH TO STRINGER 5RH AT FR 65 FAA AD 96-13 PREP.: REMOVE LININGS, HATRACKS, CEILING PANELS AND ALI REFERENC INSULATION 536706-01-1  536707-0604-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 58 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 45600 FH FAA AD  CIRCUMFERENTIAL JOINT FRAME 58 FROM STRINGER 12 LH I: 12000 FC 2007-04-11  TO STRINGER 12 RH INTERNAL. OR  13600 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536707-01-1  ACCESS: 843  536707-0604-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 58 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 55600 FH FAA AD  CIRCUMFERENTIAL JOINT FRAME 58 FROM STRINGER 12 LH I: 12000 FC 2007-04-11  TO STRINGER 12 RH INTERNAL. OR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536707-0604-2 * * * * * C O N T I N U E * * * * *  16600 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536707-01-2  ACCESS: 843  536707-0604-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 58 MEC DET T: 34000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 78800 FH FAA AD  CIRCUMFERENTIAL JOINT FRAME 58 FROM STRINGER 12 LH I: 10500 FC 2007-04-11  TO STRINGER 12 RH INTERNAL. OR  24300 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536707-01-3  ACCESS: 843  536708-0604-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 65 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 45600 FH FAA AD  AT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11  LH/RH INTERNAL OR  13600 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536708-01-1  ACCESS: 843  536708-0604-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 65 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 55600 FH FAA AD  AT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11  LH/RH INTERNAL OR  16600 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536708-01-2  ACCESS: 843  536708-0604-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 65 MEC DET T: 34000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 78800 FH FAA AD  AT FRAME 65 FROM STRINGER 12 TO CROWN CENTER LINE I: 10500 FC 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 24300 FH 536708-01-3  ACCESS: REMOVE LINING AND INSULATION  ACCESS: 843  536709-0604-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 45600 FH FAA AD  AT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11  LH/RH INTERNAL OR  13600 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536709-01-1  ACCESS: 834  536709-0604-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 55600 FH FAA AD  AT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE I: 12000 FC 2007-04-11  LH/RH INTERNAL OR  16600 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536709-01-2  ACCESS: 834  536709-0604-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 34000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF STRINGER COUPLINGS AT 78800 FH FAA AD  AT FRAME 72 FROM STRINGER 12 TO CROWN CENTER LINE I: 10500 FC 2007-04-11  LH/RH INTERNAL OR  24300 FH ALI REFERENC ACCESS: REMOVE LINING AND INSULATION 536709-01-3  ACCESS: 834  536710-0602-1 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF SKIN IN AREA OF STRINGER 45600 FH  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  CROWN CENTER LINE LH/RH. OR 2007-04-11  20500 FH  ALI REFERENC 536710-01-1  536710-0602-2 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 40000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF SKIN IN AREA OF STRINGER 55600 FH FAA AD  COUPLING RUN OUT AT FRAME 72 FROM STRINGER 12 TO I: 18000 FC 2007-04-11  CROWN CENTER LINE LH/RH. OR  25000 FH ALI REFERENC 536710-01-2  536710-0602-3 253 FUSELAGE INTERNAL STRUCTURE FRAME 72 MEC DET T: 34000 FC ALI EASA AD  254 OR 2006-0071  DETAILED INSPECTION OF SKIN IN AREA OF STRINGER 78800 FH FAA AD  COUPLING RUN OUT AT FRAME 72 FROM STRINGER 12 TO I: 15000 FC 2007-04-11  CROWN CENTER LINE LH/RH. OR  34800 FH ALI REFERENC 536710-01-3  536711-0606-1 152 AFT CARGO COMPARTMENT DOOR LOOK MEC DET T: 48000 FC ALI EASA AD  154 STRUCTURE I: 10000 FC 2006-0071  FAA AD  DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR 2007-04-11  LOCK FITTINGS, BUSHES, ECCENTRIC BOLTS AND  SURROUNDING STRUCTURE FROM FRAME 60 TO FRAME 63 AND ALI REFERENC FROM STRINGER 44 RH TO STRINGER 46 RH. 536711-01-1  PREP.: ECCENTRIC BOLTS TO BE REMOVED  ACCESS: 812  536711-0606-2 152 AFT CARGO COMPARTMENT DOOR LOOK MEC DET T: 40000 FC ALI EASA AD  154 STRUCTURE I: 10000 FC 2006-0071  FAA AD  DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR 2007-04-11  LOCK FITTINGS, BUSHES, ECCENTRIC BOLTS AND  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC FROM STRINGER 44 RH TO STRINGER 46 RH. 536711-01-2  PREP.: ECCENTRIC BOLTS TO BE REMOVED  ACCESS: 812  536711-0606-3 152 AFT CARGO COMPARTMENT DOOR LOOK MEC DET T: 34000 FC ALI EASA AD  154 STRUCTURE I: 10000 FC 2006-0071  FAA AD  DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR 2007-04-11  LOCK FITTINGS, BUSHES, ECCENTRIC BOLTS AND  SURROUNDING STRUCTURE FROM FRAME 60 TO FRAME 63 AND ALI REFERENC FROM STRINGER 44 RH TO STRINGER 46 RH. 536711-01-3  PREP.: ECCENTRIC BOLTS TO BE REMOVED  ACCESS: 812  536801-0606-1 253 SPLICE PLATE AT FRAME 72 NDT SDI T: SEE SB ALI NTM 533021  254 I: SEE SB PART 4  SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT NTM 533021  CIRCUMFERENTIAL SKIN SPLICE AT FRAME 72 FROM STRINGER PART 6  4 TO STRINGER 12 LH/RH. CN 2006-0071 FAA AD 96-13 PREP.: HATRACKS, LINING AND INSULATION AND BOLT SB 53-0262  REMOVAL  ALI REFERENC 536801-01-1  536901-0606-1 311 FUSELAGE TAIL SECTION NDT SDI T: 20200 FC ALI NTM 531900  312 I: 7700 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071 STABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13 STRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256  BETWEEN STRINGER 24 AND STRINGER 27 LH/RH.  ALI REFERENC NOTE: AREA 3 INSPECTION AND COLDWORKING 536901-01-1  PREP.: FOR ACCESS SEE SB  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536901-0606-2 311 FUSELAGE TAIL SECTION NDT SDI T: 54000 FC ALI NTM 531900  312 I: 3800 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071 STABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13 STRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256  BETWEEN STRINGER 24 AND STRINGER 27 LH/RH.  ALI REFERENC NOTE: AREA 3 AFTER COLDWORKING PROCESS 536901-02-1  PREP.: FOR ACCESS SEE SB  536901-0606-3 311 FUSELAGE TAIL SECTION NDT SDI T: 52000 FC ALI NTM 531900  312 I: 3800 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071 STABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13 STRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256  BETWEEN STRINGER 24 AND STRINGER 27 LH/RH.  ALI REFERENC NOTE: AREA 3 INSPECTION AND COLDWORKING 536901-02-2  PREP.: FOR ACCESS SEE SB  536901-0606-5 311 FUSELAGE TAIL SECTION NDT SDI T: 43000 FC ALI NTM 531900  312 I: 3800 FC CN PART 6  SPECIAL DETAILED INSPECTION OF LOWER HORIZONTAL FAA AD CN 2006-0071 STABILIZER CUT OUT LONGERONS, CORNER FITTINGS, SKIN FAA AD 96-13 STRAP AND SKIN BETWEEN FRAME 87 AND FRAME 89 AND SB 53-0256  BETWEEN STRINGER 24 AND STRINGER 27 LH/RH.  ALI REFERENC NOTE: AREA 3 AFTER COLDWORKING PROCESS 536901-02-3  PREP.: FOR ACCESS SEE SB  ACCESS: 312AR  536902-0606-1 311 FUSELAGE TAIL SECTION NDT SDI T: 24000 FC ALI NTM 531900  312 I: 12000 FC PART 4  SPECIAL DETAILED INSPECTION (US) OF OF FUSELAGE EASA AD  HORIZONTAL STABILIZER ATTACH FITTINGS LH/RH AND THE 2006-0071  UPPER AND LOWER FRAME LUGS OF FRAME 91 LH/RH. FAA AD  2007-04-11  ACCESS: 313AL SB 53-0258  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 536902-0606-1 * * * * * C O N T I N U E * * * * *  ALI REFERENC 536902-01-1  536903-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD  312 I: 6600 FC 2006-0071  DETAILED INSPECTION OF LONGITUDINAL BRACE EXTERNAL FAA AD  SURFACE IN CORNER AREAS OF VERTICAL STABILIZER 2007-04-11  ATTACHMENT FITTING CUT OUTS AT FRAME 81/82,  FRAME 84/85 AND FRAME 86/87 LH/RH. ALI REFERENC 536903-01-1  ACCESS: 311AZ 311BZ 323AL 323BL  323AR 323BR  536903-0604-2 311 FUSELAGE TAIL SECTION MEC DET T: 40000 FC ALI EASA AD  312 I: 6600 FC 2006-0071  DETAILED INSPECTION OF LONGITUDINAL BRACE EXTERNAL FAA AD  SURFACE IN CORNER AREAS OF VERTICAL STABILIZER 2007-04-11  ATTACHMENT FITTING CUT OUTS AT FRAME 81/82,  FRAME 84/85 AND FRAME 86/87 LH/RH. ALI REFERENC 536903-01-2  ACCESS: 311AZ 311BZ 323AL 323BL  323AR 323BR  536903-0604-3 311 FUSELAGE TAIL SECTION MEC DET T: 34000 FC ALI EASA AD  312 I: 6600 FC 2006-0071  DETAILED INSPECTION OF LONGITUDINAL BRACE EXTERNAL FAA AD  SURFACE IN CORNER AREAS OF VERTICAL STABILIZER 2007-04-11  ATTACHMENT FITTING CUT OUTS AT FRAME 81/82,  FRAME 84/85 AND FRAME 86/87 LH/RH. ALI REFERENC 536903-01-3  ACCESS: 311AZ 311BZ 323AL 323BL  323AR 323BR  536905-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD  312 I: 6000 FC 2006-0071  DETAILED INSPECTION OF INTERNAL STRUCTURE AT FIN TO FAA AD  FUSELAGE FORWARD, MID AND AFT ATTACH FITTINGS IN 2007-04-11  RIVETING AREA OF SKIN TO LONGITUDINAL BRACE AND OF  LONGITUDINAL BRACE OF VERTICAL STABILIZER ATTACH ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 536905-01-1  AND STRINGER 6 LH/RH TO CROWN CENTERLINE.  ACCESS: 312AR  536905-0604-2 311 FUSELAGE TAIL SECTION MEC DET T: 40000 FC ALI EASA AD  312 I: 6000 FC 2006-0071  DETAILED INSPECTION OF INTERNAL STRUCTURE AT FIN TO FAA AD  FUSELAGE FORWARD, MID AND AFT ATTACH FITTINGS IN 2007-04-11  RIVETING AREA OF SKIN TO LONGITUDINAL BRACE AND OF  LONGITUDINAL BRACE OF VERTICAL STABILIZER ATTACH ALI REFERENC FITTINGS FRAME 81/82, FRAME 84/85, FRAME 86/87 536905-01-2  AND STRINGER 6 LH/RH TO CROWN CENTERLINE.  ACCESS: 312AR  536905-0604-3 311 FUSELAGE TAIL SECTION MEC DET T: 34000 FC ALI EASA AD  312 I: 6000 FC 2006-0071  DETAILED INSPECTION OF INTERNAL STRUCTURE AT FIN TO FAA AD  FUSELAGE FORWARD, MID AND AFT ATTACH FITTINGS IN 2007-04-11  RIVETING AREA OF SKIN TO LONGITUDINAL BRACE AND OF  LONGITUDINAL BRACE OF VERTICAL STABILIZER ATTACH ALI REFERENC FITTINGS FRAME 81/82, FRAME 84/85, FRAME 86/87 536905-01-3  AND STRINGER 6 LH/RH TO CROWN CENTERLINE.  ACCESS: 312AR  538001-0603-1 145 FUSELAGE OVERWING PANELS MEC GVI T: 5 YE CPCP MRB REFERENC 146 I: 5 YE 538001-C603- GENERAL VISUAL INSPECTION OF FUSELAGE OVERWING PANELS  BETWEEN 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 G3  TO BE APPLIED UNDER FAIRING ONLY.  PREP.: FAIRING TO BE REMOVED  ACCESS: 577AB 577AT 577BB 577BT 577CT 577DT  577ET 577GT  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 538001-0603-1 * * * * * C O N T I N U E * * * * *  677AB 677AT 677BB 677BT 677CT 677DT  677ET 677GT  538011-0602-1 100 LOWER FUSELAGE-LONGT.JOINTS MEC DET T: 5 YE CPCP MRB REFERENC I: 30 MO 538011-C602- DETAILED INSPECTION OF EXTERNAL SURFACE OF  LONGITUDINAL JOINTS, FROM FRAME 18 TO FRAME 72, BELOW  PASSENGER FLOOR LEVEL (STRINGER 26) TO STRINGER  33 LH/RH.  NOTE: THIS TASK IS APPLICABLE IN THOSE AREAS  NOT COVERED BY SB 53-0178.  538013-0602-1 137 KRUEGER SLOT FLAP CUT-OUT DOUBLER MEC DET I: 5 YE CPCP MRB REFERENC 138 538013-C602- 513 DETAILED INSPECTION OF KRUEGER SLOT FLAP  613 CUTOUT DOUBLER EXTERNAL SURFACE, AS FAR AS VISIBLE.  538014-0603-1 513 KRUEGER FLAP MEC DET I: 5 YE CPCP MRB REFERENC 613 538014-C603- DETAILED INSPECTION OF KRUEGER FLAP INTERNAL  SUPPORT STRUCTURE.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2  OR G3 AFTER INSPECTION  PREP.: KRUEGER FLAP EXTENDED  538015-0603-1 513 FUS.STRUCT. UNDER WING ROOT FAIRING MEC DET I: 5 YE CPCP ISB 53-0328  613 ISB  DETAILED INSPECTION OF FUSELAGE STRUCTURE MRB REFERENC BETWEEN FRAME 38 AND FRAME 40 UNDER WING ROOT FAIRING 538015-C603- NOTE 1. FOR PRE MOD 04201 A/C (PRE MSN 255), ISB  53-0238 IS ALSO APPLICABLE  2. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 512BB 513BB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

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SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 538015-0603-1 * * * * * C O N T I N U E * * * * *  612BB 613BB  538015-0603-2 513 FUS.STRUCT. UNDER WING ROOT FAIRING MEC DET I: 5 YE CPCP ISB 53-0328  613 ISB  DETAILED INSPECTION OF FUSELAGE STRUCTURE MRB REFERENC BETWEEN FRAME 38 AND FRAME 40 UNDER WING ROOT FAIRING 538015-C603- NOTE: 1. FOR PRE MOD 04201 A/C (PRE MSN 255), ISB  53-0328 IS ALSO APPLICABLE  2. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  PREP.: KRUEGER FLAP EXTENDED, VERTICAL SCREWED  PROTECTIVE PANEL (COVER PLATE) REMOVED.  ACCESS: 513AB  613AB  538021-0602-1 100 LOWER FUSELAGE-CIRCUMFERENTIAL JOINTS MEC DET T: 5 YE CPCP MRB REFERENC I: 30 MO 538021-C602- DETAILED INSPECTION OF CIRCUMFERENTIAL JOINTS  FROM FRAME 18 TO FRAME 72, BETWEEN FLOOR LEVEL  (STRINGER 26) AND STRINGER 33, L/H WITHOUT FAIRING  REMOVAL.  NOTE: THIS TASK IS APPLICABLE IN THOSE AREAS  NOT COVERED BY SB 53-0178.  538031-0603-1 171 TAIL BUMPER CAVITY MEC DET I: 5 YE CPCP SIL 53-041  DETAILED INSPECTION OF TAIL BUMPER CAVITY MRB REFERENC BETWEEN FRAME 74 AND FRAME 79. 538031-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 171BL  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 538050-0603-1 110 FWD PRESSURE BULKHEAD MEC DET I: 9 YE CPCP AMM SSI 5311 MRB S  DETAILED INSPECTION OF FORWARD FACE OF FORWARD MRB REFERENC PRESSURE BULKHEAD (FRAME 1).  538050-C602- NOTE: SHIELD TO BE REMOVED  ACCESS: 110AL  538051-0602-1 100 LWR.FUSELAGE DOOR CUT-OUTS MEC DET T: 5 YE CPCP AMM SSI 5313 I: 30 MO MRB S AMM SSI 5313 DETAILED INSPECTION OF EXTERNAL SURROUNDINGS AMM SSI 5313 OF CARGO, SERVICING AND ACCESS DOOR CUT-OUTS (25 AMM SSI 5314 CM/10 INCHES AROUND CUT-OUT), INCLUDING CARGO DOOR AMM SSI 5331 EDGES AND SKIN PANEL AROUND GLIDE ANTENNA CUT-OUT. AMM SSI 5331 AMM SSI 5333 NOTE: ACCESS PANEL 134BR AS APPLICABLE AMM SSI 5334 AMM SSI 5338 ACCESS: 121AL 121BL 121CL 121DL 122AR 122BR AMM SSI 5338 122CR 132BR 134AR 134BR 135AL 135BL  136AR 136BR 152AR 171AL 172AR 172BR MRB REFERENC 811 812 813  538051-C602- 538052-0603-1 100 NLG BAY, SURROUND PANELS MEC DET T: 5 YE CPCP AMM SSI 5332 123 I: 30 MO MRB S  124 DETAILED INSPECTION OF EXTERNAL AND INTERNAL MRB REFERENC SKIN PANELS, SURROUNDING NOSE LANDING GEAR BAY CUTOUT  (25 CM/10 INCHES AROUND CUT-OUT). 538052-C603- ACCESS: 713  134AR 136AR 714  538053-0603-1 100 MLG BAY, SURROUND PANELS MEC DET T: 5 YE CPCP MRB REFERENC 147 I: 30 MO 538053-C603- 148 DETAILED INSPECTION OF EXTERNAL SKIN PANELS,  SURROUNDING MAIN LANDING GEAR BAY CUTOUT  (25 CM/10 INCHES AROUND CUT-OUT).  ACCESS: 734  744  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 538071-0602-1 100 CUT-OUT OF AIR COND. SYSTEM DOOR MEC DET T: 5 YE CPCP MRB REFERENC I: 30 MO 538071-C602- DETAILED INSPECTION OF EXTERNAL SURROUNDINGS  (25CM/10 INCHES AROUND FAIRING EDGES) OF AIR  CONDITIONING SYSTEM DOOR  ACCESS: 134AR 136AR  538081-0602-1 100 LOWER FUSELAGE-LONGITUDINAL JOINTS MEC DET T: 5 YE CPCP MRB REFERENC I: 30 MO 538081-C602- DETAILED INSPECTION OF LONGITUDINAL JOINT  BELOW STRINGER 33 LH/RH, BETWEEN FRAME 18 AND FRAME  72 WITHOUT FAIRING REMOVAL, EXTERNAL SURFACE.  NOTE: THIS TASK IS APPLICABLE IN THOSE AREAS NOT  COVERED BY SB 53-0178.  538091-0602-1 100 LOWER FUSELAGE-CIRCUMFERENTIAL JOINTS MEC DET T: 5 YE CPCP MRB REFERENC I: 30 MO 538091-C602- DETAILED INSPECTION OF CIRCUMFERENTIAL JOINTS  BELOW STRINGER 33 LH/RH, BETWEEN FRAME 18 AND FRAME  72 WITHOUT FAIRING REMOVAL, EXTERNAL SURFACE.  NOTE: THIS TASK IS ONLY APPLICABLE IN THOSE  AREAS NOT COVERED BY SB 53-0178  538102-0603-1 121 WASTE/WATER CONNECTION BOX MEC GVI T: 5 YE CPCP MRB REFERENC I: 30 MO 538102-C603- VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTURE  AROUND WASTE WATER CONNECTION BOX BETWEEN FRAME 12  AND FRAME 12A FROM STRINGER 37 TO AVIONICS  COMPARTMENT FLOOR LEVEL, LH.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 131AZ  538111-0603-1 121 FUSELAGE INTERNAL STRUCTURE MEC DET I: 5 YE CPCP AMM SSI 5332 122 MRB S  DETAILED INSPECTION OF FUSELAGE INTERNAL  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 538111-0603-1 * * * * * C O N T I N U E * * * * *  STRUCTURE BELOW PASSENGER DOORS BETWEEN FRAME 11 AND  FRAME 20, AND BELOW GALLEY AND TOILET AREAS FROM 538111-C603- CABIN FLOOR LEVEL TO AVIONIC COMPARTMENT FLOOR PANELS  NOTE 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 INSPECT  THE STRUCTURE WITHOUT REMOVAL OF ELECTRICAL  DEVICE.  ACCESS: 131AZ  132AZ  538121-0603-1 121 BILGE AREAS MEC DET T: 5 YE CPCP SIL 53-061  122 I: 30 MO  DETAILED INSPECTION OF BILGE AREA UNDERNEATH MRB REFERENC AVIONIC COMPARTMENT FLOOR PANELS FROM FRAME 1 TO 538121-C603- FRAME 20.  NOTE: 01. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  NOTE: 02. IMPROVE DRAINAGE IN ACCORDANCE WITH  SB 53-0234 IS RECOMMENDED.  NOTE: 03. IMPROVE CORROSION RESISTANCE ON STRINGER 44  AT FRAME 17 IS RECOMMENDED IN ACCORDANCE  WITH SIL 53-061 IN BILGE AREA.  NOTE: 04. INSULATION TO BE REMOVED.  ACCESS: 121CF 121DF 121EF 121FF 121GF 121HF  121JF 121KF 121LF 121MF 121NF 121PF  121QF 121TF 121UF 121VF 121WF 121YF  121ZF  122AF 122BF 122CF 122DF 122EF 122GF  122HF 122JF 122KF 122LF 122MF 122NF  122PF 122QF  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 538153-0602-1 131 UPPER FUSELAGE - UDC DOOR CUT OUT MEC DET I: 5 YE CPCP MRB REFERENC 231 538153-C602- 233 DETAILED INSPECTION OF UPPER (MAIN) DECK CARGO  DOOR SURROUNDING PANELS (25 CM/10 IN. AROUND CUT OUT)  AND CUT OUT EDGES.  NOTE: WHEN DOOR MECHANISM NOT FITTED, CUT OUT EDGE  INSPECTED AS FAR AS VISIBLE.  ACCESS: 835  538161-0602-1 200 CABIN WINDOW FRAMES MEC DET I: 5 YE CPCP MRB REFERENC 538161-C602- DETAILED INSPECTION OF VISIBLE PART OF  PASSENGER WINDOW FORGINGS BETWEEN FRAME 18 AND FRAME  77, EXTERNAL SURFACE.  538171-0602-1 210 COCKPIT WINDOW FRAMES MEC DET I: 5 YE CPCP AMM SSI 5311 MRB S AMM SSI 5311 DETAILED INSPECTION OF EXTERNAL SURFACE OF  COCKPIT WINDOW SURROUNDINGS. MRB REFERENC 538171-C602- 538173-0603-1 123 NLG BAY MEC GVI I: 5 YE CPCP AMM SSI 5312 124 MRB S AMM SSI 5312 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY AMM SSI 5312 INCLUDING NOSE LANDING GEAR DOOR HINGES. AMM SSI 5312 AMM SSI 5312 NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION MRB REFERENC ACCESS: 713 538173-C603- 714  538233-0603-1 131 STRUCTURE BELOW MID PAX DOOR MEC GVI I: 5 YE CPCP MRB REFERENC 132 538233-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL  STRUCTURE BELOW MID PASSENGER/CREW DOOR BETWEEN FRAME  27 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: 
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A300 MAINTENANCE PLANNING D

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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  538235-0603-1 131 STRUCTURE BELOW UDC DOOR MEC GVI I: 5 YE CPCP MRB REFERENC 538235-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL  STRUCTURE BELOW UPPER DECK CARGO DOOR, BETWEEN FRAME  19 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  538245-0603-1 132 FWD CARGO COMP DOOR CUTOUT MEC GVI T: 9 YE CPCP MRB REFERENC I: 5 YE 538245-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL  STRUCTURE AROUND FORWARD CARGO COMPARTMENT DOOR  CUT-OUT FROM FRAME 19 TO FRAME 26, AND BETWEEN  STRINGER 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 INSPECTION  ACCESS: 811  538265-0603-1 132 FWD CARGO COMP DOOR FRAMES MEC GVI T: 5 YE CPCP MRB REFERENC 134 I: 30 MO 538265-C603- GENERAL VISUAL INSPECTION OF FUSELAGE FORWARD CARGO  COMPARTMENT 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: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 538265-0603-1 * * * * * C O N T I N U E * * * * *  FRAMES 20A AND 25A (24B FOR 96 INCHES CARGO  COMPARTMENT DOORS), FROM STRINGER 36RH TO ATTACHMENT  TO SILL BEAM, SILL BEAM UPPER FLANGE AS FAR AS  VISIBLE AND SILL BEAM STRUCTURE INCLUDING LOCK  FITTINGS.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 811  538295-0603-1 135 FRAMES 39 AND 54 MEC DET I: 5 YE CPCP MRB REFERENC 136 538295-C603- 153 DETAILED INSPECTION OF FRAME 39 AND FRAME 54  154 BELOW CARGO FLOOR LEVEL.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 137ALF 137AMF  138PF 138QF 811  151AF 151BF 151CF  152AF 152BF 812  538295-0603-2 135 FRAMES 39 AND 54 MEC DET I: 4 YE ISB CN 2003-317( 136 FAA AD  153 DETAILED INSPECTION OF FRAME 39 AND FRAME 54 2005-15-09  154 BELOW CARGO FLOOR LEVEL. ISB 53-0286  NOTE 1: INSULATION TO BE REMOVED.  ACCESS: 137ALF 137AMF  138PF 138QF 811  151AF 151BF 151CF  152AF 152BF 812  538325-0603-1 120 FUSELAGE - DRAIN VALVES MEC DET I: 5 YE CPCP MRB REFERENC 130 538325-C603- 140 DETAILED INSPECTION OF FUSELAGE INTERNAL  150 STRUCTURE AROUND DRAIN VALVES AND DRAIN PLUGS AT  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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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.  170  PREP.: REMOVE/INSTALL INSULATIONS, CARGO FLOOR  PANELS AND BALLMATS.  ACCESS: 811  812  538435-0603-1 143 AIR CONDITIONING COMPARTM. MEC DET I: 5 YE CPCP AMM SSI 5315 144 MRB S  DETAILED INSPECTION OF AFT FACE AT PRESSURE MRB REFERENC BULKHEAD INCLUDING FRAME 39 AND 25 CM OF SKIN.  538435-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 147GZ 147HZ  148GZ 148HZ  538537-0603-1 143 KEEL BEAM INTERNAL STRUCTURE MEC DET I: 5 YE CPCP AMM SSI 5305 144 MRB S  147 DETAILED INSPECTION OF KEEL BEAM INTERNAL MRB REFERENC 148 STRUCTURE.  538537-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 143AF 143BF 143CF 143DF  147AF 147BF 147CF 147FZ 147GZ 733  148AF 148GZ 734  538547-0603-1 147 MLG FUSELAGE CUTOUT MEC DET I: 5 YE CPCP AMM SSI 5335 148 MRB S AMM SSI 5335 DETAILED INSPECTION OF MAIN LANDING GEAR  FUSELAGE CUTOUT SURROUNDING, INTERNAL AND EXTERNAL MRB REFERENC SURFACE.(25 CM/10 INCHES AROUND CUT-OUT)  538547-C603- ACCESS: 734  744  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

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THRESHOLD (T) 

INTERVAL (I)

 538553-0603-1 152 AFT CARGO COMPT.DOOR CUTOUT MEC GVI T: 9 YE CPCP MRB REFERENC I: 5 YE 538553-C603- GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT  DOOR CUT-OUT FROM FRAME 59 TO FRAME 64 BETWEEN  STRINGER 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 INSPECTION  ACCESS: 812  538555-0603-1 151 CABIN FLOOR STRUCTURE MEC GVI T: 5 YE CPCP MRB REFERENC 152 I: 30 MO 538555-C603- GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE  BELOW TOILETS (IF FITTED), BETWEEN FRAME 54C AND  FRAME 60.  NOTE 01: CEILING PANELS IN GALLEY/TOILET AREA  TO BE REMOVED.  NOTE 02: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1  AND TYPE 2 AFTER INSPECTION  NOTE 03: THIS TASK MAY BE COMBINED WITH CORROSION  INSPECTION 531610-C603-1 AND 531620-C603-1  ACCESS: 812  538557-0603-1 152 AFT CARGO COMPT.DOOR FRAMES MEC GVI T: 5 YE CPCP AMM SSI 5317 154 I: 30 MO MRB S  GENERAL VISUAL INSPECTION OF FUSELAGE AFT CARGO MRB REFERENC COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL  FRAMES (FRAME 59A AND FRAME 63A) FROM STR 36RH TO 538557-C603- ATTACHMENT TO SILL BEAM, SILL BEAM UPPER FLANGE AS  FAR AS VISIBLE AND SILL BEAM STRUCTURE INCLUDING  LOCK FITTINGS.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 812  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 538587-0603-1 162 BULK CARGO COMP.DOOR CUTOUT MEC DET I: 5 YE CPCP MRB REFERENC 538587-C603- DETAILED INSPECTION OF INTERNAL STRUCTURE  AROUND BULK CARGO COMPARTMENT DOOR CUTOUT FROM FRAME  66 TO FRAME 70 BETWEEN STRINGER 32RH AND CARGO FLOOR  LEVEL.  NOTE 01: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  NOTE 02: SIDE LINING, INSULATION TO BE REMOVED.  ACCESS: 813  538589-0603-1 162 BULK CARGO COMP.DOOR FRAMES MEC GVI T: 5 YE CPCP SIL 53-030  I: 30 MO  GENERAL VISUAL INSPECTION OF REAR (BULK) CARGO MRB REFERENC COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL 538589-C603- FRAMES (FRAME 67 AND FRAME 69) FROM STRINGER 41RH TO  ATTACHMENT TO SILL BEAM AND SILL BEAM AS FAR AS  VISIBLE.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 813  538592-0603-1 162 BULK CARGO COMPARTMENT DOOR FRAMES NDT SDI I: 10 YE EUAD NTM 513108  ISB PART 1  SPECIAL DETAILED INSPECTION OF BULK CARGO COMPARTMENT EUAD  DOOR AREA AT FRAME 67 BETWEEN STRINGER 33 AND 200-262-313( STRINGER 48 AND AT FRAME 69 BETWEEN STRINGER 33 AND ISB 53-0339  STRINGER 47.  NOTE: SIDE LININGS, INSULATION TO BE REMOVED.  ACCESS: 813  538593-0603-1 162 BULK CARGO COMP. DOOR SILL BEAM MEC DET T: 5 YE CPCP MRB REFERENC I: 30 MO 538593-C603- DETAILED INSPECTION OF REAR (BULK) CARGO DOOR  SILL 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: 
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A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

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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 REMOVED  NOTE 02: FLOOR PANELS, INSULATION TO BE REMOVED  NOTE 03: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 813  538617-0603-1 171 AFT CABIN - FLOOR STRUCTURE MEC DET T: 5 YE CPCP MRB REFERENC 172 I: 30 MO 538617-C603- DETAILED INSPECTION OF FUSELAGE INTERNAL  STRUCTURE BELOW GALLEY AND TOILETS AND DRAINAGE HOLES  IN FRAME 80.  NOTE 01: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1  AND TYPE 2 AFTER INSPECTION  NOTE 02: ENSURE DRAIN HOLES ARE FREE FROM ANY  OBSTRUCTIONS (TASK 513000-0502-3).  ACCESS: 162AZ  538679-0603-1 231 STRUCTURE AROUND UDC DOOR MEC DET T: 9 YE CPCP MRB REFERENC I: 5 YE 538679-C603- DETAILED INSPECTION OF INTERNAL STRUCTURE  AROUND UPPER (MAIN) DECK CARGO DOOR ABOVE CABIN FLOOR  LEVEL UP TO STRINGER 15 LH, BETWEEN FRAME 19 AND  FRAME 28.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  PREP.: SIDE PANELS, DOOR FRAME PANELS AND INSULATION  TO BE REMOVED.  538691-0603-1 233 STRUCTURE AROUND UDC DOOR MEC DET T: 9 YE CPCP MRB REFERENC I: 5 YE 538691-C603- * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 538691-0603-1 * * * * * C O N T I N U E * * * * *  DETAILED INSPECTION OF INTERNAL STRUCTURE  AROUND UPPER (MAIN) DECK CARGO DOOR ABOVE STRINGER 15  UP TO STRINGER 3 LH, BETWEEN FRAME 19 AND FRAME 28.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTON  PREP.: SIDE PANELS, DOOR FRAME PANELS AND INSULATION  TO BE REMOVED.  538693-0603-1 230 UDC DOOR FRAMES MEC DET I: 5 YE CPCP MRB REFERENC 538693-C603- DETAILED INSPECTION OF FUSELAGE DOOR FRAMES  LOWER PORTION (50 CM/20 INCHES), APERTURE FACE OF  UPPER (MAIN) DECK CARGO DOOR.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 835  538709-0603-1 221 FUSELAGE - DOOR FRAMES MEC DET T: 5 YE CPCP SIL 53-030  222 I: 30 MO  231 DETAILED INSPECTION OF FUSELAGE DOOR CUT-OUT, MRB REFERENC 232 LOWER PORTION OF LATERAL FRAMES (50CM / 20 INCHES 538709-C603- 251 ABOVE FLOOR LEVEL) OF FORWARD, MID, AFT PAX/CREW  252 DOORS AND EMERGENCY EXITS.  261  262 NOTE 01: LOWER DOOR FRAME PANELS TO BE REMOVED  NOTE 02: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 831  841  832  842  834  844  833  843  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 538769-0603-1 311 FRAME 91 MEC DET T: 9 YE CPCP MRB REFERENC 312 I: 5 YE 538769-C603- DETAILED INSPECTION OF THE ASSEMBLY CROWN TO  BOTTOM CENTER LINE INCLUDING FRAME 91 TAIL CONE  ATTACHMENT FITTINGS.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 313AL  538779-0603-1 311 HORIZONTAL TAIL PLANE CUT-OUT MEC DET T: 9 YE CPCP AMM SSI 5319 312 I: 5 YE MRB S AMM SSI 5319 DETAILED INSPECTION OF HORIZONTAL TAIL PLANE NTM 531900  CUTOUT BETWEEN FRAME 86 AND FRAME 91 INCLUDING CORNER PART 7  FITTINGS AND LONGERONS.  MRB REFERENC NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION 538779-C603- ACCESS: 313AL  312AR  538789-0603-1 311 FUSELAGE TAIL-MACHINED FRAMES MEC DET T: 9 YE CPCP AMM SSI 5319 312 I: 5 YE MRB S AMM SSI 5319 DETAILED INSPECTION OF ALL MACHINED FRAMES AT AMM SSI 5319 UPPER LOBE FROM STRINGER 14 LH/RH TO CROWN CENTER AMM SSI 5319 LINE AND VERTICAL STABILIZER ATTACH FITTINGS AMM SSI 5319 INCLUDING RIVETING OF FITTING TO FRAMES AND LATERAL AMM SSI 5319 FRAMES.  MRB REFERENC NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION 538789-C603- ACCESS: 312AR  538789-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 20000 FC ALI EASA AD  312 I: 11500 FC FAA AD 2006-0071  DETAILED INSPECTION OF MACHINED FRAMES AND SHEARTIES FAA AD  AT UPPER LOBE FROM STRINGER 14 LH/RH TO CROWN CENTER 2007-04-11  LINE AND VERTICAL STABILIZER ATTACH FITTINGS  INCLUDING RIVETING OF FITTING TO FRAMES AND LATERAL ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 538789-0604-1 * * * * * C O N T I N U E * * * * *  FRAMES. 538789-01-1  ACCESS: 312AR  538791-0603-1 311 FUSELAGE TAIL-FRAME BRACING MEC DET T: 9 YE CPCP AMM SSI 5319 312 I: 5 YE MRB S AMM SSI 5319 DETAILED INSPECTION OF FRAME BRACING, BETWEEN AMM SSI 5319 FRAME 81 AND FRAME 82, FRAME 84 AND FRAME 85, FRAME  86 AND FRAME 87. MRB REFERENC NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, 538791-C603- G2 OR G3 AFTER INSPECTION  ACCESS: 312AR  538829-0603-1 315 FUSELAGE - APU COMPARTMENT MEC GVI T: IMPL.AGE CPCP MRB REFERENC 316 15 YE 538829-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL I: 9 YE  STRUCTURE BETWEEN FRAME 95 AND 100.  ACCESS: 313AL 315AL  316AR  538839-0603-1 310 FUSELAGE TAIL-UNDERNEATH FIN FAIRING MEC DET I: 5 YE CPCP AMM SSI 5319 MRB S  DETAILED INSPECTION OF FUSELAGE EXTERNAL MRB REFERENC SURFACE UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO  FUSELAGE ATTACHMENT FITTINGS INCLUDING TRANSVERSE 538839-C603- LOAD FITTINGS.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  EXCLUDING THE CONICAL FIN TO FUSELAGE  ATTACHMENT BOLTS.  ACCESS: 323AL 323AR 323BL 323BR  538839-0604-1 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD  312 OR 2006-0071  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 538839-0604-1 * * * * * C O N T I N U E * * * * *  DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE 54200 FH FAA AD  UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 5200 FC 2007-04-11  FUSELAGE ATTACHMENT FITTINGS. OR  5800 FH ALI REFERENC ACCESS: 323BL 538839-01-1  323BR  538839-0604-2 311 FUSELAGE TAIL SECTION MEC DET T: 48000 FC ALI EASA AD  312 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE 54200 FH FAA AD  UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 5200 FC 2007-04-11  FUSELAGE ATTACHMENT FITTINGS. OR  5800 FH ALI REFERENC ACCESS: 323BL 538839-01-2  323BR  538839-0604-3 311 FUSELAGE TAIL SECTION MEC DET T: 34000 FC ALI EASA AD  312 OR 2006-0071  DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE 75100 FH FAA AD  UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 4000 FC 2007-04-11  FUSELAGE ATTACHMENT FITTINGS. OR  8800 FH ALI REFERENC ACCESS: 323BL 538839-01-3  323BR  539001-0603-1 241 FUSELAGE CENTER SECTION NDT SDI T: 10800 FC CN NTM 513104  242 OR FAA AD PART 1  SPECIAL DETAILED INSPECTION OF STIFFENERS ON THE FR 13900 FH ISB CN  40 I: 2000 FC 1998-028-242 OR FAA AD  ACCESS: OPEN SIDEWALL PANELS AS REQUIRED 2600 FH 2000-20-15  ISB 53-0332  ACCESS: 131CZ  132EZ  539001-0603-2 241 FUSELAGE CENTER SECTION NDT SDI T: 7500 FC CN NTM 513104  242 OR FAA AD PART 1  SPECIAL DETAILED INSPECTION OF STIFFENERS ON THE FR 14600 FH ISB CN  40 I: 1400 FC 1998-028-242 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 539001-0603-2 * * * * * C O N T I N U E * * * * *  OR FAA AD  ACCESS: ACCESS: OPEN SIDEWALL PANELS AS REQUIRED 2800 FH 2000-20-15  ISB 53-0332  ACCESS: 131CZ  132EZ  539001-0603-3 241 FUSELAGE CENTER SECTION NDT SDI T: 7200 FC CN NTM 513104  242 OR FAA AD PART 1  SPECIAL DETAILED INSPECTION OF STIFFENERS ON THE FR 14000 FH CN  40 I: 1400 FC 1998-028-242 OR FAA AD  ACCESS: ACCESS: OPEN SIDEWALL PANELS AS REQUIRED 2800 FH 2000-20-15  SB 53-0332  ACCESS: 131CZ  132EZ  539003-0603-1 148 CENTER SECTION FRAME 39 TO FRAME 54 MEC DET I: 9000 FC ISB ISB 53-0104  DETAILED INSPECTION OF TWO SPOTFACES ON  ATTACHMENT BRACKETS  539005-0603-1 713 NOSE GEAR AFT DOOR NDT SDI T: 4000 FC ISB NTM 515000  714 I: 2000 FC ISB 53-0277  SPECIAL DETAILED INSPECTION OF AFT HINGE BOLT  ASSEMBLY  ACCESS: REMOVE THE NOSE GEAR AFT PANEL AND FLOOR  PANEL AND FLOOR PANELS 121PF, 122JF  539006-0603-1 141 WING CENTER BOX NDT SDI I: ISB ISB NTM 513000  142 53-0287 PART 1  SPECIAL DETAILED INSPECTION OF AREA OF RIB 1 NTM 513010  PART 1  ACCESS: 542CB CN : TBD  642CB ISB 53-0287  539007-0603-2 141 CENTER SECTION NDT SDI I: ISB CN CN  142 53-0296 FAA AD F-1998-481-2 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 539007-0603-2 * * * * * C O N T I N U E * * * * *  SPECIAL DETAILED INSPECTION OF THE AFT FITTING AT FR ISB FAA AD  40. 2002-07-05  ISB 53-0296  ACCESS: 147FZ 147GZ  148GZ  539008-0603-1 121 ELECTRONIC RACK 101VU MEC DET T: 7000 FC CN CN  122 I: 2300 FC FAA AD 1992-253-138 DETAILED INSPECTION OF THE LOWER ATTACHMENT ISB FAA AD 96-12 BEAM. ISB 53-0300  ACCESS: 121BL  539009-0603-1 151 EMERGENCY EXIT NDT SDI T: 18 MO CN NTM 512013  152 I: 18 MO FAA AD PART 1  241 SPECIAL DETAILED INSPECTION OF THE SKIN PANEL ISB NTM 514000  242 PART 1  251 CN  252 1997-357-231 FAA AD 98-20 ISB 53-0301  539010-0603-1 831 DOORS MEC DET T: 10000 FC CN CN  841 I: 600 FC FAA AD 1997-124-223 DETAILED INSPECTION OF THE DOOR STOPS ISB FAA AD 98-20 ISB 53-0309  ACCESS: OPEN THE DOORS  539010-0603-2 831 DOORS MEC DET T: 20000 FC CN CN  841 I: 4500 FC FAA AD 1997-124-223 DETAILED INSPECTION OF THE DOOR STOPS ISB FAA AD 98-20 ISB 53-0309  ACCESS: OPEN THE DOORS  539011-0603-1 251 EMERGENCY EXIT DOOR FRAMES NDT SDI T: 10 YE ISB NTM 533054  252 I: 5 YE PART 6  SPECIAL DETAILED INSPECTION OF EMERGENCY EXIT ISB 53-0311  DOORFRAMES STRUCTURE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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THRESHOLD (T) 

INTERVAL (I)

 539011-0603-1 * * * * * C O N T I N U E * * * * *  ACCESS: REMOVE THE DOORFRAME LININGS, REMOVE THE  INSULATION TO THE INSPECTED AREA  539012-0603-1 147 CENTER SECTION NDT SDI T: 11000 FC ISB NTM 513010  148 I: 2100 FC PART 1  SPECIAL DETAILED INSPECTION OF THE FORWARD CANTED NTM 513105  FRAME PART 6  ISB 53-0314  ACCESS: OPEN THE MAIN LANDING GEAR DOORS R 539013-0603-1 123 NLG BAY NDT SDI T: 10000 FC ISB NTM 513010  124 I: 3400 FC PART 1  SPECIAL DETAILED INSPECTION OF LOWER HOLES OF THE NTM 513104  KEEL BEAM OF NLG BAY CONNECTING FITTING IN NLG BAY PART 1  BETWEEN FR 13 AND FR 14. ISB 53-0327  ACCESS: REMOVE INSULATION AS REQUIRED  ACCESS: 121NF 122HF 713 811  132AZ 714 831  539014-0603-1 131 FUSELAGE MEC DET T: ISB ISB ISB 53-0341  132 53-0341  135 DETAILED INSPECTION OF THE SKIN PANELS AT I: 1400 FC  136 THE LAP JOINT BETWEEN STRINGERS 42 AND 43 AND  137 BETWEEN FRAMES 37 AND 39 LH AND RH CRACKS  138  ACCESS: 131ABF 131AFF  132LF 132NF  137AM  138QF  539015-0603-1 145 CENTER SECTION NDT SDI I: ISB CN NTM 513010  146 53-0350 FAA AD PART 1  241 SPECIAL DETAILED INSPECTION OF HOLES FR 47 SPLICE ISB CN 2002-184( 242 FITTING BETWEEN STRG 24 AND STRG 25 LH AND RH SIDES. FAA AD  2004-20-14  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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 539015-0603-1 * * * * * C O N T I N U E * * * * *  ACCESS: REMOVE THE PASSENGER SEATS, LOWER SIDEWALL ISB 53-0350  PANELS, INSULATION AT FR 47  539016-0603-1 231 FUSELAGE FORWARD SECTION NDT SDI I: 2500 FC ISB NTM 531405  232 PART 4  SPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW CN 2002-639( STRINGER 11 BETWEEN FRAME 28A AND FRAME 31 LH/RH. FAA AD  2000-02-39  ACCESS: REMOVE THE FWD UPPER, CENTER UPPER AND AFT ISB 53-0354  UPPER DOOR-FRAME PANELS  539016-0603-2 231 FUSELAGE FORWARD SECTION NDT SDI I: 6500 FC ISB NTM 531405  232 PART 4  SPECIAL DETAILED INSPECTION OF SKIN LAP JOINT BELOW CN 2002-639( STRINGER 11 BETWEEN FRAME 28A AND FRAME 31 LH/RH. FAA AD  2000-02-39  ACCESS: REMOVE THE FWD UPPER, CENTER UPPER AND AFT ISB 53-0354  UPPER DOOR-FRAME PANELS  539017-0603-1 131 FUSELAGE FORWARD AND AFT INTERMEDIATE NDT SDI T: 30300 FC CN NTM 531406  132 SECTION I: 4100 FC ISB PART 4  153 NTM 531601  154 SPECIAL DETAILED INSPECTION OF SKIN LAP JOINTS BELOW PART 4  STRINGER 27 BETWEEN FRAME 28A AND FRAME 30A LH AND CN 2002-639( RH, AND AT STRINGER 52 BETWEEN FRAME 56 AND FRAME 58 FAA AD  LH AND RH. 2004-08-05  ISB 53-0356  ACCESS: REMOVE THE INSULATION IN THE AREA TO INSPECT.  539017-0603-2 131 FUSELAGE FORWARD AND AFT INTERMEDIATE NDT SDI T: 30300 FC AD NTM 531406  132 SECTION I: 4100 FC CN PART 4  153 ISB NTM 531601  154 SPECIAL DETAILED INSPECTION OF SKIN LAP JOINTS BELOW PART 4  STRINGER 27 BETWEEN FRAME 28A AND FRAME 30A RH, AND AD 2004-08-0 AT STRINGER 52 BETWEEN FRAME 56 AND FRAME 58 LH AND CN 2002-639( RH. ISB 53-0356  ACCESS: REMOVE THE INSULATION IN THE AREA TO INSPECT.  * * * * * E N D * * * * *  STRUCTURE PROGRAM : FUSELAGE REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 540001-0602-1 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 5600 FC MRB S AMM SSI 5400 416  425 DETAILED INSPECTION OF JUNCTION OF RIB NO. 8  426 AND SIDE PANEL.  540001-0602-2 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 4600 FC MRB S AMM SSI 5400 416  425 DETAILED INSPECTION OF JUNCTION OF RIB NO. 8  426 AND SIDE PANEL.  540001-0602-3 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 4400 FC MRB S AMM SSI 5400 416  425 DETAILED INSPECTION OF JUNCTION OF RIB NO. 8  426 AND SIDE PANEL.  540002-0604-1 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 27300 FC MRB S AMM SSI 5400 416  425 DETAILED INSPECTION OF JUNCTION OF RIB NO.8  426 AND SIDE PANEL.  ACCESS: 415AL  416AR  425AL  426AR  540002-0604-2 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 22600 FC MRB S AMM SSI 5400 416  425 DETAILED INSPECTION OF JUNCTION OF RIB NO.8  426 AND SIDE PANEL.  ACCESS: 415AL  416AR  425AL  426AR  540002-0604-3 415 JUNCTION RIB 8 & SIDE PANEL MEC DET I: 19200 FC MRB S AMM SSI 5400 416  425 DETAILED INSPECTION OF JUNCTION OF RIB NO.8  426 AND SIDE PANEL.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 540002-0604-3 * * * * * C O N T I N U E * * * * *  ACCESS: 415AL  416AR  425AL  426AR  540003-0602-1 473 RIB 18 TO SIDE PANEL JUNCT. MEC DET I: 8400 FC MRB S AMM SSI 5400 474  483 DETAILED INSPECTION OF RIB 18 TO SIDE  484 PANEL JUNCTION.  540003-0602-2 473 RIB 18 TO SIDE PANEL JUNCT. MEC DET I: 7000 FC MRB S AMM SSI 5400 474  483 DETAILED INSPECTION OF RIB 18 TO SIDE  484 PANEL JUNCTION.  540003-0602-3 473 RIB 18 TO SIDE PANEL JUNCT. MEC DET I: 6600 FC MRB S AMM SSI 5400 474  483 DETAILED INSPECTION OF RIB 18 TO SIDE  484 PANEL JUNCTION.  540004-0602-1 473 RIB 18 & SIDE PANEL JUNCT. MEC DET I: 5600 FC MRB S AMM SSI 5400 474  483 DETAILED INSPECTION OF JUNCTION OF RIB 18  484 WITH SIDE PANELS.  540004-0602-2 473 RIB 18 & SIDE PANEL JUNCT. MEC DET I: 4600 FC MRB S AMM SSI 5400 474  483 DETAILED INSPECTION OF JUNCTION OF RIB 18  484 WITH SIDE PANELS.  540004-0602-3 473 RIB 18 & SIDE PANEL JUNCT. MEC DET I: 4400 FC MRB S AMM SSI 5400 474  483 DETAILED INSPECTION OF JUNCTION OF RIB 18  484 WITH SIDE PANELS, INCLUDING ZONES 474/484.  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
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A300 MAINTENANCE PLANNING D

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INTERVAL (I)

 540004-0603-1 473 RIB 18 TO SIDE PANEL JUNCTION NDT SDI I: 8400 FC MRB S AMM SSI 5400 474 NTM 541000  483 DETAILED AND SPECIAL DETAILED INSPECTION OF RIB 18 PART 2  484 INCLUDING JUNCTION WITH SIDE PANELS AND UPPER SPAR.  ACCESS: 473AL 473CL  474AR 474CR  483AL 483CL  484AR 484CR  540004-0603-2 473 RIB 18 TO SIDE PANEL JUNCTION NDT SDI I: 7000 FC MRB S AMM SSI 5400 474 NTM 541000  483 DETAILED AND SPECIAL DETAILED INSPECTION OF RIB 18 PART 2  484 INCLUDING JUNCTION WITH SIDE PANELS AND UPPER SPAR.  ACCESS: 473AL 473CL  474AR 474CR  483AL 483CL  484AR 484CR  540004-0603-3 473 RIB 18 TO SIDE PANEL JUNCTION NDT SDI I: 6600 FC MRB S AMM SSI 5400 474 NTM 541000  483 DETAILED AND SPECIAL DETAILED INSPECTION OF RIB 18 PART 2  484 INCLUDING JUNCTION WITH SIDE PANELS AND UPPER SPAR.  ACCESS: 473AL 473CL  474AR 474CR  483AL 483CL  484AR 484CR  540005-0604-1 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 27300 FC MRB S AMM SSI 5400 416 NTM 541000  425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 2  426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.  ACCESS: 413EL 415AL  416AR  423EL 425AL  426AR  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5400 416 NTM 541000  425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 2  426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.  ACCESS: 413EL 415AL  416AR  425AL  426AR  540005-0604-3 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 19200 FC MRB S AMM SSI 5400 416 NTM 541000  425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 2  426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.  ACCESS: 413EL 415AL  416AR  423EL 425AL  426AR  540006-0603-1 470 NACELLES/PYLON RIB 1 TO 18 MEC DET I: 4000 FH ISB CN  480 1990-222-116 DETAILED EXTERNAL AND INTERNAL INSPECTION OF FAA AD 96-08 THE BOLT/NUT ASSEMBLIES DIAMETER 6.35 MM (0.21 IN) ISB 54-0045  BETWEEN RIB 8 AND RIB 18 AND CHECK NUTS FOR TIGHTNESS  NOTE: ENGINE FIRE EXTINGUISHER BOTTLES REMOVED  ACCESS: 413CL 413DL 414CR 414DR 415AL 416AR  471AL 471BL 472AR 472BR 473AL 473BL  473CL 473DL 474BR 474CR 474DR 475AL  475BL 475CL 476AR 476BR  423CL 423DL 424CR 424DR 425AL 426AR  481AL 481BL 482AR 482BR 483BL 483CL  483DL 484AR 484BR 484CR 484DR 485AL  485BL 485CL 486AR 486BR  540006-0604-1 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 27300 FC MRB S AMM SSI 5400 416 NTM 541000  425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 2  426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 540006-0604-1 * * * * * C O N T I N U E * * * * *  ACCESS: 413GL 415AL  416AR  423GL 425AL  426AR  540006-0604-2 415 LOWER SPAR BETWEEN RIB 7/9 MEC SDI I: 22600 FC MRB S AMM SSI 5400 416 NTM 541000  425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 2  426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.  ACCESS: 413GL 415AL  416AR  423GL 425AL  426AR  540006-0604-3 415 LOWER SPAR BETWEEN RIB 7/9 NDT SDI I: 19200 FC MRB S AMM SSI 5400 416 NTM 541000  425 DETAILED AND SPECIAL DETAILED INSPECTION OF LOWER PART 2  426 SPAR CAPS AND WEB BETWEEN RIB 7 AND 9.  ACCESS: 413GL 415AL  416AR  423GL 425AL  426AR  540007-0602-1 473 JUNCTION OF SIDE PANEL MEC DET I: 8400 FC MRB S AMM SSI 5400 474 AMM SSI 5400 483 DETAILED INSPECTION OF SIDE PANEL TO  484 UPPER SPAR JUNCTION BETWEEN RIB 12 AND 18.  540007-0602-2 473 JUNCTION OF SIDE PANEL MEC DET I: 7000 FC MRB S AMM SSI 5400 474 AMM SSI 5400 483 DETAILED INSPECTION OF SIDE PANEL TO  484 UPPER SPAR JUNCTION BETWEEN RIB 12 AND 18.  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5400 474 AMM SSI 5400 483 DETAILED INSPECTION OF SIDE PANEL TO  484 UPPER SPAR JUNCTION BETWEEN RIB 12 AND 18.  540009-0604-1 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 27300 FC MRB S AMM SSI 5400 474 NTM 541000  483 DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  484 SPAR CAPS AND WEB BETWEEN RIB 12 AND 18.  ACCESS: 471BL 473AL 473BL  472BR 474BR  481BL 483BL  482BR 484AR 484BR  540009-0604-2 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 22600 FC MRB S AMM SSI 5400 474 NTM 541000  483 DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  484 SPAR CAPS AND WEB BETWEEN RIB 12 AND 18.  ACCESS: 471BL 473AL 473BL  472BR 474BR  481BL 483BL  482BR 484AR 484BR  540009-0604-3 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 19200 FC MRB S AMM SSI 5400 474 NTM 541000  483 DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  484 SPAR CAPS AND WEB BETWEEN RIB 12 AND 18.  ACCESS: 471BL 473AL 473BL  472BR 474BR  481BL 483BL  482BR 484AR 484BR  540010-0604-1 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 27300 FC MRB S AMM SSI 5400 474 NTM 541000  483 VISUAL AND SPECIAL DETAILED INSPECTION OF UPPER SPAR PART 2  484 CAP AND WEB.BETWEEN RIB 12 AND 18.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 540010-0604-1 * * * * * C O N T I N U E * * * * *  ACCESS: 471BL 473AL 473BL  472BR 474AR 474BR  481BL 483AL 483BL  482BR 484AR 484BR  540010-0604-2 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 22600 FC MRB S AMM SSI 5400 474 NTM 541000  483 VISUAL AND SPECIAL DETAILED INSPECTION OF UPPER SPAR PART 2  484 CAP AND WEB.BETWEEN RIB 12 AND 18.  ACCESS: 471BL 473AL 473BL  472BR 474AR 474BR  481BL 483AL 483BL  482BR 484AR 484BR  540010-0604-3 473 UPPER SPAR BETW. RIB 12-18 NDT SDI I: 19200 FC MRB S AMM SSI 5400 474 NTM 541000  483 VISUAL AND SPECIAL DETAILED INSPECTION OF UPPER SPAR PART 2  484 CAP AND WEB.BETWEEN RIB 12 AND 18.  ACCESS: 471BL 473AL 473BL  472BR 474AR 474BR  481BL 483AL 483BL  482BR 484AR 484BR  540011-0603-2 471 SPIGOT RECEPTACLE FITTING MEC DET T: 7,5 YE ISB AMM SSI 5400 472 I: 5 YE MRB S ISB 54-0076  473 DETAILED INSPECTION OF SPIGOT RECEPTACLE  474 FITTING INCLUDING SPHERICAL BEARING AND BUSH.  481  482 PREP.: SPHERICAL BEARING AND BUSH TO BE REMOVED  483  484  ACCESS: 471AL 471BL  472AR 472BR  473AL  474AR  481AL 481BL  482AR 482BR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 540011-0603-2 * * * * * C O N T I N U E * * * * *  483AL  484AR  540011-0603-3 471 SPIGOT RECEPT. FITTING MEC DET I: 10 YE MRB S AMM SSI 5400 472  473 DETAILED INSPECTION OF SPIGOT RECEPTACLE  474 FITTING INCLUDING SPHERICAL BEARING AND BUSH.  481  482 NOTE: SPHERICAL BEARING AND BUSH TO BE REMOVED  483  484  ACCESS: 471AL 471BL  472AR 472BR  473AL  481AL 481BL  482AR 482BR  484AR  540011-0603-4 471 SPIGOT RECEPTACLE FITTING MEC DET T: 7,5 YE ISB ISB 54-0076  472 I: 7,5 YE  473 DETAILED INSPECTION OF SPIGOT RECEPTACLE  474 FITTING INCLUDING SPHERICAL BEARING AND BUSH.  481  482 PREP.: SPHERICAL BEARING AND BUSH TO BE REMOVED  483  484  ACCESS: 471AL 471BL  472AR 472BR  473AL  474AR  481AL 481BL  482AR 482BR  483AL  484AR  540012-0603-1 413 NACELLES/PYLONS - RIB 8 MEC DET T: 10700 FH ISB ISB 54-0089  414 I: 10700 FH  423 DETAILED INSPECTION OF THE TRUSS BARS AT THE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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.  PREP: -BLEED AIR PRECOOLER AND COLD AIR INLET DUCT  TO BE REMOVED  -HYDRAULIC BRACKETS AT RIB 8 TO BR REMOVED  ACCESS: 413EL  423EL  541001-0604-1 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 27300 FC MRB S AMM SSI 5410 416 NTM 541000  425 SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2  426 AND SIDE PANELS FROM RIB 1 TO 2.  ACCESS: 413EL 451AL  452AR  423EL  461AL 462AR  541001-0604-2 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 22600 FC MRB S AMM SSI 5410 416 NTM 541000  425 SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2  426 AND SIDE PANELS FROM RIB 1 TO 2.  ACCESS: 413EL 451AL  452AR  423EL  461AL 462AR  541001-0604-3 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 19200 FC MRB S AMM SSI 5410 416 NTM 541000  425 SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2  426 AND SIDE PANELS FROM RIB 1 TO 2.  ACCESS: 413EL 451AL  452AR  423EL  461AL 462AR  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5410 425 NTM 541000  SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2  AND SIDE PANELS FROM RIB 1 TO 2 INCLUDING ZONES  416/426  ACCESS: 413GL 451AL 452AR  423GL 461AL 462AR  541002-0604-2 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 22600 FC MRB S AMM SSI 5410 425 NTM 541000  SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2  AND SIDE PANELS FROM RIB 1 TO 2 INCLUDING ZONES  416/426  ACCESS: 413GL 451AL 452AR  423GL 461AL 462AR  541002-0604-3 415 SPAR-SIDE PANEL RIB 1 TO 2 NDT SDI I: 19200 FC MRB S AMM SSI 5410 425 NTM 541000  SPECIAL DETAILED INSPECTION OF JUNCTION BETWEEN SPAR PART 2  AND SIDE PANELS FROM RIB 1 TO 2 INCLUDING ZONES  416/426  ACCESS: 413GL 451AL 452AR  423GL 461AL 462AR  541003-0604-1 415 LUGS PYLON-WING ATTACH MEC SDI I: 27300 FC MRB S AMM SSI 5410 425 NTM 544000  DETAILED AND SPECIAL DETAILED INSPECTION OF PYLON TO PART 4  WING ATTACH FITTING LUGS AT RIB 12, WITH LINKS NTM 544000  REMOVED, INCLUDING ZONES 416 426 473 474 483 484 PART 6  ACCESS: 471AL 472AR  481AL 482AR  541003-0604-2 415 LUGS PYLON-WING ATTACH MEC SDI I: 22600 FC MRB S AMM SSI 5410 425 NTM 544000  DETAILED AND SPECIAL DETAILED INSPECTION OF PYLON TO PART 4  WING ATTACH FITTING LUGS AT RIB 12, WITH LINKS NTM 544000  REMOVED, 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 541003-0604-2 * * * * * C O N T I N U E * * * * *  ACCESS: 471AL 472AR  481AL 482AR  541003-0604-3 471 LUGS PYLON-WING ATTACH MEC SDI I: 19200 FC MRB S AMM SSI 5410 481 NTM 544000  DETAILED AND SPECIAL DETAILED INSPECTION OF PYLON TO PART 4  WING ATTACH FITTING LUGS AT RIB 12, WITH LINKS NTM 544000  REMOVED, INCLUDING ZONES 415 416 425 426 473 474 483 PART 6  484  PREP: ENGINE TO BE REMOVED  ACCESS: 471AL 472AR  481AL 482AR  541005-0604-1 415 RIB 12 & ATTACH FITTING MEC DET I: 27300 FC MRB S AMM SSI 5410 425  DETAILED INSPECTION OF RIB 12 AND PORTION OF  THE WING ATTACHMENT FITTING INSIDE THE PYLON  INCLUDING ZONES 416, 426, 473, 474, 483 AND 484  ACCESS: 415AL 416AR 473AL  425AL 426AR 484AR  541005-0604-2 415 RIB 12 & ATTACH FITTING MEC DET I: 22600 FC MRB S AMM SSI 5410 425  DETAILED INSPECTION OF RIB 12 AND PORTION OF  THE WING ATTACHMENT FITTING INSIDE THE PYLON  INCLUDING ZONES 416, 426, 473, 474, 483 AND 484  ACCESS: 415AL 416AR 473AL  425AL 426AR 484AR  541005-0604-3 415 RIB 12 & ATTACH FITTING MEC DET I: 19200 FC MRB S AMM SSI 5410 425  DETAILED INSPECTION OF RIB 12 AND PORTION OF  THE WING ATTACHMENT FITTING INSIDE THE PYLON  INCLUDING 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 541005-0604-3 * * * * * C O N T I N U E * * * * *  ACCESS: 415AL 416AR 473AL  425AL 426AR 484AR  541007-0604-1 473 LUGS PYLON-WING ATTACH NDT SDI I: 27300 FC MRB S AMM SSI 5410 483 NTM 544000  SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4  FITTING LUG AT RIB 18 INCLUDING ZONES 474 AND 484 NTM 544000  PART 6  ACCESS: 473BL 474BR  483BL 484BR  541007-0604-2 473 LUGS PYLON-WING ATTACH NDT SDI I: 22600 FC MRB S AMM SSI 5410 483 NTM 544000  SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4  FITTING LUG AT RIB 18 INCLUDING ZONES 474 AND 484 NTM 544000  PART 6  ACCESS: 473BL 474BR  483BL 484BR  541007-0604-3 473 LUGS PYLON-WING ATTACH NDT SDI I: 19200 FC MRB S AMM SSI 5410 483 NTM 544000  SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4  FITTING LUG AT RIB 18 INCLUDING ZONES 474 AND 484 NTM 544000  PART 6  ACCESS: 473BL 474BR  483BL 484BR  541008-0603-1 473 LUG PYLON-WING ATTACH NDT SDI I: 8400 FC MRB S AMM SSI 5410 483 NTM 544000  SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4  FITTING LUG AT RIB 18 NTM 544000  PART 6  ACCESS: 473BL 474BR  483BL 484BR  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5410 483 NTM 544000  SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4  FITTING LUG AT RIB 18 NTM 544000  PART 6  ACCESS: 473BL 474BR  483BL 484BR  541008-0603-3 473 LUG PYLON-WING ATTACH NDT SDI I: 6600 FC MRB S AMM SSI 5410 483 NTM 544000  SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACH PART 4  FITTING LUG AT RIB 18 NTM 544000  PART 6  ACCESS: 473BL 474BR  483BL 484BR  541009-0604-1 473 PYLON-WING ATTACH RIB 18 MEC SDI I: 27300 FC MRB S AMM SSI 5410 483 NTM 541000 P SPECIAL DETAILED INSPECTION OF JUNCTION OF PYLON TO 2  WING ATTACHMENT FITTING TO RIB 18 AND SIDE WALLS  INCLUDING ZONES 474/484.  ACCESS: 473AL 473CL 474CR  483CL 484AR 484CR  541009-0604-2 473 PYLON-WING ATTACH RIB 18 MEC SDI I: 22600 FC MRB S AMM SSI 5410 483 NTM 541000 P SPECIAL DETAILED INSPECTION OF JUNCTION OF PYLON TO 2  WING ATTACHMENT FITTING TO RIB 18 AND SIDE WALLS  INCLUDING ZONES 474/484.  541009-0604-3 473 PYLON-WING ATTACH RIB 18 MEC SDI I: 19200 FC MRB S AMM SSI 5410 483 NTM 541000 P SPECIAL DETAILED INSPECTION OF JUNCTION OF PYLON TO 2  WING ATTACHMENT FITTING TO RIB 18 AND SIDE WALLS  INCLUDING ZONES 474/484.  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 541010-0603-1 470 PYLON OUTER LATERAL PANELS NDT SDI T: 30000 FH ISB NTM 544004  480 OR PART 4  SPECIAL DETAILED INSPECTION OF PYLON OUTER LATERAL 15000 FC EASA AD  PANEL BETWEEN RIB 12 AND RIB 18. I: 3000 FH 1990-116(B)  OR FAA AD 96-08 ACCESS: 473AL 15 MO ISB 54-0084  484AR  541011-0604-1 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 27300 FC MRB S AMM SSI 5410 425 NTM 541000  DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  SPAR CAPS AND WEB BETWEEN RIB 8 AND 12, INCLUDING  ZONES 416/426  ACCESS: 415AL 416AR  425AL 426AR  541011-0604-2 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 22600 FC MRB S AMM SSI 5410 425 NTM 541000  DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  SPAR CAPS AND WEB BETWEEN RIB 8 AND 12, INCLUDING  ZONES 416/426  ACCESS: 415AL 416AR  425AL 426AR  541011-0604-3 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 19200 FC MRB S AMM SSI 5410 425 NTM 541000  DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  SPAR CAPS AND WEB BETWEEN RIB 8 AND 12, INCLUDING  ZONES 416/426  ACCESS: 415AL 416AR  425AL 426AR  541012-0604-1 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 27300 FC MRB S AMM SSI 5410 425 NTM 541000  DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  SPAR CAPS AND WEB BETWEEN RIB 8 AND 12 INCLUDING  ZONES 416/426  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 541012-0604-1 * * * * * C O N T I N U E * * * * *  ACCESS: 415AL 416AR  425AL 426AR  541012-0604-2 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 22600 FC MRB S AMM SSI 5410 425 NTM 541000  DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  SPAR CAPS AND WEB BETWEEN RIB 8 AND 12 , INCLUDING  ZONES 416/426  ACCESS: 415AL 416AR  425AL 426AR  541012-0604-3 415 UPPER SPAR & WEB RIB 8-12 MEC SDI I: 19200 FC MRB S AMM SSI 5410 425 NTM 541000  DETAILED AND SPECIAL DETAILED INSPECTION OF UPPER PART 2  SPAR CAPS AND WEB BETWEEN RIB 8 AND 12 INCLUDING  ZONES 416/426.  ACCESS: 415AL 416AR  425AL 426AR  541101-0603-1 415 NACELLES/PYLONS ENG DET T: 8000 FH CN CN EU  416 I: 750 FH FAA AD 1990-222-116 425 DETAILED INSPECTION OF RIB 6 SKIN PANEL LH AND RH ISB FAA AD  426 AROUND FIRST CORE COWL FITTING. 2000-10-01  ISB 54-0066  NOTE: CORECOWL DOORS TO BE OPENED.  541102-0603-1 415 NACELLES/PYLONS NDT SDI T: 7000 FH ISB ISB 54-068  416 I: 1200 FH  425 SPECIAL DETAILED INSPECTION OF INNER TEE BRACKETS  426 ON AFFECTED RIBS ON LH AND RH ENGINE PYLONS.  NOTE : PRECOOLER, RODS AND AIR DUCTS TO BE REMOVED.  541105-0603-1 415 NACELLE/PYLON-LOWER SPAR NDT SDI T: 9000 FC CN NTM 544010  416 I: 2500 FC FAA AD PART 6 OR 9  425 SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  1992-049-130 ACCESS: 415AL FAA AD 95-10 416AR ISB 54-0071  425AL  426AR  541105-0603-2 415 NACELLE/PYLON-LOWER SPAR NDT SDI T: 6000 FC CN NTM 544010  416 I: 2500 FC FAA AD PART 6 OR 9  425 SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD  426 UPPER SURFACE BETWEEN RIB 9 AND RIB 10. 1992-049-130 FAA AD 95-10 ACCESS: 415AL ISB 54-0071  416AR  425AL  426AR  541107-0603-1 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 10900 FC CN NTM 544011  423 I: 6700 FC FAA AD PART 6 OR 9  SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD  BETWEEN RIB 6 AND RIB 7. 1993-228-154 FAA AD  PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE 2000-10-18  REMOVED ISB 54-0073  ACCESS: 413GL  423GL  541107-0603-2 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 8600 FC CN NTM 544011  423 I: 5700 FC FAA AD PART 6 OR 9  SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD  BETWEEN RIB 6 AND RIB 7. 1993-228-154 FAA AD  PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE 2000-10-18  REMOVED ISB 54-0073  ACCESS: 413GL  423GL  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 544011  423 I: 6700 FC FAA AD PART 6 OR 9  SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD  BETWEEN RIB 6 AND RIB 7. 1993-228-154 FAA AD  PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE 2000-10-18  REMOVED ISB 54-0073  ACCESS: 413GL  423GL  541107-0603-4 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 30300 FC CN NTM 544011  423 I: 21300 FC FAA AD PART 6 OR 9  SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD  BETWEEN RIB 6 AND RIB 7. 1993-228-154 FAA AD  NOTE: THRESHOLD COUNTED FROM MOD 10335 EMBODIMENT. 2000-10-18  ISB 54-0073  PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE  REMOVED  ACCESS: 413GL  423GL  541107-0603-5 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 24000 FC CN NTM 544011  423 I: 18200 FC FAA AD PART 6 OR 9  SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD  BETWEEN RIB 6 AND RIB 7. 1993-228-154 FAA AD  NOTE: THRESHOLD COUNTED FROM MOD 10335 EMBODIMENT. 2000-10-18  ISB 54-0073  PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE  REMOVED  ACCESS: 413GL  423GL  541107-0603-6 413 PYLON LOWER SPAR RIB 6 AND RIB 7. NDT SDI T: 30300 FC CN NTM 544011  423 I: 21300 FC FAA AD PART 6 OR 9  SPECIAL DETAILED INSPECTION OF PYLON LOWER SPAR ISB EASA AD  BETWEEN RIB 6 AND RIB 7. 1993-228-154 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  2000-10-18  PREP.:PRECOOLER UPPER PANEL RODS AND AIR DUCT TO BE ISB 54-0073  REMOVED  ACCESS: 413GL  423GL  543001-0602-1 415 SIDE SKIN RIB 1-18 MEC DET T: 11200 FC ALI EASA AD  416 OR FAA AD 2006-0071  425 DETAILED INSPECTION OF SIDE SKIN PANELS 12700 FH FAA AD  426 BETWEEN RIB 1 AND RIB 18. I: 8400 FC 2007-04-11  473 OR  474 PREP.: COWLS TO BE OPENED. 9500 FH ALI REFERENC 483 543001-01-1  484  543001-0602-2 415 SIDE SKIN RIB 1-18 MEC DET T: 10100 FC ALI EASA AD  416 OR FAA AD 2006-0071  425 DETAILED INSPECTION OF SIDE SKIN PANELS 14000 FH FAA AD  426 BETWEEN RIB 1 AND RIB 18. I: 7600 FC 2007-04-11  473 OR  474 PREP.: COWLS TO BE OPENED. 10500 FH ALI REFERENC 483 543001-01-2  484  543001-0602-3 415 SIDE SKIN RIB 1-18 MEC DET T: 8800 FC ALI EASA AD  416 OR FAA AD 2006-0071  425 DETAILED INSPECTION OF SIDE SKIN PANELS 20400 FH FAA AD  426 BETWEEN RIB 1 AND RIB 18. I: 6600 FC 2007-04-11  473 OR  474 PREP.: COWLS TO BE OPENED 15300 FH ALI REFERENC 483 543001-01-3  484  543001-0602-4 415 SIDE SKIN RIB 1-18 NDT SDI T: 22400 FH AD NTM 513000  425 I: SEE ISB ISB PART 1  DETAILED AND SPECIAL DETAILED INSPECTION OF INNER AD EU  DOUBLER AROUND THE FIRE EXTINGUISHER BOTTLE ACCESS 1992-082-131 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 ISB 54-0070  ACCESS: 473AL  484AR  543002-0602-4 415 SIDE SKIN AT RIB 8 MEC DET T: 5350 FC AD AD EU-2008-0 416 I: 4300 FC ISB ISB 54-0075  425 DETAILED INSPECTION OF PYLON SIDE PANELS AT  426 RIB 8 (UPPER SECTION).  543002-0602-5 415 SIDE SKIN AT RIB 8 NDT SDI T: 12900 FC AD NTM 544003 P 416 I: 21600 FC ISB 6  425 SPECIAL DETAILED INSPECTION AND DETAILED INSPECTION AD EU-2008-0 426 ON PYLON SIDE PANELS AT RIB 8 (UPPER SECTION). ISB 54-0075  NOTE: THRESHOLD COUNTED FROM MOD 10431 EMBODIMENT  ACCESS: 413CL 413DL  414CR 414DR  423CL 423DL  424CR 424DR  544007-0604-1 471 LINKS PYLON-WING RIB 12 NDT SDI I: 27300 FC MRB S AMM SSI 5440 481 NTM 544000  SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4  TO WING AT RIB 12, WITH LINKS REMOVED INCLUDING ZONES  472/482  PREP: ENGINE AND LINKS REMOVED  ACCESS: 471AL 472AR  481AL 482AR  544007-0604-2 471 LINKS PYLON-WING RIB 12 NDT SDI I: 22600 FC MRB S AMM SSI 5440 481 NTM 544000  SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4  TO WING AT RIB 12, WITH LINKS REMOVED INCLUDING ZONES  472/482  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 544007-0604-2 * * * * * C O N T I N U E * * * * *  PREP: ENGINE AND LINKS REMOVED  ACCESS: 471AL 472AR  481AL 482AR  544007-0604-3 471 LINKS PYLON-WING RIB 12 NDT SDI I: 19200 FC MRB S AMM SSI 5440 481 NTM 544000  SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4  TO WING AT RIB 12, WITH LINKS REMOVED INCLUDING ZONES  472/482  PREP: ENGINE AND LINKS REMOVED  ACCESS: 471AL 472AR  481AL 482AR  544009-0604-1 473 LINKS PYLON-WING RIB 18 NDT SDI I: 27300 FC MRB S AMM SSI 5440 483 NTM 544000  SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4  TO WING AT RIB 18 INCLUDING ZONES 474/484  ACCESS: 473BL 474BR  483BL 484BR  544009-0604-2 473 LINKS PYLON-WING RIB 18 NDT SDI I: 22600 FC MRB S AMM SSI 5440 483 NTM 544000  SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4  TO WING AT RIB 18 INCLUDING ZONES 474/484  ACCESS: 473BL 474BR  483BL 484BR  544009-0604-3 473 LINKS PYLON-WING RIB 18 NDT SDI I: 19200 FC MRB S AMM SSI 5440 483 NTM 544000  SPECIAL DETAILED INSPECTION OF LINKS ATTACHING PYLON PART 4  TO WING AT RIB 18 INCLUDING ZONES 474/484  PREP.: ENGINE AND LINKS REMOVED.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 544009-0604-3 * * * * * C O N T I N U E * * * * *  ACCESS: 473BL 474BR  483BL 484BR  544011-0603-1 413 THRUST REV.COWL FITTING MEC DET I: ISB ISB AMM SSI 5440 423 54-060 MRB S CN  DETAILED INSPECTION OF THRUST REVERSER COWL 90-222-116(B HINGE FITTINGS INCLUDING ZONES 414, 415/416, 424 AND FAA AD  425/426. 2000-10-01  ISB 54-060  ACCESS: 451AL 452AR  461AL 462AR  544012-0603-1 413 THRUST REV. COWL FITTING MEC DET I: ISB ISB AMM SSI 5440 423 54-063 MRB S CN  DETAILED INSPECTION OF THRUST REVERSER COWL 90-222-116(B HINGE FITTINGS INCLUDING ZONES 414, 415/416, 424 AND FAA AD  425/426. 2000-10-01  ISB 54-063  ACCESS: 451AL 452AR  461AL 462AR  544200-0603-1 415 PYLON - ENGINE FWD ATTACHMENT FITTING MEC DET T: 5 YE CPCP AMM 710000  416 I: 5 YE MRB S  425 DETAILED INSPECTION OF ENGINE FWD ATTACHMENT AND MRB REFERENC 426 PYLON LOWER SPAR IN AREA OF FWD ATTACH FITTINGS  544200-C603- PREP.: ENGINE TO BE REMOVED  544200-0603-2 410 PYLON - ENGINE AFT ATTACHMENT FITTING MEC DET T: 5 YE CPCP AMM 710000  420 I: 5 YE MRB S  DETAILED INSPECTION OF ENGINE AFT ATTACHMENT AND MRB REFERENC PYLON LOWER SPAR IN AREA OF AFT ATTACH FITTING  544200-C603- PREP.: ENGINE TO BE REMOVED  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5440 420 OR MRB S AMM SSI 5440 DETAILED INSPECTION OF FWD ATTACHMENT FITTING 6600 FC AMM 710000  INCLUDING BOLT AND SPIGOT HOLES  PREP.: ENGINE TO BE REMOVED  546001-0606-1 415 PYLON FITTING NDT SDI T: 25000 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION OF PYLON ENGINE 28500 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4300 FC 2006-0071  451 PANEL. OR FAA AD  452 4900 FH 2007-04-11  461  462 ALI REFERENC 546001-01-1  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-2 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 35300 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 6200 FC 2006-0071  451 PANEL. OR FAA AD  452 7000 FH 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0607-4. ALI REFERENC 546001-01-3  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-3 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 33300 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4600 FC 2006-0071  451 PANEL. OR FAA AD  452 6400 FH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 462 TASK 546001-0607-6. 546001-01-5  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-4 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 43100 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC 2006-0071  451 PANEL. OR FAA AD  452 5800 FH 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0607-8. ALI REFERENC 546001-01-7  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-5 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 55700 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 5200 FC 2006-0071  451 PANEL. OR FAA AD  452 12000 FH 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0607-9. ALI REFERENC 546001-01-8  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-6 415 PYLON FITTING NDT SDI T: 30000 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 69600 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC 2006-0071  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 546001-0606-6 * * * * * C O N T I N U E * * * * *  451 PANEL. OR FAA AD  452 9700 FH 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0608-2. ALI REFERENC 546001-01-10  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-7 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 4800 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-0071  451 PANEL. FAA AD  452 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0607-3. ALI REFERENC 546001-01-2  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-8 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 4800 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-0071  451 PANEL. FAA AD  452 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0607-5. ALI REFERENC 546001-01-4  ACCESS: 451AL  452AR  461AL  462AR  546001-0606-9 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR FAA AD PART 4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-0071  451 PANEL. FAA AD  452 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0607-7. ALI REFERENC 546001-01-6  ACCESS: 451AL  452AR  461AL  462AR  546001-0607-1 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR FAA AD PART 4  425 SPECIAL DETAILED INSPECTION (US) OF PYLON ENGINE 9700 FH EASA AD  426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL 2006-0071  451 PANEL. FAA AD  452 2007-04-11  461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS  462 TASK 546001-0608-1. ALI REFERENC 546001-01-9  ACCESS: 451AL  452AR  461AL  462AR  546001-0607-2 415 PYLON FITTING NDT SDI T: 25000 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 28500 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4300 FC FAA AD 96-13 451 PANEL. OR  452 4900 FH ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-1  462 TASK 546001-0606-1.  ACCESS: 451AL  452AR  461AL  462AR  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 546001-0607-3 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 4800 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13 451 PANEL.  452 ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-2  462 TASK 546001-0606-7.  ACCESS: 451AL  452AR  461AL  462AR  546001-0607-4 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 35300 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 6200 FC FAA AD 96-13 451 PANEL. OR  452 7000 FH ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-3  462 TASK 546001-0606-2.  ACCESS: 451AL  452AR  461AL  462AR  546001-0607-5 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 4800 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13 451 PANEL.  452 ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-4  462 TASK 546001-0606-8.  ACCESS: 451AL  452AR  461AL  462AR  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 546001-0607-6 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 33300 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4600 FC FAA AD 96-13 451 PANEL. OR  452 6400 FH ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-5  462 TASK 546001-0606-3.  ACCESS: 451AL  452AR  461AL  462AR  546001-0607-7 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 5800 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13 451 PANEL.  452 ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-6  462 TASK 546001-0606-9.  ACCESS: 451AL  452AR  461AL  462AR  546001-0607-8 415 PYLON FITTING NDT SDI T: 31000 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 43100 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC FAA AD 96-13 451 PANEL. OR  452 5800 FH ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-7  462 TASK 546001-0606-4.  ACCESS: 451AL  452AR  461AL  462AR  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 546001-0607-9 415 PYLON FITTING NDT SDI T: 24000 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 55700 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 5200 FC FAA AD 96-13 451 PANEL. OR  452 12000 FH ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-8  462 TASK 546001-0606-5.  ACCESS: 451AL  452AR  461AL  462AR  546001-0608-1 415 PYLON FITTING NDT SDI I: 4200 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 9700 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL FAA AD 96-13 451 PANEL.  452 ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-9  462 TASK 546001-0607-1.  ACCESS: 451AL  452AR  461AL  462AR  546001-0608-2 415 PYLON FITTING NDT SDI T: 30000 FC ALI NTM 544001  416 OR CN PART 6  425 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON ENGINE 69600 FH FAA AD CN 2006-0071 426 FORWARD MOUNT FITTING AND JUNCTION WITH LATERAL I: 4200 FC FAA AD 96-13 451 PANEL. OR  452 9700 FH ALI REFERENC 461 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 546001-02-10  462 TASK 546001-0606-6.  ACCESS: 451AL  452AR  461AL  462AR  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

R 546014-0606-1 471 PYLON ATTACH FITTING MEC DET T: 29000 FC ALI EASA AD  472 OR FAA AD 2006-0071  481 DETAILED INSPECTION OF PYLON TO WING ATTACH 33000 FH FAA AD  482 FITTING LUGS AND LINKS AT PYLON RIB 12. I: 2900 FC 2007-04-11  OR  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 3300 FH ALI REFERENC 546014-0607-1 AND 546014-0608-1 546014-01-1  ACCESS: 471AL  472AR  481AL  482AR R 546014-0606-2 471 PYLON ATTACH FITTING MEC DET I: 1800 FC ALI EASA AD  472 OR FAA AD 2006-0071  481 DETAILED INSPECTION OF PYLON TO WING ATTACH 2000 FH FAA AD  482 FITTING LUGS AND LINKS AT PYLON RIB 12. 2007-04-11  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK ALI REFERENC 546014-0607-2 AND 546014-0608-2 546014-01-2  ACCESS: 471AL  472AR  481AL  482AR R 546014-0606-3 471 PYLON ATTACH FITTING MEC DET T: 29000 FC ALI EASA AD  472 OR FAA AD 2006-0071  481 DETAILED INSPECTION OF PYLON TO WING ATTACH 40300 FH FAA AD  482 FITTING LUGS AND LINKS AT PYLON RIB 12. I: 4300 FC 2007-04-11  OR  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 6000 FH ALI REFERENC 546014-0607-3 AND 546014-0608-3 546014-01-3  ACCESS: 471AL  472AR  481AL  482AR R 546014-0606-4 471 PYLON ATTACH FITTING MEC DET I: 1800 FC ALI EASA AD  472 OR FAA AD 2006-0071  481 DETAILED INSPECTION OF PYLON TO WING ATTACH 2500 FH  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  2007-04-11  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK  546014-0607-4 AND 546014-0608-4 ALI REFERENC 546014-01-4  ACCESS: 471AL  472AR  481AL  482AR R 546014-0606-5 471 PYLON ATTACH FITTING MEC DET T: 29000 FC ALI EASA AD  472 OR FAA AD 2006-0071  481 DETAILED INSPECTION OF PYLON TO WING ATTACH 67300 FH FAA AD  482 FITTING LUGS AND LINKS AT PYLON RIB 12. I: 1800 FC 2007-04-11  OR  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 4200 FH ALI REFERENC 546014-0607-5 AND 546014-0608-5 546014-01-5  ACCESS: 471AL  472AR  481AL  482AR R 546014-0607-1 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 544002  472 OR FAA AD PART 4  481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 33000 FH EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 7000 FC 2006-0071  OR FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 8000 FH 2007-04-11  546014-0606-1 AND 546014-0608-1  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-1  ACCESS: 471AL  472AR  481AL  482AR  546014-0607-2 471 PYLON ATTACH FITTING NDT SDI I: 5900 FC ALI NTM 544000  472 OR FAA AD PART 4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-0071  FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11  546014-0606-2 AND 546014-0608-2.  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-2  ACCESS: 471AL  472AR  481AL  482AR  546014-0607-3 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 544000  472 OR FAA AD PART 4  481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 40300 FH EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 7700 FC 2006-0071  OR FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 10700 FH 2007-04-11  546014-0606-3 AND 546014-0608-3.  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-3  ACCESS: 471AL  472AR  481AL  482AR  546014-0607-4 471 PYLON ATTACH FITTING NDT SDI I: 5900 FC ALI NTM 544000  472 OR FAA AD PART 4  481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 8200 FH EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-0071  FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11  546014-0606-4 AND 546014-0608-4.  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-4  ACCESS: 471AL  472AR  481AL  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 546014-0607-4 * * * * * C O N T I N U E * * * * *  482AR  546014-0607-5 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 544000  472 OR FAA AD PART 4  481 SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING 67300 FH EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 5900 FC 2006-0071  OR FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 13700 FH 2007-04-11  546014-0606-5 AND 546014-0608-5.  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-02-5  ACCESS: 471AL  472AR  481AL  482AR  546014-0608-1 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 544002  472 OR FAA AD PART 6  481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 33000 FH EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 10800 FC 2006-0071  OR FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 12300 FH 2007-04-11  546014-0606-1 AND 546014-0607-1.  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-03-1  ACCESS: 471AL  472AR  481AL  482AR  546014-0608-2 471 PYLON ATTACH FITTING NDT SDI I: 8800 FC ALI NTM 544002  472 OR CN PART 6  481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 10000 FH FAA AD EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-0071  FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11  546014-0606-2 AND 546014-0607-2.  ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 546014-03-2  ACCESS: 471AL  472AR  481AL  482AR  546014-0608-3 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 544002  472 OR CN PART 6  481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 40300 FH FAA AD EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. I: 8900 FC 2006-0071  OR FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 12300 FH 2007-04-11  546014-0606-3 AND 546014-0607-3.  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-03-3  ACCESS: 471AL  472AR  481AL  482AR  546014-0608-4 471 PYLON ATTACH FITTING NDT SDI I: 8800 FC ALI NTM 544002  472 OR CN PART 6  481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 12200 FH FAA AD EASA AD  482 ATTACH FITTING LUGS AND LINKS AT PYLON RIB 12. 2006-0071  FAA AD  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 2007-04-11  546014-0606-4 AND 546014-0607-4.  ALI REFERENC PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION 546014-03-4  ACCESS: 471AL  472AR  481AL  482AR  546014-0608-5 471 PYLON ATTACH FITTING NDT SDI T: 29000 FC ALI NTM 544002  472 OR CN PART 6  481 SPECIAL DETAILED INSPECTION (HF-EC) OF PYLON TO WING 67300 FH FAA AD  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  OR 2006-0071  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 20400 FH FAA AD  546014-0606-5 AND 546014-0607-5. 2007-04-11  PREP: REMOVE ENGINE, LINKS AND BUSHES FOR INSPECTION ALI REFERENC 546014-03-5  ACCESS: 471AL  472AR  481AL  482AR  548021-0603-1 410 PYLON INTERNAL SURFACE MEC DET T: 9 YE CPCP MRB REFERENC 420 I: 5 YE 548021-C603- 470 DETAILED INSPECTION OF PYLON INTERNAL  480 STRUCTURE FROM RIB 1 TO RIB 18 AND FROM LOWER SPAR TO  UPPER SPAR.  NOTE: THIS TASK CAN BE PERFORMED AT OPPORTUNITY  OF ENGINE REMOVAL.  PREP.: PRECOOLER TO BE REMOVED.  ACCESS: 473AL 474AR  483AL 484AR  548023-0603-1 410 PYLON LOWER SPAR MEC DET T: 9 YE CPCP MRB REFERENC 420 I: 2,5 YE 548023-C603- 470 DETAILED INSPECTION OF PYLON LOWER SPAR UPPER  480 SURFACE FROM RIB 8 TO 18, INCLUDING JUNCTION WITH  RIBS AND LATERAL PANELS  ACCESS: 473AL 474AR  483AL 484AR  548031-0603-1 415 PYLON EXTERNAL SURFACE MEC DET T: 10 YE CPCP MRB REFERENC 416 I: 5 YE 543101-C602- 425 DETAILED INSPECTION OF PYLON BOX EXTERNAL SURFACE 548031-C603- 426 FROM RIB 1 TO RIB 18 AND FROM LOWER SPAR TO UPPER  473 SPAR.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 548031-0603-1 * * * * * C O N T I N U E * * * * *  474  483 PREP.:COWLS OPENED, THERMAL INSULATION  484 TO BE REMOVED  ACCESS: 451AL 452AR 473AL  461AL 462AR 484AR  548041-0603-1 473 PYLON TO WING FWD ATTACHMENT MEC DET T: 9 YE CPCP AMM SSI 5410 474 I: 5 YE MRB S  483 DETAILED INSPECTION OF PYLON TO WING FORWARD MRB REFERENC 484 ATTACHMENT.  548041-C603- PREP.:ENGINE REMOVED LINKS AND BOLTS REMOVAL  (AT RIB 12)  ACCESS: 473BL  474BR  483BL  484BR  548041-0603-2 473 PYLON TO WING FWD ATTACHMENT MEC DET T: 9 YE CPCP MRB REFERENC 474 I: 9 YE 548041-C603- 483 DETAILED INSPECTION OF PYLON TO WING FORWARD  484 ATTACHMENT.  PREP.:ENGINE REMOVED LINKS AND BOLTS REMOVAL  (AT RIB 12)  ACCESS: 473BL  474BR  483BL  484BR  548051-0603-1 473 PYLON TO WING AFT ATTACHMENT MEC DET T: 7.5 YE CPCP MRB REFERENC 474 I: 5 YE 548051-C603- 483 DETAILED INSPECTION OF PYLON TO WING REAR  484 ATTACHMENT.  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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AT  RIB 18.  NOTE 1: APPLICATION OF SB 54-0059 IS RECOMMENDED  (REPLACEMENT OF ORIGINAL BOLTS BY  INCONEL 718 BOLTS)  ACCESS: 473BL  474BR  483BL  484BR  548051-0603-2 470 PYLON TO WING AFT ATTACHMENT MEC DET T: 7.5 YE CPCP MRB REFERENC 480 I: 7.5 YE 548051-C603- DETAILED INSPECTION OF PYLON TO WING REAR  ATTACHMENT.  NOTE 01: LINKS BOLTS AND BEARING TO BE REMOVED  AT RIB 18  NOTE 02: ENGINE TO BE REMOVED  NOTE 03: APPLICATION OF SB 54-0059 IS RECOMMENDED  (REPLACEMENT OF ORIGINAL BOLTS BY  INCONEL 718 BOLTS)  ACCESS: 473BL 474BR  483BL 484BR  548051-0603-3 470 PYLON TO WING AFT ATTACHMT MEC DET T: 10 YE CPCP MRB REFERENC 473 I: 10 YE 548051-C603- 474 DETAILED INSPECTION OF PYLON TO WING REAR  480 ATTACHMENT.  483  484 NOTE 01: LINKS BOLTS AND BEARING TO BE REMOVED  AT RIB 18  NOTE 02: ENGINE TO BE REMOVED  NOTE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  483BL 484BR  549001-0603-1 415 PYLON MEC SDI T: 10000 FH ISB ISB 54-0072  416 I: 5000 FH  425 SPECIAL DETAILED INSPECTION OF TEMPERATURE SENSORS  426 FOR POSIBLE CHAFING AGAINST THE PYLON FORWARD  SHACKLES AND LUGS  ACCESS: 471AL  472AR  481AL  482AR  549002-0603-1 415 PYLON NDT SDI T: 15000 FH ISB NTM 544005  416 I: 15000 FH PART 6  425 SPECIAL DETAILED AND DETAILED INSPECTION OF THE ISB 54-096  426 LOWER SIDE OF RIB 5 IN THE PYLON BOX.  PREP.: PRECOOLER TO BE REMOVED.  ACCESS: 413GL  423GL  * * * * * E N D * * * * *  STRUCTURE PROGRAM : NACELLES/PYLONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5510 ATTACHMENT MRB S  MRB REFERENC DETAILED INSPECTION OF HORIZONTAL STABILIZER  TRIM ACTUATOR ATTACH ARMS, SUPPORTING STRUCTURE AND 551001-C602- STABILIZER FRONT SPAR.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACE  ONLY IN INTERVALS NOT EXCEEDING 9 YEARS  ACCESS: 312AR  551001-0602-2 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 2500 FC CPCP AMM SSI 5510 ATTACHMENT MRB S  MRB REFERENC DETAILED INSPECTION OF HORIZONTAL STABILIZER  TRIM ACTUATOR ATTACH ARMS, SUPPORTING STRUCTURE AND 551001-C602- STABILIZER FRONT SPAR.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACE  ONLY IN INTERVALS NOT EXCEEDING 9 YEARS.  ACCESS: 312AR  551001-0602-3 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 1900 FC CPCP AMM SSI 5510 ATTACHMENT MRB S  MRB REFERENC DETAILED INSPECTION OF HORIZONTAL STABILIZER  TRIM ACTUATOR ATTACH ARMS, SUPPORTING STRUCTURE AND 551001-C602- STABILIZER FRONT SPAR.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACE  ONLY IN INTERVALS NOT EXCEEDING 9 YEARS.  ACCESS: 312AR  551002-0604-1 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 27300 FC MRB S AMM SSI 5510 ATTACHMENT NTM 555112  PART 4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 555112  TRIM ACTUATOR ATTACH ARM LUGS AND SUPPORT FITTINGS. PART 6  PREP.: ATTACH ARMS REMOVED.  ACCESS: 312AR  551002-0604-2 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 22600 FC MRB S AMM SSI 5510 ATTACHMENT NTM 555112  PART 4  DETAILED OR NDT INSPECTION OF HORIZONTAL STABILIZER NTM 555112  TRIM ACTUATOR ATTACH ARM LUGS AND SUPPORT FITTINGS. PART 6  PREP.: ATTACH ARMS REMOVED.  ACCESS: 312AR  551002-0604-3 319 HORIZONTAL STABILIZER TRIM ACTUATOR MEC DET I: 19200 FC MRB S AMM SSI 5510 ATTACHMENT NTM 555112  PART 4  DETAILED OR NDT INSPECTION OF HORIZONTAL STABILIZER NTM 555112  TRIM ACTUATOR ATTACH ARM LUGS AND SUPPORT FITTINGS. PART 6  PREP.: ATTACH ARMS REMOVED.  ACCESS: 312AR  551003-0604-1 334 LATERAL HINGE SUPP.FITTING MEC DET I: 27300 FC MRB S AMM SSI 5510 344  DETAILED INSPECTION OF LATERAL HINGE SUPPORT  FITTING AT HORIZONTAL STABILIZER REAR SPAR RIB 4 AND  SUPPORTING STRUCTURE.  ACCESS: 334AT  344AT  551003-0604-2 334 LATERAL HINGE SUPP.FITTING MEC DET I: 22600 FC MRB S AMM SSI 5510 344  DETAILED INSPECTION OF LATERAL HINGE SUPPORT  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AND  SUPPORTING STRUCTURE.  ACCESS: 334AT  344AT  551003-0604-3 334 LATERAL HINGE SUPP.FITTING MEC DET I: 19200 FC MRB S AMM SSI 5510 344  DETAILED INSPECTION OF LATERAL HINGE SUPPORT  FITTING AT HORIZONTAL STABILIZER REAR SPAR RIB 4 AND  SUPPORTING STRUCTURE.  ACCESS: 334AT  344AT  551004-0603-1 319 ATTACHMENT LUG AT FR 91 NDT SDI I: 1200 FC ISB NTM 531948  PART 6  SPECIAL DETAILED INSPECTION OF FRAME 91, UPPER AND CN  LOWER FRAME LUGS, LH AND RH. 1990-020-102 FAA AD 91-05 NOTE: THIS TASK IS ONLY APPLICABLE FOR LUGS MADE OF ISB 53-0269  2014 MATERIAL  ACCESS: 313AL  551009-0604-1 319 CENTER TORQUE BOX MEC DET I: 27300 FC MRB S AMM SSI 5510 DETAILED INSPECTION OF STRUCTURE OF HORIZONTAL  STABILIZER CENTER TORQUE BOX  - THROUGH LIGHTENING HOLES IN SPARS -  ACCESS: 312AR 313AL  551009-0604-2 319 CENTER TORQUE BOX MEC DET I: 22600 FC MRB S AMM SSI 5510 DETAILED INSPECTION OF STRUCTURE OF HORIZONTAL  STABILIZER 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 551009-0604-2 * * * * * C O N T I N U E * * * * *  ACCESS: 312AR 313AL  551009-0604-3 319 CENTER TORQUE BOX MEC DET I: 19200 FC MRB S AMM SSI 5510 DETAILED INSPECTION OF STRUCTURE OF HORIZONTAL  STABILIZER CENTER TORQUE BOX  - THROUGH LIGHTENING HOLES IN SPARS -  ACCESS: 312AR 313AL  551015-0602-1 319 SKIN SPLICES HORIZ. STAB. MEC DET I: 10700 FC MRB S AMM SSI 5510 DETAILED INSPECTION OF SKIN SPLICES ON UPPER  HORIZONTAL STABILIZER CENTER TORQUE BOX.  ACCESS: 312AR  551015-0602-2 319 SKIN SPLICES HORIZ. STAB. MEC DET I: 10000 FC MRB S AMM SSI 5510 DETAILED INSPECTION OF SKIN SPLICES ON UPPER  HORIZONTAL STABILIZER CENTER TORQUE BOX.  ACCESS: 312AR  551015-0602-3 319 SKIN SPLICES HORIZ. STAB. MEC DET I: 7900 FC MRB S AMM SSI 5510 DETAILED INSPECTION OF SKIN SPLICES ON UPPER  HORIZONTAL STABILIZER CENTER TORQUE BOX.  ACCESS: 312AR  551023-0604-1 333 REAR SPAR WEB HORIZ.STAB. MEC DET I: 27300 FC MRB S AMM SSI 5510 343  DETAILED INSPECTION REAR SPAR WEB AFT FACE OF  HORIZONTAL STABILIZER BETWEEN RIBS 3 AND 6  ACCESS: 334AT  344AT  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5510 343  DETAILED INSPECTION REAR SPAR WEB AFT FACE OF  HORIZONTAL STABILIZER BETWEEN RIBS 3 AND 6  ACCESS: 334AT  344AT  551023-0604-3 333 REAR SPAR WEB HORIZ.STAB. MEC DET I: 19200 FC MRB S AMM SSI 5510 343  DETAILED INSPECTION REAR SPAR WEB AFT FACE OF  HORIZONTAL STABILIZER BETWEEN RIBS 3 AND 6  ACCESS: 334AT  344AT  551025-0604-1 333 HORIZ.STAB.AT RIB 4 MEC DET I: 27300 FC MRB S AMM SSI 5510 343  DETAILED INSPECTION OF MACHINED FITTING AT AFT  END OF HORIZONTAL STABILIZER RIB 4 ATTACHED TO  FORWARD FACE OF REAR SPAR  - THROUGH LIGHTENING HOLES IN SPAR -  ACCESS: 334AT  344AT  551025-0604-2 333 HORIZ.STAB.AT RIB 4 MEC DET I: 22600 FC MRB S AMM SSI 5510 343  DETAILED INSPECTION OF MACHINED FITTING AT AFT  END OF HORIZONTAL STABILIZER RIB 4 ATTACHED TO  FORWARD FACE OF REAR SPAR  - THROUGH LIGHTENING HOLES IN SPAR -  ACCESS: 334AT  344AT  551025-0604-3 333 HORIZ.STAB.AT RIB 4 MEC DET I: 19200 FC MRB S AMM SSI 5510 343  DETAILED INSPECTION OF MACHINED FITTING AT AFT  END OF HORIZONTAL STABILIZER RIB 4 ATTACHED TO  FORWARD FACE OF REAR SPAR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  344AT  551028-0604-1 333 HORIZ.STAB.SPLICE RIB 3 & 4 NDT SDI I: 17700 FC MRB S AMM SSI 5510 343 NTM 551112  DETAILED AND SPECIAL DETAILED INSPECTION INTERNAL PART 4  HORIZONTAL STABILIZER OUTER PANEL SPLICES TO CENTER  TORQUE BOX AT UPPER SKIN BETWEEN RIBS 3 AND 4 AND  BETWEEN STRINGER 10 AND FRONT SPAR  ACCESS: 333CT  343CT  551028-0604-2 333 HORIZ.STAB.SPLICE RIB 3 & 4 NDT SDI I: 17700 FC MRB S AMM SSI 5510 343 NTM 551112  DETAILED AND SPECIAL DETAILED INSPECTION INTERNAL PART 4  HORIZONTAL STABILIZER OUTER PANEL SPLICES TO CENTER  TORQUE BOX AT UPPER SKIN BETWEEN RIBS 3 AND 4 AND  BETWEEN STRINGER 10 AND FRONT SPAR  ACCESS: 333CT  343CT  551028-0604-3 333 HORIZ.STAB.SPLICE RIB 3 & 4 NDT SDI I: 15100 FC MRB S AMM SSI 5510 343 NTM 551112  DETAILED AND SPECIAL DETAILED INSPECTION INTERNAL PART 4  HORIZONTAL STABILIZER OUTER PANEL SPLICES TO CENTER  TORQUE BOX AT UPPER SKIN BETWEEN RIBS 3 AND 4 AND  BETWEEN STRINGER 10 AND FRONT SPAR  551029-0603-1 319 HORIZONTAL STABILIZER REAR SPAR MEC DET I: 6800 FC CPCP AMM SSI 5510 MRB S  DETAILED INSPECTION OF HORIZONTAL STABILIZER MRB REFERENC HINGE BEARING SUPPORT FITTINGS AND UPPER AND LOWER  ATTACH FITTINGS AND STABILIZER REAR SPAR, AFT FACE 551029-C603- AT RIB 3.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  551029-0603-2 319 HORIZONTAL STABILIZER REAR SPAR MEC DET I: 6200 FC CPCP AMM SSI 5510 MRB S  DETAILED INSPECTION OF HORIZONTAL STABILIZER MRB REFERENC HINGE BEARING SUPPORT FITTINGS AND UPPER AND LOWER  ATTACH FITTINGS AND STABILIZER REAR SPAR, AFT FACE 551029-C603- FROM RIBS 3LH TO 3RH  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION TO EXTERNAL SURFACHE  ONLY IN INTERVALS NOT EXCEEDING 9 YEARS.  551029-0603-3 319 HORIZONTAL STABILIZER REAR SPAR MEC DET I: 4900 FC CPCP AMM SSI 5510 MRB S  DETAILED INSPECTION OF HORIZONTAL STABILIZER MRB REFERENC HINGE BEARING SUPPORT FITTINGS AND UPPER AND LOWER  ATTACH FITTINGS AND STABILIZER REAR SPAR, AFT FACE 551029-C603- FROM RIBS 3LH TO 3RH  NOTE: 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 5510 DETAILED INSPECTION OF HORIZONTAL STABILIZER  STRUCTURE AROUND HINGE BEARING SUPPORT FITTINGS  ACCESS: 313AL 334AT 344AT  551030-0604-2 319 HORIZ.STAB. STRUCTURE MEC DET I: 22600 FC MRB S AMM SSI 5510 DETAILED INSPECTION OF HORIZONTAL STABILIZER  STRUCTURE AROUND HINGE BEARING SUPPORT FITTINGS  ACCESS: 313AL 334AT 344AT  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5510 DETAILED INSPECTION OF HORIZONTAL STABILIZER  STRUCTURE AROUND HINGE BEARING SUPPORT FITTINGS  ACCESS: 313AL 334AT 344AT  551033-0603-1 319 STABILIZERS-THS CENTER BOX NDT SDI T: 11400 FC ISB AMM SSI 5510 I: 6000 FC MRB S NTM 513000  SPECIAL DETAILED INSPECTION OF INTEGRAL TOP SKIN OF NTM 513010  THE THS LEVEL. NTM 516000  NTM 551112  NOTE: 01. THS SUPPORT FITTING TO BE REMOVED CN  02. ALTERNATIVE METHOD COULD BE USED WITHOUT 1989-157-099 THS SUPPORT FITTING REMOVED. FAA AD 90-22 ISB 55-0035  552004-0603-1 335 ELEVATOR MEC DET I: 9 YE CPCP AMM SSI 5520 345 MRB S AMM SSI 5520 DETAILED INSPECTION OF HORIZONTAL STABILIZER AMM SSI 5520 ELEVATOR FRONT SPAR FORWARD FACE INCLUDING HINGE  FITTINGS. MRB REFERENC ACCESS: 334AT 334BT 334CT 334DT 334ET 334FT 552004-C603- 334GT 334HT 334JT 334KT 334LT 335AB  335AT 335BB 335BT 335CB 335CT 335DB  335DT 335EB 335ET  344AT 344BT 344CT 344DT 344ET 344FT  344GT 344HT 344JT 344KT 344LT 345AB  345AT 345BB 345BT 345CB 345CT 345DB  345DT 345EB 345ET  552007-0602-1 335 ELEVATOR TRAILING EDGE MEC DET I: 30 MO MRB S  345  DETAILED INSPECTION OF ELEVATOR TRAILING EDGE  FOR CORROSION.  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5530 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  AT VERTICAL STABILIZER RIB 16.  553005-0602-2 323 SKIN SPLICE-VERTICAL STAB. MEC DET I: 10300 FC MRB S AMM SSI 5530 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  AT VERTICAL STABILIZER RIB 16.  553005-0602-3 323 SKIN SPLICE-VERTICAL STAB. MEC DET I: 8900 FC MRB S AMM SSI 5530 DETAILED INSPECTION OF EXTERNAL SKIN SPLICE  AT VERTICAL STABILIZER RIB 16.  553017-0603-1 323 VERTICAL STABILIZER SKIN MEC DET T: 20000 FC ISB CN 83-102-53 I: 1500 FC FAA AD 86-19 DETAILED INSPECTION OF VERTICAL STABILIZER ISB 55-026  ATTACH FITTINGS LH AND RH FOR CRACKS.  ACCESS: 311AZ 311BZ 312AR  555021-0603-1 330 ELEVATOR HINGE ARM NO.1 & 7 MEC DET I: 5 YE MRB S  340  DETAILED INSPECTION OF ELEVATOR HINGE ARMS  NO.1 AND 7.  ACCESS: 334AB 334BT 334EB 335AB 335AT 335ET  344AB 344BT 344EB 345AB 345AT 345ET  556001-0606-1 333 HORIZONTAL STABILIZER TOP SKIN NDT SDI T: SEE SB ALI NTM 551112  343 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER FAA AD CN 2006-0071 CENTER BOX INTEGRAL SKIN JUST OUTBOARD OF RIB 3, FROM ISB FAA AD 96-13 THE REAR SPAR TO STRINGER 10 LH/RH. ISB 55-0036  ACCESS: 333CT 333DT ALI REFERENC 343CT 343DT 556001-01-1  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 556002-0602-1 323 VERTICAL STABILIZER SKIN MEC DET T: 37000 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER SKIN 41800 FH FAA AD  PANELS LH/RH FROM FRONT TO REAR SPAR AND FROM I: 6000 FC 2007-04-11  FIN/FUSELAGE FAIRING TO TIP RIB 12, EXTERNAL SURFACE. OR  6700 FH ALI REFERENC 556002-01-1  556002-0602-2 323 VERTICAL STABILIZER SKIN MEC DET T: 34000 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER SKIN 46200 FH FAA AD  PANELS LH/RH FROM FRONT TO REAR SPAR AND FROM I: 6000 FC 2007-04-11  FIN/FUSELAGE FAIRING TO TIP RIB 12, EXTERNAL SURFACE. OR  8100 FH ALI REFERENC 556002-01-2  556002-0602-3 323 VERTICAL STABILIZER SKIN MEC DET T: 28000 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER SKIN 61800 FH FAA AD  PANELS LH/RH FROM FRONT TO REAR SPAR AND FROM I: 6000 FC 2007-04-11  FIN/FUSELAGE FAIRING TO TIP RIB 12, EXTERNAL SURFACE. OR  13200 FH ALI REFERENC 556002-01-3  556003-0606-1 323 VERTICAL STABILIZER ATTACHMENT MEC DET ST: 34000 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 38400 FH  CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH SI: 4400 FC ALI REFERENC INCLUSIVE RIVETING TO SKIN. OR 556003-01-1  5000 FH  ACCESS: 323AL 323AR 323BL 323BR  556003-0606-2 323 VERTICAL STABILIZER ATTACHMENT MEC DET I: 3300 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 3700 FH  CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH ALI REFERENC INCLUSIVE RIVETING TO SKIN. 556003-01-2  ACCESS: 323AL 323AR 323BL 323BR  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 OR FAA AD 96-13 DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 42200 FH  CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH SI: 4900 FC ALI REFERENC INCLUSIVE RIVETING TO SKIN. OR 556003-01-3  6700 FH  ACCESS: 323AL 323AR 323BL 323BR  556003-0606-4 323 VERTICAL STABILIZER ATTACHMENT MEC DET I: 3100 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 4200 FH  CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH ALI REFERENC INCLUSIVE RIVETING TO SKIN. 556003-01-4  ACCESS: 323AL 323AR 323BL 323BR  556003-0606-5 323 VERTICAL STABILIZER ATTACHMENT MEC DET ST: 26000 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 57500 FH  CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH SI: 3900 FC ALI REFERENC INCLUSIVE RIVETING TO SKIN. OR 556003-01-5  8600 FH  ACCESS: 323AL 323AR 323BL 323BR  556003-0606-6 323 VERTICAL STABILIZER ATTACHMENT MEC DET I: 2600 FC ALI CN 2006-0071 OR FAA AD 96-13 DETAILED INSPECTION OF VERTICAL STABILIZER, FORWARD, 5700 FH  CENTER AND REAR MAIN FUSELAGE ATTACH FITTINGS, LH/RH ALI REFERENC INCLUSIVE RIVETING TO SKIN. 556003-01-6  ACCESS: 323AL 323AR 323BL 323BR  556004-0606-1 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 27000 FC ALI EASA AD  OR FAA AD 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 30500 FH FAA AD  STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 6000 FC 2007-04-11  ANGLES, FROM RIB 1 TO RIB 12. OR  6700 FH ALI REFERENC ACCESS: 311AZ 311BZ 312AR 556004-01-1  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 556004-0606-2 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 27000 FC ALI EASA AD  OR FAA AD 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 30500 FH FAA AD  STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 12700 FC 2007-04-11  ANGLES, FROM RIB 1 TO RIB 12. OR  14300 FH ALI REFERENC ACCESS: 311AZ 311BZ 312AR 556004-01-4  556004-0606-3 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 24500 FC ALI EASA AD  OR FAA AD 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 33300 FH FAA AD  STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 5500 FC 2007-04-11  ANGLES, FROM RIB 1 TO RIB 12. OR  7400 FH ALI REFERENC ACCESS: 311AZ 311BZ 312AR 556004-01-2  556004-0606-4 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 24500 FC ALI EASA AD  OR FAA AD 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 33300 FH FAA AD  STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 11800 FC 2007-04-11  ANGLES, FROM RIB 1 TO RIB 12. OR  16000 FH ALI REFERENC ACCESS: 311AZ 311BZ 312AR 556004-01-5  556004-0606-5 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 19500 FC ALI EASA AD  OR FAA AD 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 43000 FH FAA AD  STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 4600 FC 2007-04-11  ANGLES, FROM RIB 1 TO RIB 12. OR  10100 FH ALI REFERENC ACCESS: 311AZ 311BZ 312AR 556004-01-3  556004-0606-6 323 VERTICAL STABILIZER INTERNAL STRUCTURE MEC DET T: 19500 FC ALI EASA AD  OR FAA AD 2006-0071  DETAILED INSPECTION OF VERTICAL STABILIZER INTERNAL 43000 FH FAA AD  STRUCTURE, ATTACHMENT AREAS OF STRUTS TO SHEAR I: 9900 FC 2007-04-11  ANGLES, FROM RIB 1 TO RIB 12. OR  21800 FH ALI REFERENC ACCESS: 311AZ 311BZ 312AR 556004-01-6  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 556005-0604-1 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 58200 FC ALI NTM 555115  343 OR PART 6  SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER 65700 FH EASA AD  REAR SPAR WEB JOINING PART AT RIB 3, RIVETING UPPER I: 7600 FC 2006-0071  AREA BETWEEN RIB 3 AND RIB 4 LH/RH. OR FAA AD  8600 FH 2007-04-11  NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN  RIB 4 AND RIB 5. ALI REFERENC 556005-01-1  ACCESS: 333CT 333DT 334AT  343CT 343DT 344AT  556005-0604-2 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 50300 FC ALI NTM 555115  343 OR PART 6  SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER 68400 FH EASA AD  REAR SPAR WEB JOINING PART AT RIB 3, RIVETING UPPER I: 6800 FC 2006-0071  AREA BETWEEN RIB 3 AND RIB 4 LH/RH. OR FAA AD  9200 FH 2007-04-11  NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN  RIB 4 AND RIB 5. ALI REFERENC 556005-01-2  ACCESS: 333CT 333DT 334AT  343CT 343DT 344AT  556005-0604-3 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 40200 FC ALI NTM 555115  343 OR PART 6  SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER 88800 FH EASA AD  REAR SPAR WEB JOINING PART AT RIB 3, RIVETING UPPER I: 5500 FC 2006-0071  AREA BETWEEN RIB 3 AND RIB 4 LH/RH. OR FAA AD  12200 FH 2007-04-11  NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN  RIB 4 AND RIB 5. ALI REFERENC 556005-01-3  ACCESS: 333CT 333DT 334AT  343CT 343DT 344AT  556006-0604-1 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 48000 FC ALI NTM 555116  343 OR PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54200 FH EASA AD  HORIZONTAL STABILIZER REAR SPAR WEB RIVETING UPPER I: 7200 FC 2006-0071  AREA BETWEEN RIB 3 AND RIB 4 LH/RH OR FAA AD  8100 FH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 556006-01-1  ACCESS: 333CT 333DT 334AT  343CT 343DT 344AT  556006-0604-2 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 40000 FC ALI NTM 555116  343 OR PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54400 FH EASA AD  HORIZONTAL STABILIZER REAR SPAR WEB RIVETING UPPER I: 6400 FC 2006-0071  AREA BETWEEN RIB 3 AND RIB 4 LH/RH OR FAA AD  8700 FH 2007-04-11  NOTE: GRACE PERIOD = 1000 FC  ALI REFERENC ACCESS: 333CT 333DT 334AT 556006-01-2  343CT 343DT 344AT  556006-0604-3 333 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 34000 FC ALI NTM 555116  343 OR PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 75100 FH EASA AD  HORIZONTAL STABILIZER REAR SPAR WEB RIVETING UPPER I: 5200 FC 2006-0071  AREA BETWEEN RIB 3 AND RIB 4 LH/RH OR FAA AD  11400 FH 2007-04-11  NOTE: GRACE PERIOD = 1000 FC  ALI REFERENC ACCESS: 333CT 333DT 334AT 556006-01-3  343CT 343DT 344AT  556007-0604-1 319 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 48000 FC ALI NTM 555117  OR PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54200 FH EASA AD  HORIZONTAL STABILIZER CENTER BOX UPPER SKIN REAR CAP I: 18700 FC 2006-0071  RIVETING AT ATTACHMENT TO REAR SPAR BETWEEN RIB 2 AND OR FAA AD  RIB 3 LH/RH. 21100 FH 2007-04-11  NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN ALI REFERENC RIB 2 AND RIB 3, LH/RH. 556007-01-1  NOTE 1: GRACE PERIOD = 1000 FC  ACCESS: 313AL  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 556007-0604-2 319 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 40000 FC ALI NTM 555117  OR PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 54400 FH EASA AD  HORIZONTAL STABILIZER CENTER BOX UPPER SKIN REAR CAP I: 16600 FC 2006-0071  RIVETING AT ATTACHMENT TO REAR SPAR BETWEEN RIB 2 AND OR FAA AD  RIB 3 LH/RH. 22500 FH 2007-04-11  NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN ALI REFERENC RIB 2 AND RIB 3, LH/RH. 556007-01-2  NOTE 1: GRACE PERIOD = 1000 FC  ACCESS: 313AL  556007-0604-3 319 HORIZONTAL STABILIZER INTERNAL STRUCTURE NDT SDI T: 34000 FC ALI NTM 555117  OR PART 6  SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF 75100 FH EASA AD  HORIZONTAL STABILIZER CENTER BOX UPPER SKIN REAR CAP I: 13500 FC 2006-0071  RIVETING AT ATTACHMENT TO REAR SPAR BETWEEN RIB 2 AND OR FAA AD  RIB 3 LH/RH. 29800 FH 2007-04-11  NOTE: THROUGH REAR SPAR LIGHTENING HOLE BETWEEN ALI REFERENC RIB 2 AND RIB 3, LH/RH. 556007-01-3  NOTE 1: GRACE PERIOD = 1000 FC  ACCESS: 313AL  556008-0604-1 300 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 55100 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL 62200 FH FAA AD  BOX UPPER SKIN EXTERNAL SURFACE BETWEEN RIB 3 AND I: 43800 FC 2007-04-11  RIB 4 AND BETWEEN REAR SPAR AND STRINGER 11 LH/RH. OR  49400 FH ALI REFERENC 556008-01-1  556008-0604-2 300 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 47700 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL 64800 FH FAA AD  BOX UPPER SKIN EXTERNAL SURFACE BETWEEN RIB 3 AND I: 38900 FC 2007-04-11  RIB 4 AND BETWEEN REAR SPAR AND STRINGER 11 LH/RH. OR  52900 FH ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 556008-0604-2 * * * * * C O N T I N U E * * * * *  556008-01-2  556008-0604-3 300 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 38100 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL 84200 FH FAA AD  BOX UPPER SKIN EXTERNAL SURFACE BETWEEN RIB 3 AND I: 31800 FC 2007-04-11  RIB 4 AND BETWEEN REAR SPAR AND STRINGER 11 LH/RH. OR  70200 FH ALI REFERENC 556008-01-3  556009-0604-1 319 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 48000 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR 54200 FH FAA AD  SPAR WEB JOINING PART AT RIB 3, RIVETING AREA BETWEEN I: 10400 FC 2007-04-11  RIB 2 AND RIB 3, LH/RH OR  11700 FH ALI REFERENC ACCESS: 313AL 556009-01-1  556009-0604-2 319 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 40000 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR 54300 FH FAA AD  SPAR WEB JOINING PART AT RIB 3, RIVETING AREA BETWEEN I: 9200 FC 2007-04-11  RIB 2 AND RIB 3, LH/RH OR  12600 FH ALI REFERENC ACCESS: 313AL 556009-01-2  556009-0604-3 319 HORIZONTAL STABILIZER EXTERNAL STRUCTURE MEC DET T: 34000 FC ALI EASA AD  OR 2006-0071  DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR 75100 FH FAA AD  SPAR WEB JOINING PART AT RIB 3, RIVETING AREA BETWEEN I: 7500 FC 2007-04-11  RIB 2 AND RIB 3, LH/RH OR  16700 FH ALI REFERENC ACCESS: 313AL 556009-01-3  558011-0603-1 323 VERTICAL STAB.-SPAR BOX MEC DET T: 15 YE CPCP MRB REFERENC I: 9 YE 558011-C603- DETAILED INSPECTION OF VERTICAL STABILIZER  INTERNAL STRUCTURE FROM RIB 12 TO 26.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  325EL 325ER 325FL 325GL 325HL 325JL  325KL  558021-0603-1 322 VERTICAL STABILIZER - FRONT SPAR MEC GVI I: 9 YE CPCP MRB REFERENC 324 558021-C603- GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER  FRONT 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  324AT 324BT  558041-0603-1 323 FUSELAGE EXTERNAL SURFACE VERTICAL MEC DET T: 5 YE CPCP AMM SSI 5550 STABILIZER RIB 1 I: 5 YE MRB S AMM SSI 5550 SIL SIL 55-033  DETAILED INSPECTION OF FIN TO FUSELAGE  ATTACHMENT FITTINGS AND VERTICAL STABILIZER RIB 1 MRB REFERENC UPPER AND LOWER SURFACE INCLUDING FORKED LINKS AND  TRANSVERSE LOAD FITTINGS. 558041-C603- NOTE 1: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION, EXCLUDING THE  CONICAL FIN TO FUSELAGE ATTACHMENT BOLTS  ATTACHMENT BOLTS  NOTE 2: CHECK THE CORRECT ALIGNMENT OF THE TORQUE  MARKS  ACCESS: 311AZ 311BZ 312AR 323AL 323AR 323BR  325BL  558061-0603-1 326 RUDDER - INTERNAL STRUCTURE MEC BSI T: 15 YE CPCP NTM 514000  I: 9 YE PART 1  NDT INSPECTION OF RUDDER INTERNAL STRUCTURE THROUGH  LIGHTENING HOLES. MRB REFERENC 558061-C603- * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 558061-0603-1 * * * * * C O N T I N U E * * * * *  NOTE: BOROSCOPE INSPECTION  ACCESS: 325AL 325AR 325BL 325BR 325CL 325CR  325DL 325DR 325EL 325ER 325FL 325GL  325HL 325JL 325KL 326AL 326AR 326BL  326BR 326CL 326CR 326DL 326DR 326EL  326ER 326FL 326GL 326HL 326JL 326KL  326LL  558065-0603-1 326 RUDDER FRONT SPAR MEC GVI T: 15 YE CPCP MRB REFERENC I: 9 YE 558065-C603- GENERAL VISUAL INSPECTION OF RUDDER FRONT SPAR  FORWARD FACE .  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 325AL 325AR 325BL 325CL 325DL 325EL  325FL 325GL 325HL 325JL 325KL 326AL  326AR 326BL 326BR 326CL 326CR 326DL  326DR 326EL 326ER 326FL 326GL 326HL  326JL 326KL 326LL  558081-0603-1 325 VERTICAL STABILIZER TRAILING EDGE MEC GVI I: 5 YE CPCP MRB REFERENC 558081-C603- GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER  TRAILING EDGE.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 325AL 325BL 325CL 325DL 325EL 325FL  325GL 325HL 325JL 325KL  558085-0603-1 325 RUDDER HINGE ARMS AND FITTINGS MEC DET I: 5 YE CPCP AMM SSI 5530 326 MRB S AMM SSI 5530 DETAILED INSPECTION OF RUDDER HINGE ARMS 1 TO AMM SSI 5530 7 AND ATTACH FITTINGS OF RUDDER HINGE ARMS AND AMM SSI 5530 HYDRAULIC ACTUATORS INCLUDING SUPPORT STRUCTURE ON AMM SSI 5530 VERTICAL STABILIZER REAR SPAR AND RUDDER FRONT SPAR. AMM SSI 5540 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 558085-0603-1 * * * * * C O N T I N U E * * * * *  AMM SSI 5540 NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, AMM SSI 5540 G2 OR G3 AFTER INSPECTION AMM SSI 5540 AMM SSI 5540 ACCESS: 325BL 325DL 325FL 325HL 325KL AMM SSI 5550 326BL 326DL 326FL 326HL 326KL AMM SSI 5550 AMM SSI 5550 AMM SSI 5550 AMM SSI 5550 AMM SSI 5550 AMM SSI 5550 SIL 55-013  MRB REFERENC 558085-C603- 558085-C603- 558089-0603-1 325 VERT.STAB.-MACHINED PLATES MEC DET I: 5 YE CPCP MRB REFERENC 558089-C603- DETAILED INSPECTION OF INTEGRAL MACHINED  PLATES ON VERTICAL STABILIZER REAR SPAR AFT FACE  BETWEEN RIB 11 AND RIB 16.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION  ACCESS: 325DL  558193-0603-1 335 ELEVATOR INTERN. STRUCTURE MEC DET T: 15 YE CPCP MRB REFERENC 345 I: 9 YE 558193-C603- DETAILED INSPECTION OF HORIZONTAL STABILIZER  ELEVATOR INTERNAL STRUCTURE THROUGH LIGHTENING HOLES.  ACCESS: 334AT 334BT 334CT 334DT 334ET 334FT  334GT 334HT 334JT 334KT 334LT 335AB  335AT 335BB 335BT 335CB 335CT 335DB  335DT 335EB 335ET  344AT 344BT 344CT 344DT 344ET 344FT  344GT 344HT 344JT 344KT 344LT 345AB  345AT 345BB 345BT 345CB 345CT 345DB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 558193-0603-1 * * * * * C O N T I N U E * * * * *  345DT 345EB 345ET  558215-0603-1 334 HINGE ARMS, FITTING MEC DET I: 8200 FC CPCP AMM SSI 5510 344 OR 5 YE MRB S AMM SSI 5510 DETAILED INSPECTION OF FITTING ON HORIZONTAL  STABILIZER REAR SPAR AND HINGE ARMS FOR ELEVATORS AT MRB REFERENC RIBS 6, 9, 10, 11, 14, 17 AND 20.  558215-C603- NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 AND  G2 AFTER INSPECTION  ACCESS: 334AB 334BB 334BT 334CB 334CT 334DB  334DT 334EB 334ET 334FT 334GT 334HT  334JT 334KT 334LT  344AB 344BB 344BT 344CB 344CT 344DB  344DT 344EB 344ET 344FT 344GT 344HT  344JT 344KT 344LT  * * * * * E N D * * * * *  STRUCTURE PROGRAM : STABILIZERS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 641 I: 12400 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENTS TO  FRONT SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENC 571001-01-1  571001-0602-2 541 TOP SKIN AT FRONT SPAR MEC DET T: 20000 FC ALI CN 2006-0071 641 I: 12000 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENTS TO  FRONT SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENC 571001-01-2  571002-0602-1 541 TOP SKIN AT CENTER / AFT SPAR MEC DET T: 20600 FC ALI CN 2006-0071 542 I: 12400 FC FAA AD 96-13 641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  642 CENTER SPAR AND REAR SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENC 571002-01-1  571002-0602-2 541 TOP SKIN AT CENTER / AFT SPAR MEC DET T: 20000 FC ALI CN 2006-0071 542 I: 12000 FC FAA AD 96-13 641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  642 CENTER SPAR AND REAR SPAR, RIB 1 TO RIB 9 INCLUSIVE. ALI REFERENC 571002-01-2  571003-0602-1 541 TOP SKIN AT RIB 2 TO 9 MEC DET T: 20600 FC ALI CN 2006-0071 542 I: 12400 FC FAA AD 96-13 641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  642 RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- AND REAR ALI REFERENC SPAR. 571003-01-1  571003-0602-2 541 TOP SKIN AT RIB 2 TO 9 MEC DET T: 20000 FC ALI CN 2006-0071 542 I: 12000 FC FAA AD 96-13 641 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  642 RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- AND REAR ALI REFERENC SPAR. 571003-01-2  571005-0602-1 542 BOTTOM SKIN AT REAR SPAR MEC DET T: 13200 FC ALI CN 2006-0071 642 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 14900 FH  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC OR 571005-01-1  3700 FH  571005-0602-2 542 BOTTOM SKIN AT REAR SPAR MEC DET T: 12800 FC ALI CN 2006-0071 642 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 17400 FH  REAR SPAR, RIB 1 TO RIB 3 INCLUSIVE. I: 3200 FC ALI REFERENC OR 571005-01-2  4300 FH  571005-0602-3 542 BOTTOM SKIN AT REAR SPAR MEC DET T: 12000 FC ALI CN 2006-0071 642 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 26500 FH  REAR SPAR, RIB 1 TO RIB 3 INCLUSIVE. I: 3000 FC ALI REFERENC OR 571005-01-3  6600 FH  571006-0602-1 541 BOTTOM SKIN AT FRONT- AND CENTER SPAR MEC DET T: 22400 FC ALI CN 2006-0071 542 OR FAA AD 96-13 641 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT 25300 FH  642 TO FRONT AND CENTER SPARS BETWEEN RIB 1 AND RIB 9 I: 10100 FC ALI REFERENC INCLUSIVE, AND AT ATTACHMENT TO REAR SPAR, RIB 3 AND OR 571006-01-1  RIB 9 INCLUSIVE. 11400 FH  571006-0602-2 541 BOTTOM SKIN AT FRONT- AND CENTER SPAR MEC DET T: 21700 FC ALI CN 2006-0071 542 OR FAA AD 96-13 641 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT 29700 FH  642 TO FRONT AND CENTER SPARS BETWEEN RIB 1 AND RIB 9 I: 9800 FC ALI REFERENC INCLUSIVE, AND AT ATTACHMENT TO REAR SPAR, RIB 3 AND OR 571006-01-2  RIB 9 INCLUSIVE. 13400 FH  571006-0602-3 541 BOTTOM SKIN AT FRONT- AND CENTER SPAR MEC DET T: 20400 FC ALI CN 2006-0071 542 OR FAA AD 96-13 641 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT 46300 FH  642 TO FRONT AND CENTER SPARS BETWEEN RIB 1 AND RIB 9 I: 9200 FC ALI REFERENC INCLUSIVE, AND AT ATTACHMENT TO REAR SPAR, RIB 3 AND OR 571006-01-3  RIB 9 INCLUSIVE. 20900 FH  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 542 OR FAA AD 96-13 641 DETAILED INSPECTION OF BOTTOM SKIN AND JOINT STRAPS 20700 FH  642 ATTACHMENT TO RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- I: 11000 FC ALI REFERENC AND REAR SPAR. OR 571007-01-1  12400 FH  571007-0602-2 541 BOTTOM SKIN AND JOINT STRAPS MEC DET T: 17500 FC ALI CN 2006-0071 542 OR FAA AD 96-13 641 DETAILED INSPECTION OF BOTTOM SKIN AND JOINT STRAPS 24000 FH  642 ATTACHMENT TO RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- I: 10500 FC ALI REFERENC AND REAR SPAR. OR 571007-01-2  14400 FH  571007-0602-3 541 BOTTOM SKIN AND JOINT STRAPS MEC DET T: 16600 FC ALI CN 2006-0071 542 OR FAA AD 96-13 641 DETAILED INSPECTION OF BOTTOM SKIN AND JOINT STRAPS 37700 FH  642 ATTACHMENT TO RIB 2 TO RIB 9 INCLUSIVE BETWEEN FRONT- I: 10000 FC ALI REFERENC AND REAR SPAR. OR 571007-01-3  22700 FH  571009-0602-1 500 WING - TOP SKIN PANEL NUMBER 3 MEC DET T: 14800 FC ISB ISB 57-210  600 I: 2500 FC  DETAILED INSPECTION OF WING TOP SKIN PANEL  NUMBER 3.  ACCESS: 581EB 581FB 581GB 581HB  681EB 681FB 681GB 681HB  571013-0602-1 540 ACCESS DOOR AND BOTTOM SKIN MEC DET I: 6700 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF EXTERNAL BOTTOM SKIN  AT DOOR CUTOUTS AND PUMP APERTURES AND ACCESS DOORS  BETWEEN RIBS 1 AND 9.  571013-0603-1 540 BOTTOM SKIN AND ACCESS DOORS AT CUTOUTS MEC DET I: 5 YE MRB S AMM SSI 5710 640  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571013-0603-1 * * * * * C O N T I N U E * * * * *  NOTE: DOOR OPENED  ACCESS: 541AB 541BB 541CB 542CB 542DB 542EB  641AB 641BB 641CB 642CB 642DB 642EB  571013-0604-1 540 ACCESS DOOR AND BOTTOM SKIN MEC DET I: 17700 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF FUEL PUMP APERTURES  BETWEEN RIB 1 AND 2.  PREP.: FUEL PUMPS REMOVED  571014-0602-1 540 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 6500 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF EXTERNAL BOTTOM  SKIN AT DOOR CUTOUTS AND PUMP APERTURES BETWEEN  RIBS 1 AND 9.  571014-0602-2 540 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 6100 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF EXTERNAL BOTTOM  SKIN AT DOOR CUTOUTS AND PUMP APERTURES BETWEEN  RIBS 1 AND 9.  571014-0604-1 540 FUEL PUMP APERTURES MEC DET I: 17700 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF FUEL PUMP APERTURES  BETWEEN RIB 1 AND 2  PREP.: FUEL PUMPS REMOVED.  571014-0604-2 540 FUEL PUMP APERTURES MEC DET I: 15100 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF FUEL PUMP APERTURES  BETWEEN RIB 1 AND 2.  PREP.: FUEL PUMPS REMOVED.  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 642  DETAILED INSPECTION OF FLAP TRACK NO.2  ATTACHMENT AT RIB 5 AND FALSE SPAR  ACCESS: 532AF 532AM  632AF 632AM  571016-0604-1 541 WING RIB 7 TO 8 MEC DET I: 7700 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF INTERNAL STRUCTURE TOP  AND BOTTOM FROM RIBS 7 TO 8 IN PYLON ATTACHMENT AREA  ACCESS: 541CB  641CB  571016-0604-2 541 WING RIB 7 TO 8 MEC DET I: 7400 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF INTERNAL STRUCTURE TOP  AND BOTTOM FROM RIBS 7 TO 8 IN PYLON ATTACHMENT AREA  ACCESS: 541CB  641CB  571016-0604-3 541 WING RIB 7 TO 8 MEC DET I: 7000 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF INTERNAL STRUCTURE TOP  AND BOTTOM FROM RIBS 7 TO 8 IN PYLON ATTACHMENT AREA  ACCESS: 541CB  641CB  571017-0602-1 523 TOP SKIN AT PYLON ATTACHMENT MEC DET T: 20600 FC ALI CN 2006-0071 541 I: 6200 FC FAA AD 96-13 623 DETAILED INSPECTION OF TOP REINFORCING AND ADJACENT  641 SKIN AT ENGINE PYLON ATTACHMENT TO RIB 7 AND RIB 8 ALI REFERENC AND FRONT SPAR. 571017-01-1  571017-0602-2 523 TOP SKIN AT PYLON ATTACHMENT MEC DET T: 20000 FC ALI CN 2006-0071 541 I: 6000 FC FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 641 SKIN AT ENGINE PYLON ATTACHMENT TO RIB 7 AND RIB 8 571017-01-2  AND FRONT SPAR.  571018-0603-1 523 BOTTOM EXTERNAL REINFORCING NDT SDI T: 13400 FC ALI NTM 574110  541 OR PART 4  623 SPECIAL DETAILED INSPECTION OF BOTTOM EXTERNAL 15100 FH CN 2006-0071 641 REINFORCING AND ADJACENT SKIN AT PYLON ATTACHMENT RIB I: 6700 FC FAA AD 96-13 7 TO RIB 8 AND FRONT SPAR TO INCLUDE PYLON FORWARD OR  PICK UP FITTING AND SUPPORT STRUCTURE. 7600 FH ALI REFERENC 571018-01-1  ACCESS: 512AT 512LB 523AB  471AL 471BL 472AR 472BR 473BL 474BR  612AT 612LB 623AB  481AL 481BL 482AR 482BR 483BL 484BR  571018-0603-2 523 BOTTOM EXTERNAL REINFORCING NDT SDI T: 13000 FC ALI NTM 574110  541 OR PART 4  623 SPECIAL DETAILED INSPECTION OF BOTTOM EXTERNAL 17800 FH CN 2006-0071 641 REINFORCING AND ADJACENT SKIN AT PYLON ATTACHMENT RIB I: 6500 FC FAA AD 96-13 7 TO RIB 8 AND FRONT SPAR TO INCLUDE PYLON FORWARD OR  PICK UP FITTING AND SUPPORT STRUCTURE. 8900 FH ALI REFERENC 571018-01-2  ACCESS: 512AT 512LB 523AB  471AL 471BL 472AR 472BR 473BL 474BR  612AT 612LB 623AB  481AL 481BL 482AR 482BR 483BL 484BR  571018-0603-3 523 BOTTOM EXTERNAL REINFORCING NDT SDI T: 12200 FC ALI NTM 574110  541 OR PART 4  623 SPECIAL DETAILED INSPECTION OF BOTTOM EXTERNAL 27700 FH CN 2006-0071 641 REINFORCING AND ADJACENT SKIN AT PYLON ATTACHMENT RIB I: 6100 FC FAA AD 96-13 7 TO RIB 8 AND FRONT SPAR TO INCLUDE PYLON FORWARD OR  PICK UP FITTING AND SUPPORT STRUCTURE. 13800 FH ALI REFERENC 571018-01-3  ACCESS: 512AT 512LB 523AB  471AL 471BL 472AR 472BR 473BL 474BR  612AT 612LB 623AB  481AL 481BL 482AR 482BR 483BL 484BR  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 641  DETAILED INSPECTION OF FRONT SPAR AND  ATTACHMENTS, AFT FACE, FROM RIBS 1 TO 9 INCLUSIVE  ACCESS: 541AB 541BB 541CB 542EB  641AB 641BB 641CB 642EB  571019-0604-2 541 FRONT SPAR AND ATTACHMENTS MEC DET I: 17700 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF FRONT SPAR AND  ATTACHMENTS, AFT FACE, FROM RIBS 1 TO 9 INCLUSIVE  ACCESS: 541AB 541BB 541CB 542EB  641AB 641BB 641CB 642EB  571019-0604-3 541 FRONT SPAR AND ATTACHMENTS MEC DET I: 15100 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF FRONT SPAR AND  ATTACHMENTS, AFT FACE, FROM RIBS 1 TO 9 INCLUSIVE  ACCESS: 541AB 541BB 541CB 542EB  641AB 641BB 641CB 642EB  571020-0603-1 470 WING TO PYLON SPIGOT MEC DET I: 4 YE ISB ISB 57-0101  480  DETAILED INSPECTION OF WING TO PYLON THRUST  LOAD SPIGOT SLEEVE FOR CORROSION  NOTE 01: SPIGOT SLEEVE REMOVED  NOTE 02: AFTER REWORK IN ACCORDANCE WITH SB 57 - 101,  INTERVAL CAN BE EXTENDED TO 8 YE  ACCESS: 471AL 471BL 472AR 472BR  481AL 481BL 482AR 482BR  571021-0604-1 541 CENTER SPAR FORWARD FACE MEC DET I: 17700 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF CENTER SPAR FORWARD  FACE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571021-0604-1 * * * * * C O N T I N U E * * * * *  ACCESS: 541CB  641CB  571021-0604-2 541 CENTER SPAR FORWARD FACE MEC DET I: 17700 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF CENTER SPAR FORWARD  FACE AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8  ACCESS: 541CB  641CB  571021-0604-3 541 CENTER SPAR FORWARD FACE MEC DET I: 15100 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF CENTER SPAR FORWARD  FACE AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8  ACCESS: 541CB  641CB  571022-0604-1 541 CENTER SPAR FORWARD FACE MEC DET I: 27300 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF CENTER SPAR FORWARD  FACE AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 AND  BETWEEN RIBS 8 AND 9.  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571022-0604-2 541 CENTER SPAR FORWARD FACE MEC DET I: 22600 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF CENTER SPAR FORWARD  FACE AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 AND  BETWEEN RIBS 8 AND 9.  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 641  DETAILED INSPECTION OF CENTER SPAR FORWARD  FACE AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 AND  BETWEEN RIBS 8 AND 9.  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571023-0604-1 542 CENTER SPAR AFT FACE MEC DET I: 17700 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF CENTER SPAR AFT FACE  AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8  ACCESS: 542DB 542EB  642DB 642EB  571023-0604-2 542 CENTER SPAR AFT FACE MEC DET I: 17700 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF CENTER SPAR AFT FACE  AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8  ACCESS: 542DB 542EB  642DB 642EB  571023-0604-3 542 CENTER SPAR AFT FACE MEC DET I: 15100 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF CENTER SPAR AFT FACE  AND INTERNAL STRUCTURE BETWEEN RIBS 7 AND 8  ACCESS: 542DB 542EB  642DB 642EB  571024-0604-1 542 CENTER SPAR AFT FACE MEC DET I: 27300 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF CENTER SPAR AFT FACE  AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 AND  BETWEEN RIBS 8 AND 9  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 642  DETAILED INSPECTION OF CENTER SPAR AFT FACE  AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 AND  BETWEEN RIBS 8 AND 9  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB  571024-0604-3 542 CENTER SPAR AFT FACE MEC DET I: 19200 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF CENTER SPAR AFT FACE  AND INTERNAL STRUCTURE BETWEEN RIBS 1 TO 7 AND  BETWEEN RIBS 8 AND 9  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB  571025-0604-1 542 REAR SPAR FORWARD FACE MEC DET I: 27300 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  FROM RIBS 1 TO 3  ACCESS: 542CB  642CB  571025-0604-2 542 REAR SPAR FORWARD FACE MEC DET I: 22600 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  FROM RIBS 1 TO 3  ACCESS: 542CB  642CB  571025-0604-3 542 REAR SPAR FORWARD FACE MEC DET I: 19200 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  FROM RIBS 1 TO 3  ACCESS: 542CB  642CB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 642  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  FROM RIBS 3 TO 9  ACCESS: 542DB 542EB  642DB 642EB  571026-0604-2 542 REAR SPAR FORWARD FACE MEC DET I: 17700 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  FROM RIBS 3 TO 9  ACCESS: 542DB 542EB  642DB 642EB  571026-0604-3 542 REAR SPAR FORWARD FACE MEC DET I: 15100 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  FROM RIBS 3 TO 9  ACCESS: 542DB 542EB  642DB 642EB  571027-0604-1 541 RIB 7,8 HALF RIBS AND ATTA. MEC DET I: 27300 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF RIBS 7 AND 8, HALF RIBS  AND ATTACHMENTS TO BOTTOM SKIN, FRONT SPAR AND CENTER  SPAR  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571027-0604-2 541 RIB 7,8 HALF RIBS AND ATTA. MEC DET I: 22600 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF RIBS 7 AND 8, HALF RIBS  AND ATTACHMENTS TO BOTTOM SKIN, FRONT SPAR AND CENTER  SPAR  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 641  DETAILED INSPECTION OF RIBS 7 AND 8, HALF RIBS  AND ATTACHMENTS TO BOTTOM SKIN, FRONT SPAR AND CENTER  SPAR  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571028-0602-1 571 REAR SPAR AND BOTTOM ANGLE MEC DET I: 6700 FC ALI CN 2006-0071 671 OR FAA AD 96-13 DETAILED INSPECTION OF REAR SPAR AND BOTTOM ANGLE 7600 FH  MEMBER, AFT FACE BETWEEN RIB 1 AND RIB 3. ALI REFERENC 571028-01-1  PREP.: MAIN LANDING GEAR DOORS OPEN.  571028-0602-2 571 REAR SPAR AND BOTTOM ANGLE MEC DET I: 6500 FC ALI CN 2006-0071 671 OR FAA AD 96-13 DETAILED INSPECTION OF REAR SPAR AND BOTTOM ANGLE 8800 FH  MEMBER, AFT FACE BETWEEN RIB 1 AND RIB 3. ALI REFERENC 571028-01-2  PREP.: MAIN LANDING GEAR DOORS OPEN.  571028-0602-3 571 REAR SPAR AND BOTTOM ANGLE MEC DET I: 6100 FC ALI CN 2006-0071 671 OR FAA AD 96-13 DETAILED INSPECTION OF REAR SPAR AND BOTTOM ANGLE 13500 FH  MEMBER, AFT FACE BETWEEN RIB 1 AND RIB 3. ALI REFERENC 571028-01-3  PREP.: 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 5710 642  DETAILED INSPECTION OF RIBS 4,5,6 AND  ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPAR  ACCESS: 542CB 542DB  642CB 642DB  571029-0604-2 542 RIB 4,5,6 AND ATT.TO SKIN MEC DET I: 7400 FC MRB S AMM SSI 5710 642  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AND  ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPAR  ACCESS: 542CB 542DB  642CB 642DB  571029-0604-3 542 RIB 4,5,6 AND ATT.TO SKIN MEC DET I: 7000 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF RIBS 4,5,6 AND  ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPAR  ACCESS: 542CB 542DB  642CB 642DB  571030-0604-1 542 RIB 2,3,7,8 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF RIBS 2,3,7,8 AND  ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPAR  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB  571030-0604-2 542 RIB 2,3,7,8 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF RIBS 2,3,7,8 AND  ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPAR  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB  571030-0604-3 542 RIB 2,3,7,8 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710 642  DETAILED INSPECTION OF RIBS 2,3,7,8 AND  ATTACHMENTS TO SKIN,CENTER SPAR AND REAR SPAR  ACCESS: 542CB 542DB 542EB  642CB 642DB 642EB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 641 I: 11200 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  STRINGERS BETWEEN FRONT- AND CENTER SPAR, RIB 1 ALI REFERENC TO RIB 9. 571031-01-1  571031-0602-2 541 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 17500 FC ALI CN 2006-0071 641 I: 10500 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  STRINGERS BETWEEN FRONT- AND CENTER SPAR, RIB 1 ALI REFERENC TO RIB 9. 571031-01-2  571033-0602-1 541 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 13200 FC ALI CN 2006-0071 641 OR FAA AD 96-13 DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN 14900 FH  AND RIVETS AT STRINGER RUNOUTS AFT OF FRONT SPAR I: 3300 FC ALI REFERENC FROM RIB 2 TO 8 INCLUSIVE. OR 571033-01-1  3700 FH  571033-0602-2 541 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 12800 FC ALI CN 2006-0071 641 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 17500 FH  STRINGER RUNOUTS AFT OF FRONT SPAR RIB 2 TO RIB 8 I: 3200 FC ALI REFERENC INCLUSIVE. OR 571033-01-2  4400 FH  571033-0602-3 541 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 12400 FC ALI CN 2006-0071 641 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 28100 FH  STRINGER RUNOUTS AFT OF FRONT SPAR RIB 2 TO RIB 8 I: 3100 FC ALI REFERENC INCLUSIVE. OR 571033-01-3  7000 FH  571035-0602-1 542 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 18600 FC ALI CN 2006-0071 642 I: 11200 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  STRINGERS BETWEEN CENTER- AND REAR SPAR, RIB 1 TO ALI REFERENC RIB 9. 571035-01-1  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 642 I: 10500 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  STRINGERS BETWEEN CENTER- AND REAR SPAR, RIB 1 TO ALI REFERENC RIB 9. 571035-01-2  571036-0602-1 541 BOTTOM SKIN AND STRINGERS MEC DET I: 10100 FC MRB S AMM SSI 5710 641  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT AND CENTER SPAR AND  RIBS 1 TO 9  571036-0602-2 541 BOTTOM SKIN AND STRINGERS MEC DET I: 9900 FC MRB S AMM SSI 5710 641  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT AND CENTER SPAR AND  RIBS 1 TO 9  571036-0602-3 541 BOTTOM SKIN AND STRINGERS MEC DET I: 9200 FC MRB S AMM SSI 5710 641  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT AND CENTER SPAR AND  RIBS 1 TO 9  571036-0604-1 541 BOTTOM SKIN AND STRINGERS MEC DET I: 27300 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT AND CENTER SPAR FROM RIBS 1  TO 9  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571036-0604-2 541 BOTTOM SKIN AND STRINGERS MEC DET I: 22600 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT AND CENTER SPAR FROM RIBS 1  TO 9  ACCESS: 541AB 541BB 541CB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571036-0604-2 * * * * * C O N T I N U E * * * * *  641AB 641BB 641CB  571036-0604-3 541 BOTTOM SKIN AND STRINGERS MEC DET I: 19200 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT AND CENTER SPAR FROM RIBS 1  TO 9  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571037-0603-1 512 WING BOTTOM SKIN PANEL NUMBER 1 NDT SDI T: 5600 FC ISB NTM 513104  612 I: 900 FC PART 1  SPECIAL DETAILED INSPECTION OF WING BOTTOM SKIN PANEL NTM 570001  NUMBER 1 (REBATED SECTION). PART 6  ISB 57-130  ACCESS: 472AR 512LB  481AL 612LB  571037-0603-2 512 WING BOTTOM SKIN PANEL NUMBER 1 NDT SDI T: 5600 FC ISB NTM 513104  612 I: 900 FC PART 1  SPECIAL DETAILED INSPECTION OF WING BOTTOM SKIN PANEL NTM 570001  NUMBER 1 (REBATED SECTION). PART 6  ISB 57-130  NOTE: TASK VALID FOR RETROFIT 04959 - HOLES  FILLED WITH AERODYNAMIC FILLER.  ACCESS: 472AR 512LB  481AL 612LB  571037-0603-3 512 WING BOTTOM SKIN PANEL NUMBER 1 NDT SDI T: 18400 FC ISB NTM 513104  612 I: 900 FC PART 1  SPECIAL DETAILED INSPECTION OF WING BOTTOM SKIN PANEL NTM 570001  NUMBER 1 (REBATED SECTION). PART 6  ISB 57-130  NOTE: TASK VALID FOR RETROFIT 04959 - HOLES  FILLED WITH INTERFERENCE FIT BOLTS  ACCESS: 472AR 512LB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571037-0603-3 * * * * * C O N T I N U E * * * * *  481AL 612LB  571039-0604-1 541 RIB 2 - 6 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF RIBS 2 TO 6 AND  ATTACHMENTS TO SKIN,FRONT SPAR AND CENTER SPAR  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571039-0604-2 541 RIB 2 - 6 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF RIBS 2 TO 6 AND  ATTACHMENTS TO SKIN,FRONT SPAR AND CENTER SPAR  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571039-0604-3 541 RIB 2 - 6 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710 641  DETAILED INSPECTION OF RIBS 2 TO 6 AND  ATTACHMENTS TO SKIN,FRONT SPAR AND CENTER SPAR  ACCESS: 541AB 541BB 541CB  641AB 641BB 641CB  571040-0602-1 542 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 22500 FC ALI CN 2006-0071 642 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AND STRINGERS 25400 FH  BETWEEN CENTER- AND REAR SPAR AND RIB 1 TO RIB 9. I: 13500 FC ALI REFERENC OR 571040-01-1  15200 FH  571040-0602-2 542 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 21600 FC ALI CN 2006-0071 642 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AND STRINGERS 29400 FH  BETWEEN CENTER- AND REAR SPAR AND RIB 1 TO RIB 9. I: 13000 FC ALI REFERENC OR 571040-01-2  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571040-0602-2 * * * * * C O N T I N U E * * * * *  17700 FH  571040-0602-3 542 BOTTOM SKIN AT STRINGER ATTACHMENT MEC DET T: 20500 FC ALI CN 2006-0071 642 OR FAA AD 96-13 DETAILED INSPECTION OF BOTTOM SKIN AND STRINGERS 45300 FH  BETWEEN CENTER- AND REAR SPAR AND RIB 1 TO RIB 9. I: 12300 FC ALI REFERENC OR 571040-01-3  27200 FH  571041-0604-1 540 UPPER PART OF RIB 9 MEC DET I: 27300 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF UPPER PART OF RIB 9 AND  ATTACHMENTS TO TOP SKIN,FRONT SPAR AND REAR SPAR  ACCESS: 542EB 543AB  642EB 643AB  571041-0604-2 540 UPPER PART OF RIB 9 MEC DET I: 22600 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF UPPER PART OF RIB 9 AND  ATTACHMENTS TO TOP SKIN,FRONT SPAR AND REAR SPAR  ACCESS: 542EB 543AB  642EB 643AB  571041-0604-3 540 UPPER PART OF RIB 9 MEC DET I: 19200 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF UPPER PART OF RIB 9 AND  ATTACHMENTS TO TOP SKIN,FRONT SPAR AND REAR SPAR  ACCESS: 542EB 543AB  642EB 643AB  571042-0604-1 540 LOWER PART OF RIB 9 MEC DET I: 17700 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF LOWER PART OF RIB 9 AND  ATTACHMENTS TO BOTTOM SKIN BETWEEN FRONT SPAR AND  REAR SPAR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571042-0604-1 * * * * * C O N T I N U E * * * * *  ACCESS: 542EB 543AB  642EB 643AB  571042-0604-2 540 LOWER PART OF RIB 9 MEC DET I: 17700 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF LOWER PART OF RIB 9 AND  ATTACHMENTS TO BOTTOM SKIN BETWEEN FRONT SPAR AND  REAR SPAR  ACCESS: 542EB 543AB  642EB 643AB  571042-0604-3 540 LOWER PART OF RIB 9 MEC DET I: 15100 FC MRB S AMM SSI 5710 640  DETAILED INSPECTION OF LOWER PART OF RIB 9 AND  ATTACHMENTS TO BOTTOM SKIN BETWEEN FRONT SPAR AND  REAR SPAR  ACCESS: 542EB 543AB  642EB 643AB  571045-0602-1 543 TOP SKIN ATTACHMENT TO FRONT SPAR MEC DET T: 20300 FC ALI CN 2006-0071 643 I: 12200 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN ATTACHMENT IN FRONT  SPAR, REAR SPAR AND RIB 9 TO RIB 15 INCLUSIVE. ALI REFERENC 571045-01-1  571045-0602-2 543 TOP SKIN ATTACHMENT TO FRONT SPAR MEC DET T: 20000 FC ALI CN 2006-0071 643 I: 12000 FC FAA AD 96-13 DETAILED INSPECTION OF TOP SKIN ATTACHMENT IN FRONT  SPAR, REAR SPAR AND RIB 9 TO RIB 15 INCLUSIVE. ALI REFERENC 571045-01-2  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571045-0602-2 * * * * * C O N T I N U E * * * * *  571047-0602-1 543 BOTTOM SKIN RIBS 9 TO 15 MEC DET T: 13400 FC ALI EASA AD  643 OR 2006-0071  DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 15100 FH FAA AD  TO FRONT SPAR AND REAR SPAR, RIB 9 TO RIB 15, AND TO I: 6700 FC 2007-04-11  RIB 10 TO RIB 14 INCLUSIVE. OR  7600 FH ALI REFERENC 571047-01-1  571047-0602-2 543 BOTTOM SKIN RIBS 9 TO 15 MEC DET T: 12800 FC ALI EASA AD  643 OR 2006-0071  DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 17500 FH FAA AD  TO FRONT SPAR AND REAR SPAR, RIB 9 TO RIB 15, AND TO I: 6400 FC 2007-04-11  RIB 10 TO RIB 14 INCLUSIVE. OR  8700 FH ALI REFERENC 571047-01-2  571047-0602-3 543 BOTTOM SKIN RIBS 9 TO 15 MEC DET T: 12000 FC ALI EASA AD  643 OR 2006-0071  DETAILED INSPECTION OF BOTTOM SKIN AT ATTACHMENT TO 27200 FH FAA AD  TO FRONT SPAR AND REAR SPAR, RIB 9 TO RIB 15, AND TO I: 6000 FC 2007-04-11  RIB 10 TO RIB 14 INCLUSIVE. OR  13600 FH ALI REFERENC 571047-01-3  571049-0602-1 543 ACCESS DOORS BOTT.SKIN MEC DET I: 10100 FC MRB S AMM SSI 5710 643  DETAILED EXTERNAL INSPECTION OF ACCESS DOORS AND  BOTTOM SKIN AT ACCESS DOOR CUTOUTS BETWEEN  RIBS 10 TO 13  571049-0602-2 543 ACCESS DOORS BOTT.SKIN MEC DET I: 9700 FC MRB S AMM SSI 5710 643  DETAILED EXTERNAL INSPECTION OF ACCESS DOORS AND  BOTTOM SKIN AT ACCESS DOOR CUTOUTS BETWEEN  RIBS 10 TO 13  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 643  DETAILED EXTERNAL INSPECTION OF ACCESS DOORS AND  BOTTOM SKIN AT ACCESS DOOR CUTOUTS BETWEEN  RIBS 10 TO 13  571049-0603-1 543 ACCESS DOORS, BOTTOM SKIN MEC DET I: 5 YE MRB S AMM SSI 5710 643  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUT-OUTS BETWEEN RIBS 10 AND 13  ACCESS: 543AB 543BB 543CB  643AB 643BB 643CB  571051-0604-1 543 FRONT SPAR AND ATT.TO RIBS MEC DET I: 17700 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  ATTACHMENTS TO RIBS BETWEEN RIB 9 AND 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571051-0604-2 543 FRONT SPAR AND ATT.TO RIBS MEC DET I: 15100 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  ATTACHMENTS TO RIBS BETWEEN RIB 9 AND 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571051-0604-3 543 FRONT SPAR AND ATT.TO RIBS MEC DET I: 15100 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  ATTACHMENTS TO RIBS BETWEEN RIB 9 AND 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571053-0604-1 543 REAR SPAR AND ATT.TO RIBS MEC DET I: 27300 FC MRB S AMM SSI 5710 643  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FACE  AND ATTACHMENTS TO RIBS BETWEEN RIBS 9 AND 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571053-0604-2 543 REAR SPAR AND ATT.TO RIBS MEC DET I: 22600 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  AND ATTACHMENTS TO RIBS BETWEEN RIBS 9 AND 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571053-0604-3 543 REAR SPAR AND ATT.TO RIBS MEC DET I: 19200 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  AND ATTACHMENTS TO RIBS BETWEEN RIBS 9 AND 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571055-0602-1 543 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 20300 FC ALI CN 2006-0071 550 I: 12200 FC FAA AD 96-13 643 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TO  650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO ALI REFERENC RIB 15. 571055-01-1  571055-0602-2 543 TOP SKIN AT STRINGER ATTACHMENT MEC DET T: 20000 FC ALI CN 2006-0071 550 I: 12000 FC FAA AD 96-13 643 DETAILED INSPECTION OF TOP SKIN AT ATTACHMENT TOMENTS  650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO ALI REFERENC RIB 15. 571055-01-2  571057-0602-1 543 BOTTOM SKIN AT STRINGER MEC DET T: 13400 FC ALI EASA AD  550 OR 2006-0071  643 DETAILED INSPECTION OF BOTTOM SKIN AT STRINGER 15300 FH FAA AD  650 RUNOUTS, RIB 9 TO RIB 15. I: 6700 FC 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571057-0602-1 * * * * * C O N T I N U E * * * * *  OR ALI REFERENC 7600 FH 571057-01-1  571057-0602-2 543 BOTTOM SKIN AT STRINGER MEC DET T: 12800 FC ALI EASA AD  550 OR 2006-0071  643 DETAILED INSPECTION OF BOTTOM SKIN AT STRINGER 17800 FH FAA AD  650 RUNOUTS, RIB 9 TO RIB 15. I: 6400 FC 2007-04-11  OR  8900 FH ALI REFERENC 571057-01-2  571057-0602-3 543 BOTTOM SKIN AT STRINGER MEC DET T: 12000 FC ALI EASA AD  550 OR 2006-0071  643 DETAILED INSPECTION OF BOTTOM SKIN AT STRINGER 27800 FH FAA AD  650 RUNOUTS, RIB 9 TO RIB 15. I: 6000 FC 2007-04-11  OR  13900 FH ALI REFERENC 571057-01-3  571058-0602-1 543 BOTTOM SKIN MEC DET I: 10100 FC ALI EASA AD  550 OR 2006-0071  643 DETAILED INSPECTION OF EXTERNAL BOTTOM SKIN AND 11400 FH FAA AD  650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO 2007-04-11  RIB 15.  ALI REFERENC 571058-01-1  571058-0602-2 543 BOTTOM SKIN MEC DET I: 9600 FC ALI EASA AD  550 OR 2006-0071  643 DETAILED INSPECTION OF EXTERNAL BOTTOM SKIN AND 13100 FH FAA AD  650 STRINGERS BETWEEN FRONT- AND REAR SPAR, RIB 9 TO 2007-04-11  RIB 15.  ALI REFERENC 571058-01-2  571058-0602-3 543 BOTTOM SKIN MEC DET I: 9000 FC ALI EASA AD  550 OR 2006-0071  643 DETAILED INSPECTION OF EXTERNAL BOTTOM SKIN AND 20400 FH  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  RIB 15. 2007-04-11  ALI REFERENC 571058-01-3  571058-0604-1 543 BOTTOM SKIN AND STRINGERS MEC DET I: 27300 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR FROM RIBS  9 TO 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571058-0604-2 543 BOTTOM SKIN AND STRINGERS MEC DET I: 22600 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR FROM RIBS  9 TO 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571058-0604-3 543 BOTTOM SKIN AND STRINGERS MEC DET I: 19200 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR FROM RIBS  9 TO 15  ACCESS: 543AB 543BB 543CB 543DB 550BB  643AB 643BB 643CB 643DB 650BB  571059-0604-1 543 RIB 10 - 15 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF RIBS 10 TO 15  INCLUSIVE, AND ATTACHMENTS TO SKIN  ACCESS: 543AB 543BB 543CB 543DB 550BB 550DB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  571059-0604-2 543 RIB 10 - 15 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF RIBS 10 TO 15  INCLUSIVE, AND ATTACHMENTS TO SKIN  ACCESS: 543AB 543BB 543CB 543DB 550BB 550DB  643AB 643BB 643CB 643DB 650BB 650DB  571059-0604-3 543 RIB 10 - 15 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF RIBS 10 TO 15  INCLUSIVE, AND ATTACHMENTS TO SKIN  ACCESS: 543AB 543BB 543CB 543DB 550BB 550DB  643AB 643BB 643CB 643DB 650BB 650DB  571061-0603-1 543 ATTACH.OF FLAP TRACKS 3 & 4 MEC DET I: 6000 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF FORWARD EXTERNAL  PICK-UP ATTACHMENTS OF FLAP TRACK 3 AND 4 AT RIB 11  AND 15.  ACCESS: 533AF 534AF  633AF 634AF  571062-0602-1 543 FLAP TRACKS 3 AND 4 ATTACH. MEC DET I: 6000 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF ATTACHMENTS OF FLAP  TRACKS TO REAR SPAR AT TRACK 3 AND 4.  NOTE: FLAP EXTENDED  571064-0604-1 543 FORWARD FLAP TRACK ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF PICK UP ATTACHMENTS OF  FLAP 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  643AB 643BB 650BB 650DB  571064-0604-2 543 FORWARD FLAP TRACK ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF PICK UP ATTACHMENTS OF  FLAP TRACKS NO. 3 AND 4 AT RIBS 11 AND 15  ACCESS: 543AB 543BB 550BB 550DB  643AB 643BB 650BB 650DB  571064-0604-3 543 FORWARD FLAP TRACK ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710 643  DETAILED INSPECTION OF PICK UP ATTACHMENTS OF  FLAP TRACKS NO. 3 AND 4 AT RIBS 11 AND 15  ACCESS: 543AB 543BB 550BB 550DB  643AB 643BB 650BB 650DB  571065-0602-1 550 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETS  AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS FROM  RIB 15 TO 27 INCLUSIVE  571065-0602-2 550 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETS  AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS FROM  RIB 15 TO 27 INCLUSIVE  571065-0602-3 550 TOP SKIN MEC DET I: 11200 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETS  AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS FROM  RIB 15 TO 27 INCLUSIVE  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571067-0602-1 550 BOTTOM SKIN MEC DET I: 9700 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  RIVETS AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS  FROM RIB 15 TO 27 INCLUSIVE  571067-0602-2 550 BOTTOM SKIN MEC DET I: 9500 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  RIVETS AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS  FROM RIB 15 TO 27 INCLUSIVE  571067-0602-3 550 BOTTOM SKIN MEC DET I: 9100 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  RIVETS AT ATTACHMENT TO FRONT SPAR,REAR SPAR AND RIBS  FROM RIB 15 TO 27 INCLUSIVE  571069-0603-1 550 ACCESS DOORS, BOTTOM SKIN MEC DET I: 5 YE MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 13 AND 22  NOTE: IN CASE OF FINDING AND IF A/C IS POST MOD 1824  PERFORM AT THE SAME TIME INSPECTION OF OTHER  DOORS/CUTOUTS LISTED IN TASK REF 571069-0604-1  ACCESS: 543DB 550BB 550DB 550EB 550FB 550GB  550KB 550LB  643DB 650BB 650DB 650EB 650FB 650GB  650KB 650LB  571069-0604-1 550 ACCESS DOORS AND BOTT.SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUT-OUTS BETWEEN RIBS 17 AND 18  AND BETWEEN RIBS 19 AND 22  NOTE: DOOR OPENED  ACCESS: 550FB 550GB 550KB 550LB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571069-0604-1 * * * * * C O N T I N U E * * * * *  650FB 650GB 650KB 650LB  571070-0602-1 550 ACCESS DOORS AND BOTTOM SKIN AT CUTOUTS MEC DET I: 9700 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS,FROM RIB 13 TO 27  571070-0602-2 550 ACCESS DOORS AND BOTTOM SKIN AT CUTOUTS MEC DET I: 9500 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS,FROM RIB 13 TO 27  571070-0602-3 550 ACCESS DOORS AND BOTTOM SKIN AT CUTOUTS MEC DET I: 9100 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS,FROM RIB 13 TO 27  571070-0603-1 550 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 5 YE MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS BETWEEN RIB 22 AND 27.  NOTE: THIS TASK COVERS THE PRE MOD 1824 CASE BETWEEN  RIBS 23 AND 26.  ACCESS: 550LB 550MB 550NB 550PB 550QB  650LB 650MB 650NB 650PB 650QB  571070-0604-1 550 ACCESS DOORS, BOTTOM SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 23 AND 26  NOTE: DOOR OPENED  ACCESS: 550MB 550NB 550PB  650MB 650NB 650PB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 23 AND 26  NOTE: DOOR OPENED  ACCESS: 550MB 550NB 550PB  650MB 650NB 650PB  571070-0604-3 550 ACCESS DOORS, BOTTOM SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF ACCESS DOORS AND BOTTOM  SKIN AT ACCESS DOOR CUTOUTS BETWEEN RIBS 23 AND 26  NOTE: DOOR OPENED  ACCESS: 550MB 550NB 550PB  650MB 650NB 650PB  571071-0604-1 550 FRONT SPAR AND RIBS ATTACH MEC DET I: 17700 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  ATTACHMENTS OF RIBS FROM RIB 15 TO 27 INCLUSIVE  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571071-0604-2 550 FRONT SPAR AND RIBS ATTACH MEC DET I: 17700 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  ATTACHMENTS OF RIBS FROM RIB 15 TO 27 INCLUSIVE  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 650  DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  ATTACHMENTS OF RIBS FROM RIB 15 TO 27 INCLUSIVE  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571072-0603-1 550 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 5 YE MRB S AMM SSI 5710 650  DETAILED INSPECTION OF WING BOTTOM SKIN AT  ACCESS DOOR CUTOUTS BETWEEN RIBS 13 AND 22  NOTE: THIS TASK COVERS THE PRE MOD 1824 CASE BETWEEN  RIBS 19 AND 22.  ACCESS: 543DB 550BB 550DB 550EB 550FB 550GB  550KB 550LB  643DB 650BB 650DB 650EB 650FB 650GB  650KB 650LB  571072-0604-2 550 BOTTOM SKIN AT DOOR CUTOUTS MEC DET I: 19200 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF WING BOTTOM SKIN AT  ACCESS DOOR CUTOUTS BETWEEN RIBS 17 AND 18 AND  BETWEEN RIBS 19 AND 22  NOTE: DOORS OPENED  ACCESS: 550FB 550GB 550KB 550LB  650FB 650GB 650KB 650LB  571073-0604-1 550 REAR SPAR AND RIBS ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  AND ATTACHMENTS OF RIBS FROM RIBS 15 TO 27 INCLUSIVE  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 650QB  571073-0604-2 550 REAR SPAR AND RIBS ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  AND ATTACHMENTS OF RIBS FROM RIBS 15 TO 27 INCLUSIVE  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571073-0604-3 550 REAR SPAR AND RIBS ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF REAR SPAR FORWARD FACE  AND ATTACHMENTS OF RIBS FROM RIBS 15 TO 27 INCLUSIVE  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571075-0604-1 550 RIB 16-27 AND ATT.TO SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF RIBS 16 TO 27 AND  ATTACHMENTS TO SKIN  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571075-0604-2 550 RIB 16-27 AND ATT.TO SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF RIBS 16 TO 27 AND  ATTACHMENTS TO SKIN  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  650KB 650LB 650MB 650NB 650PB 650QB  571075-0604-3 550 RIB 16-27 AND ATT.TO SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF RIBS 16 TO 27 AND  ATTACHMENTS TO SKIN  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571077-0602-1 550 TOP SKIN AT STRINGER ATTACH MEC DET I: 11400 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETS  AT ATTACHMENTS TO STRINGERS BETWEEN FRONT SPAR AND  REAR SPAR AND RIBS 15 TO 27  571077-0602-2 550 TOP SKIN AT STRINGER ATTACH MEC DET I: 11400 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETS  AT ATTACHMENTS TO STRINGERS BETWEEN FRONT SPAR AN  REAR SPAR AND RIBS 15 TO 27  571077-0602-3 550 TOP SKIN AT STRINGER ATTACH MEC DET I: 11200 FC MRB S AMM SSI 5710 650  DETAILED EXTERNAL INSPECTION OF TOP SKIN AND RIVETS  AT ATTACHMENTS TO STRINGERS BETWEEN FRONT SPAR AND  REAR SPAR AND RIBS 15 TO 27  571080-0602-1 550 BOTTOM SKIN AT STRINGER RUN-OUTS AND MEC DET I: 9700 FC MRB S AMM SSI 5710 650 ATTACHMENTS AMM SSI 5710 DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  RIVETS AT STRINGER ATTACHMENTS AND RUN-OUTS BETWEEN  FRONT SPAR AND REAR SPAR, FROM RIB 15 TO 27  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 650 ATTACHMENTS AMM SSI 5710 DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  RIVETS AT STRINGER ATTACHMENTS AND RUN-OUTS BETWEEN  FRONT SPAR AND REAR SPAR, FROM RIB 15 TO 27  571080-0602-3 550 BOTTOM SKIN AT STRINGER RUN-OUTS AND MEC DET I: 9100 FC MRB S AMM SSI 5710 650 ATTACHMENTS AMM SSI 5710 DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AND  RIVETS AT STRINGER ATTACHMENTS AND RUN-OUTS BETWEEN  FRONT SPAR AND REAR SPAR, FROM RIB 15 TO 27  571080-0604-1 550 BOTTOM SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR, FROM RIB  15 TO 27  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571080-0604-2 550 BOTTOM SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR, FROM RIB  15 TO 27  ACCESS: 550DB 550EB 550FB 550GB 550HB 550JB  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571080-0604-3 550 BOTTOM SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR, FROM RIB  15 TO 27  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  550KB 550LB 550MB 550NB 550PB 550QB  650DB 650EB 650FB 650GB 650HB 650JB  650KB 650LB 650MB 650NB 650PB 650QB  571083-0603-1 550 ATTACH.OF FLAP TRACK 5 & 6 MEC DET I: 6000 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF FWD EXTERNAL PICK-UP  ATTACHMENTS OF FLAP TRACKS 5 AND 6 AT RIBS 18 AND 22  ACCESS: 535AF 536AF  635AF 636AF  571084-0602-1 550 FLAP TRACK 5 AND 6 ATTACH. MEC DET I: 3000 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF NO.5 AND 6 FLAP  TRACK ATTACHMENTS TO REAR SPAR  NOTE: FLAP EXTENDED  571085-0602-1 560 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710 660  DETAILED EXTERNAL INSPECTION OF TOP SKIN AT  ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROM  RIB 27 TO 29 INCLUSIVE  571085-0602-2 560 TOP SKIN MEC DET I: 11400 FC MRB S AMM SSI 5710 660  DETAILED EXTERNAL INSPECTION OF TOP SKIN AT  ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROM  RIB 27 TO 29 INCLUSIVE  571085-0602-3 560 TOP SKIN MEC DET I: 11200 FC MRB S AMM SSI 5710 660  DETAILED EXTERNAL INSPECTION OF TOP SKIN AT  ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROM  RIB 27 TO 29 INCLUSIVE  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5710 650  DETAILED INSPECTION OF INTERNAL FORWARD  PICK-UP ATTACHMENTS OF FLAP TRACKS NO.5 AND 6 AT RIBS  18 AND 22  ACCESS: 550FB 550GB 550KB 550LB  650FB 650GB 650KB 650LB  571086-0604-2 550 FORWARD FLAP TRACK ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF INTERNAL FORWARD  PICK-UP ATTACHMENTS OF FLAP TRACKS NO.5 AND 6 AT RIBS  18 AND 22  ACCESS: 550FB 550GB 550KB 550LB  650FB 650GB 650KB 650LB  571086-0604-3 550 FORWARD FLAP TRACK ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710 650  DETAILED INSPECTION OF INTERNAL FORWARD  PICK-UP ATTACHMENTS OF FLAP TRACKS NO.5 AND 6 AT RIBS  18 AND 22  ACCESS: 550FB 550GB 550KB 550LB  650FB 650GB 650KB 650LB  571087-0602-1 560 BOTTOM SKIN MEC DET I: 9700 FC MRB S AMM SSI 5710 660  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AT  ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROM  RIB 27 TO 29  571087-0602-2 560 BOTTOM SKIN MEC DET I: 9500 FC MRB S AMM SSI 5710 660  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AT REFERENC ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROM  RIB 27 TO 29  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571087-0602-3 560 BOTTOM SKIN MEC DET I: 9100 FC MRB S AMM SSI 5710 660  DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN AT  ATTACHMENTS TO FRONT SPAR, REAR SPAR AND RIBS FROM  RIB 27 TO 29  571091-0604-1 560 FRONT AND REAR SPAR AND RIBS ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  REAR SPAR FORWARD FACE AND ATTACHMENTS OF RIBS FROM  RIB 27 TO 29 INCLUSIVE.  ACCESS: 560AB 560BB  660AB 660BB  571091-0604-2 560 FRONT AND REAR SPAR AND RIBS ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  REAR SPAR FORWARD FACE AND ATTACHMENTS OF RIBS FROM  RIB 27 TO 29 INCLUSIVE.  ACCESS: 560AB 560BB  660AB 660BB  571091-0604-3 560 FRONT AND REAR SPAR AND RIBS ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED INSPECTION OF FRONT SPAR AFT FACE AND  REAR SPAR FORWARD FACE AND ATTACHMENTS OF RIBS FROM  RIB 27 TO 29 INCLUSIVE.  ACCESS: 560AB 560BB  660AB 660BB  571097-0602-1 560 BOTTOM SKIN MEC DET I: 6400 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AND RIVETS AT STRINGER ATTACHMENTS BETWEEN FRONT  SPAR AND REAR SPAR INCLUDING APPERTURES, BETWEEN RIBS  27 AND 29  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571097-0602-2 560 BOTTOM SKIN MEC DET I: 6300 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN  AND RIVETS AT STRINGER ATTACHMENTS BETWEEN FRONT SPAR  AND REAR SPAR INCLUDING APPERTURES, BETWEEN RIBS 27  AND 29  571097-0602-3 560 BOTTOM SKIN MEC DET I: 6200 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED EXTERNAL INSPECTION OF BOTTOM SKIN  AND RIVETS AT STRINGER ATTACHMENTS BETWEEN FRONT SPAR  AND REAR SPAR INCLUDING APPERTURES, BETWEEN RIBS 27  AND 29  571097-0604-1 560 BOTTOM SKIN MEC DET I: 27300 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR INCLUDING  APERTURES FROM RIBS 27 TO 29  ACCESS: 560AB 560BB  660AB 660BB  571097-0604-2 560 BOTTOM SKIN MEC DET I: 22600 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR INCLUDING  APERTURES FROM RIBS 27 TO 29  ACCESS: 560AB 560BB  660AB 660BB  571097-0604-3 560 BOTTOM SKIN MEC DET I: 19200 FC MRB S AMM SSI 5710 660 AMM SSI 5710 DETAILED INSPECTION OF BOTTOM SKIN AND  STRINGERS BETWEEN FRONT SPAR AND REAR SPAR INCLUDING  APERTURES FROM RIBS 27 TO 29  ACCESS: 560AB 560BB  660AB 660BB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 571127  600 57-206 PART 1  SPECIAL DETAILED INSPECTION OF CRACKED HOLES REPAIRED PART 4  BY COLD WORKING. PART 6  CN  2000-434-321 ISB 57-206  571100-0603-1 530 FLAP TRACK 2 TO 6 CARRIAGE DRIVE MEC DET I: 5 YE CPCP MRB REFERENC 630 ASSEMBLIES 571100-C603- DETAILED INSPECTION OF FLAP TRACK 2 TO 6  CARRIAGE DRIVE ASSEMBLIES, INCLUDING TAB DRIVE LEVER  MOUNTINGS 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 5711 632 OR MRB S NTM 574111  SPECIAL DETAILED INSPECTION OF INTERNAL STRUCTURE OF 10 YE PART 7  FLAP TRACK BEAM N° 2.  MRB REFERENC NOTE: 01. SCREW JACK REMOVED  02. FLAPS FULLY EXTENDED, FLAP TRACK FAIRING 571103-C604- DETACHED  BOROSCOPE NOTE 1: FLEXIBLE BOROSCOPE DOES NOT REQUIRE  SCREW YACK REMOVAL.  (NTM 57.41.11 PART 7)  BOROSCOPE NOTE 2: RIGID BOROSCOPE REQUESTS SCREW  JACK REMOVAL  ACCESS: 532AF 532AM  632AF 632AM  571103-0604-2 532 FLAP TRACK 2 BEAM INTERIOR NDT SDI I: 22600 FC CPCP AMM SSI 5711 632 OR MRB S NTM 574111  SPECIAL DETAILED INSPECTION OF FLAP TRACK 2 BEAM 10 YE PART 7  INTERIOR  NOTE: 01. SCREW JACK REMOVED  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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- DETACHED  BOROSCOPE NOTE 1: FLEXIBLE BOROSCOPE DOES NOT REQUIRE  SCREW YACK REMOVAL.  (NTM 57.41.11 PART 7)  BOROSCOPE NOTE 2: RIGID BOROSCOPE REQUESTS SCREW  JACK REMOVAL  ACCESS: 532AF 532AM  632AF 632AM  571103-0604-3 532 FLAP TRACK 2 BEAM INTERIOR NDT SDI I: 19200 FC CPCP AMM SSI 5711 632 OR MRB S NTM 574111  SPECIAL DETAILED INSPECTION OF FLAP TRACK 2 BEAM 10 YE PART 7  INTERIOR  MRB REFERENC NOTE: 01. SCREW JACK REMOVED  02. FLAPS FULLY EXTENDED, FLAP TRACK FAIRING 571103-C604- DETACHED  BOROSCOPE NOTE 1: FLEXIBLE BOROSCOPE DOES NOT REQUIRE  SCREW YACK REMOVAL.  (NTM 57.41.11 PART 7)  BOROSCOPE NOTE 2: RIGID BOROSCOPE REQUESTS SCREW  JACK REMOVAL  ACCESS: 532AF 532AM  632AF 632AM  571105-0604-1 530 FLAP TRACK 3, 4, 5 AND 6 BEAM INTERIOR NDT SDI I: 27300 FC CPCP AMM SSI 5711 630 OR MRB S AMM SSI 5711 SPECIAL DETAILED INSPECTION OF FLAP TRACK 3, 4, 5 AND 10 YE AMM SSI 5711 6 BEAM INTERIOR. AMM SSI 5711 NTM 574111  BOROSCOPE NOTES AS FOLLOWS: PART 7  NOTE 1: FLEXIBLE BOROSCOPE DOES NOT  REQUIRE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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- SCREW JACK REMOVAL 571105-C604- NOTE 3: SCREW JACK REMOVED  NOTE 4: FLAPS FULLY EXTENDED, FLAP TRACK FAIRINGS  DETACHED  ACCESS: 533AF 533AM 534AF 534AM 535AF 535AM  536AF 536AM  633AF 633AM 634AF 634AM 635AF 635AM  636AF 636AM  571105-0604-2 533 FLAP TRACK 3, 4, 5 AND 6 BEAM INTERIOR NDT SDI I: 22600 FC CPCP AMM SSI 5711 633 OR MRB S AMM SSI 5711 SPECIAL DETAILED INSPECTION OF FLAP TRACK 3, 4, 5 AND 10 YE AMM SSI 5711 6 BEAM INTERIOR AMM SSI 5711 NTM 574111  BOROSCOPE NOTES: 01. FLEXIBLE BOROSCOPE DOES NOT PART 7  REQUIRE SCREW JACK REMOVAL  (NTM 57.41.11. PART 7) MRB REFERENC 02. RIGID BOROSCOPE REQUESTS  SCREW JACK REMOVAL 571103-C604- 571105-C604- NOTE: 01. FLAPS FULLY EXTENDED, FLAP TRACK FAIRINGS  DETACHED  ACCESS: 533AF 533AM 534AF 534AM 535AF 535AM  536AF 536AM  633AF 633AM 634AF 634AM 635AF 635AM  636AF 636AM  571105-0604-3 533 FLAP TRACK 3, 4, 5 AND 6 BEAM INTERIOR NDT SDI I: 19200 FC CPCP AMM SSI 5711 633 OR MRB S AMM SSI 5711 SPECIAL DETAILED INSPECTION OF FLAP TRACK 3, 4, 5 AND 10 YE AMM SSI 5711 6 BEAM INTERIOR AMM SSI 5711 NTM 574111  BOROSCOPE NOTES: 01. FLEXIBLE BOROSCOPE DOES NOT PART 7  REQUIRE SCREW JACK REMOVAL  (NTM 57.41.11. PART 7) MRB REFERENC 02. RIGID BOROSCOPE REQUESTS  SCREW JACK REMOVAL 571103-C604- 571105-C604- * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FAIRINGS  DETACHED  ACCESS: 533AF 533AM 534AF 534AM 535AF 535AM  536AF 536AM  633AF 633AM 634AF 634AM 635AF 635AM  636AF 636AM  571106-0604-1 533 FLAP TRACK 3, 4, 5 AND 6 BEAM EXTERIOR NDT SDI I: 17700 FC CPCP AMM SSI 5711 633 OR MRB S AMM SSI 5711 SPECIAL DETAILED INSPECTION TRACK NO. 3, 4, 5 AND 6 5 YE AMM SSI 5711 BEAM EXTERIOR. AMM SSI 5711 NTM 572511  ACCESS: 533AF 533AM 534AF 534AM 535AF 535AM PART 4  536AF 536AM NTM 572512  633AF 633AM 634AF 634AM 635AF 635AM PART 4  636AF 636AM NTM 572513  PART 6  571106-0604-3 533 FLAP TRACK 3, 4, 5 AND 6 BEAM EXTERIOR NDT SDI I: 15100 FC CPCP AMM SSI 5711 633 OR MRB S AMM SSI 5711 SPECIAL DETAILED INSPECTION OF TRACK NO. 3, 4, 5 AND 5 YE AMM SSI 5711 6 BEAM EXTERIOR. AMM SSI 5711 NTM 572511  ACCESS: 533AF 533AM 534AF 534AM 535AF 535AM PART 4  536AF 536AM NTM 572512  633AF 633AM 634AF 634AM 635AF 635AM PART 4  636AF 636AM NTM 572513  PART 6  571113-0604-1 523 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711 623  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FACE  AND ATTACHED STRUCTURE BETWEEN RIB 9 AND 17  NOTE: HEAT SHIELD REMOVED  ACCESS: 523CB 523DB 523EB 523FB 523GB 523HB  523JB 523KB 523LB 523MB  623CB 623DB 623EB 623FB 623GB 623HB  623JB 623KB 623LB 623MB  571113-0604-2 523 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711 623  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 9 AND 17  NOTE: HEAT SHIELD REMOVED  ACCESS: 523CB 523DB 523EB 523FB 523GB 523HB  523JB 523KB 523LB 523MB  623CB 623DB 623EB 623FB 623GB 623HB  623JB 623KB 623LB 623MB  571113-0604-3 523 FRONT SPAR AND ATTACH.STRU. MEC DET I: 15100 FC MRB S AMM SSI 5711 623  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 9 AND 17  NOTE: HEAT SHIELD REMOVED  ACCESS: 523CB 523DB 523EB 523FB 523GB 523HB  523JB 523KB 523LB 523MB  623CB 623DB 623EB 623FB 623GB 623HB  623JB 623KB 623LB 623MB  571115-0604-1 512 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711 612  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 1 AND 9  NOTE: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571115-0604-1 * * * * * C O N T I N U E * * * * *  INSPECTION  ACCESS: 512AB 512BB 512CB 512DB 512EB 512FB  512GB 512HB 512JB 512KB 512LB 523AB  523BB 523CB  612AB 612BB 612CB 612DB 612EB 612FB  612GB 612HB 612JB 612KB 612LB 623AB  623BB 623CB  571115-0604-2 512 FRONT SPAR AND ATTACH.STRU. MEC DET I: 17700 FC MRB S AMM SSI 5711 612  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 1 AND 9  NOTE: HEAT SHIELD REMOVAL AT 24400 FC AND FURTHER  INSPECTION  ACCESS: 512AB 512BB 512CB 512DB 512EB 512FB  512GB 512HB 512JB 512KB 512LB 523AB  523BB 523CB  612AB 612BB 612CB 612DB 612EB 612FB  612GB 612HB 612JB 612KB 612LB 623AB  623BB 623CB  571115-0604-3 512 FRONT SPAR AND ATTACH.STRU. MEC DET I: 15100 FC MRB S AMM SSI 5711 612  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 1 AND 9  NOTE: HEAT SHIELD REMOVAL AT 24400 FC AND FURTHER  INSPECTION  ACCESS: 512AB 512BB 512CB 512DB 512EB 512FB  512GB 512HB 512JB 512KB 512LB 523AB  523BB 523CB  612AB 612BB 612CB 612DB 612EB 612FB  612GB 612HB 612JB 612KB 612LB 623AB  623BB 623CB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5711 624  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 17 AND 27  NOTE: HEAT SHIELD REMOVED  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  571117-0604-2 524 FRONT SPAR AND ATTACH.STRU. MEC DET I: 22600 FC MRB S AMM SSI 5711 624  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 17 AND 27  NOTE: HEAT SHIELD REMOVED  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  571117-0604-3 524 FRONT SPAR AND ATTACH.STRU. MEC DET I: 19200 FC MRB S AMM SSI 5711 624  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND ATTACHED STRUCTURE BETWEEN RIB 17 AND 27  NOTE: HEAT SHIELD REMOVED  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  571118-0604-1 524 FRONT SPAR AND RIB ATTACH. MEC DET I: 27300 FC MRB S AMM SSI 5711 624  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND RIB ATTACHMENTS BETWEEN RIB 27 AND 29  ACCESS: 524KB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571118-0604-1 * * * * * C O N T I N U E * * * * *  624KB  571118-0604-2 524 FRONT SPAR AND RIB ATTACH. MEC DET I: 22600 FC MRB S AMM SSI 5711 624  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND RIB ATTACHMENTS BETWEEN RIB 27 AND 29  ACCESS: 524KB  624KB  571118-0604-3 524 FRONT SPAR AND RIB ATTACH. MEC DET I: 19200 FC MRB S AMM SSI 5711 624  DETAILED INSPECTION OF FRONT SPAR FORWARD FACE  AND RIB ATTACHMENTS BETWEEN RIB 27 AND 29  ACCESS: 524KB  624KB  571131-0604-1 572 FALSE SPAR SHROUD MEC DET I: 27300 FC MRB S AMM SSI 5711 672  DETAILED INSPECTION OF FALSE SPAR  SHROUD AFT FACE AND OTHER ATTACHMENTS BETWEEN RIB 5  AND 6A.  NOTE: FLAP EXTENDED  ACCESS: 572GB 572LB  672GB 672LB  571131-0604-2 572 FALSE SPAR SHROUD MEC DET I: 22600 FC MRB S AMM SSI 5711 672  DETAILED INSPECTION OF FALSE SPAR  SHROUD AFT FACE AND OTHER ATTACHMENTS BETWEEN RIB 5  AND 6A.  NOTE: FLAP EXTENDED  ACCESS: 572GB 572LB  672GB 672LB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5711 672  DETAILED INSPECTION OF FALSE SPAR  SHROUD AFT FACE AND OTHER ATTACHMENTS BETWEEN RIB 5  AND 6A.  NOTE: FLAP EXTENDED  ACCESS: 572GB 572LB  672GB 672LB  571132-0604-1 575 ALL SPEED AILERON JACK LUGS MEC DET I: 27300 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF JACK ATTACHMENT LUGS  AND AILERON HINGE RIB ATTACHMENTS AT FALSE SPAR  BETWEEN RIB 6A AND 7A  ACCESS: 575CB 575CT  675CB 675CT  571132-0604-2 575 ALL SPEED AILERON JACK LUGS MEC DET I: 22600 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF JACK ATTACHMENT LUGS  AND AILERON HINGE RIB ATTACHMENTS AT FALSE SPAR  BETWEEN RIB 6A AND 7A  ACCESS: 575CB 575CT  675CB 675CT  571132-0604-3 575 ALL SPEED AILERON JACK LUGS MEC DET I: 19200 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF JACK ATTACHMENT LUGS  AND AILERON HINGE RIB ATTACHMENTS AT FALSE SPAR  BETWEEN RIB 6A AND 7A  ACCESS: 575CB 575CT  675CB 675CT  571135-0604-1 575 ALL SPEED AILERON JACK BAY MEC DET I: 27300 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF ALL SPEED AILERON JACK  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571135-0604-1 * * * * * C O N T I N U E * * * * *  BAY  ACCESS: 575CB 575CT 576AB  675CB 675CT 676AB  571135-0604-2 575 ALL SPEED AILERON JACK BAY MEC DET I: 22600 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF ALL SPEED AILERON JACK  BAY  ACCESS: 575CB 575CT 576AB  675CB 675CT 676AB  571135-0604-3 575 ALL SPEED AILERON JACK BAY MEC DET I: 19200 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF ALL SPEED AILERON JACK  BAY  ACCESS: 575CB 575CT 576AB  675CB 675CT 676AB  571136-0602-1 575 TOP SKIN AT RIBS 6A AND 7A. MEC DET I: 9000 FC MRB S AMM SSI 5711 675  DETAILED EXTERNAL INSPECTION OF TOP  SKIN AND RIVETS AT ATTACHMENT TO RIBS 6A AND 7A  571137-0604-1 575 RIB 5.PORT.AFT OF REAR SPAR MEC DET I: 17700 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF RIB 5 PORTION AFT OF  REAR SPAR  ACCESS: 575AB  675AB  571137-0604-2 575 RIB 5.PORT.AFT OF REAR SPAR MEC DET I: 17700 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF RIB 5 PORTION AFT OF  REAR SPAR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571137-0604-2 * * * * * C O N T I N U E * * * * *  ACCESS: 575AB  675AB  571137-0604-3 575 RIB 5.PORT.AFT OF REAR SPAR MEC DET I: 15100 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF RIB 5 PORTION AFT OF  REAR SPAR  ACCESS: 575AB  675AB  571139-0602-1 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6700 FC MRB S AMM SSI 5711 675  DETAILED EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE FROM RIB 3 TO 5  NOTE: FLAP EXTENDED  571139-0602-2 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6500 FC MRB S AMM SSI 5711 675  DETAILED EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE FROM RIB 3 TO 5  NOTE: FLAP EXTENDED  571139-0602-3 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6100 FC MRB S AMM SSI 5711 675  DETAILED EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE FROM RIB 3 TO 5  NOTE: FLAP EXTENDED  571139-0604-1 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE FROM RIB 3 TO 9 INCLUSIVE  ACCESS: 575AB 575AT 575BB 575EB 575FB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  571139-0604-2 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE FROM RIB 3 TO 9 INCLUSIVE  ACCESS: 575AB 575AT 575BB 575EB 575FB  675AB 675AT 675BB 675EB 675FB  571139-0604-3 575 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE FROM RIB 3 TO 9 INCLUSIVE  ACCESS: 575AB 575AT 575BB 575EB 575FB  675AB 675AT 675BB 675EB 675FB  571141-0604-1 575 FALSE SPAR AND ATTACHMENTS MEC DET I: 27300 FC MRB S AMM SSI 5711 675 AMM SSI 5711 DETAILED INSPECTION OF FALSE SPAR FORWARD FACE  AND ATTACHMENTS BETWEEN RIB 5 AND 6A INCLUSIVE.  INCLUDING RIB 5A AND ITS ATTACHMENTS.  ACCESS: 575AB  675AB  571141-0604-2 575 FALSE SPAR AND ATTACHMENTS MEC DET I: 22600 FC MRB S AMM SSI 5711 675 AMM SSI 5711 DETAILED INSPECTION OF FALSE SPAR FORWARD FACE  AND ATTACHMENTS BETWEEN RIB 5 AND 6A INCLUSIVE.  INCLUDING RIB 5A AND ITS ATTACHMENTS.  ACCESS: 575AB  675AB  571141-0604-3 575 FALSE SPAR AND ATTACHMENTS MEC DET I: 19200 FC MRB S AMM SSI 5711 675 AMM SSI 5711 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FACE  AND ATTACHMENTS BETWEEN RIB 5 AND 6A INCLUSIVE.  INCLUDING RIB 5A AND ITS ATTACHMENTS.  ACCESS: 575AB  675AB  571146-0602-1 575 BOTT.SKIN AT RIB 5 AND 5A. MEC DET I: 3000 FC MRB S AMM SSI 5711 675  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AT ATTACHMENT TO RIBS 5 AND 5A,AFT OF REAR SPAR  571147-0604-1 575 RIBS 6 TO 9 JACK BEAM AND ATTACHMENTS MEC DET I: 27300 FC MRB S AMM SSI 5711 675 AMM SSI 5711 DETAILED INSPECTION OF RIBS 6, 6A, 7A, 8, 9  AND THEIR ATTACHMENTS AFT OF REAR SPAR, INCLUDING  JACK BEAM AND SUPPORT STRUCTURE  ACCESS: 575AB 575BB 575DB 575EB 575FB 575GB  675AB 675BB 675DB 675EB 675FB 675GB  571147-0604-2 575 RIBS 6 TO 9 JACK BEAM AND ATTACHMENTS MEC DET I: 22600 FC MRB S AMM SSI 5711 675 AMM SSI 5711 DETAILED INSPECTION OF RIBS 6, 6A, 7A, 8, 9  AND THEIR ATTACHMENTS AFT OF REAR SPAR, INCLUDING  JACK BEAM AND SUPPORT STRUCTURE  ACCESS: 575AB 575BB 575DB 575EB 575FB 575GB  675AB 675BB 675DB 675EB 675FB 675GB  571147-0604-3 575 RIBS 6 TO 9 JACK BEAM AND ATTACHMENTS MEC DET I: 19200 FC MRB S AMM SSI 5711 675 AMM SSI 5711 DETAILED INSPECTION OF RIBS 6, 6A, 7A, 8, 9  AND THEIR ATTACHMENTS AFT OF REAR SPAR, INCLUDING  JACK BEAM AND SUPPORT STRUCTURE  ACCESS: 575AB 575BB 575DB 575EB 575FB 575GB  675AB 675BB 675DB 675EB 675FB 675GB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5711 675  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AT ATTACHMENTS OF RIBS,STIFFENERS,FALSE SPAR  AND INTERCOSTALS, AFT OF REAR SPAR BETWEEN RIB 5A  AND 9  571150-0602-1 575 TOP SKIN ACCESS DOOR MEC DET I: 9000 FC MRB S AMM SSI 5711 675  DETAILED EXTERNAL INSPECTION OF ACCESS  DOORS AND TOP SKIN ACCESS DOOR APERTURES, AFT OF REAR  SPAR AND INBOARD OF RIB 6A  571153-0602-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 3300 FC MRB S AMM SSI 5711 681  DETAILED VISUAL EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 9  AND 19  NOTE: FLAP FULLY EXTENDED  571153-0602-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 3200 FC MRB S AMM SSI 5711 681  DETAILED EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 9  AND 19  NOTE: FLAP EXTENDED  571153-0602-3 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 3000 FC MRB S AMM SSI 5711 681  DETAILED EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 9  AND 19  NOTE: FLAP FULLY EXTENDED  571153-0604-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711 681  DETAILED 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 19  ACCESS: 581CB 581DB 581EB 581FB 581GB  681CB 681DB 681EB 681FB 681GB  571153-0604-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711 681  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 9 AND 19  ACCESS: 581CB 581DB 581EB 581FB 581GB  681CB 681DB 681EB 681FB 681GB  571153-0604-3 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711 681  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 9 AND 19  ACCESS: 581CB 581DB 581EB 581FB 581GB  681CB 681DB 681EB 681FB 681GB  571155-0602-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6400 FC MRB S AMM SSI 5711 681  DETAILED VISUAL EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 19  AND 22  NOTE: FLAP FULLY EXTENDED  571155-0602-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 6300 FC MRB S AMM SSI 5711 681  DETAILED EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 19  AND 22  NOTE: FLAP EXTENDED  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5711 681  DETAILED EXTERNAL INSPECTION OF REAR  SPAR AFT FACE AND ATTACHED STRUCTURE BETWEEN RIB 19  AND 22  NOTE: FLAP FULLY EXTENDED  571155-0604-1 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711 681  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 19 AND 27 INCLUSIVE  (INCLUDING ZONE 591/691).  ACCESS: 581HB 581JB 581KB 591AB 591BB 591CB  681HB 681JB 681KB 691AB 691BB 691CB  571155-0604-2 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711 681  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 19 AND 27 INCLUSIVE  (INCLUDING ZONE 591/691).  ACCESS: 581HB 581JB 581KB 591AB 591BB 591CB  681HB 681JB 681KB 691AB 691BB 691CB  571155-0604-3 581 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711 681  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 19 AND 27 INCLUSIVE  (INCLUDING ZONE 591/691).  ACCESS: 581HB 581JB 581KB 591AB 591BB 591CB  681HB 681JB 681KB 691AB 691BB 691CB  571156-0604-1 591 REAR SPAR AND ATTACH.STRUC. MEC DET I: 27300 FC MRB S AMM SSI 5711 691  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 27 AND 29  ACCESS: 591DB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571156-0604-1 * * * * * C O N T I N U E * * * * *  691DB  571156-0604-2 591 REAR SPAR AND ATTACH.STRUC. MEC DET I: 22600 FC MRB S AMM SSI 5711 691  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 27 AND 29  ACCESS: 591DB  691DB  571156-0604-3 591 REAR SPAR AND ATTACH.STRUC. MEC DET I: 19200 FC MRB S AMM SSI 5711 691  DETAILED INSPECTION OF REAR SPAR AFT FACE AND  ATTACHED STRUCTURE BETWEEN RIB 27 AND 29  ACCESS: 591DB  691DB  571157-0602-1 542 BOTT.SKIN REINFORCING PLATE MEC DET I: 6700 FC MRB S AMM SSI 5711 642  DETAILED VISUAL EXTERNAL INSPECTION OF BOTTOM  SKIN REINFORCING PLATE AT RIB 5  571157-0602-2 542 BOTT.SKIN REINFORCING PLATE MEC DET I: 6500 FC MRB S AMM SSI 5711 642  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN REINFORCING PLATE AT RIB 5  571157-0602-3 542 BOTT.SKIN REINFORCING PLATE MEC DET I: 6100 FC MRB S AMM SSI 5711 642  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN REINFORCING PLATE AT RIB 5  571159-0602-1 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 6700 FC MRB S AMM SSI 5711 650  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571159-0602-1 * * * * * C O N T I N U E * * * * *  NOTE: FUEL PUMP REMOVED  ACCESS: 550AB 550CB  650AB 650CB  571159-0602-2 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 6400 FC MRB S AMM SSI 5711 650  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AT FUEL PUMP ATTACHMENT HOLES FROM RIB 14 TO 15  NOTE: FUEL PUMP REMOVED  ACCESS: 550AB 550CB  650AB 650CB  571159-0602-3 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 6000 FC MRB S AMM SSI 5711 650  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AT FUEL PUMP ATTACHMENT HOLES FROM RIB 14 TO 15  NOTE: FUEL PUMP REMOVED  ACCESS: 550AB 550CB  650AB 650CB  571159-0604-1 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 27300 FC MRB S AMM SSI 5711 650  DETAILED INSPECTION OF BOTTOM SKIN AT FUEL  PUMP ATTACHMENT HOLES FROM RIB 14 TO 15  ACCESS: 550BB  650BB  571159-0604-2 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 22600 FC MRB S AMM SSI 5711 650  DETAILED INSPECTION OF BOTTOM SKIN 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571159-0604-2 * * * * * C O N T I N U E * * * * *  ACCESS: 550BB  650BB  571159-0604-3 550 BOTTOM SKIN AT FUEL PUMP MEC DET I: 19200 FC MRB S AMM SSI 5711 650  DETAILED INSPECTION OF BOTTOM SKIN AT FUEL  PUMP ATTACHMENT HOLES FROM RIB 14 TO 15  ACCESS: 550BB  650BB  571161-0604-1 523 FRONT SPAR JOINT PLATE INS. MEC DET I: 27300 FC MRB S AMM SSI 5711 623  DETAILED INSPECTION OF FRONT SPAR JOINT PLATE  INSTALLATION AT RIB 9  NOTE: HEAT SHIELD REMOVED  ACCESS: 523CB  623CB  571161-0604-2 523 FRONT SPAR JOINT PLATE INS. MEC DET I: 22600 FC MRB S AMM SSI 5711 623  DETAILED INSPECTION OF FRONT SPAR JOINT PLATE  INSTALLATION AT RIB 9  NOTE: HEAT SHIELD REMOVED  ACCESS: 523CB  623CB  571161-0604-3 523 FRONT SPAR JOINT PLATE INS. MEC DET I: 19200 FC MRB S AMM SSI 5711 623  DETAILED INSPECTION OF FRONT SPAR JOINT PLATE  INSTALLATION AT RIB 9  NOTE: HEAT SHIELD REMOVED  ACCESS: 523CB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 571161-0604-3 * * * * * C O N T I N U E * * * * *  623CB  571165-0604-1 575 BOTTOM SKIN AT ACCESS DOOR MEC DET I: 17700 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF BOTTOM SKIN IN ACCESS  DOOR AREA AFT OF REAR SPAR  NOTE: DOORS OPENED  ACCESS: 575AB 575BB  675AB 675BB  571165-0604-2 575 BOTTOM SKIN AT ACCESS DOOR MEC DET I: 17700 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF BOTTOM SKIN IN ACCESS  DOOR AREA AFT OF REAR SPAR  NOTE: DOORS OPENED  ACCESS: 575AB 575BB  675AB 675BB  571165-0604-3 575 BOTTOM SKIN AT ACCESS DOOR MEC DET I: 15100 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF BOTTOM SKIN IN ACCESS  DOOR AREA AFT OF REAR SPAR  NOTE: DOORS OPENED  ACCESS: 575AB 575BB  675AB 675BB  571167-0604-1 575 BOTTOM SKIN IN PYLON AREA MEC DET I: 27300 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF BOTTOM SKIN INNER  SURFACE IN PYLON FAIRING AREA AFT OF REAR SPAR  ACCESS: 575BB  675BB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5711 675  DETAILED INSPECTION OF BOTTOM SKIN INNER  SURFACE IN PYLON FAIRING AREA AFT OF REAR SPAR  ACCESS: 575BB  675BB  571167-0604-3 575 BOTTOM SKIN IN PYLON AREA MEC DET I: 19200 FC MRB S AMM SSI 5711 675  DETAILED INSPECTION OF BOTTOM SKIN INNER  SURFACE IN PYLON FAIRING AREA AFT OF REAR SPAR  ACCESS: 575BB  675BB  571169-0602-1 575 BOTTOM SKIN IN BOOSTER BAY MEC DET I: 3000 FC MRB S AMM SSI 5711 675  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN IN BOOSTER BAY REGION  571173-0603-1 577 FLAP TRACK 1 BEAM EXTERIOR MEC DET I: 5 YE CPCP AMM SSI 5711 677 MRB S  DETAILED INSPECTION OF FLAP TRACK NO. 1 BEAM MRB REFERENC EXTERIOR  571173-C603- ACCESS: 577DT 577ET  677DT 677ET  571174-0603-1 577 FLAP TRACK 1 BEAM INTERIOR NDT BSI I: 5 YE CPCP AMM SSI 5711 677 MRB S NTM 574111  NDT INSPECTION OF FLAP TRACK NO.1 BEAM INTERIOR PART 7  NOTE: TOP FRONT AND REAR ATTACH BOLTS OF AFT FITTING MRB REFERENC REMOVED  571174-C603- ACCESS: 577DT 577ET  677DT 677ET  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 513104  671 I: 5000 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105  WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1  BOTTOM FACE BUILT SLOT. CN  1994-207-168 ACCESS: 571AB FAA AD 95-24 671AB ISB 57-0213  571175-0603-2 571 WING INNER REAR SPAR AT BUILD SLOT NDT SDI T: 19000 FC CN NTM 513104  671 I: 6000 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105  WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1  BOTTOM FACE BUILT SLOT. CN  1994-207-168 ACCESS: 571AB FAA AD 95-24 671AB ISB 57-0213  571175-0603-3 571 WING INNER REAR SPAR AT BUILD SLOT NDT SDI T: 17000 FC CN NTM 513104  671 I: 5000 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105  WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1  BOTTOM FACE OF BUILD SLOT. CN  1994-207-168 ACCESS: 571AB FAA AD 95-24 671AB ISB 57-0213  571175-0603-4 571 WING INNER REAR SPAR AT BUILD SLOT NDT SDI T: NOTE CN NTM 513104  671 I: 5000 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF AFT FACE OF REAR SPAR ISB NTM 513105  WEB IN AREA IMMEDIATELY ADJACENT TO OUTBOARD END AND PART 1  BOTTOM FACE OF BUILT SLOT. CN  1994-207-168 NOTE: ON A/C ON WHICH SB 57-221 (MOD 11130) HAS FAA AD 95-24 BEEN EMBODIED, NEXT INSPECTION IS DUE 33000 FC ISB 57-0213  FROM TIME OF MOD EMBODIEMENT.  ACCESS: 571AB  671AB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 83-102-53 620 I: 3000 FC FAA AD 86-19 DETAILED INSPECTION OF BEND RADIUS OF THE ISB 57-0109  LANDING ANGLE AT THE UPPER FLANGE OF THE NOSE RIB  NO.8  ACCESS: 523BB  623BB  571213-0603-1 543 WING - RIB 13 MEC DET T: 5800 FC ISB ISB 57-181  643 I: 2900 FC  DETAILED INSPECTION OF WEB OF RIB 13 BETWEEN  STRINGER 11 AND 12.  ACCESS: 543CB 543DB  643CB 643DB  572003-0602-1 512 D-NOSE ASSEMBLY SKIN MEC DET I: 9000 FC MRB S AMM SSI 5720 612  DETAILED EXTERNAL INSPECTION OF D-NOSE  ASSEMBLY SKIN AND SUB SPAR, JACK AND TRACK APERTURE,  JOINT PLATES, ATTACHMENTS AND FITTINGS AT INNER  LEADING EDGE  NOTE: SLAT EXTENDED  572004-0604-1 512 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720 612 AMM SSI 5720 DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AND  INTERNAL SLAT FAIRING STRIP AT INNER LEADING EDGE  ACCESS: 512BB 512CB 512DB 512EB 512FB 512GB  512HB 512JB 512KB 512LB  612BB 612CB 612DB 612EB 612FB 612GB  612HB 612JB 612KB 612LB  572004-0604-2 512 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720 612 AMM SSI 5720 DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AND  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 EDGE  ACCESS: 512BB 512CB 512DB 512EB 512FB 512GB  512HB 512JB 512KB 512LB  612BB 612CB 612DB 612EB 612FB 612GB  612HB 612JB 612KB 612LB  572004-0604-3 512 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720 612 AMM SSI 5720 DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AND  INTERNAL SLAT FAIRING STRIP AT INNER LEADING EDGE  ACCESS: 512BB 512CB 512DB 512EB 512FB 512GB  512HB 512JB 512KB 512LB  612BB 612CB 612DB 612EB 612FB 612GB  612HB 612JB 612KB 612LB  572015-0602-1 523 D-NOSE ASSY INTER.LEAD.EDGE MEC DET I: 3000 FC MRB S AMM SSI 5720 623  DETAILED EXTERNAL INSPECTION OF D-NOSE  ASSEMBLY SKIN AND SUB SPAR ATTACHMENTS, JACK AND  TRACK APERTURES, FITTINGS AND JOINT PLATES AT INTER-  MEDIATE LEADING EDGE.  PREP.: SLAT EXTENDED  572016-0604-1 523 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720 623  DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT  INTERMEDIATE LEADING EDGE  ACCESS: 523AB 523BB 523CB 523DB 523EB 523FB  523GB 523HB 523JB 523KB 523LB 523MB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5720 623  DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT  INTERMEDIATE LEADING EDGE  ACCESS: 523AB 523BB 523CB 523DB 523EB 523FB  523GB 523HB 523JB 523KB 523LB 523MB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB  572016-0604-3 523 D-NOSE ASSY IN.LEADING EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720 623  DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT  INTERMEDIATE LEADING EDGE  ACCESS: 523AB 523BB 523CB 523DB 523EB 523FB  523GB 523HB 523JB 523KB 523LB 523MB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB  572021-0602-1 524 D-NOSE ASSY OUTER LEAD.EDGE MEC DET I: 9000 FC MRB S AMM SSI 5720 624  DETAILED EXTERNAL INSPECTION OF D-NOSE  ASSEMBLY SKIN AND SUB SPAR ATTACHMENTS, JACK AND  TRACK APERTURES, FITTINGS AND JOINT PLATES AT OUTER  LEADING EDGE  NOTE: SLAT EXTENDED  572022-0604-1 524 D-NOSE ASSY OUT.LEAD.EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720 624  DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT OUTER  LEADING EDGE  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5720 624  DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT OUTER  LEADING EDGE  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  572022-0604-3 524 D-NOSE ASSY OUT.LEAD.EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720 624  DETAILED INSPECTION OF INTERNAL D-NOSE  ASSEMBLY SUB SPAR, ATTACHMENTS AND FITTINGS AT OUTER  LEADING EDGE  ACCESS: 524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  572063-0603-1 512 SLAT TRACK INNER LEADING EDGE MEC DET I: 6000 FC ALI CN 2006-0071 612 FAA AD 96-13 DETAILED INSPECTION OF SLAT TRACK RIBS AND  ATTACHMENTS, INNER LEADING EDGE. ALI REFERENC 572063-01-1  ACCESS: 512BB 512EB 512FB 512JB 512KB  612BB 612EB 612FB 612JB 612KB  572065-0604-1 523 SLAT TRACK RIBS MEC DET I: 27300 FC MRB S AMM SSI 5720 623  DETAILED INSPECTION OF SLAT TRACK RIBS AND  ATTACHMENTS OF INTERMEDIATE LEADING EDGE  ACCESS: 523BB 523CB 523EB 523FB 523HB 523JB  523LB 523MB  623BB 623CB 623EB 623FB 623HB 623JB  623LB 623MB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5720 623  DETAILED INSPECTION OF SLAT TRACK RIBS AND  ATTACHMENTS OF INTERMEDIATE LEADING EDGE  ACCESS: 523BB 523CB 523EB 523FB 523HB 523JB  523LB 523MB  623BB 623CB 623EB 623FB 623HB 623JB  623LB 623MB  572065-0604-3 523 SLAT TRACK RIBS MEC DET I: 19200 FC MRB S AMM SSI 5720 623  DETAILED INSPECTION OF SLAT TRACK RIBS AND  ATTACHMENTS OF INTERMEDIATE LEADING EDGE  ACCESS: 523BB 523CB 523EB 523FB 523HB 523JB  523LB 523MB  623BB 623CB 623EB 623FB 623HB 623JB  623LB 623MB  572067-0604-1 524 SLAT TRACK OUTER LEAD.EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720 624  DETAILED INSPECTION OF SLAT TRACK RIBS AND  ATTACHMENTS OF OUTER LEADING EDGE  ACCESS: 524BB 524CB 524EB 524FB 524GB 524HB  524KB  624BB 624CB 624EB 624FB 624GB 624HB  624KB  572067-0604-2 524 SLAT TRACK OUTER LEAD.EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720 624  DETAILED INSPECTION OF SLAT TRACK RIBS AND  ATTACHMENTS OF OUTER LEADING EDGE  ACCESS: 524BB 524CB 524EB 524FB 524GB 524HB  524KB  624BB 624CB 624EB 624FB 624GB 624HB  624KB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5720 624  DETAILED INSPECTION OF SLAT TRACK RIBS AND  ATTACHMENTS OF OUTER LEADING EDGE  ACCESS: 524BB 524CB 524EB 524FB 524GB 524HB  524KB  624BB 624CB 624EB 624FB 624GB 624HB  624KB  572069-0604-1 512 SLAT JACK AND PYLON RIBS MEC DET I: 27300 FC MRB S AMM SSI 5720 612  DETAILED INSPECTION OF SLAT JACK AND PYLON  RIBS AND ATTACHMENTS OF INNER LEADING EDGE  ACCESS: 512BB 512CB 512DB 512GB 512HB 512JB  512KB  612BB 612CB 612DB 612GB 612HB 612JB  612KB  572069-0604-2 512 SLAT JACK AND PYLON RIBS MEC DET I: 22600 FC MRB S AMM SSI 5720 612  DETAILED INSPECTION OF SLAT JACK AND PYLON  RIBS AND ATTACHMENTS OF INNER LEADING EDGE  ACCESS: 512BB 512CB 512DB 512GB 512HB 512JB  512KB  612BB 612CB 612DB 612GB 612HB 612JB  612KB  572069-0604-3 512 SLAT JACK AND PYLON RIBS MEC DET I: 19200 FC MRB S AMM SSI 5720 612  DETAILED INSPECTION OF SLAT JACK AND PYLON  RIBS AND ATTACHMENTS OF INNER LEADING EDGE  ACCESS: 512BB 512CB 512DB 512GB 512HB 512JB  512KB  612BB 612CB 612DB 612GB 612HB 612JB  612KB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5720 623  DETAILED INSPECTION OF SLAT JACK RIBS AND  ATTACHMENTS OF INTERMEDIATE LEADING EDGE  ACCESS: 523CB 523DB 523EB 523JB 523KB 523LB  623CB 623DB 623EB 623JB 623KB 623LB  572071-0604-2 523 SLAT JACK RIBS INTER.L.EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720 623  DETAILED INSPECTION OF SLAT JACK RIBS AND  ATTACHMENTS OF INTERMEDIATE LEADING EDGE  ACCESS: 523CB 523DB 523EB 523JB 523KB 523LB  623CB 623DB 623EB 623JB 623KB 623LB  572071-0604-3 523 SLAT JACK RIBS INTER.L.EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720 623  DETAILED INSPECTION OF SLAT JACK RIBS AND  ATTACHMENTS OF INTERMEDIATE LEADING EDGE  ACCESS: 523CB 523DB 523EB 523JB 523KB 523LB  623CB 623DB 623EB 623JB 623KB 623LB  572073-0604-1 524 SLAT JACK RIBS OUTER.L.EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720 624  DETAILED INSPECTION OF SLAT JACK RIBS AND  ATTACHMENTS OF OUTER LEADING EDGE  ACCESS: 524CB 524DB 524EB 524HB 524JB 524KB  624CB 624DB 624EB 624HB 624JB 624KB  572073-0604-2 524 SLAT JACK RIBS OUTER.L.EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720 624  DETAILED INSPECTION OF SLAT JACK RIBS AND  ATTACHMENTS OF OUTER LEADING EDGE  ACCESS: 524CB 524DB 524EB 524HB 524JB 524KB  624CB 624DB 624EB 624HB 624JB 624KB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5720 624  DETAILED INSPECTION OF SLAT JACK RIBS AND  ATTACHMENTS OF OUTER LEADING EDGE  ACCESS: 524CB 524DB 524EB 524HB 524JB 524KB  624CB 624DB 624EB 624HB 624JB 624KB  572075-0602-1 512 BOTTOM SKIN LEADING EDGE MEC DET I: 10100 FC MRB S AMM SSI 5720 612  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND LEADING EDGE  572075-0602-2 512 BOTTOM SKIN LEADING EDGE MEC DET I: 9900 FC MRB S AMM SSI 5720 612  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND LEADING EDGE  572075-0602-3 512 BOTTOM SKIN LEADING EDGE MEC DET I: 9200 FC MRB S AMM SSI 5720 612  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND LEADING EDGE  572077-0602-1 523 BOTTOM SKIN INTER.LEAD.EDGE MEC DET I: 10100 FC MRB S AMM SSI 5720 623  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND INTERMEDIATE LEADING EDGE  572077-0602-2 523 BOTTOM SKIN INTER.LEAD.EDGE MEC DET I: 9700 FC MRB S AMM SSI 5720 623  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND INTERMEDIATE LEADING EDGE  572077-0602-3 523 BOTTOM SKIN INTER.LEAD.EDGE MEC DET I: 9000 FC MRB S AMM SSI 5720 623  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND INTERMEDIATE LEADING EDGE  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5720 624  DETAILED VISUAL EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND OUTER LEADING EDGE  572079-0602-2 524 BOTTOM SKIN OUTER LEAD.EDGE MEC DET I: 9500 FC MRB S AMM SSI 5720 624  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND OUTER LEADING EDGE  572079-0602-3 524 BOTTOM SKIN OUTER LEAD.EDGE MEC DET I: 9200 FC MRB S AMM SSI 5720 624  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN BETWEEN FRONT SPAR AND OUTER LEADING EDGE  572081-0602-1 581 BOTT.SKIN AFT OF REAR SPAR MEC DET I: 10100 FC MRB S AMM SSI 5720 681  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AFT OF REAR SPAR FROM RIB 9 TO 29  572081-0602-2 581 BOTT.SKIN AFT OF REAR SPAR MEC DET I: 9700 FC MRB S AMM SSI 5720 681  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AFT OF REAR SPAR FROM RIB 9 TO 29  572081-0602-3 581 BOTT.SKIN AFT OF REAR SPAR MEC DET I: 9000 FC MRB S AMM SSI 5720 681  DETAILED EXTERNAL INSPECTION OF BOTTOM  SKIN AFT OF REAR SPAR FROM RIB 9 TO 29  572085-0604-1 591 TRAILING EDGE MEC DET I: 27300 FC MRB S AMM SSI 5720 691  DETAILED INSPECTION OF "A" FRAMES, TIE BEAM,  CANTILEVERS AND HINGE BRACKETS IN TRAILING EDGE  ACCESS: 591BB 591CB 591DB  691BB 691CB 691DB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 572085-0604-2 591 TRAILING EDGE MEC DET I: 22600 FC MRB S AMM SSI 5720 691  DETAILED INSPECTION OF "A" FRAMES, TIE BEAM,  CANTILEVERS AND HINGE BRACKETS IN TRAILING EDGE  ACCESS: 591BB 591CB 591DB  691BB 691CB 691DB  572085-0604-3 591 TRAILING EDGE MEC DET I: 19200 FC MRB S AMM SSI 5720 691  DETAILED INSPECTION OF "A" FRAMES, TIE BEAM,  CANTILEVERS AND HINGE BRACKETS IN TRAILING EDGE  ACCESS: 591BB 591CB 591DB  691BB 691CB 691DB  572089-0604-1 581 AIRBRAKE AND SPOILER HINGE MEC DET I: 27300 FC MRB S AMM SSI 5720 681  DETAILED INSPECTION OF AIRBRAKE AND SPOILER  HINGE AND JACK RIBS AT TRAILING EDGE  ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB  581JB 581KB  681CB 681DB 681EB 681FB 681GB 681HB  681JB 681KB  572089-0604-2 581 AIRBRAKE AND SPOILER HINGE MEC DET I: 22600 FC MRB S AMM SSI 5720 681  DETAILED INSPECTION OF AIRBRAKE AND SPOILER  HINGE AND JACK RIBS AT TRAILING EDGE  ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB  581JB 581KB  681CB 681DB 681EB 681FB 681GB 681HB  681JB 681KB  572089-0604-3 581 AIRBRAKE AND SPOILER HINGE MEC DET I: 19200 FC MRB S AMM SSI 5720 681  DETAILED INSPECTION OF AIRBRAKE AND SPOILER  HINGE AND JACK RIBS AT TRAILING EDGE  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  581JB 581KB  681CB 681DB 681EB 681FB 681GB 681HB  681JB 681KB  572090-0603-1 570 OUT.SHROUD BOX HNG.BRACKETS MEC DET T: 5000 FC ISB CN  670 I: 1000 FC 1998-449-265 DETAILED INSPECTION OF OUTER SHROUD BOX AFT FAA AD 90-11 HINGE BRACKETS. ISB 57-0142  PREP: FLAPS EXTENDED  INNER AIRBRAKES DEPLOYED  ACCESS: 577CT 577DT  677CT 677DT  572090-0604-1 575 LOWER SKIN PANEL INBOARD OF RIB 9 AND NDT SDI T: SEE SB AD NTM 570001  675 AFT OF REAR SPAR I: SEE SB SB PART 6  NTM 573319  SPECIAL DETAILED INSPECTION OF BOTTOM SKIN PANEL PART 2  INBOARD OF RIB 9 AND AFT OF REAR SPAR. AD 2008-06-1 SB 57-0177  ACCESS: 575FB  675FB  572090-0604-2 575 LOWER SKIN PANEL INBOARD OF RIB 9 AND MEC DET T: SEE SB AD AD 2008-06-1 675 AFT OF REAR SPAR I: SEE SB SB SB 57-0177  DETAILED VISUAL INSPECTION OF BOTTOM SKIN PANEL  INBOARD OF RIB 9 AND AFT OF REAR SPAR.  ACCESS: 575FB  675FB  572091-0604-1 572 INNER AIRBRAKE HINGE BOLTS MEC DET T: 20 YE CPCP MRB REFERENC 672 I: 10 YE MRB S  DETAILED INSPECTION OF INNER AIRBRAKE HINGE 572091-C604- BOLTS SINGLE HINGE POSITIONS.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 572091-0604-1 * * * * * C O N T I N U E * * * * *  PREP: FLAPS EXTENDED  REMOVE MOVABLE HINGE BRACKET FAIRINGS AND BOLTS  572092-0604-1 572 INNER AIRBRAKE HINGE BOLTS NDT SDI I: 17700 FC MRB S AMM SSI 5720 672 NTM 575412  SPECIAL DETAILED INSPECTION OF INNER AIRBRAKE HINGE PART 8  BOLTS (DOUBLE HINGE POSITION).  NOTE: DOUBLE HINGE BOLTS REMOVED  572092-0604-2 572 INNER AIRBRAKE HINGE BOLTS NDT SDI I: 17700 FC MRB S AMM SSI 5720 672 NTM 575412  SPECIAL DETAILED INSPECTION OF INNER AIRBRAKE HINGE PART 8  BOLTS (DOUBLE HINGE POSITION).  NOTE: DOUBLE HINGE BOLTS REMOVED  572092-0604-3 572 INNER AIRBRAKE HINGE BOLTS NDT SDI I: 15100 FC MRB S AMM SSI 5720 672 NTM 575412  SPECIAL DETAILED INSPECTION OF INNER AIRBRAKE HINGE PART 8  BOLTS (DOUBLE HINGE POSITIONS).  NOTE: DOUBLE HINGE BOLTS REMOVED  572093-0604-1 582 AIRBRAKES, SPOILER ACTUATOR BRACKETS NDT SDI T: 48000 FC ALI NTM 572093  583 I: 5500 FC PART 6  584 SPECIAL DETAILED INSPECTION OF OUTER AIRBRAKES AND EASA AD  682 SPOILER 3 ACTUATOR BRACKET LUGS. 2006-0071  683 FAA AD  684 PREP.: DETACH JACK ATTACHMENT 2007-04-11  ALI REFERENC 572093-01-1  572094-0604-1 582 AIRBRAKES, SPOILER ACTUATOR BRACKETS NDT SDI T: 48000 FC ALI NTM 572094  583 I: 10000 FC PART 8  584 SPECIAL DETAILED INSPECTION OF OUTER AIRBRAKES AND EASA AD  682 SPOILER 3 JACK ATTACHMENT PIN. 2006-0071  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 572094-0604-1 * * * * * C O N T I N U E * * * * *  683 FAA AD  684 PREP.: DETACH JACK ATTACHMENT 2007-04-11  ALI REFERENC 572094-01-1  572095-0604-1 576 ALL SPEED AILERON MEC DET T: 20 YE CPCP MRB REFERENC 676 I: 10 YE MRB S  DETAILED INSPECTION OF ALL SPEED AILERON 572095-C604- HINGE BOLTS.  PREP: REMOVE BOLTS  ACCESS: 575CB 575CT 575GB 576AB 576BB 576CB  576DB 576EB  675CB 675CT 675GB 676AB 676BB 676CB  676DB 676EB  572099-0604-1 581 AIRBRAKES AND SPOILERS MEC DET T: 20 YE CPCP MRB REFERENC 681 I: 10 YE MRB S  DETAILED INSPECTION OF AIRBRAKE AND SPOILER 572099-C604- HINGE BOLTS  PREP: EXTEND FLAPS, SPOILERS AND AIRBRAKES  ACCESS: 581AT 581BT 581CT 581ET  681AT 681BT 681CT 681ET  572103-0604-1 592 LOW SPEED AILERON MEC DET T: 20 YE CPCP MRB REFERENC 692 I: 10 YE MRB S  DETAILED INSPECTION OF LOW SPEED AILERON HINGE 572103-C604- BOLTS  PREP: REMOVE BOLTS  ACCESS: 591AB 591BB 591CB 591DB 591EB 591FB  591GB 591HB 592AT 592BB  691AB 691AT 691BB 691BT 691CB 691DB  691EB 691FB 691GB 691HB 692AT 692BB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 572105-0604-1 591 LOW SPEED AILERON MEC DET T: 20 YE CPCP MRB REFERENC 691 I: 10 YE MRB S  DETAILED INSPECTION OF LOW SPEED AILERON 572105-C604- CANTILEVERS CENTRE AND OUTER FAILSAFE ATTACHMENT  BOLTS  PREP: REMOVE BOLTS  ACCESS: 591CB 591DB  691CB 691DB  572107-0603-1 581 QUADRANT AIRBRAKE CONTROL MEC DET I: 6000 FC MRB S AMM SSI 5721 681  DETAILED INSPECTION OF QUADRANT AIRBRAKE  CONTROL AT RIB 14  ACCESS: FLAPS EXTENDED  572109-0604-1 577 FLAP MEC DET T: 20 YE CPCP  677 I: 10 YE MRB S  DETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572109-C604- OF THE NO.1 TRACK BEAM FORWARD ATTACHMENT  PREP: LOWER THE FLAPS  REMOVE BOLTS AND BUSH  572111-0604-1 577 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 677 I: 10 YE MRB S  DETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572111-C604- OF THE BEAM NO.1 AFT ATTACHMENT  PREP: LOWER THE FLAPS  REMOVE BOLTS AND BUSH  572113-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 632 I: 10 YE MRB S  DETAILED INSPECTION OF FAILSAFE BOLT OF THE 572113-C604- NO.2 FLAP TRACK BEAM FORWARD ATTACHMENT  PREP: REMOVE FIXED FAIRING AND BOLTS  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 572115-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 632 I: 10 YE MRB S  DETAILED INSPECTION OF THE FAILSAFE PINS OF 572115-C604- THE NO.2 FLAP TRACK BEAM FORWARD ATTACHMENT  PREP: REMOVE FIXED FAIRING AND PINS  572117-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 632 I: 10 YE MRB S  DETAILED INSPECTION OF FAILSAFE BOLT AND BUSH 572117-C604- OF THE NO.2 FLAP TRACK FRONT CARRIAGE TO REAR  CARRIAGE ATTACHMENT  PREP: LOWER THE FLAPS  REMOVE BOLT AND BUSH  572119-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 632 I: 10 YE MRB S  DETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572119-C604- OF THE NO.2 FLAP TAB ROD TO REAR CARRIAGE ATTACHMENT  NOTE: LOWER THE FLAPS  REMOVE BOLT AND BUSH  572121-0604-1 532 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 632 I: 10 YE MRB S  DETAILED INSPECTION OF FAILSAFE BOLT AND PIN 572121-C604- OF THE NO.2 FLAP TAB ROD AT THE TAB CONNECTION  PREP: LOWER THE FLAPS  REMOVE BOLT AND BUSH  572123-0604-1 533 BOLT FWD FLAP TRACK NO.3 NDT SDI I: 27300 FC MRB S AMM SSI 5721 633 NTM 574111  SPECIAL DETAILED INSPECTION OF FAILSAFE BOLT OF TRACK PART 8  BEAM NO.3 FORWARD ATTACHMENT  NOTE: BOLT REMOVED  ACCESS: 533AF  633AF  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5721 633 NTM 574111  SPECIAL DETAILED INSPECTION OF FAILSAFE BOLT OF TRACK PART 8  BEAM NO.3 FORWARD ATTACHMENT  NOTE: BOLT REMOVED  ACCESS: 533AF  633AF  572123-0604-3 533 BOLT FWD FLAP TRACK NO.3 NDT SDI I: 19200 FC MRB S AMM SSI 5721 633 NTM 574111  SPECIAL DETAILED INSPECTION OF FAILSAFE BOLT OF TRACK PART 8  BEAM NO.3 FORWARD ATTACHMENT  NOTE: BOLT REMOVED  ACCESS: 533AF  633AF  572125-0604-1 530 BOLT FORWARD FLAP TRACK NO4/5/6 NDT SDI I: 17700 FC MRB S AMM SSI 5721 630 NTM 574111  SPECIAL DETAILED INSPECTION OF FAILSAFE BOLTS OF PART 8  TRACK BEAMS 4,5,6 FWD ATTACHMENT  NOTE: BOLTS REMOVED  ACCESS: 534AF 535AF 536AF  634AF 635AF 636AF  572125-0604-2 530 BOLT FORWARD FLAP TRACK NO4/5/6 NDT SDI I: 17700 FC MRB S AMM SSI 5721 630 NTM 574111  SPECIAL DETAILED INSPECTION OF FAILSAFE BOLTS OF PART 8  TRACK BEAMS 4,5,6 FWD ATTACHMENT  NOTE: BOLTS REMOVED  ACCESS: 534AF 535AF 536AF  634AF 635AF 636AF  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5721 630 NTM 574111  SPECIAL DETAILED INSPECTION OF FAILSAFE BOLTS OF PART 8  TRACK BEAMS 4,5,6 FWD ATTACHMENT  NOTE: BOLTS REMOVED  ACCESS: 534AF 535AF 536AF  634AF 635AF 636AF  572127-0604-1 533 FLAP TRACK BEAMS MEC DET T: 20 YE CPCP MRB REFERENC 534 I: 10 YE MRB S  535 DETAILED INSPECTION OF FAILSAFE PINS OF THE NO 572127-C604- 633 3,4 AND 5 FLAP TRACK BEAMS FORWARD ATTACHMENT.  634  635 PREP: REMOVE FIXED FAIRING AND PINS  572129-0604-1 536 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 636 I: 10 YE MRB S  DETAILED INSPECTION OF FAILSAFE PINS OF THE 572129-C604- NO.6 FLAP TRACK BEAMS FORWARD ATTACHMENT  PREP: REMOVE FIXED FAIRINGS AND PINS  572131-0604-1 533 FLAP MEC DET T: 20 YE CPCP MRB REFERENC 534 I: 10 YE MRB S  535 DETAILED INSPECTION OF PIN AND HOLLOW PIN OF 572131-C604- 536 THE FLAP TRACK 3, 4, 5 AND 6 CARRIAGES  633  634 PREP REMOVE THE FIXED FAIRING AND PINS  635  636  572199-0603-1 513 FORWARD WING MEC DET T: 10 YE CPCP MRB REFERENC 613 I: 5 YE MRB S  DETAILED INSPECTION OF THE OUTER WING TOP SKIN 572199-C603- UPPER SURFACE FORWARD OF FRONT SPAR AT WING ROOT AREA  UNDER FORWARD WING TO FUSELAGE FAIRING  PREP.: FORWARD WING TO FUSELAGE FAIRINGS TO BE  REMOVED  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 572512-0603-1 500 WING FLAP TRACKS MEC DET I: 12000 FC ISB ISB 57-091  600  DETAILED INSPECTION OF FLAP TRACK NO. 3, 4,  5 AND 6.  PREP: REMOVE MOVABLE FAIRINGS AT REAR END  SET FLAPS TO RET (1ST NOTCH) POSITION  572512-0603-2 532 WING FLAP TRACKS NDT SDI I: ISB ISB NTM 572511  632 57-116 PART 4  SPECIAL DETAILED INSPECTION OF FLAP BEAM NO. 2 SIDE NTM 572512  AND BASE MEMBERS FOR CRACKS PART 4  CN  ACCESS: 532AF 532AM 1986-187-076 632AF 632AM FAA AD 95-21 ISB 57-116  572512-0603-3 500 WING FLAP TRACKS MEC DET T: 6000 FC ISB ISB 57-219  600 I: 4000 FC  DETAILED INSPECTION OF FLAP TRACK NO.2  PREP: REMOVE MOVABLE FAIRINGS AT FLAP TRACK NO.2  SET FLAPS TO THE RET (1ST NOTCH) POSITION  572512-0603-4 500 WING FLAP TRACKS MEC DET T: 12000 FC ISB ISB 57-219  600 I: 12000 FC  DETAILED INSPECTION OF FLAP TRACK NO.2  PREP: REMOVE MOVABLE FAIRINGS AT FLAP TRACK NO.2  SET FLAPS TO THE RET (1ST NOTCH) POSITION  574111-0603-1 470 REAR ATTACH.-WING TO PYLON NDT SDI I: 6000 FH ISB NTM 574111  480 PART 4  SPECIAL DETAILED INSPECTION OF LUGS OF WING TO PYLON ISB 57-115  REAR ATTACHMENT FITTING FOR CRACKS  ACCESS: 473BL 474BR  483BL 484BR  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 574112-0603-1 470 PYLON SPIGOT FITTING NDT SDI I: 6000 FH ISB NTM 574112  480 PART 4  SPECIAL DETAILED INSPECTION OF PYLON SPIGOT FITTING ISB 57-115  FOR CRACKS  ACCESS: 471BL 472BR  481BL 482BR  574113-0603-1 471 WINGS-PYLON THRUST AND SIDELOAD FITTING MEC DET T: 2800 FC AD AD EASA AD  481 I: 2800 FC ISB 2007-0243  DETAILED INSPECTION OF PYLON THRUST AND AD 2009-01-0 SIDELOAD FITTING (SPIGOT) CN  1997-358-232 PREP: BLEED AIR DUCT TO BE REMOVED ISB 57-0232  ACCESS: 471BL 472BR  481BL 482BR  574211-0602-1 571 ATTACHMENT - MAIN GEAR NDT SDI I: 400 FC ISB NTM 573310  671 ISB 57-085  SPECIAL DETAILED INSPECTION OF MLG ACTUATING CYLINDER  ATTACHMENT FITTING BOLTS (LOCATED ON TOP SKIN BETWEEN  RIB 5 AND REAR SPAR) R 574212-0602-1 571 WINGS - TRAILING EDGE MEC DET T: 400 FC AD AD 2006-12-1 671 I: 400 FC CN CN 2009-0081  DETAILED INSPECTION OF MAIN LANDING GEAR RIB 5 EUAD EUAD F-2003- ATTACHMENT FITTING LOWER FLANGE FOR CRACKS. FAA AD FAA AD  ISB 2000-05-07  PREP.:REMOVE MAIN LANDING GEAR ACTUATING CYLINDER OIT ISB 57A0246  ASSEMBLY AND DISCONNECT HYDRAULIC PIPES. OIT  9991.0017 09  ACCESS: 575AB  675AB R 574212-0602-2 571 WINGS - TRAILING EDGE NDT SDI T: 400 FC AD NTM 513104  671 I: 400 FC CN PART 1  SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR EUAD NTM 516000  RIB 5 ATTACHMENT FITTING LOWER FLANGE. FAA AD PART 1  ISB NTM 516001  PREP.: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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 2006-12-1 CN 2009-0081  ACCESS: 575AB EUAD F-2003- 675AB FAA AD  2000-05-07  ISB 57A0246  OIT  9991.0017 09 R 574212-0602-3 571 WINGS - TRAILING EDGE MEC DET T: SEE ISB EUAD EUAD F-2005- 671 I: SEE ISB FAA AD FAA AD  DETAILED INSPECTION OF MAIN LANDING GEAR RIB 5 ISB 2006-12-13  ATTACHMENT FITTING LOWER FLANGE FOR CRACKS. ISB 57A0234  PREP.:REMOVE MAIN LANDING GEAR ACTUATING CYLINDER  ASSEMBLY AND DISCONNECT HYDRAULIC PIPES.  ACCESS: 575AB  675AB R 574212-0602-4 571 WINGS - TRAILING EDGE NDT SDI T: SEE ISB EUAD NTM 513104  671 I: SEE ISB FAA AD PART 1  SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR RIB ISB NTM 574212  5 ATTACHMENT FITTING LOWER FLANGE. PART 6  EUAD F-2005- PREP.:REMOVE MAIN LANDING GEAR ACTUATING CYLINDER FAA AD  ASSEMBLY AND DISCONNECT HYDRAULIC PIPES. 2006-12-13  ISB 57A0234  ACCESS: 575AB  675AB  574300-0603-1 581 SPOILER JACK ATTACHMENTS MEC DET T: ISB ISB AMM 276151/4 681 57-133 ISB 57-133  DETAILED INSPECTION OF THE BEAM ASSEMBLY I: 3000 FH  ATTACHMENT BOLTS OF OUTER AIRBRAKE AND SPOILER FOR  LOOSENESS OR FAILURE  ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB  581JB 581KB  681CB 681DB 681EB 681FB 681GB 681HB  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 574300-0603-1 * * * * * C O N T I N U E * * * * *  681JB 681KB  575001-0603-1 511 SLAT TRACK 1 NDT SDI I: 11100 FC MRB S AMM SSI 5750 611 NTM 575810  SPECIAL DETAILED INSPECTION OF SLAT TRACK NO.1 AT PART 6  LOCATION OF FIRST LOWER ROLLER WHEN RETRACTED  NOTE: SLAT EXTENDED  575005-0603-1 511 SLAT TRACK 3 NDT SDI I: 11100 FC MRB S AMM SSI 5750 611 NTM 575811  SPECIAL DETAILED INSPECTION OF SLAT TRACK NO.3 AT PART 6  LOCATION OF FIRST LOWER ROLLER WHEN RETRACTED  NOTE: SLAT EXTENDED  575009-0604-1 511 SLAT RIB LOWER LUG NDT SDI I: 17700 FC MRB S AMM SSI 5750 611 NTM 575810  SPECIAL DETAILED INSPECTION OF SLAT RIB LOWER LUG AT PART 6  ATTACHMENT TO TRACKS 1 AND 3 NTM 575811  PART 6  NOTE: SLAT EXTENDED,TRACK AND BEARING HOUSING REMOVED  575009-0604-2 511 SLAT RIB LOWER LUG NDT SDI I: 17700 FC MRB S AMM SSI 5750 611 NTM 575810  SPECIAL DETAILED INSPECTION OF SLAT RIB LOWER LUG AT PART 6  ATTACHMENT TO TRACKS 1 AND 3 NTM 575811  PART 6  NOTE: SLAT EXTENDED,TRACK AND BEARING HOUSING REMOVED  575009-0604-3 511 SLAT RIB LOWER LUG NDT SDI I: 15100 FC MRB S AMM SSI 5750 611 NTM 575810  SPECIAL DETAILED INSPECTION OF SLAT RIB LOWER LUG AT PART 6  ATTACHMENT TO TRACKS 1 AND 3  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 575009-0604-3 * * * * * C O N T I N U E * * * * *  NTM 575811  NOTE: SLAT EXTENDED,TRACK AND BEARING HOUSING REMOVED PART 6  575010-0603-1 511 SLAT 1 TRACKS 1 TO 3 NDT SDI T: 10 YE CPCP NTM 575010  611 I: 5 YE PART 8  SPECIAL DETAILED INSPECTION OF SLAT 1 TRACKS 1 TO 3  MRB REFERENC NOTE: SLAT EXTENDED, SUCCESSIVE REMOVAL OF PINS AND 575010-C603- SLEEVES.  575011-0602-1 511 SLAT RIB LUGS & SKIN MEC DET I: 8300 FC MRB S AMM SSI 5750 611  DETAILED INSPECTION OF SLAT RIB UPPER  LUGS AT ATTACHMENT TO TRACKS 1 AND 3  NOTE: SLAT EXTENDED  575013-0603-1 511 SLAT RIB LOWER LUG MEC DET I: 11100 FC MRB S AMM SSI 5750 611  DETAILED INSPECTION OF SLAT RIB LOWER LUG AT  ATTACHMENT TO TRACK 2.  NOTE: SLAT EXTENDED, DETACH FAIRING PLATE  575015-0604-1 511 SLAT RIB UPPER LUG-TRACK 2 NDT SDI I: 27300 FC MRB S AMM SSI 5750 611 NTM 575812  SPECIAL DETAILED INSPECTION OF SLAT RIB UPPER LUG PART 6  ATTACHMENT TO TRACK NO.2  NOTE: SLAT IN EXTENDED POSITION, TRACK DETACHED  FROM LUGS AND BEARING HOUSING REMOVED  575015-0604-2 511 SLAT RIB UPPER LUG-TRACK 2 NDT SDI I: 22600 FC MRB S AMM SSI 5750 611 NTM 575812  SPECIAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 575015-0604-2 * * * * * C O N T I N U E * * * * *  ATTACHMENT TO TRACK NO.2  NOTE: SLAT IN EXTENDED POSITION, TRACK DETACHED  FROM LUGS AND BEARING HOUSING REMOVED  575015-0604-3 511 SLAT RIB UPPER LUG-TRACK 2 NDT SDI I: 19200 FC MRB S AMM SSI 5750 611 NTM 575812  SPECIAL DETAILED INSPECTION OF SLAT RIB UPPER LUG PART 6  ATTACHMENT TO TRACK NO.2  NOTE: SLAT IN EXTENDED POSITION, TRACK DETACHED  FROM LUGS AND BEARING HOUSING REMOVED  575017-0603-1 511 SLAT RIB LUGS AT ATT. MEC DET I: 11100 FC MRB S AMM SSI 5750 611  DETAILED INSPECTION OF SLAT RIB LUGS AT  ATTACHMENT TO JACKS 1 AND 2.  NOTE: SLAT EXTENDED, DETACH FORK ATTACHMENT  575021-0604-1 511 SLAT SKIN, AREA OF TRACK 2 NDT SDI T: 36500 FC ALI NTM 575813  611 I: 9000 FC PART 6  SPECIAL DETAILED INSPECTION OF SLAT 1 SKIN AT TRACK EASA AD  RIB 2. 2006-0071  FAA AD  PREP.: SLAT EXTENDED 2007-04-11  ALI REFERENC 575021-01-1  575023-0603-1 511 SLAT 1 LOWER SKIN NDT SDI I: 11100 FC MRB S AMM SSI 5750 611 NTM 575814  SPECIAL DETAILED INSPECTION OF SLAT LOWER SKIN IN PART 6  AREA OF LOWER GIRDER OF AUXILIARY SPAR AT RIB 20  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5750 611  DETAILED INSPECTION OF EXTERNAL LUGS OF  HINGE BRACKET AT RIB 21 OF SLAT 1  NOTE: SLAT EXTENDED  575051-0604-1 521 SLAT RIB LUGS MEC DET I: 27300 FC MRB S AMM SSI 5750 621  DETAILED INSPECTION OF SLAT RIB LUGS AT  ATTACHMENT TO TRACKS 4 TO 7 AND JACKS 3 AND 4.  NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGS  AND FORK ATTACHMENT AT JACK RIB LUGS DETACHED  575051-0604-2 521 SLAT RIB LUGS MEC DET I: 22600 FC MRB S AMM SSI 5750 621  DETAILED INSPECTION OF SLAT RIB LUGS AT  ATTACHMENT TO TRACKS 4 TO 7 AND JACKS 3 AND 4.  NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGS  AND FORK ATTACHMENT AT JACK RIB LUGS DETACHED  575051-0604-3 521 SLAT RIB LUGS MEC DET I: 19200 FC MRB S AMM SSI 5750 621  DETAILED INSPECTION OF SLAT RIB LUGS AT  ATTACHMENT TO TRACKS 4 TO 7 AND JACKS 3 AND 4.  NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGS  AND FORK ATTACHMENT AT JACK RIB LUGS DETACHED  575061-0604-1 521 SLAT SKIN, AREA OF TRACK 5 AND 6 NDT SDI T: 27000 FC ALI NTM 575910  621 I: 2800 FC PART 6  SPECIAL DETAILED INSPECTION OF SLAT 2 SKIN IN AREA OF EASA AD  TRACK RIBS 5, 6 AND 7 AT THE ATTACHMENT OF THE LOWER 2006-0071  GIRDER. FAA AD  2007-04-11  PREP.: SLAT EXTENDED  ALI REFERENC 575061-01-1  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5750 622  DETAILED INSPECTION OF SLAT RIB LUGS AT  ATTACHMENT TO TRACKS 8 TO 11 AND JACKS 5 AND 6  NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGS  AND FORK ATTACHMENTS AT JACK RIB LUGS DETACHED  575081-0604-2 522 SLAT RIB LUGS AT ATTACHMENT MEC DET I: 22600 FC MRB S AMM SSI 5750 622  DETAILED INSPECTION OF SLAT RIB LUGS AT  ATTACHMENT TO TRACKS 8 TO 11 AND JACKS 5 AND 6  NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGS  AND FORK ATTACHMENTS AT JACK RIB LUGS DETACHED  575081-0604-3 522 SLAT RIB LUGS AT ATTACHMENT MEC DET I: 19200 FC MRB S AMM SSI 5750 622  DETAILED INSPECTION OF SLAT RIB LUGS AT  ATTACHMENT TO TRACKS 8 TO 11 AND JACKS 5 AND 6  NOTE: SLAT EXTENDED, FAIRING PLATES AT TRACK RIB LUGS  AND FORK ATTACHMENTS AT JACK RIB LUGS DETACHED  575082-0604-1 521 SLAT 2 AND SLAT 3 NDT SDI T: 10 YE EUAD NTM 575082  522 I: 5 YE PART 2  621 SPECIAL DETAILED INSPECTION OF SLAT 2 AND 3, SLEEVES EUAD 2006-00 622 UPPER AND LOWER LUG, ECCENTRIC BOLT AT TRACKS 4 TO 11  MRB REFERENC PREP.: SLAT EXTENDET, SUCCESSIVE REMOVAL OF PINS 575082-C604- AND SLEEVES.  575087-0604-1 522 SLAT SKIN, AREA OF TRACK 9 NDT SDI T: 27000 FC ALI NTM 575912  622 I: 2800 FC PART 6  SPECIAL DETAILED INSPECTION OF SLAT 3 SKIN IN AREA OF EASA AD  HORIZONTAL FLANGES OF TRACK RIBS 8, 9 AND 10 AT THE 2006-0071  ATTACHMENT OF THE LOWER GIRDER. FAA AD  2007-04-11  PREP.: SLAT EXTENDED  ALI REFERENC 575087-01-1  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 575088  522 I: 6000 FC PART 6  621 SPECIAL DETAILED INSPECTION OF TRAILING EDGE SKIN AT EASA AD  622 TRACK 5, 6, 9 AND 10 AND JACK 4 AND 5. INSPECT FOR 2006-0071  CRACKS FROM FASTENER HOLE TO THE EDGE OF SKIN. (25 CM FAA AD  ON BOTH SIDES OF JACKS AND TRACKS) 2007-04-11  PREP.: SLAT EXTENDED ALI REFERENC 575088-01-1  575101-0604-1 574 LUGS FWD HINGE FLAP TRACK 1 NDT SDI I: 17700 FC MRB S AMM SSI 5751 674 NTM 575110  SPECIAL DETAILED INSPECTION OF LUGS OF FORWARD HINGE PART 4  BRACKET OF INNER FLAP AT TRACK 1  575101-0604-2 574 LUGS FWD HINGE FLAP TRACK 1 NDT SDI I: 17700 FC MRB S AMM SSI 5751 674 NTM 575110  SPECIAL DETAILED INSPECTION OF LUGS OF FORWARD HINGE PART 4  BRACKET OF INNER FLAP AT TRACK 1  575101-0604-3 574 LUGS FWD HINGE FLAP TRACK 1 NDT SDI I: 15100 FC MRB S AMM SSI 5751 674 NTM 575110  SPECIAL DETAILED INSPECTION OF LUGS OF FORWARD HINGE PART 4  BRACKET OF INNER FLAP AT TRACK 1  575103-0604-1 574 LUGS FWD HINGE FLAP TRACK 2 NDT SDI I: 27300 FC MRB S AMM SSI 5751 674 NTM 575111  SPECIAL DETAILED INSPECTION OF LUG OF FWD HINGE PART 6  BRACKET OF INNER FLAP AT TRACK 2  PREP: FLAP AND TAB REMOVED, BEARING HOUSING REMOVED  575103-0604-2 574 LUGS FWD HINGE FLAP TRACK 2 NDT SDI I: 22600 FC MRB S AMM SSI 5751 674  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 575111  BRACKET OF INNER FLAP AT TRACK 2 PART 6  PREP: FLAP AND TAB REMOVED, BEARING HOUSING REMOVED  575103-0604-3 574 LUGS FWD HINGE FLAP TRACK 2 NDT SDI I: 19200 FC MRB S AMM SSI 5751 674 NTM 575111  SPECIAL DETAILED INSPECTION OF LUG OF FWD HINGE PART 6  BRACKET OF INNER FLAP AT TRACK 2  PREP: FLAP AND TAB REMOVED, BEARING HOUSING REMOVED  575104-0604-1 574 FLAP AND TABS - INNER NDT SDI T: 37000 FC ALI NTM 575104  674 I: 5000 FC PART 6  SPECIAL DETAILED INSPECTION OF INNER FLAP ATTACHMENT EASA AD  OF TAB BRACKET AT HINGE 5.(RIB 14) 2006-0071  FAA AD  PREP.: FAIRING TO BE REMOVED 2007-04-11  ALI REFERENC 575104-01-1  575105-0604-1 574 LUGS REAR SUPPORT FLAP TR.2 NDT SDI I: 17700 FC MRB S AMM SSI 5751 674 NTM 575112  SPECIAL DETAILED INSPECTION OF LUGS OF REAR SUPPORT PART 4  BRACKET OF INNER FLAP AT TRACK 2  NOTE: FLAP EXTENDED, LINK DETACHED AND FLAP LIFTED  575105-0604-2 574 LUGS REAR SUPPORT FLAP TR.2 NDT SDI I: 17700 FC MRB S AMM SSI 5751 674 NTM 575112  SPECIAL DETAILED INSPECTION OF LUGS OF REAR SUPPORT PART 4  BRACKET OF INNER FLAP AT TRACK 2  NOTE: FLAP EXTENDED, LINK DETACHED AND FLAP LIFTED  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5751 674 NTM 575112  SPECIAL DETAILED INSPECTION OF LUGS OF REAR SUPPORT PART 4  BRACKET OF INNER FLAP AT TRACK 2  NOTE: FLAP EXTENDED, LINK DETACHED AND FLAP LIFTED  575107-0602-1 574 LUGS OF LINK FOR CONNECTION MEC DET I: 11100 FC MRB S AMM SSI 5751 674  DETAILED EXTERNAL INSPECTION OF LUGS  OF LINK FOR CONNECTION OF INNER FLAP TO FLAP TRACK 2  NOTE: FLAP EXTENDED  575109-0604-1 574 CONNECT.BETW.INN.FLAP TAB MEC DET I: 27300 FC MRB S AMM SSI 5751 674  DETAILED INSPECTION OF CONNECTIONS BETWEEN  INNER FLAP TAB AND INNER FLAP  (EXCEPT AT TRACK 2)  NOTE: FLAP EXTENDED, FAIRING REMOVED  575109-0604-2 574 CONNECT.BETW.INN.FLAP TAB MEC DET I: 22600 FC MRB S AMM SSI 5751 674  DETAILED INSPECTION OF CONNECTIONS BETWEEN  INNER FLAP TAB AND INNER FLAP  (EXCEPT AT TRACK 2)  NOTE: FLAP EXTENDED, FAIRING REMOVED  575109-0604-3 574 CONNECT.BETW.INN.FLAP TAB MEC DET I: 19200 FC MRB S AMM SSI 5751 674  DETAILED INSPECTION OF CONNECTIONS BETWEEN  INNER FLAP TAB AND INNER FLAP  (EXCEPT AT TRACK 2)  NOTE: FLAP EXTENDED, FAIRING REMOVED  575115-0602-1 574 FLAP LOWER SKIN MEC DET I: 5500 FC MRB S AMM SSI 5751 674  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 575115-0602-1 * * * * * C O N T I N U E * * * * *  DETAILED EXTERNAL INSPECTION  OF INNER FLAP LOWER SKIN AROUND REAR SUPPORT BRACKET  AT TRACK 2  NOTE: FLAP EXTENDED  575119-0604-1 574 RIVETING OF LOWER SKIN MEC DET I: 27300 FC MRB S AMM SSI 5751 674  DETAILED INSPECTION OF RIVETING OF LOWER SKIN  OF INNER FLAP TO RIBS 21A, 23A AND 25A BELOW FAIRING  AT TRACK 1  NOTE: FLAP EXTENDED, FAIRING REMOVED  575119-0604-2 574 RIVETING OF LOWER SKIN MEC DET I: 22600 FC MRB S AMM SSI 5751 674  DETAILED INSPECTION OF RIVETING OF LOWER SKIN  OF INNER FLAP TO RIBS 21A, 23A AND 25A BELOW FAIRING  AT TRACK 1  NOTE: FLAP EXTENDED, FAIRING REMOVED  575119-0604-3 574 RIVETING OF LOWER SKIN MEC DET I: 19200 FC MRB S AMM SSI 5751 674  DETAILED INSPECTION OF RIVETING OF LOWER SKIN  OF INNER FLAP TO RIBS 21A, 23A AND 25A BELOW FAIRING  AT TRACK 1  NOTE: FLAP EXTENDED, FAIRING REMOVED  575121-0602-1 574 FLAP UPPER SKIN MEC DET I: 11100 FC MRB S AMM SSI 5751 674  DETAILED EXTERNAL INSPECTION OF  RIVETING OF UPPER SKIN OF INNER FLAP BETWEEN RIBS 21A  AND 23A FORWARD OF FRONT SPAR  NOTE: FLAP EXTENDED  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5751 674  DETAILED INSPECTION OF RIVETING OF LOWER SKIN  OF INNER FLAP TO RIB 20D NEAR INBOARD TAB HINGE  BRACKET.  PREP.: FLAP EXTENDED, INBOARD HINGE FAIRING REMOVED.  575123-0602-1 574 INNER FLAP TAB CONNECTION MEC DET I: 5500 FC MRB S AMM SSI 5751 674  DETAILED EXTERNAL INSPECTION OF CONNECTION  OF INNER FLAP TAB TO INNER FLAP AT TRACK 2 AND AREA  OF LOWER LUG OF DRIVE BRACKET OF INNER FLAP TAB.  PREP.: FLAP EXTENDED  575125-0602-1 574 INNER FLAP RIB 1C MEC DET I: 3000 FC ISB ISB 57-0215  674  DETAILED INSPECTION OF THE INNER FLAP RIB 1C.  575126-0602-1 574 FLAPS AND TABS - INNER NDT SDI T: SEE ISB CN NTM 514000  674 I: 1000 FC FAA AD PART 7  SPECIAL DETAILED INSPECTION OF NOSE RIB 7 OF THE ISB NTM 575108  INNER FLAP FOR CRACKS. PART 6  CN F-2005-19 NOTE: INNER FLAP REMOVED CN 2006-0179  FAA AD  2006-13-04  ISB 57-0240  575127-0602-1 587 INBOARD CENTER FLAP TAB HINGE BRACKETS MEC DET T: 5300 FC ISB ISB 57-0214  687 I: 750 FC  DETAILED INSPECTION OF ALL INBOARD CENTER FLAP  TAB ATTACHMENT BRACKETS.  575127-0602-2 587 INBOARD CENTER FLAP TAB HINGE BRACKETS NDT SDI T: 6000 FC AD NTM 575127  687 I: 850 FC ISB PART 6  SPECIAL DETAILED INSPECTION OF CENTRE HINGE BRACKET AD EU-2007-0 OF CENTER FLAP INBOARD TAB ISB 57-0250  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 575127  687 I: 850 FC ISB PART 6  SPECIAL DETAILED INSPECTION OF CENTRE HINGE BRACKET AD EU-2007-0 OF CENTER FLAP INBOARD TAB ISB 57-0250  PREP: FLAPS EXTENDED.  575153-0602-1 587 LUGS OF LINK SUPP.BRACKET MEC DET I: 11100 FC MRB S AMM SSI 5751 687  DETAILED INSPECTION OF LUGS OF LINK  SUPPORT BRACKETS OF CENTER FLAP AND ATTACHMENTS  TO RIBS AT FLAP TRACKS 3 AND 4  NOTE: FLAP EXTENDED  575167-0602-1 587 CENTER FLAP LOWER SKIN MEC DET I: 5500 FC MRB S AMM SSI 5751 687  DETAILED INSPECTION OF EDGE OF CUTOUT  IN LOWER SKIN OF CENTER FLAP FORWARD OF FRONT SPAR  AT FLAP TRACKS 3 AND 4  NOTE: FLAP EXTENDED  575169-0602-1 587 CENTER FLAP LOWER SKIN MEC DET I: 11100 FC MRB S AMM SSI 5751 687  DETAILED INSPECTION OF LOWER SKIN AND  DOUBLER OF CENTER FLAP BETWEEN FRONT SPAR AND REAR  SPAR AT TRACKS 3 AND 4, 200MM INBOARD AND OUTBOARD OF  TRACK LINE  NOTE: FLAP EXTENDED  575171-0603-1 587 LUGS OF CONNECTING LINK NDT SDI T: 49000 FC ALI NTM 575210  687 I: 4100 FC PART 4 AND 6  SPECIAL DETAILED INSPECTION OF LUGS OF CONNECTING EASA AD  LINKS 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 575171-0603-1 * * * * * C O N T I N U E * * * * *  FAA AD  PREP.: FLAP REMOVED AND LINKS DETACHED 2007-04-11  ALI REFERENC 575171-01-1  575175-0602-1 587 CENTER FLAP TAB LUGS MEC DET I: 5500 FC MRB S AMM SSI 5751 687  DETAILED INSPECTION OF LUGS CONNECTING  CENTER FLAP TABS TO TAB DRIVE RODS  NOTE: FLAP EXTENDED  575203-0602-1 588 LUGS OF LINK SUPP.BRACKET MEC DET I: 11100 FC MRB S AMM SSI 5752 688  DETAILED INSPECTION OF LUGS OF LINK  SUPPORT BRACKETS OF OUTER FLAP AND ATTACHMENTS TO  RIBS AT FLAP TRACKS 5 AND 6  NOTE: FLAP EXTENDED  575217-0602-1 588 OUTER FLAP LOWER SKIN MEC DET I: 11100 FC MRB S AMM SSI 5752 688  DETAILED INSPECTION OF EDGES OF CUTOUTS  IN LOWER SKIN OF OUTER FLAP FORWARD OF FRONT SPAR AT  FLAP TRACKS 5 AND 6  NOTE: FLAP EXTENDED  575221-0602-1 588 OUTER FLAP LOWER SKIN MEC DET I: 2700 FC MRB S AMM SSI 5752 688  DETAILED INSPECTION OF LOWER SKIN AND  DOUBLER OF OUTER FLAP BETWEEN FRONT SPAR AND REAR  SPAR AT TRACKS NO.5 AND 6, 200MM INBOARD AND OUTBOARD  OF TRACK LINE  575223-0603-1 588 LUGS OF CONNECTING LINK NDT SDI T: 49000 FC ALI NTM 575310  688 I: 4100 FC PART 4 AND 6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AD  LINKS BETWEEN OUTER FLAP AND TRACKS 5 AND 6. 2006-0071  FAA AD  PREP.: FLAP REMOVED AND LINKS DETACHED 2007-04-11  ALI REFERENC 575223-01-1  575227-0602-1 588 OUTER FLAP TAB LUGS MEC DET I: 5500 FC MRB S AMM SSI 5752 688  DETAILED INSPECTION OF LUGS CONNECTING  OUTER FLAP TABS TO TAB DRIVE RODS  575251-0604-1 576 ALL SPEED AILERON LUGS MEC DET I: 27300 FC MRB S AMM SSI 5752 676  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  INNER HINGE BRACKET OF ALL SPEED AILERON  NOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHT  POSITION  ACCESS: 575CB 575CT 575GB 576AB 576BB 576CB  576DB 576EB  675CB 675CT 675GB 676AB 676BB 676CB  676DB 676EB  575251-0604-2 576 ALL SPEED AILERON LUGS MEC DET I: 22600 FC MRB S AMM SSI 5752 676  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  INNER HINGE BRACKET OF ALL SPEED AILERON  NOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHT  POSITION  ACCESS: 575CB 575CT 575GB 576AB 576BB 576CB  576DB 576EB  675CB 675CT 675GB 676AB 676BB 676CB  676DB 676EB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5752 676  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  INNER HINGE BRACKET OF ALL SPEED AILERON  NOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHT  POSITION  ACCESS: 575CB 575CT 575GB 576AB 576BB 576CB  576DB 576EB  675CB 675CT 675GB 676AB 676BB 676CB  676DB 676EB  575253-0604-1 576 ALL SPEED AILERON LUGS MEC DET I: 17700 FC MRB S AMM SSI 5752 676  DETAILED INSPECTION OF OUTBOARD LUGS OF OUTER  HINGE BRACKET OF ALL SPEED AILERON AND ATTACHMENT TO  REAR SPAR  ACCESS: 575GB 576FB  675GB 676FB  575253-0604-2 576 ALL SPEED AILERON LUGS MEC DET I: 17700 FC MRB S AMM SSI 5752 676  DETAILED INSPECTION OF OUTBOARD LUGS OF OUTER  HINGE BRACKET OF ALL SPEED AILERON AND ATTACHMENT TO  REAR SPAR  ACCESS: 575GB 576FB  675GB 676FB  575253-0604-3 576 ALL SPEED AILERON LUGS MEC DET I: 15100 FC MRB S AMM SSI 5752 676  DETAILED INSPECTION OF OUTBOARD LUGS OF OUTER  HINGE BRACKET OF ALL SPEED AILERON AND ATTACHMENT TO  REAR SPAR  ACCESS: 575GB 576FB  675GB 676FB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5752 692  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  INNER HINGE BRACKET OF LOW SPEED AILERON  NOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHT  POSITION  ACCESS: 591BB 592AB 592BB 592CB 592DB 592EB  691BB 692AB 692BB 692CB 692DB 692EB  575271-0604-2 592 LOW SPEED AILERON LUGS MEC DET I: 22600 FC MRB S AMM SSI 5752 692  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  INNER HINGE BRACKET OF LOW SPEED AILERON  NOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHT  POSITION  ACCESS: 591BB 592AB 592BB 592CB 592DB 592EB  691BB 692AB 692BB 692CB 692DB 692EB  575271-0604-3 592 LOW SPEED AILERON LUGS MEC DET I: 19200 FC MRB S AMM SSI 5752 692  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  INNER HINGE BRACKET OF LOW SPEED AILERON  NOTE: BOOSTER COVER DOOR ABOVE BRACKET IN UPRIGHT  POSITION  ACCESS: 591BB 592AB 592BB 592CB 592DB 592EB  691BB 692AB 692BB 692CB 692DB 692EB  575273-0604-1 592 LOW SPEED AILERON LUGS MEC DET I: 27300 FC MRB S AMM SSI 5752 692  DETAILED INSPECTION OF LOW SPEED AILERON LUGS  OF CENTER AND OUTER HINGE BRACKETS AND ATTACHMENT TO  REAR SPAR, PLUS LUGS OF LINKS AT OUTER HINGE  ACCESS: 591DB 592FB 592GB 592HB  691DB 692FB 692GB 692HB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5752 692  DETAILED INSPECTION OF LOW SPEED AILERON LUGS  OF CENTER AND OUTER HINGE BRACKETS AND ATTACHMENT TO  REAR SPAR, PLUS LUGS OF LINKS AT OUTER HINGE  ACCESS: 591DB 592FB 592GB 592HB  691DB 692FB 692GB 692HB  575273-0604-3 592 LOW SPEED AILERON LUGS MEC DET I: 19200 FC MRB S AMM SSI 5752 692  DETAILED INSPECTION OF LOW SPEED AILERON LUGS  OF CENTER AND OUTER HINGE BRACKETS AND ATTACHMENT TO  REAR SPAR, PLUS LUGS OF LINKS AT OUTER HINGE  ACCESS: 591DB 592FB 592GB 592HB  691DB 692FB 692GB 692HB  575293-0602-1 585 UPPER SKIN OF SPOILERS AND SPEEDBRAKES MEC DET T: 17000 FC ALI EASA AD  586 I: 2700 FC 2006-0071  685 DETAILED INSPECTION OF SPEEDBRAKES AND SPOILERS FAA AD  686 UPPER SKIN. 2007-04-11  NOTE: SPOILER EXTENDET ALI REFERENC 575293-01-1  575313-0604-1 573 INNER AIRBRAKES LUGS MEC DET I: 27300 FC MRB S AMM SSI 5753 673  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  CENTER HINGE BRAKES OF BOTH INNER AIRBRAKES  NOTE: FLAP EXTENDED AND HINGE BRACKET FAIRING  REMOVED, AIRBRAKES IN DOWN AND UPWARD POSITION  575313-0604-2 573 INNER AIRBRAKES LUGS MEC DET I: 22600 FC MRB S AMM SSI 5753 673  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  CENTER HINGE BRAKES OF BOTH INNER AIRBRAKES  NOTE: FLAP EXTENDED AND HINGE BRACKET FAIRING  REMOVED, AIRBRAKES IN DOWN AND UPWARD POSITION  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5753 673  DETAILED INSPECTION OF UPPER AND LOWER LUGS OF  CENTER HINGE BRAKES OF BOTH INNER AIRBRAKES  NOTE: FLAP EXTENDED AND HINGE BRACKET FAIRING  REMOVED, AIRBRAKES IN DOWN AND UPWARD POSITION  575315-0602-1 573 INNER AIRBRAKES LUGS MEC DET I: 5500 FC MRB S AMM SSI 5753 673  DETAILED INSPECTION OF LUGS OF OUTER  HINGES OF BOTH INNER AIRBRAKES  NOTE: FLAP EXTENDED, AIRBRAKES EXTENDED AND IN  RETRACTED POSITION  575412-0602-1 572 INNER AIRBRAKES - CENTER HINGE NDT SDI T: 16000 FC CN NTM 513104  672 I: 8200 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF CENTER HINGE BRACKETS ISB NTM 513105  OF INNER AIRBRAKES NO. 1 AND NO. 2. PART 1  CN  PREP.: REMOVE DETACHABLE SECTION OF FAIRINGS AT 97-080-211(B CENTER HINGE POSITION OF INNER AIRBRAKES FAA AD 98-04 ISB 57-0229  575612-0603-1 592 AILERON - LOW SPEED LH/RH NDT SDI I: 6000 FH ISB ISB 57-0072  692  SPECIAL DETAILED INSPECTION OF LOW SPEED AILERON RIBS  AND TOP SKIN BETWEEN RIB 8 AND 15 FOR CRACKS (WITH  AILERON IN HORIZONTAL POSITION)  576001-0606-1 541 FRONT SPAR BOTTOM BOOM, RIB 1 TO 6 NDT SDI T: SEE ISB ALI NTM 570000  641 I: SEE ISB ISB PART 6  SPECIAL DETAILED INSPECTION OF FRONT SPAR BOTTOM BOOM NTM 570001  BETWEEN RIB 1 AND RIB 6. PART 6  NTM 571123  PREP.: REMOVE PAINT FINISH PART 4  EASA AD  2006-0071  FAA AD  2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576001-0606-1 * * * * * C O N T I N U E * * * * *  ISB 57-0184  ALI REFERENC 576001-01-1  576002-0606-1 540 WING - FRONT SPAR BOTTOM BOOM NDT SDI T: SEE ISB ALI NTM 571123  640 I: SEE ISB ISB PART 4  DETAILED OR SPECIAL DETAILED INSPECTION OF THE FRONT EASA AD  SPAR BOTTOM BOOM BETWEEN RIBS 6 AND 7 AND RIBS 8 AND 2006-0071  9. FAA AD  2007-04-11  PREP.: AIRCRAFT TO BE DEFUELED. ISB 57-0149  ACCESS: 542EB ALI REFERENC 642EB 576002-01-1  576003-0606-1 540 FRONT AND REAR SPAR BOTTOM BOOM, RIB 9 NDT SDI T: SEE ISB ALI NTM 571115  640 I: SEE ISB ISB PART 4  SPECIAL DETAILED INSPECTION OF FASTENER HOLES INBOARD CN 2006-0071 AND OUTBOARD OF RIB 9 ON THE FRONT AND REAR SPAR FAA AD 96-13 BOTTOM BOOMS. ISB 57-0152  PREP.: AIRCRAFT TO BE DEFUELED. ALI REFERENC 576003-01-1  ACCESS: 542EB 543AB  642EB 643AB  576004-0606-1 550 OUTER WING FRONT SPAR NDT SDI ST: 33500 FC ALI NTM 571120  650 OR PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 38200 FH CN 2006-0071 BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. SI: 11800 FC FAA AD 96-13 OR  13400 FH ALI REFERENC 576004-01-1  576004-0606-2 550 OUTER WING FRONT SPAR NDT SDI I: 10300 FC ALI NTM 571120  650 OR PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 11700 FH CN 2006-0071 BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576004-0606-2 * * * * * C O N T I N U E * * * * *  ALI REFERENC 576004-01-2  576004-0606-3 550 OUTER WING FRONT SPAR NDT SDI ST: 30000 FC ALI NTM 571120  650 OR PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 41700 FH CN 2006-0071 BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. SI: 10000 FC FAA AD 96-13 OR  13900 FH ALI REFERENC 576004-01-3  576004-0606-4 550 OUTER WING FRONT SPAR NDT SDI I: 9000 FC ALI NTM 571120  650 OR PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 12500 FH CN 2006-0071 BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. FAA AD 96-13 ALI REFERENC 576004-01-4  576004-0606-5 550 OUTER WING FRONT SPAR NDT SDI ST: 26500 FC ALI NTM 571120  650 OR PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 61500 FH CN 2006-0071 BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. SI: 7800 FC FAA AD 96-13 OR  18100 FH ALI REFERENC 576004-01-5  576004-0606-6 550 OUTER WING FRONT SPAR NDT SDI I: 7800 FC ALI NTM 571120  650 OR PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 18100 FH CN 2006-0071 BOTTOM BOOM BETWEEN RIB 21 AND RIB 24. FAA AD 96-13 ALI REFERENC 576004-01-6  576005-0606-1 540 OUTER WING FRONT AND REAR SPAR TOP BOOM NDT SDI T: SEE SB ALI NTM REF: SEE  640 RIB 9 I: SEE SB CN ISB  FAA AD CN 2006-0071 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REAR SPAR TOP BOOMS INBOARD AND OUTBOARD OF RIB 9. ISB 57-0155  PREP: AIRCRAFT TO BE DEFUELED. ALI REFERENC 576005-01-1  ACCESS: 542EB 543AB  642EB 643AB  576006-0606-2 470 BOTTOM SKIN ADJACENT TO PYLON REAR MEC DET T: SEE SB ALI CN 2006-0071 480 ATTACHMENT FITTING I: SEE SB CN FAA AD 96-13 FAA AD ISB 57-0176  DETAILED INSPECTION OF WINGS BOTTOM SKIN ADJACENT TO ISB  PYLON REAR ATTACHMENT FITTING. ALI REFERENC 576006-01-1  ACCESS: 473BL 474BR  483BL 484BR  576007-0606-1 542 OUTER WING FRONT SPAR MEC DET ST: 36000 FC ALI CN 2006-0071 642 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 40700 FH FAA AD  REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO SI: 7400 FC ALI REFERENC BOTTOM BOOM. OR 576007-01-1  8400 FH  ACCESS: 542CB 542DB  642CB 642DB  576007-0606-2 542 OUTER WING FRONT SPAR MEC DET I: 5700 FC ALI CN 2006-0071 642 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 6400 FH FAA AD  REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO ALI REFERENC BOTTOM BOOM. 576007-01-2  ACCESS: 542CB 542DB  642CB 642DB  576007-0606-3 542 OUTER WING FRONT SPAR MEC DET ST: 30000 FC ALI CN 2006-0071 642 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 40800 FH FAA AD  REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO SI: 6300 FC ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576007-0606-3 * * * * * C O N T I N U E * * * * *  BOTTOM BOOM. OR 576007-01-3  8600 FH  ACCESS: 542CB 542DB  642CB 642DB  576007-0606-4 542 OUTER WING FRONT SPAR MEC DET I: 5000 FC ALI CN 2006-0071 642 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 6800 FH FAA AD  REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO ALI REFERENC BOTTOM BOOM. 576007-01-4  ACCESS: 542CB 542DB  642CB 642DB  576007-0606-5 542 OUTER WING FRONT SPAR MEC DET ST: 25000 FC ALI CN 2006-0071 642 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 55200 FH FAA AD  REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO SI: 5200 FC ALI REFERENC BOTTOM BOOM. OR 576007-01-5  11500 FH  ACCESS: 542CB 542DB  642CB 642DB  576007-0606-6 542 OUTER WING FRONT SPAR MEC DET I: 4300 FC ALI CN 2006-0071 642 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING CENTER SPAR WEB 9500 FH FAA AD  REAR FACE BETWEEN RIB 1 AND RIB 7 AT ATTACHMENT TO ALI REFERENC BOTTOM BOOM. 576007-01-6  ACCESS: 542CB 542DB  642CB 642DB  576008-0606-1 540 CENTER SPAR SEALING ANGLE MEC SDI T: SEE SB ALI NTM 571128  640 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF VERTICAL FLANGE OF FAA AD CN 2006-0071 SEALING ANGLE OUTBOARD OF RIB 8. ISB FAA AD 96-13 ISB 57-0146  PREP.: AIRCRAFT TO BE DEFUELED.  ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  641CB 642DB 642EB  576009-0606-1 550 OUTER WING REAR SPAR NDT SDI ST: 37500 FC ALI NTM 571122  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 42700 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. SI: 10500 FC FAA AD 96-13 OR  ACCESS: 550GB 550LB 12000 FH ALI REFERENC 650GB 650LB 576009-01-1  576009-0606-2 550 OUTER WING REAR SPAR NDT SDI ST: 32500 FC ALI NTM 571122  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45200 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. SI: 7500 FC FAA AD 96-13 OR  ACCESS: 550GB 550LB 10400 FH ALI REFERENC 650GB 650LB 576009-01-3  576009-0606-3 550 OUTER WING REAR SPAR NDT SDI ST: 28500 FC ALI NTM 571122  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 66100 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. SI: 5500 FC FAA AD 96-13 OR  ACCESS: 550GB 550LB 12700 FH ALI REFERENC 650GB 650LB 576009-01-5  576009-0606-4 550 OUTER WING REAR SPAR NDT SDI I: 7500 FC ALI NTM 571122  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 8500 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. FAA AD 96-13 ACCESS: 550GB 550LB ALI REFERENC 650GB 650LB 576009-01-2  576009-0606-5 550 OUTER WING REAR SPAR NDT SDI I: 6500 FC ALI NTM 571122  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 9000 FH FAA AD CN 2006-0071 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 ACCESS: 550GB 550LB ALI REFERENC 650GB 650LB 576009-01-4  576009-0606-6 550 OUTER WING REAR SPAR NDT SDI I: 5500 FC ALI NTM 571122  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 12700 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 18 AND RIB 24. FAA AD 96-13 ACCESS: 550GB 550LB ALI REFERENC 650GB 650LB 576009-01-6  576010-0606-1 540 REAR SPAR BOTTOM BOOM NDT SDI T: SEE SB ALI NTM 571116  640 I: SEE SB CN PART 4  SPECIAL DETAILED INSPECTION OF REAR SPAR BOTTOM BOOM FAA AD CN 2006-0071 BETWEEN RIB 1 AND RIB 9 IN BOTH AREAS INBOARD AND ISB FAA AD 96-13 OUTBOARD OF MAIN LANDING GEAR REINFORCING PLATE. ISB 57-0147  PREP.: AIRCRAFT TO BE DEFUELED ALI REFERENC 576010-01-1  ACCESS: 542DB 542EB  642DB 642EB  576011-0606-1 541 OUTER WING BOTTOM SKIN NDT SDI ST: 41000 FC ALI NTM 573010  542 OR CN PART 2  543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 46300 FH FAA AD CN 2006-0071 641 JOINT AT RIB 9. SI: 5500 FC FAA AD 96-13 642 OR  643 6200 FH ALI REFERENC 576011-01-1  ACCESS: 542EB  543AB  642EB  643AB  576011-0606-2 541 OUTER WING BOTTOM SKIN NDT SDI ST: 35000 FC ALI NTM 573010  542 OR CN PART 2  543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 47900 FH FAA AD CN 2006-0071 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 96-13 642 OR  643 6800 FH ALI REFERENC 576011-01-3  ACCESS: 542EB  543AB  642EB  643AB  576011-0606-3 541 OUTER WING BOTTOM SKIN NDT SDI ST: 29500 FC ALI NTM 573010  542 OR CN PART 2  543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 67000 FH FAA AD CN 2006-0071 641 SKIN JOINT AT RIB 9. SI: 4200 FC FAA AD 96-13 642 OR  643 9500 FH ALI REFERENC 576011-01-5  ACCESS: 542EB  543AB  642EB  643AB  576011-0606-4 541 OUTER WING BOTTOM SKIN NDT SDI I: 2800 FC ALI NTM 573010  542 OR CN PART 2  543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 3200 FH FAA AD CN 2006-0071 641 SKIN JOINT AT RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576011-01-2  ACCESS: 542EB  543AB  642EB  643AB  576011-0606-5 541 OUTER WING BOTTOM SKIN NDT SDI I: 2400 FC ALI NTM 573010  542 OR CN PART 2  543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 3300 FH FAA AD CN 2006-0071 641 SKIN JOINT AT RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576011-01-4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576011-0606-5 * * * * * C O N T I N U E * * * * *  ACCESS: 542EB  543AB  642EB  643AB  576011-0606-6 541 OUTER WING BOTTOM SKIN NDT SDI I: 2000 FC ALI NTM 573010  542 OR CN PART 2  543 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMT RIB 4500 FH FAA AD CN 2006-0071 641 SKIN JOINT AT RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576011-01-6  ACCESS: 542EB  543AB  642EB  643AB  576012-0606-1 540 BOTTOM SKIN STRINGERS ADJACENT RIB 14 NDT SDI T: SEE SB ALI NTM 571310  640 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF WINGS BOTTOM SKIN FAA AD CN 2006-0071 STRINGER 10 TO STRINGER 17 RUNOUTS, STRINGERS ISB FAA AD 96-13 ADJECENT TO RIB 14. ISB 57-0148  PREP.: AIRCRAFT TO BE DEFUELED. ALI REFERENC 576012-01-1  ACCESS: 543DB 550BB  643DB 650BB  576013-0604-1 500 OUTER WING BOTTOM SKIN MEC DET ST: 28000 FC ALI CN 2006-0071 600 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 31600 FH FAA AD  MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 2900 FC ALI REFERENC HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, OR 576013-01-1  AND RIB 14 AND RIB 22. 3300 FH  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-1  576013-0604-2 500 OUTER WING BOTTOM SKIN MEC DET I: 2600 FC ALI CN 2006-0071 600 OR CN FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN 576013-01-2  HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13,  AND RIB 14 AND RIB 22.  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-2  576013-0604-3 500 OUTER WING BOTTOM SKIN MEC DET ST: 24000 FC ALI CN 2006-0071 600 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 32900 FH FAA AD  MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 2200 FC ALI REFERENC HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, OR 576013-01-3  AND RIB 14 AND RIB 22. 3000 FH  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-3  576013-0604-4 500 OUTER WING BOTTOM SKIN MEC DET I: 2200 FC ALI CN 2006-0071 600 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 3000 FH FAA AD  MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN ALI REFERENC HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, 576013-01-4  AND RIB 14 AND RIB 22.  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-4  576013-0604-5 500 OUTER WING BOTTOM SKIN MEC DET ST: 19000 FC ALI CN 2006-0071 600 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 43100 FH FAA AD  MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 1900 FC ALI REFERENC HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, OR 576013-01-5  AND RIB 14 AND RIB 22. 4300 FH  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-5  576013-0604-6 500 OUTER WING BOTTOM SKIN MEC DET I: 1900 FC ALI CN 2006-0071 600 OR CN FAA AD 96-13 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 4300 FH FAA AD  MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN ALI REFERENC HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, 576013-01-6  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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.  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0606-6  576013-0606-1 500 OUTER WING BOTTOM SKIN NDT SDI ST: 28000 FC ALI NTM 573011  600 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 31600 FH FAA AD CN 2006-0071 AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 5800 FC FAA AD 96-13 HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND OR  RIB 14 AND RIB 22. 6500 FH ALI REFERENC 576013-02-1  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-1  576013-0606-2 500 OUTER WING BOTTOM SKIN NDT SDI I: 5100 FC ALI NTM 573011  600 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 5800 FH FAA AD CN 2006-0071 AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN FAA AD 96-13 HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND  RIB 14 AND RIB 22. ALI REFERENC 576013-02-2  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-2  576013-0606-3 500 OUTER WING BOTTOM SKIN NDT SDI ST: 24000 FC ALI NTM 573011  600 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 32900 FH FAA AD CN 2006-0071 AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 5000 FC FAA AD 96-13 HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND OR  RIB 14 AND RIB 22. 6800 FH ALI REFERENC 576013-02-3  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-3  576013-0606-4 500 OUTER WING BOTTOM SKIN NDT SDI I: 4400 FC ALI NTM 573011  600 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 6000 FH FAA AD CN 2006-0071 AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN FAA AD 96-13 HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND  RIB 14 AND RIB 22. ALI REFERENC 576013-02-4  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-4  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576013-0606-5 500 OUTER WING BOTTOM SKIN NDT SDI ST: 19000 FC ALI NTM 573011  600 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 43100 FH FAA AD CN 2006-0071 AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN SI: 3800 FC FAA AD 96-13 HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND OR  RIB 14 AND RIB 22. 8600 FH ALI REFERENC 576013-02-5  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-5  576013-0606-6 500 OUTER WING BOTTOM SKIN NDT SDI I: 3700 FC ALI NTM 573011  600 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 8400 FH FAA AD CN 2006-0071 AT MAGNETIC (MANUAL) LEVEL INDICATORS, SLAT CAN DRAIN FAA AD 96-13 HOLES BETWEEN RIB 1 AND RIB 8, RIB 9 AND RIB 13, AND  RIB 14 AND RIB 22. ALI REFERENC 576013-02-6  NOTE : THIS TASK IS AN ALTERNATIVE TO 576013-0604-6  576014-0606-1 540 BOTTOM SKIN AT MAGNETIC LEVEL INDICATOR NDT SDI T: SEE SB ALI NDT 573010  640 I: SEE SB CN PART 6  VISUAL OR SPECIAL DETAILED INSPECTION OF OUTER WING FAA AD CN 2006-0071 BOTTOM SKIN AT MAGNETIC LEVEL INDICATOR (MLI) AND ISB FAA AD 96-13 SLAT CAN DRAIN HOLE BETWEEN RIB 8 AND RIB 9. ISB 57-0153  ALI REFERENC 576014-01-1  576016-0606-1 540 WING-REAR SPAR NDT SDI T: SEE SB ALI NTM 571112  640 I: SEE SB CN PART 4  SPECIAL DETAILED INSPECTION OF REAR SPAR AT SELECTED FAA AD CN 2006-0071 BOLT LOCATION FOR ATTACHMENT OF MLG FORWARD PICK UP ISB FAA AD 96-13 FITTING AND MLG RIB 5 AFT OF REAR SPAR. ISB 57-0157  PREP.: AIRCRAFT TO BE DEFUELED. ALI REFERENC 576016-01-1  ACCESS: 542CB  642CB  576017-0606-1 540 WING - STRUCTURE AROUND MANHOLES NDT SDI T: SEE SB ALI NTM 573315  640 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF MANHOLE SURROUND FAA AD CN 2006-0071 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 ISB 57-0230  PREP.: TANKS TO BE DEFUELED.  ALI REFERENC ACCESS: 541AB 541BB 541CB 542CB 542DB 542EB 576017-01-1  543AB  641AB 641BB 641CB 642CB 642DB 642EB  643AB  576021-0606-1 523 OUTER WING TOP SKIN MEC DET ST: 26500 FC ALI CN 2006-0071 524 SI: 3300 FC CN FAA AD 96-13 623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD  624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENC 576021-01-1  576021-0606-2 523 OUTER WING TOP SKIN MEC DET ST: 26500 FC ALI CN 2006-0071 524 SI: 3400 FC CN FAA AD 96-13 623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD  624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENC 576021-01-2  576021-0606-3 523 OUTER WING TOP SKIN MEC DET ST: 25000 FC ALI CN 2006-0071 524 SI: 3900 FC CN FAA AD 96-13 623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD  624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENC 576021-01-3  576021-0606-4 523 OUTER WING TOP SKIN MEC DET I: 2600 FC ALI CN 2006-0071 524 CN FAA AD 96-13 623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD  624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENC 576021-01-4  576021-0606-5 523 OUTER WING TOP SKIN MEC DET I: 2600 FC ALI CN 2006-0071 524 CN FAA AD 96-13 623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD  624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENC 576021-01-5  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 524 CN FAA AD 96-13 623 DETAILED INSPECTION OF OUTER WING TOP SKIN FORWARD FAA AD  624 OF FRONT SPAR OUTBOARD OF RIB 9. ALI REFERENC 576021-01-6  576029-0605-1 541 OUTER WING FRONT SPAR NDT SDI ST: 36500 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 41200 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 SI: 3000 FC FAA AD 96-13 AND RIB 9 OR  3400 FH ALI REFERENC NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-1  AS TASK 576029-0606-1  ACCESS: 541CB 542EB  641CB 642EB  576029-0605-2 541 OUTER WING FRONT SPAR NDT SDI I: 2000 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 2200 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 FAA AD 96-13 AND RIB 9  ALI REFERENC NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-2  AS TASK 576029-0606-2  ACCESS: 541CB 542EB  641CB 642EB  576029-0605-3 541 OUTER WING FRONT SPAR NDT SDI ST: 40500 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 55500 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 SI: N/A FAA AD 96-13 AND RIB 9  ALI REFERENC NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-3  AS TASK 576029-0606-3  ACCESS: 541CB 542EB  641CB 642EB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576029-0605-4 541 OUTER WING FRONT SPAR NDT SDI I: 5700 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 7800 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 FAA AD 96-13 AND RIB 9  ALI REFERENC NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-4  AS TASK 576029-0606-4  ACCESS: 541CB 542EB  641CB 642EB  576029-0605-5 541 OUTER WING FRONT SPAR NDT SDI ST: 34000 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 77200 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 SI: N/A FAA AD 96-13 AND RIB 9  ALI REFERENC NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-5  AS TASK 576029-0606-5  ACCESS: 541CB 542EB  641CB 642EB  576029-0605-6 541 OUTER WING FRONT SPAR NDT SDI I: 4700 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 10700 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 1 AND RIB 7 AND BETWEEN RIB 8 FAA AD 96-13 AND RIB 9  ALI REFERENC NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME 576029-01-6  AS TASK 576029-0606-6  ACCESS: 541CB 542EB  641CB 642EB  576029-0606-1 541 OUTER WING FRONT SPAR NDT SDI ST: 36500 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF 2 BOLTS JUST INBOARD 41200 FH FAA AD CN 2006-0071 OF RIB 7 OF OUTER WING FRONT SPAR. SI: 3000 FC FAA AD 96-13 OR  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 3400 FH ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576029-0606-1 * * * * * C O N T I N U E * * * * *  TASK 576029-0605-1 576029-02-1  ACCESS: 541CB 542EB  641CB 642EB  576029-0606-2 541 OUTER WING FRONT SPAR NDT SDI I: 2000 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF 2 BOLTS JUST INBOARD 2200 FH FAA AD CN 2006-0071 OF RIB 7 OF OUTER WING FRONT SPAR. FAA AD 96-13 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENC TASK 576029-0605-2 576029-02-2  ACCESS: 541CB 542EB  641CB 642EB  576029-0606-3 541 OUTER WING FRONT SPAR NDT SDI ST: 40500 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 55500 FH FAA AD CN 2006-0071 OF RIB 7 OF OUTER WING FRONT SPAR. SI: N/A FAA AD 96-13 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENC TASK 576029-0605-3 576029-02-3  ACCESS: 541CB 542EB  641CB 642EB  576029-0606-4 541 OUTER WING FRONT SPAR NDT SDI I: 5700 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 7800 FH FAA AD CN 2006-0071 OF RIB 7 OF OUTER WING FRONT SPAR. FAA AD 96-13 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENC TASK 576029-0605-4 576029-02-4  ACCESS: 541CB 542EB  641CB 642EB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576029-0606-5 541 OUTER WING FRONT SPAR NDT SDI ST: 34000 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 77200 FH FAA AD CN 2006-0071 OF RIB 7 OF OUTER WING FRONT SPAR. SI: N/A FAA AD 96-13 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENC TASK 576029-0605-5 576029-02-5  ACCESS: 541CB 542EB  641CB 642EB  576029-0606-6 541 OUTER WING FRONT SPAR NDT SDI I: 4700 FC ALI NTM 571123  641 OR CN PART 4  SPECIAL DETAILED INSPECTION OF 5 BOLTS JUST INBOARD 10700 FH FAA AD CN 2006-0071 OF RIB 7 OF OUTER WING FRONT SPAR. FAA AD 96-13 NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENC TASK 576029-0605-6 576029-02-6  ACCESS: 541CB 542EB  641CB 642EB  576031-0606-1 543 OUTER WING FRONT SPAR NDT SDI T: 33500 FC ALI NTM  550 OR CN 571119 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 37800 FH FAA AD CN 2006-0071 650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. I: 3500 FC FAA AD 96-13 OR  3900 FH ALI REFERENC 576031-01-1  576031-0606-2 543 OUTER WING FRONT SPAR NDT SDI I: 1900 FC ALI NTM  550 OR CN 571119 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 2100 FH FAA AD CN 2006-0071 650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. FAA AD 96-13 ALI REFERENC 576031-01-2  576031-0606-3 543 OUTER WING FRONT SPAR NDT SDI T: 34000 FC ALI NTM  550 OR CN 571119 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 46600 FH FAA AD CN 2006-0071 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 OR  4800 FH ALI REFERENC 576031-01-3  576031-0606-4 543 OUTER WING FRONT SPAR NDT SDI I: 1650 FC ALI NTM  550 OR CN 571119 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 2300 FH FAA AD CN 2006-0071 650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. FAA AD 96-13 ALI REFERENC 576031-01-4  576031-0606-5 543 OUTER WING FRONT SPAR NDT SDI T: 28000 FC ALI NTM  550 OR CN 571119 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 63500 FH FAA AD CN 2006-0071 650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. I: 3500 FC FAA AD 96-13 OR  7900 FH ALI REFERENC 576031-01-5  576031-0606-6 543 OUTER WING FRONT SPAR NDT SDI I: 1400 FC ALI NTM  550 OR CN 571119 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR 3200 FH FAA AD CN 2006-0071 650 BOTTOM BOOM BETWEEN RIB 9 AND RIB 21. FAA AD 96-13 ALI REFERENC 576031-01-6  576035-0606-1 542 OUTER WING REAR SPAR NDT SDI T: 36000 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 40700 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 6700 FC 2006-0071  MAIN LANDING GEAR REINFORCING . OR FAA AD  7600 FH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576035-0606-1 * * * * * C O N T I N U E * * * * *  ACCESS: 542DB 542EB ALI REFERENC 642DB 642EB 576035-01-1  576035-0606-2 542 OUTER WING REAR SPAR NDT SDI I: 3700 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 4200 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071  MAIN LANDING GEAR REINFORCING . FAA AD  2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-2  576035-0606-3 542 OUTER WING REAR SPAR NDT SDI T: 36000 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 40700 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 5700 FC 2006-0071  MAIN LANDING GEAR REINFORCING . OR FAA AD  6400 FH 2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-3  576035-0606-4 542 OUTER WING REAR SPAR NDT SDI I: 3100 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 3500 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071  MAIN LANDING GEAR REINFORCING . FAA AD  2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-4  576035-0606-5 542 OUTER WING REAR SPAR NDT SDI T: 33500 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 5300 FC 2006-0071  MAIN LANDING GEAR REINFORCING . OR FAA AD  7300 FH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576035-0606-5 * * * * * C O N T I N U E * * * * *  ACCESS: 542DB 542EB ALI REFERENC 642DB 642EB 576035-01-5  576035-0606-6 542 OUTER WING REAR SPAR NDT SDI I: 3200 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 4400 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071  MAIN LANDING GEAR REINFORCING . FAA AD  2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-6  576035-0606-7 542 OUTER WING REAR SPAR NDT SDI T: 33500 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 4500 FC 2006-0071  MAIN LANDING GEAR REINFORCING . OR FAA AD  6200 FH 2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-7  576035-0606-8 542 OUTER WING REAR SPAR NDT SDI I: 2700 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 3700 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071  MAIN LANDING GEAR REINFORCING . FAA AD  2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-8  576035-0606-9 542 OUTER WING REAR SPAR NDT SDI T: 27000 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 61300 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 4200 FC 2006-0071  MAIN LANDING GEAR REINFORCING . OR FAA AD  9500 FH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576035-0606-9 * * * * * C O N T I N U E * * * * *  ACCESS: 542DB 542EB ALI REFERENC 642DB 642EB 576035-01-9  576035-0607-1 542 OUTER WING REAR SPAR NDT SDI I: 2800 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 6300 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071  MAIN LANDING GEAR REINFORCING . FAA AD  2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-10  576035-0607-2 542 OUTER WING REAR SPAR NDT SDI T: 27500 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 62400 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF I: 3600 FC 2006-0071  MAIN LANDING GEAR REINFORCING . OR FAA AD  8200 FH 2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-11  576035-0607-3 542 OUTER WING REAR SPAR NDT SDI I: 2400 FC ALI NTM  642 OR FAA AD 571116 PART  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 5400 FH EASA AD  BOTTOM BOOM BETWEEN RIB 1 AND RIB 9 EXCEPT IN WAY OF 2006-0071  MAIN LANDING GEAR REINFORCING . FAA AD  2007-04-11  ACCESS: 542DB 542EB  642DB 642EB ALI REFERENC 576035-01-12  576037-0606-1 543 OUTER WING REAR SPAR NDT SDI ST: 38000 FC ALI NTM  550 OR FAA AD 571121 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 43300 FH EASA AD  650 BOTTOM BETWEEN RIB 9 AND RIB 18. SI: 7000 FC 2006-0071  OR FAA AD  ACCESS: 543BB 8000 FH 2007-04-11  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576037-0606-1 * * * * * C O N T I N U E * * * * *  550DB ALI REFERENC 643BB 576037-01-1  650DB  576037-0606-2 543 OUTER WING REAR SPAR NDT SDI I: 7000 FC ALI NTM  550 OR FAA AD 571121 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 8000 FH EASA AD  650 BOTTOM BETWEEN RIB 9 AND RIB 18. 2006-0071  FAA AD  ACCESS: 543BB 2007-04-11  550DB  643BB ALI REFERENC 650DB 576037-01-2  576037-0606-3 543 OUTER WING REAR SPAR NDT SDI ST: 33000 FC ALI NTM  550 OR FAA AD 571121 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH EASA AD  650 BOTTOM BETWEEN RIB 9 AND RIB 18. SI: 7000 FC 2006-0071  OR FAA AD  ACCESS: 543BB 9700 FH 2007-04-11  550DB  643BB ALI REFERENC 650DB 576037-01-3  576037-0606-4 543 OUTER WING REAR SPAR NDT SDI I: 5400 FC ALI NTM  550 OR FAA AD 571121 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 7500 FH EASA AD  650 BOTTOM BETWEEN RIB 9 AND RIB 18. 2006-0071  FAA AD  ACCESS: 543BB 2007-04-11  550DB  643BB ALI REFERENC 650DB 576037-01-4  576037-0606-5 543 OUTER WING REAR SPAR NDT SDI ST: 27000 FC ALI NTM  550 OR FAA AD 571121 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 62600 FH EASA AD  650 BOTTOM BETWEEN RIB 9 AND RIB 18. SI: 7000 FC 2006-0071  OR  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  550DB 2007-04-11  643BB  650DB ALI REFERENC 576037-01-5  576037-0606-6 543 OUTER WING REAR SPAR NDT SDI I: 4700 FC ALI NTM  550 OR FAA AD 571121 PART  643 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 10900 FH EASA AD  650 BOTTOM BETWEEN RIB 9 AND RIB 18. 2006-0071  FAA AD  ACCESS: 543BB 2007-04-11  550DB  643BB ALI REFERENC 650DB 576037-01-6  576041-0606-1 541 OUTER WING TOP BOOM NDT SDI T: 34000 FC ALI NTM  542 I: 4400 FC CN 571124 PART  543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND FAA AD CN 2006-0071 641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576041-01-1  ACCESS: 542EB 575FB 575GB  543AB 543CB 581CB  642EB 675FB 675GB  643AB 643CB 681CB  576041-0606-2 541 OUTER WING TOP BOOM NDT SDI I: 2300 FC ALI NTM  542 CN 571124 PART  543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071 641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576041-01-2  ACCESS: 542EB 575FB 575GB  543AB 543CB 581CB  642EB 675FB 675GB  643AB 643CB 681CB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576041-0606-3 541 OUTER WING TOP BOOM NDT SDI T: 29000 FC ALI NTM  542 I: 5800 FC CN 571124 PART  543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071 641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576041-01-3  ACCESS: 542EB 575FB 575GB  543AB 543CB 581CB  642EB 675FB 675GB  643AB 643CB 681CB R 576041-0606-4 541 OUTER WING TOP BOOM NDT SDI I: 3400 FC ALI NTM  542 CN 571124 PART  543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071 641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576041-01-6  ACCESS: 542EB 575FB 575GB  543AB 543CB 581CB  642EB 675FB 675GB  643AB 643CB 681CB R 576041-0606-5 541 OUTER WING TOP BOOM NDT SDI T: 25500 FC ALI NTM  542 I: 5800 FC CN 571124 PART  543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071 641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13 642  643 ALI REFERENC 576041-01-4  ACCESS: 542EB 575FB 575GB  543AB 543CB 581CB  642EB 675FB 675GB  643AB 643CB 681CB R 576041-0606-6 541 OUTER WING TOP BOOM NDT SDI I: 3400 FC ALI NTM  542 CN 571124 PART  543 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT ANDP FAA AD CN 2006-0071 641 REAR SPAR TOP BOOMS, INBOARD AND OUTBOARD OF RIB 9. FAA AD 96-13 642  643 ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  543AB 543CB 581CB  642EB 675FB 675GB  643AB 643CB 681CB  576047-0606-1 541 WING CENTER SPAR NDT SDI ST: 29000 FC ALI NTM 571127  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 32800 FH FAA AD AND PART 6  642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM SI: 4500 FC CN 2006-0071 BETWEEN RIB 1 AND RIB 6. OR FAA AD 96-13 5100 FH  ACCESS: 541AB 541BB ALI REFERENC 542CB 576047-01-1  641AB 641BB 576047-02-1  642CB  576047-0606-2 541 WING CENTER SPAR NDT SDI I: 3000 FC ALI NTM 571127  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 3400 FH FAA AD AND PART 6  642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM CN 2006-0071 BETWEEN RIB 1 AND RIB 6. FAA AD 96-13 ACCESS: 541AB 541BB ALI REFERENC 542CB 576047-01-2  641AB 641BB 576047-02-2  642CB  576047-0606-3 541 WING CENTER SPAR NDT SDI ST: 31000 FC ALI NTM 571127  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 42200 FH FAA AD AND PART 6  642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM SI: 5200 FC CN 2006-0071 BETWEEN RIB 1 AND RIB 6. OR FAA AD 96-13 7100 FH  ACCESS: 541AB 541BB ALI REFERENC 542CB 576047-01-3  641AB 641BB 576047-02-3  642CB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576047-0606-4 541 WING CENTER SPAR NDT SDI I: 3400 FC ALI NTM 571127  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 4600 FH FAA AD AND PART 6  642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM CN 2006-0071 BETWEEN RIB 1 AND RIB 6. FAA AD 96-13 ACCESS: 541AB 541BB ALI REFERENC 542CB 576047-01-4  641AB 641BB 576047-02-4  642CB  576047-0606-5 541 WING CENTER SPAR NDT SDI ST: 24000 FC ALI NTM 571127  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 53000 FH FAA AD AND PART 6  642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM SI: 5200 FC CN 2006-0071 BETWEEN RIB 1 AND RIB 6. OR FAA AD 96-13 11500 FH  ACCESS: 541AB 541BB ALI REFERENC 542CB 576047-01-5  641AB 641BB 576047-02-5  642CB  576047-0606-6 541 WING CENTER SPAR NDT SDI I: 3400 FC ALI NTM 571127  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 7500 FH FAA AD AND PART 6  642 SKIN, SKIN JOINT STRAP AND CENTER SPAR BOTTOM BOOM CN 2006-0071 BETWEEN RIB 1 AND RIB 6. FAA AD 96-13 ACCESS: 541AB 541BB ALI REFERENC 542CB 576047-01-6  641AB 641BB 576047-02-6  642CB  576051-0606-1 541 PYLON REAR ATTACHMENT NDT SDI ST: 33000 FC ALI NTM 574113  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 37300 FH FAA AD EASA AD  642 DIAPHRAGM. SI: 3700 FC 2006-0071  OR FAA AD  ACCESS: 541CB 4200 FH 2007-04-11  542DB  641CB ALI REFERENC 642DB 576051-01-1  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576051-0606-2 541 PYLON REAR ATTACHMENT NDT SDI ST: 28000 FC ALI NTM 574113  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 38400 FH FAA AD EASA AD  642 DIAPHRAGM. SI: 3200 FC 2006-0071  OR FAA AD  ACCESS: 541CB 4400 FH 2007-04-11  542DB  641CB ALI REFERENC 642DB 576051-01-3 R 576051-0606-3 541 PYLON REAR ATTACHMENT NDT SDI ST: 24000 FC ALI NTM 574113  542 OR EASA AD PART 4  641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 54500 FC FAA AD EASA AD  642 DIAPHRAGM. SI: 2900 FC 2006-0071  OR FAA AD  ACCESS: 541CB 6600 FH 2007-04-11  542DB  641CB ALI REFERENC 642DB 576051-01-5  576051-0606-4 541 PYLON REAR ATTACHMENT NDT SDI I: 3500 FC ALI NTM 574113  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 3900 FH FAA AD CN 2006-0071 642 DIAPHRAGM. FAA AD 96-13 ACCESS: 541CB ALI REFERENC 542DB 576051-01-2  641CB  642DB R 576051-0606-5 541 PYLON REAR ATTACHMENT NDT SDI I: 3000 FC ALI NTM 574113  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 4100 FH FAA AD CN 2006-0071 642 DIAPHRAGM. FAA AD 96-13 ACCESS: 541CB ALI REFERENC 542DB 576051-01-4  641CB  642DB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576051-0606-6 541 PYLON REAR ATTACHMENT NDT SDI I: 2600 FC ALI NTM 574113  542 OR CN PART 4  641 SPECIAL DETAILED INSPECTION OF PYLON REAR ATTACHMENT 5900 FH FAA AD CN 2006-0071 642 DIAPHRAGM. FAA AD 96-13 ACCESS: 541CB ALI REFERENC 542DB 576051-01-6  641CB  642DB  576053-0605-1 540 WING TOP SKIN CENTER SPAR MEC DET T: SEE SB ALI CN 2006-0071 640 I: SEE SB CN FAA AD 96-13 DETAILED OR NDT INSPECTION OF TOP SKIN FAA AD ISB 57-0158  AT CENTER SPAR JOINT BETWEEN RIB 1 AND RIB 7. ISB  ALI REFERENC 576053-01-1  576055-0606-1 540 WINGS - FRONT SPAR BOTTOM BOOM NDT SDI T: SEE SB ALI NTM 570000  640 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF WING FRONT SPAR BOTTOM FAA AD NTM 570001  BOOM BETWEEN RIB 9 AND RIB 21, AND CENTER SPAR BOOM ISB PART 6  JOINT AT RIB 5. NTM 571119  PART 4  PREP.: AIRCRAFT TO BE DEFUELED CN 2006-0071 ACCESS: SEE SB FAA AD 96-13 ISB 57-0162  ALI REFERENC 576055-01-1  576056-0606-1 540 WINGS - FRONT AND REAR SPAR TOP BOOMS MEC SDI T: SEE SB ALI NTM 570000  640 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF THE WING FRONT AND FAA AD NTM 570001  REAR SPAR TOP BOOMS TO SKIN JOINT BETWEEN RIB 9 AND ISB PART 6  RIB 18. NTM 573314  PART 6  PREP.: AIRCRAFT TO BE DEFUELED. CN 2006-0071 FAA AD 96-13 ISB 57-0164  ALI REFERENC 576056-01-1  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 571125  643 11 I: SEE SB CN PART 4  FAA AD CN 2006-0071 SPECIAL DETAILED INSPECTION OF THE BOTTOM BOOM ISB FAA AD 96-13 ATTACHMENT HOLES IN FRONT SPAR WEB BETWEEN RIB 10 AND ISB 57-0151  RIB 11.  ALI REFERENC ACCESS: 523EB 576057-01-1  623EB  576058-0606-1 542 WING TOP SKIN AT RIB 9 NDT SDI T: SEE ISB ALI NTM 573318  642 I: SEE ISB CN PART 4  DETAILED AND SPECIAL DETAILED INSPECTION OF WING TOP FAA AD CN 2006-0071 SKIN AND STRINGER JOINT AT RIB 9. ISB FAA AD 96-13 ISB 57-0193  ACCESS: 542EB 543AB  642EB 643AB ALI REFERENC 576058-01-1  576059-0606-1 543 WING SKIN JOINTS NDT SDI T: SEE SB ALI NTM 570000  550 I: SEE SB CN PART 6  643 SPECIAL DETAILED INSPECTION OF BOTTOM SKIN TO REAR FAA AD NTM 570001  650 SPAR JOINT BETWEEN RIB 11 AND RIB 18. ISB PART 6  NTM 571121  ACCESS: 543BB 543CB 543DB PART 4  550BB 550CB 550DB 550EB 550FB 581CB CN 2006-0071 581DB 581EB 581FB 581GB FAA AD 96-13 643BB 643DB ISB 57-0119  650BB 650CB 650DB 650EB 650FB 681CB  681DB 681EB 681FB 681GB ALI REFERENC 576059-01-1  576060-0605-1 550 WING TOP SKIN MEC DET T: SEE SB ALI CN 2006-0071 650 I: SEE SB CN FAA AD 96-13 DETAILED INSPECTION OF WING TOP SKIN AT FRONT FAA AD ISB 57-0187  SPAR BETWEEN RIB 1 AND RIB 7. ISB  ALI REFERENC 576060-01-1  576062-0606-1 543 WING REAR SPAR BOTTOM BOOM NDT SDI T: 38000 FC ALI NTM 571121  643 OR CN PART 4  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. I: 7000 FC FAA AD 96-13 OR  ACCESS: 543AB 8000 FH ALI REFERENC 643AB 576062-01-1  576062-0606-2 543 WING REAR SPAR BOTTOM BOOM NDT SDI T: 33000 FC ALI NTM 571121  643 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 45900 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. I: 7000 FC FAA AD 96-13 OR  ACCESS: 543AB 9700 FH ALI REFERENC 643AB 576062-01-2  576062-0606-3 543 WING REAR SPAR BOTTOM BOOM NDT SDI I: 5400 FC ALI NTM 571121  643 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 7500 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. FAA AD 96-13 ACCESS: 543AB ALI REFERENC 643AB 576062-01-3  576062-0606-4 543 WING REAR SPAR BOTTOM BOOM NDT SDI T: 27000 FC ALI NTM 571121  643 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 62600 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. I: 7000 FC FAA AD 96-13 OR  ACCESS: 543AB 16200 FH ALI REFERENC 643AB 576062-01-4  576062-0606-5 543 WING REAR SPAR BOTTOM BOOM NDT SDI I: 4700 FC ALI NTM 571121  643 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 10900 FH FAA AD CN 2006-0071 BOTTOM BOOM BETWEEN RIB 9 AND RIB 11. FAA AD 96-13 ACCESS: 543AB ALI REFERENC 643AB 576062-01-5  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 571311  543 OR CN PART 4  550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 39700 FH FAA AD CN 2006-0071 641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES I: 5400 FC FAA AD 96-13 643 EXEPT AT STRINGER 19. OR  650 7400 FH ALI REFERENC 576063-01-1  576063-0606-2 541 FRONT AND REAR SPAR BOTTOM BOOM NDT SDI I: 3100 FC ALI NTM 571311  543 OR CN PART 4  550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 4200 FH FAA AD CN 2006-0071 641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES FAA AD 96-13 643 EXEPT AT STRINGER 19.  650 ALI REFERENC 576063-01-2  576063-0606-3 541 FRONT AND REAR SPAR BOTTOM BOOM NDT SDI T: 25000 FC ALI NTM 571311  543 OR CN PART 4  550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 56700 FH FAA AD CN 2006-0071 641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES I: 4500 FC FAA AD 96-13 643 EXEPT AT STRINGER 19. OR  650 10200 FH ALI REFERENC 576063-01-3  576063-0606-4 541 FRONT AND REAR SPAR BOTTOM BOOM NDT SDI I: 2500 FC ALI NTM 571311  543 OR CN PART 4  550 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT AND 5700 FH FAA AD CN 2006-0071 641 REAR SPAR BOTTOM BOOM AT ALL STRINGER RUN OUT PLATES FAA AD 96-13 643 EXEPT AT STRINGER 19.  650 ALI REFERENC 576063-01-4  576064-0606-1 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI ST: 35000 FC ALI NTM 571311  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 39500 FH FAA AD CN 2006-0071 BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB SI: 7000 FC FAA AD 96-13 13 AND RIB 14. OR  7900 FH ALI REFERENC 576064-01-1  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 571311  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 7900 FH FAA AD CN 2006-0071 BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB FAA AD 96-13 13 AND RIB 14.  ALI REFERENC 576064-01-2  576064-0606-3 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI ST: 31000 FC ALI NTM 571311  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 42500 FH FAA AD CN 2006-0071 BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB SI: 7000 FC FAA AD 96-13 13 AND RIB 14. OR  9600 FH ALI REFERENC 576064-01-3  576064-0606-4 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI I: 5400 FC ALI NTM 571311  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 7400 FH FAA AD CN 2006-0071 BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB FAA AD 96-13 13 AND RIB 14.  ALI REFERENC 576064-01-4  576064-0606-5 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI ST: 26000 FC ALI NTM 571311  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 59000 FH FAA AD CN 2006-0071 BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB SI: 7000 FC FAA AD 96-13 13 AND RIB 14. OR  15900 FH ALI REFERENC 576064-01-5  576064-0606-6 550 REAR SPAR BOTTOM BOOM STRINGER 19 NDT SDI I: 4700 FC ALI NTM 571311  650 OR CN PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT 10700 FH FAA AD CN 2006-0071 BOTTOM BOOM AT STRINGER 19 RUN OUT PLATE BETWEEN RIB FAA AD 96-13 13 AND RIB 14.  ALI REFERENC 576064-01-6  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 550 SI: 2900 FC CN FAA AD 96-13 640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD  650 WATER DRAIN VALVES BETWEEN RIB 5 AND 14 AND 15 AND ALI REFERENC 22 AND AT MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 576065-01-1  AND RIB 14.  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0607-1.  576065-0606-2 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 2600 FC ALI CN 2006-0071 550 CN FAA AD 96-13 640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD  650 WATER DRAIN VALVES BETWEEN RIB 5 AND 14 AND 15 AND 22 ALI REFERENC AND AT MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 576065-01-2  AND RIB 14.  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0607-2.  576065-0606-3 540 BOTTOM SKIN AT DRAIN VALVES MEC DET ST: 24000 FC ALI CN 2006-0071 550 SI: 2200 FC CN FAA AD 96-13 640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD  650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT ALI REFERENC MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14. 576065-01-3  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0607-3.  576065-0606-4 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 2200 FC ALI CN 2006-0071 550 CN FAA AD 96-13 640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD  650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT ALI REFERENC MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14. 576065-01-4  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0607-4.  576065-0606-5 540 BOTTOM SKIN AT DRAIN VALVES MEC DET ST: 19000 FC ALI CN 2006-0071 550 SI: 1900 FC CN FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT 576065-01-5  MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0607-5.  576065-0606-6 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 1900 FC ALI CN 2006-0071 550 CN FAA AD 96-13 640 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT FAA AD  650 WATER DRAIN VALVES BETWEEN RIB 5 AND RIB 22 AND AT ALI REFERENC MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14. 576065-01-6  NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0607-6.  576065-0607-1 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI ST: 28000 FC ALI NTM 573011  550 SI: 5800 FC CN PART 6  640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071 650 AT WATER DRAIN VALVES FROM RIB 5 TO RIB 14 FROM RIB FAA AD 96-13 15 TO RIB 22 AND AT MAGNETIC LEVEL INDICATORS BETWEEN  RIB 13 AND RIB 14. ALI REFERENC 576065-02-1  NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0606-1.  576065-0607-2 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI I: 5100 FC ALI NTM 573011  550 CN PART 6  640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071 650 AT WATER DRAIN VALVES FROM RIB 5 TO RIB 14, FROM RIB FAA AD 96-13 15 TO RIB 22 AND AT MAGNETIC LEVEL INDICATORS BETWEEN  RIB 13 AND RIB 14. ALI REFERENC 576065-02-2  NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK  576065-0606-2.  576065-0607-3 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI ST: 24000 FC ALI NTM 573011  550 SI: 5000 FC CN PART 6  640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.  ALI REFERENC NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-3  576065-0606-3.  576065-0607-4 540 BOTTOM SKIN AT DRAIN VALVES NDT SDI I: 4400 FC ALI NTM 573011  550 CN PART 6  640 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FAA AD CN 2006-0071 650 AT WATER DRAIN VALVES BETWEEN RIB 5 TO 22 AND AT FAA AD 96-13 MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.  ALI REFERENC NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-4  576065-0606-4.  576065-0607-5 540 BOTTOM SKIN AT DRAIN VALVES MEC DET ST: 19000 FC ALI NTM 573011  550 SI: 3800 FC CN PART 6  640 NDT INSPECTION OF OUTER WING BOTTOM FAA AD CN 2006-0071 650 SKIN AT WATER DRAIN VALVES BETWEEN RIB 5 TO 22 AND AT FAA AD 96-13 MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.  ALI REFERENC NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-5  576065-0606-5.  576065-0607-6 540 BOTTOM SKIN AT DRAIN VALVES MEC DET I: 3700 FC ALI NTM 573011  550 CN PART 6  640 NDT INSPECTION OF OUTER WING BOTTOM FAA AD CN 2006-0071 650 SKIN AT WATER DRAIN VALVES BETWEEN RIB 5 TO 22 AND AT FAA AD 96-13 MAGNETIC LEVEL INDICATORS BETWEEN RIB 13 AND RIB 14.  ALI REFERENC NOTE: 01. THIS TASK IS AN ALTERNATIVE TO THE TASK 576065-02-6  576065-0606-6.  576066-0606-1 540 BOTTOM SKIN CENTER SPAR, RIBS 1-6 NDT SDI T: SEE SB ALI NTM 571127  640 I: SEE SB CN PART 4 AND 6  SPECIAL DETAILED INSPECTION OF BOTTOM SKIN TO CENTER FAA AD CN 2006-0071 SPAR JOINT BETWEEN RIB 1 AND RIB 6. (EXCLUDING RIB 5) FAA AD 96-13 ACCESS: 541AB 541BB 541CB 542CB 542DB ALI REFERENC * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  576067-0606-1 550 BOTTOM SKIN MANHOLE, RIBS 11-21 NDT SDI T: 25500 FC ALI NTM 573315  650 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 28800 FH FAA AD CN 2006-0071 MANHOLE SURROUNDS BETWEEN RIB 11 AND RIB 21. I: 8400 FC FAA AD 96-13 OR  ACCESS: 543AB 543BB 543CB 543DB 550BB 550DB 9500 FH ALI REFERENC 550EB 550FB 550GB 550HB 550JB 576067-01-1  643AB 643BB 643CB 643DB 650BB 650DB  650EB 650FB 650GB 650HB 650JB  576067-0606-2 550 BOTTOM SKIN MANHOLE, RIBS 11-21 NDT SDI I: 7600 FC ALI NTM 573315  650 OR CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 8600 FH FAA AD CN 2006-0071 MANHOLE SURROUNDS BETWEEN RIB 11 AND RIB 21. FAA AD 96-13 ACCESS: 543AB 543BB 543CB 543DB 550BB 550DB ALI REFERENC 550EB 550FB 550GB 550HB 550JB 576067-01-2  643AB 643BB 643CB 643DB 650BB 650DB  650EB 650FB 650GB 650HB 650JB  576068-0606-1 542 WING TOP SKIN, RIB 9 NDT SDI T: 30400 FC ALI NTM 573311  543 I: 2800 FC CN PART 2  642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 573318  643 AND STRINGER JOINT AT RIB 9. PART 4  CN 2006-0071 ACCESS: 542EB FAA AD 96-13 543AB  642EB ALI REFERENC 643AB 576068-01-1  576068-02-1  576068-0606-2 542 WING TOP SKIN, RIB 9 NDT SDI I: 2500 FC ALI NTM 573311  543 CN PART 2  642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 573318  643 AND STRINGER JOINT AT RIB 9. PART 4  CN 2006-0071 ACCESS: 542EB FAA AD 96-13 * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576068-0606-2 * * * * * C O N T I N U E * * * * *  543AB ALI REFERENC 642EB 576068-01-4  643AB 576068-02-4  576068-0606-3 542 WING TOP SKIN, RIB 9 NDT SDI T: 34100 FC ALI NTM 573311  543 I: 2800 FC CN PART 2  642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 573318  643 AND STRINGER JOINT AT RIB 9. PART 4  CN 2006-0071 ACCESS: 542EB FAA AD 96-13 543AB  642EB ALI REFERENC 643AB 576068-01-2  576068-02-2  576068-0606-4 542 WING TOP SKIN, RIB 9 NDT SDI I: 2500 FC ALI NTM 573311  543 CN PART 2  642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 573318  643 AND STRINGER JOINT AT RIB 9. PART 4  CN 2006-0071 ACCESS: 542EB FAA AD 96-13 543AB  642EB ALI REFERENC 643AB 576068-01-5  576068-02-5  576068-0606-5 542 WING TOP SKIN, RIB 9 NDT SDI T: 30200 FC ALI NTM 573311  543 I: 2800 FC CN PART 2  642 SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN FAA AD NTM 573318  643 AND STRINGER JOINT AT RIB 9. PART 4  CN 2006-0071 ACCESS: 542EB FAA AD 96-13 543AB  642EB ALI REFERENC 643AB 576068-01-3  576068-02-3  576068-0606-6 542 WING TOP SKIN, RIB 9 NDT SDI I: 2500 FC ALI NTM 573311  543 CN PART 2  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 573318  643 AND STRINGER JOINT AT RIB 9. PART 4  CN 2006-0071 ACCESS: 542EB FAA AD 96-13 543AB  642EB ALI REFERENC 643AB 576068-01-6  576068-02-6  576069-0606-1 550 WINGS MANHOLE SURROUND STRUCTURE NDT SDI T: SEE SB ALI NTM 573317  650 I: SEE SB CN PART 6  SPECIAL DETAILED INSPECTION OF MANHOLE SURROUND FAA AD CN 2006-0071 STRUCTURE IN FASTENER HOLES. FAA AD 96-13 ACCESS: 550KB 550LB ALI REFERENC 650KB 650LB 576069-01-1  576070-0606-1 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI ST: 29000 FC ALI NTM 571127  542 RIB OR CN PART 4  641 32800 FH FAA AD AND PART 6  642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SI: 4500 FC CN 2006-0071 SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 OR FAA AD 96-13 AND HALF RIBS. 5100 FH  ALI REFERENC ACCESS: 541CB 576070-01-1  542DB 576070-02-1  641CB  642DB  576070-0606-2 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI I: 3000 FC ALI NTM 571127  542 RIB OR CN PART 4  641 3400 FH FAA AD AND PART 6  642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM CN 2006-0071 SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 FAA AD 96-13 AND HALF RIBS.  ALI REFERENC ACCESS: 541CB 576070-01-2  542DB 576070-02-2  641CB  642DB  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 571127  542 RIB OR CN PART 4  641 42200 FH FAA AD AND PART 6  642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SI: 5200 FC CN 2006-0071 SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 OR FAA AD 96-13 AND HALF RIBS. 7100 FH  ALI REFERENC ACCESS: 541CB 576070-01-3  542DB 576070-02-3  641CB  642DB  576070-0606-4 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI I: 3400 FC ALI NTM 571127  542 RIB OR CN PART 4  641 7100 FH FAA AD AND PART 6  642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM CN 2006-0071 SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 FAA AD 96-13 AND HALF RIBS.  ALI REFERENC ACCESS: 541CB 576070-01-4  542DB 576070-02-4  641CB  642DB  576070-0606-5 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI ST: 24000 FC ALI NTM 571127  542 RIB OR CN PART 4  641 53000 FH FAA AD AND PART 6  642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SI: 5200 FC CN 2006-0071 SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 OR FAA AD 96-13 AND HALF RIBS. 11500 FH  ALI REFERENC ACCESS: 541CB 576070-01-5  542DB 576070-02-5  641CB  642DB  576070-0606-6 541 CENTER SPAR BOTTOM BOOM RIB 6 TO HALF NDT SDI I: 3400 FC ALI NTM 571127  542 RIB OR CN PART 4  641 7500 FH FAA AD AND PART 6  642 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM CN 2006-0071 SKIN, SKIN JOINT STRAP AND CENTER SPAR BETWEEN RIB 6 FAA AD 96-13 AND HALF RIBS.  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576070-0606-6 * * * * * C O N T I N U E * * * * *  ACCESS: 541CB ALI REFERENC 542DB 576070-01-6  641CB 576070-02-6  642DB  576071-0606-1 550 BOTTOM SKIN MEC DET T: SEE SB ALI NTM 513005  650 I: SEE SB CN PART 1  NDT OR DETAILED INSPECTION OF OUTER WING BOX BOTTOM FAA AD NTM 513010  SKIN, WATER DRAIN VALVE BETWEEN RIB 14 AND RIB 15. PART 1  NTM 573004  PART 1  CN 2006-0071 FAA AD 96-13 ALI REFERENC 576071-01-1  576072-0606-1 542 TOP SKIN MEC DET T: 48000 FC ALI EASA AD  642 I: 4000 FC FAA AD 2006-0071  DETAILED INSPECTION OF OUTER WING REAR SPAR TOP FAA AD  BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2007-04-11  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENC TASK 576072-0606-2 576072-01-1  576072-0606-2 542 TOP SKIN NDT SDI T: 48000 FC ALI NTM 571128  642 I: 4000 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR EASA AD  TOP BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 576072-0606-1  ALI REFERENC 576072-02-1  576072-0606-3 542 TOP SKIN MEC DET T: 40000 FC ALI EASA AD  642 I: 4000 FC FAA AD 2006-0071  DETAILED INSPECTION OF OUTER WING REAR SPAR TOP FAA AD  BOOM 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576072-0606-3 * * * * * C O N T I N U E * * * * *  ALI REFERENC NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 576072-01-2  TASK 576072-0606-4  576072-0606-4 542 TOP SKIN NDT SDI T: 40000 FC ALI NTM 571128  642 I: 4000 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR EASA AD  TOP BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 576072-0606-3  ALI REFERENC 576072-02-2  576072-0606-5 542 TOP SKIN MEC DET T: 34000 FC ALI EASA AD  642 I: 4000 FC FAA AD 2006-0071  DETAILED INSPECTION OF OUTER WING REAR SPAR TOP FAA AD  BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2007-04-11  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS ALI REFERENC TASK 576072-0606-6 576072-01-3  576072-0606-6 542 TOP SKIN NDT SDI T: 34000 FC ALI NTM 571128  642 I: 4000 FC FAA AD PART 4  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR EASA AD  TOP BOOM AND TOP SKIN BETWEEN RIB 1 AND RIB 9. 2006-0071  FAA AD  NOTE: THIS TASK HAS TO BE DONE AT THE SAME TIME AS 2007-04-11  TASK 576072-0606-5  ALI REFERENC 576072-02-3  576073-0606-1 550 OUTER WING TOP SKIN MEC DET T: 48000 FC ALI EASA AD  650 I: 6000 FC FAA AD 2006-0071  DETAILED INSPECTION OF OUTER WING TOP SKIN AT FAA AD  ATTACHMENT TO RIB FROM RIB 10 TO RIB 18 BETWEEN 2007-04-11  FRONT AND REAR SPAR.  ALI REFERENC 576073-01-1  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 576073-0606-2 550 OUTER WING TOP SKIN MEC DET T: 40000 FC ALI EASA AD  650 I: 6000 FC FAA AD 2006-0071  DETAILED INSPECTION OF OUTER WING TOP SKIN AT FAA AD  ATTACHMENT TO RIB FROM RIB 10 TO RIB 18 BETWEEN 2007-04-11  FRONT AND REAR SPAR.  ALI REFERENC 576073-01-2  576073-0606-3 550 OUTER WING TOP SKIN MEC DET T: 34000 FC ALI EASA AD  650 I: 6000 FC FAA AD 2006-0071  DETAILED INSPECTION OF OUTER WING TOP SKIN AT FAA AD  ATTACHMENT TO RIB FROM RIB 10 TO RIB 18 BETWEEN 2007-04-11  FRONT AND REAR SPAR.  ALI REFERENC 576073-01-3  576074-0606-1 550 OUTER WING REAR SPAR NDT SDI T: 48000 FC ALI NTM 571129  650 I: 6000 FC CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FAA AD CN 2006-0071 RIB 18 ATTACHMENT POST. FAA AD 96-13 ACCESS: 550HB ALI REFERENC 650HB 576074-01-1  576074-0606-2 550 OUTER WING REAR SPAR NDT SDI T: 40000 FC ALI NTM 571129  650 I: 6000 FC CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FAA AD CN 2006-0071 RIB 18 ATTACHMENT POST. FAA AD 96-13 ACCESS: 550HB ALI REFERENC 650HB 576074-01-2  576074-0606-3 550 OUTER WING REAR SPAR NDT SDI T: 34000 FC ALI NTM 571129  650 I: 6000 FC CN PART 6  SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FAA AD CN 2006-0071 RIB 18 ATTACHMENT POST. FAA AD 96-13 ACCESS: 550HB ALI REFERENC 650HB 576074-01-3  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC 550 578011-C602- 560 DETAILED INSPECTION OF SLAT CAN DRAIN HOLES.  640  650  660  578013-0603-1 512 WING LEADING EDGE MEC GVI T: IMPL.AGE CPCP MRB REFERENC 523 10 YE 578013-C603- 524 GENERAL VISUAL INSPECTION OF WING FRONT SPAR FORWARD I: 5 YE  612 FACE.  623  624 NOTE: 01. ALUMINIUM SHIELD BETWEEN SLAT TRACK 3 TO 8  REMOVED.  02. APPLY TEMPORARY PROTECTION AFTER INSPECTION  PREP.: SLATS TO BE EXTENDED  ACCESS: 512AB 512AT 512BB 512CB 512DB 512EB  512FB 512GB 512HB 512JB 512KB 512LB  523AB 523BB 523CB 523DB 523EB 523FB  523GB 523HB 523JB 523KB 523LB 523MB  524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  612AB 612AT 612BB 612CB 612DB 612EB  612FB 612GB 612HB 612JB 612KB 612LB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  578021-0602-1 181 WING LOWER SKIN MEC DET I: 30 MO CPCP MRB REFERENC 182 MRB S  DETAILED INSPECTION OF WING LOWER SKIN BETWEEN 578021-C602- FUSELAGE AND RIB 2 LH/RH.  578021-0602-2 181 WING CENTER BOX - INBOARD AND OUTBOARD MEC DET I: ISB AD AD EASA AD  182 57-204 CN F-2008-0208  DETAILED INSPECTION OF WING BOTTOM SKIN, ISB FAA AD 98-21 INBOARD AND OUTBOARD OF THE RIB 1 EXTERNAL LOWER SB 57-0204  SURFACE SPLICE BETWEEN FR. 40 AND FR. 47  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 578023-0603-1 511 WING LEADING EDGE MEC DET I: 5 YE CPCP MRB REFERENC 611 578023-C603- DETAILED INSPECTION OF EXTERNAL SURFACE OF  SLAT NO 1.  PREP.: SLATS TO BE EXTENDED.  578031-0603-1 513 WING LEADING EDGE MEC DET T: IMPL.AGE CPCP MRB REFERENC 613 10 YE 578031-C603- DETAILED INSPECTION OF FORWARD WING ROOT, I: 5 YE  INTERNAL STRUCTURE.  NOTE: APPLY TEMPORARY PROTECTION AFTER INSPECTION  PREP.: KRUEGER FLAPS TO BE EXTENDED  ACCESS: 512AB 513AB 513AT  612AB 613AB 613AT  578101-0603-1 530 FLAP TRACK BEAMS NO 2 TO 6 MEC DET I: 5 YE CPCP MRB REFERENC 630 578101-C603- DETAILED INSPECTION OF FLAP TRACK BEAMS NUMBER  2 TO 6, EXTERNAL SURFACE.  NOTE: 01. LUBRICATION RECOMMENDED AS PER  572500-0505-1.  02. FLAPS MUST BE FULLY EXTENDED PRIOR TO  INSPECTION, FLAP TRACK FAIRINGS MUST BE  DETACHED.  578255-0603-1 582 AIR BRAKES END RIBS MEC DET T: 15 YE CPCP MRB REFERENC 682 I: 6 YE 578255-C603- DETAILED INSPECTION OF INNER AND OUTER AIR  BRAKES, SPAR END RIB, HINGES AND SERVO CONTROL FRONT  ATTACHMENT BRACKETS.  PREP.: AIRBRAKES TO BE DEPLOYED.  578261-0603-1 580 SPOILERS END RIBS MEC DET T: 15 YE CPCP MRB REFERENC 680 IMPL.AGE 578261-C603- * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 YE  SPOILER END RIB HINGES, LINKS AND SERVO CONTROL  ATTACHMENT BRACKETS.  PREP.: SPOILER TO BE DEPLOYED.  578261-0606-1 585 SPOILERS END RIBS NDT SDI T: 48000 FC ALI NTM 578261  586 I: 5500 FC FAA AD PART 6  685 SPECIAL DETAILED INSPECTION OF SPOILER 1 AND 2 EASA AD  686 ACTUATOR BRACKET LUGS. 2006-0071  FAA AD  PREP: DETACH JACK ATTACHMENT. 2007-04-11  ALI REFERENC 578261-01-1  578265-0603-1 580 AIRBRAKE AND SPOILER MEC DET I: 10 YE CPCP MRB REFERENC 680 578265-C603- DETAILED INSPECTION OF AIRBRAKES AND SPOILERS  ACTUATOR BEAM ATTACHMENT BOLTS.  PREP.: AIRBRAKES/SPOILERS TO BE DEPLOYED. BOLTS TO  BE REMOVED.  GRACE PERIOD: 5 YEARS STARTING FROM THE ISSUANCE DATE  OF CPCP REVISION 07.  ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB  581JB 581KB  681CB 681DB 681EB 681FB 681GB 681HB  681JB 681KB  578271-0603-1 576 AILERONS END RIBS MEC DET T: IMPL.AGE CPCP MRB REFERENC 592 15 YE 578271-C603- 676 DETAILED INSPECTION OF ALL SPEED AILERON AND I: 9 YE  692 LOW SPEED AILERON END RIBS, HINGES LINK, AND SERVO  CONTROL ATTACHMENT BRACKETS.  PREP.: ALL SPEED AND LOW SPEED AILERON TO BE DEPLOYED  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 578281-0603-1 570 FLAP END RIBS MEC DET T: IMPL.AGE CPCP MRB REFERENC 580 15 YE 578281-C603- 670 DETAILED INSPECTION OF INNER, CENTER AND OUTER I: 9 YE  680 FLAP END RIBS.  PREP.: EXTEND FLAPS  578301-0603-1 570 FLAP TAB HINGES MEC DET I: 4 YE CPCP MRB REFERENC 580 578301-C603- 670 DETAILED INSPECTION OF FLAP TAB HINGES, DRIVE  680 MECHANISM AND BRACKETS.  PREP.: FLAP TAB FAIRINGS TO BE REMOVED  FLAPS TO BE EXTENDED  ACCESS: 572AB 572CB 572GB 572LB 575AB 575BB  575CB 575DB 575FB 575GB 576AB 576BB  576CB 576DB 576EB 576FB 577AB 577BB  577ET 577FT 577GT  581DB 581EB 581FB 581GB 581HB 581JB  581KB  672AB 672CB 672GB 672LB 675AB 675BB  675CB 675DB 675FB 675GB 676AB 676BB  676CB 676DB 676EB 676FB 677AB 677BB  677ET 677FT 677GT  681DB 681EB 681FB 681GB 681HB 681JB  681KB  579001-0603-1 550 WING MEC DET T: 9 YE ISB ISB 57-0212  650 I: 5 YE  DETAILED INSPECTION OF MAIN LANDING GEAR  ATTACHMENT LUGS.  ACCESS: OPEN THE MAIN LANDING GEAR DOORS.  579002-0603-1 532 WING MEC DET T: 8200 FC ISB ISB 57-0237  533 OR  534 DETAILED INSPECTION OF THE REAR ATTACHMENT 5 YE  535 BOLTS OF THE FLAP TRACKS 2 THRU 6 I: 8200 FC  536 OR  632 ACCESS: EXTEND THE FLAPS. 5 YE  633  * * * * * C O N T I N U E D * * * * *  STRUCTURE PROGRAM : WINGS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 579002-0603-1 * * * * * C O N T I N U E * * * * *  634  635  636  579003-0603-1 571 WING NDT SDI T: 18000 FC CN NTM 513104  671 I: 700 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF ATTACHMENT FITTING ISB NTM 574212  GEAR RIB 5 PART 1  CN 2002-620( ACCESS: REMOVE THE MLG ACTUATING CYLINDER ASSEMBLY FAA AD  2000-05-07  ISB 57A0234  579003-0603-2 571 WING NDT SDI T: 14500 FC CN NTM 513104  671 I: 700 FC FAA AD PART 1  SPECIAL DETAILED INSPECTION OF ATTACHMENT FITTING ISB NTM 574212  GEAR RIB 5 PART 1  CN 2002-620( ACCESS: REMOVE THE MLG ACTUATING CYLINDER ASSEMBLY FAA AD  2000-05-07  ISB 57A0234  579004-0603-1 571 MAIN LANDING GEAR ATTACHMENT FITTING MEC DET T: 12000 FC ISB ISB 57-0251  671 I: 100 FC  DETAILED VISUAL INSPECTION OF MAIN LANDING GEAR  RIB 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 574211  671 I: 675 FC PART 4  SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR ISB 57-0251  RIB 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: 
MAINTENANCE PLANNING DOCUMENT 

 ISSUE:APR 01/10 ZONAL Page 1

 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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 ISSUE:APR 01/10 ZONAL Page 2

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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• 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, spillage 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. 
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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. 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

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 ZL-100-0402-1 100 LOWER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 1 C CPCP AMM SSI 5305 MRB S AMM SSI 5334 GENERAL VISUAL INSPECTION OF: MRB Z AMM SSI 5335 - RADOME FOR CONDITION AND DELAMINATION, AMM SSI 5337 - EXTERNAL SKIN FROM FRAME 1 TO FRAME 80 BETWEEN  STRINGER 33 LH AND 33 RH INCLUDING SERVICE DOORS, MRB REFERENC - SKIN AND STRUCTURE SURROUNDING FORWARD, REAR AND  BULK CARGO COMPARTMENT DOORS INCLUDING HINGES AND ZL-100  HOOK ATTACHMENT FITTINGS. 533120-C602- ACCESS: 811 812 813  ZL-100-0402-2 100 LOWER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 5 YE CPCP AMM SSI 5305 MRB S AMM SSI 5335 GENERAL VISUAL INSPECTION OF EXTERNAL SKIN OF LOWER  HALF OF FUSELAGE FROM FRAME 1 TO FRAME 80 WITH MRB REFERENC PARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINAL  LAP JOINTS FOR SEALING AND CORROSION. 533130-C602- ZL-100-0402-3 100 LOWER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 30 MO CPCP MRB REFERENC MRB Z ZL-100  GENERAL VISUAL INSPECTION OF EXTERNAL SKIN OF LOWER 533130-C602- HALF OF FUSELAGE FROM FRAME 1 TO FRAME 80 WITH  PARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINAL  LAP JOINTS FOR SEALING AND CORROSION.  ZL-110-0403-1 110 RADOME MEC GVI I: 2 C MRB Z MRB REFERENC ZL-110  VISUAL INSPECTION OF RADOME COMPONENT INSTALLATION  AND WIRING FOR GENERAL CONDITION  ACCESS: 110AL  ZL-120-0403-1 120 ELECTRONICS-ELT.COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENC ZL-120  GENERAL VISUAL INSPECTION OF ELECTRONICS-, ELECTRICAL  COMPARTMENT INCLUDING CONTROLS AND OXYGEN PIPES.  (ZONES 121/122)  ACCESS: 132AZ  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
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 ZL-120-0403-3 120 ELECTRONICS-ELT.COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENC ZL-120  GENERAL VISUAL INSPECTION OF FLIGHT CONTROL, LANDING  GEAR EMERGENCY EXTENSION AND NLG-STEERING CONTROL  INSTALLATIONS (ZONE 121/122)  ACCESS: 121AF 121BF 121CF 121DF 121EF 121FF  121GF 121HF 121JF 121KF 121LF 121MF  121NF 121PF 122AF 122BF 122CF 122DF  122EF 122FF 122GF 122HF 122JF 122KF  122LF 122MF  ZL-120-0403-4 120 ELECTRONICS-ELT.COMPARTMENT MEC GVI I: 9 YE CPCP MRB REFERENC MRB Z ZL-120  GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE BELOW 531150-C603- CABIN FLOOR LEVEL INCLUDING REAR FACE OF FORWARD  PRESSURE BULKHEAD, IN ZONE 121, 122.  PREP.: REMOVE INSULATION  ACCESS: 131AZ 132AZ  ZL-130-0403-1 130 FWD CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENC ZL-130  GENERAL VISUAL INSPECTION OF:  - FORWARD CARGO COMPARTMENT FOR GENERAL CONDITION  (ZONES 131/132),  - OXYGEN STORAGE AND PIPES AND CARGO COMPARTMENT  FIRE EXTINGUISHER BOTTLES AND MOUNTS,  - BLOW-IN AND BLOW-OUT PNELS (DECOMPRESSION PANELS)  FOR PROPER INSTALLATION.  ACCESS: 132BZ 132DZ  ZL-130-0403-2 130 FWD CARGO COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENC ZL-130  GENERAL 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: 
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 ZL-130-0403-3 131 FWD CARGO COMPARTMENT MEC GVI I: 9 YE CPCP MRB REFERENC 132 MRB Z ZL-130  137 GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531420-C603- 138 BETWEEN CABIN FLOOR AND CARGO FLOOR FRO FRAME 20  TO FRAME 39 INCLUDING CABIN FLOOR STRUCTURE  NOTE: THIS TASK CAN BE PERFORMED AT SAME TIME AS  SB 53-229, REQUIRING SIMILAR ACCESS.  PREP.: REMOVE CEILING PANELS, LININGS, INSULATION.  ACCESS: 131BZ 131CZ  132EZ  ZL-130-0403-4 131 FWD CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC 132 MRB Z ZL-130  137 GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531420-C603- 138 BETWEEN CABIN FLOOR AND CARGO FLOOR FROM FRAME 20 531430-C603- TO FRAME 39 INCLUDING CABIN FLOOR STRUCTURE.  NOTE: THIS TASK CAN BE PERFORMED AT SAME TIME AS  SB 53-0229, REQUIRING SIMILAR ACCESS.  NOTE: ONLY APPLICABLE TO C4, IF A/C WAS USED IN FULL  CARGO CONFIGURATION SINCE LAST INSPECTION  PREP.: REMOVE CEILING PANELS, LININGS AND INSULATION.  ACCESS: 131BZ 131CZ  132EZ  ZL-130-0403-5 133 BAY UNDER FWD CARGO COMP. MEC GVI I: 4 YE CPCP MRB REFERENC 134 MRB Z ZL-130  135 GENERAL VISUAL INSPECTION OF BAY UNDER CARGO 531440-C603- 136 FLOOR PANELS TO BOTTOM CENTER LINE FROM FRAME 20  TO FRAME 39 INCLUDING ROLLER TRACKS.  NOTE: FOR POST MOD 06699(SB 53-0215, 53-0216) A/C RI  MAY BE INCREASED UP TO 5 YEARS  01. INSPECT ZONE IN GENERAL INCLUDING FLIGHT CONTROLS  PRESSURE SEALS, AIR DISTRIBUTION INSTALLATIONS.  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
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 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 AREA  03. INSPECT INTERNAL STRUCTURE FOR GENERAL CONDITION.  04. TPS TO BE APPLIED ON BILGHE AREAS FROM STRINGER  41 LH/RH TO BOTTOM CENTER LINE FROM FRAME 19  TO 39.  05. APPLY TEMPORARY PROTECTION TYPE 1 AND TYPE 2  AFTER INSPECTION.  06. REINSTALL INSULATION.  PREP.: REMOVE FLOOR PANELS AND INSULATION.  ACCESS: 131ABF 131AEF 131AFF 131BF 131CF 131DF  131HF 131JF 131KF 131NF 131PF 131TF  131WF 131XF  132AF 132BF 132CF 132DF 132EF 132FF  132GF 132HF 132JF 132KF 132LF 132MF  132NF  131ABF 131AEF 131AFF 131BF 131CF 131DF  131HF 131JF 131KF 131NF 131PF 131TF  131WF 131XF  132AF 132BF 132CF 132DF 132EF 132FF  132GF 132HF 132JF 132KF 132LF 132MF  132NF  ZL-130-0403-6 137 BAY BEHIND FWD CARGO COMP. MEC GVI I: 1 C MRB Z MRB REFERENC ZL-130  GENERAL VISUAL INSPECTION OF BAY BETWEEN BULKHEAD OF  FWD CARGO COMPARTMENT AND FWD PRESSURE BULKHEAD OF  WING CENTER BOX IN GENERAL WITH PARTICULAR ATTENTION  TO WATER STORAGE SYSTEM AND ENGINE CONTROL CABLES FOR  WEAR AT PRESSURE SEALS. (INCL. ZONE 138)  ACCESS: 131BZ 131CZ 132EZ  ZL-130-0403-7 137 BAY BEHIND FWD CARGO COMP. MEC GVI I: 9 YE MRB Z MRB REFERENC ZL-130  GENERAL 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: 
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 ZL-130-0403-7 * * * * * C O N T I N U E * * * * *  ACCESS: 131BZ 131CZ 132EZ  ZL-130-0403-8 131 FORWARD CARGO COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENC 132 I: 30 MO MRB Z ZL-130  GENERAL VISUAL INSPECTION OF FLOOR STRUCTURE BELOW 532110-C603- GALLEYS AND TOILETS FROM FRAME 26 TO FRAME 33.  01. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1, G2 OR  G3 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 REFERENC FLOOR I: 30 MO 531330-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL  STRUCTURE AROUND WASTE WATER CONNECTION BOX BETWEEN  FR 26 AND FR 27 FROM STR 45 RH TO STR 48 RH.  NOTE: TEMPORARY PROTECTION SYSTEMS TYPE 1 AND TYPE 2  TO BE APPLIED.  PREP.:CARGO FLOOR PANELS AND INSULATION TO BE  REMOVED  ACCESS: 811  ZL-130-0413-2 136 REAR BAY UNDER FWD CARGO COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENC FLOOR I: 30 MO 531330-C603- GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL  STRUCTURE AROUND WASTE WATER CONNECTION BOX BETWEEN  FR 30 AND FR 31 FROM STR 50 RH TO STR 54 RH.  NOTE: TEMPORARY PROTECTION SYSTEMS TYPE 1 AND TYPE 2  TO 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: 
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 ZL-130-0413-2 * * * * * C O N T I N U E * * * * *  REMOVED.  ACCESS: 811  ZL-140-0403-1 141 WING CENTER BOX MEC GVI I: 2 C MRB Z MRB REFERENC ZL-140  GENERAL VISUAL INSPECTION OF WING CENTER BOX  INCLUDING FUEL SYSTEM INSTALLATIONS.  (INCLUDING ZONE 142)  ACCESS: 147AZ 147DZ 148AZ 148DZ  ZL-140-0403-2 141 WING CENTER BOX MEC GVI I: 5 YE CPCP MRB REFERENC 142 MRB Z ZL-140  GENERAL VISUAL INSPECTION OF WING CENTER BOX 531580-C603- STRUCTURE.  NOTE: FILLING COMPOUND EC 3524 A/B INSTALLED ON NON  DRAINABLE AREAS (SOME B2) NOT TO BE REMOVED FOR  INSPECTION.  ACCESS: 147AZ 147DZ 148AZ 148DZ 733 734  ZL-140-0403-3 141 WING CENTER BOX MEC GVI I: 5 YE CPCP MRB REFERENC 142 MRB Z ZL-140  01. GENERAL VISUAL INSPECTION OF WING CENTER BOX 531580-C603- STRUCTURE 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 NON  DRAINABLE AREAS (SOME B2) NOT TO BE REMOVED FOR  INSPECTION.  ACCESS: 147AZ 147DZ 147GZ 733  148AZ 148DZ 148GZ 734  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
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 ZL-140-0403-4 143 AIR CONDITIONING COMPM. MEC GVI I: 1 C MRB Z MRB REFERENC ZL-140  GENERAL VISUAL INSPECTION OF AIR CONDITIONING  COMPARTMENT INCLUDING:  - CONTROLS, DUCTING, WIRING,  - VAPOR SEAL (CENTER FUEL TANK).  (INCLUDING ZONE 144)  ACCESS: 147BZ 147CZ 147DZ 147FZ 147GZ 147HZ  148DZ 148GZ 148HZ  ZL-140-0403-5 143 AIR CONDITIONING COMPM. MEC GVI T: 5 YE CPCP MRB REFERENC 144 I: 5 YE MRB Z ZL-140  GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL 531583-C603- STRUCTURE IN AIR CONDITIONING COMPARTMENT FROM  FRAME 39 TO FRAME 47.  NOTE: IMPROVED DRAINAGE IN ACCORDANCE WITH SB 53-0160  IN RECOMMENDED.  ACCESS: 143AF 143BF 143CF 143DF 147FZ 147GZ  147HZ 733  148GZ 148HZ 734  ZL-140-0403-6 143 AIR CONDITIONING COMPARTM. MEC GVI I: 9 YE CPCP MRB REFERENC 144 MRB Z ZL-140  GENERAL VISUAL INSPECTION OF WING BOX LOWER SECTION 531586-C603- OF FRONT SPAR COVERED BY THE VAPOR SEAL.  PREP.: DISPLACE VAPOR SEAL.  ACCESS: 147BZ 147CZ 147FZ 147GZ 147HZ 148DZ  148GZ 148HZ  ZL-140-0403-7 147 MLG BAY & HYDRAULIC COMPT. MEC GVI I: 1 C MRB Z MRB REFERENC ZL-140  GENERAL 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: 
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 ZL-140-0403-7 * * * * * C O N T I N U E * * * * *  CEILING PANELS.  ACCESS: 147BZ 147CZ 147DZ 147FZ 147GZ 147HZ  147LZ 147MZ 147NZ 147RZ 147SZ 147TZ  147UZ 147VZ 147WZ 147XZ 148DZ 148GZ  148HZ 148LZ 148MZ 148NZ 148RZ 148SZ  148TZ 148UZ 148VZ 148WZ 148XZ  ZL-140-0403-8 147 MLG BAY & HYDRAULIC COMPT. MEC GVI T: 5 YE CPCP MRB REFERENC 148 OR 531590-C603- GENERAL VISUAL INSPECTION OF CONTROLS AND STRUCTURE 34100 FC  INCLUDING MAIN LANDING GEAR DOOR HINGES. I: 2800 FC  NOTE: FOR PREVENTION PURPOSE SB 53-0281  APPLICATION IS RECOMMENDED.  ACCESS: 147AF 147BF 147BZ 147CF 147CZ 147DZ  147FZ 147GZ 147HZ 147LZ 147MZ 147NZ  147RZ 147SZ 147TZ 147UZ 147VZ 147WZ  147XZ 733  148AF 148DZ 148GZ 148HZ 148LZ 148MZ  148NZ 148RZ 148SZ 148TZ 148UZ 148VZ  148WZ 148XZ 734  ZL-140-0403-9 145 ZONE ABOVE WING CENTER BOX MEC GVI I: 9 YE CPCP MRB REFERENC 146 MRB Z ZL-140  GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE FROM 531593-C603- FRAME 39 TO FRAME 54 AND BETWEEN CABIN FLOOR AND  CENTER 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 REFERENC 148 MRB Z ZL-140  GENERAL VISUAL INSPECTION OF CONTROLS AND STRUCTURE 531590-C603- INCLUDING MAIN LANDING GEAR DOOR HINGES.  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
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 ZL-140-0413-1 * * * * * C O N T I N U E * * * * *  NOTE: FOR PREVENTION PURPOSE SB 53-0281  APPLICATION IS RECOMMENDED.  ACCESS: 147AF 147BF 147CF 147FZ 147GZ 147HZ  733  734  ZL-150-0403-1 151 AFT CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENC ZL-150  GENERAL 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 REFERENC ZL-150  GENERAL VISUAL INSPECTION OF INSTALLATIONS INCLUDING  FLIGHT 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 REFERENC 152 I: 9 YE MRB Z ZL-150  GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL 531610-C603- STRUCTURE BETWEEN CABIN FLOOR AND CARGO FLOOR FROM  FRAME 54 TO FRAME 64 INCLUDING CABIN FLOOR STRUCTURE.  NOTE 01: THIS TASK CAN BE PERFORMED AT SAME TIME AS  SB 53-0229, REQUIRING SIMILAR ACCESS  PREP.: REMOVE CEILING PANELS, SIDE LININGS AND  INSULATION.  ACCESS: 812  ZL-150-0403-4 151 AFT CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC 152 MRB Z ZL-150  GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL 531620-C603- * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
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 ZL-150-0403-4 * * * * * C O N T I N U E * * * * *  STRUCTURE BETWEEN CABIN FLOOR AND CARGO FLOOR FROM  FRAME 54 TO FRAME 64 INCLUDING CABIN FLOOR STRUCTURE.  NOTE 1 : THIS TASK CAN BE PERFORMED AT SAME TIME AS  SB53-0229, REQUIRING SIMILAR ACCESS.  NOTE 2 : ONLY APPLICABLE TO C4, IF A/C WAS USED IN  FULL CARGO CONFIGURATION SINCE LAST  INSPECTION.  PREP.: REMOVE CEILING PANELS, SIDE LININGS AND  INSULATION.  ACCESS: 812  ZL-150-0403-5 153 BAY UNDER AFT CARGO COMPT MEC GVI T: 5 YE CPCP MRB REFERENC 154 I: 4 YE MRB Z ZL-150  GENERAL VISUAL INSPECTION OF: 531630-C603- 01. INSPECT ZONE UNDER AFT CARGO COMPARTMENT,  INCLUDING FLIGHT CONTROLS AND AIR DISTRIBUTION  INSTALLATIONS. (PRIOR TO REMOVAL OF INSULATION)  02. REMOVE INSULATION AND INSPECT INTERNAL STRUCTURE  BELOW CARGO FLOOR PANELS TO BOTTOM CENTER LINE  FROM FRAME 54 TO FRAME 64 INCLUDING ROLLER TRACKS  NOTE 1: TPS TO BE APPLIED ON BILGE AREAS FROM  STRINGER 49 LH/RH TO BOTTOM CENTER LINE FROM  FRAME 54 TO 64.03.  NOTE 2: APPLY TEMPORARY PROTECTION TYPE 1 OR TYPE 2  AFTER INSPECTION.  PREP.: REMOVE CARGO FLOOR PANELS AND BALL MATS  INSULATION.  ACCESS: 151BF 151CF 151GF 151HF 151MF 151NF  151SF 151TF 152AF 152BF 152CF 152DF  152EF 152FF 152GF 152HF  812  ZL-160-0403-1 161 BULK CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENC ZL-160  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

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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 REFERENC ZL-160  GENERAL 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 REFERENC 162 MRB Z ZL-160  GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531730-C603- BETWEEN CABIN FLOOR AND CARGO FLOOR FROM FRAME  FRAME 64 TO FRAME 70 INCLUDING CABIN FLOOR STRUCTURE.  NOTE: THIS TASK CAN BE PERFORMED AT SAME TIME AS  SB 53-0229, REQUIRING SIMILAR ACCESS.  PREP.: REMOVE CEILING PANELS, SIDE LININGS AND  INSULATION.  ACCESS: 813  ZL-160-0403-4 161 BULK CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC 162 MRB Z ZL-160  GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE 531730-C603- BETWEEN CABIN FLOOR AND CARGO FLOOR FROM FRAME  FRAME 64 TO FRAME 70 INCLUDING CABIN FLOOR STRUCTURE.  NOTE: THIS TASK CAN BE PERFORMED AT SAME TIME AS  SB 53-0229, REQUIRING SIMILAR ACCESS.  NOTE: ONLY APPLICABLE TO C4, IF A/C WAS USED IN FULL  CARGO CONFIGURATION SINCE LAST INSPECTION.  PREP.: REMOVE CEILING PANELS, SIDE LININGS AND  INSULATION.  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 ZL-160-0403-4 * * * * * C O N T I N U E * * * * *  ACCESS: 813  ZL-160-0403-5 163 BAY UNDER BULK CARGO COMPT. MEC GVI I: 5 YE CPCP MRB REFERENC 164 MRB Z ZL-160  GENERAL VISUAL INSPECTION OF FOLLOWING: 531750-C603- 01. INSPECT BAY UNDER REAR (BULK) CARGO COMPARTMENT  INCLUDING FLIGHT CONTROLS AND AIR EXTRACTION  COMPONENTS. (PRIOR TO REMOVAL OF INSULATION)  02. REMOVE INSULATION  03. INSPECT INTERNAL STRUCTURE BELOW CARGO FLOOR  PANELS TO BOTTOM CENTER LINE FROM FRAME 64 TO  FRAME 70.  04. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 AND  TYPE 2 AFTER INSPECTION.  05. INSTALL INSULATION.  PREP.: REMOVE FLOOR PANELS AND INSULATION.  ACCESS: 161AF 161BF 161CF 161DF 161EF 161FF  161GF  162AF 162BF 162CF 162DF 162EF 162FF  162GF 813  ZL-170-0403-1 171 AFT CABIN UNDERFLOOR COMPT. MEC GVI I: 1 C MRB Z MRB REFERENC ZL-170  GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR  COMPARTMENT INCLUDING FLIGHT CONTROLS, DUCTINGS AND  PRESSURE SEALS FOR GENERAL CONDITION.  (INCLUDING ZONE 172)  ACCESS: 162AZ  ZL-170-0403-2 171 AFT CABIN UNDERFLOOR COMPT. MEC GVI T: 5 YE CPCP MRB REFERENC 172 I: 5 YE MRB Z ZL-170  GENERAL VISUAL INSPECTION OF: 531830-C603- 01. INSPECT FLIGHT CONTROLS BELOW FLOOR PANELS AND  INSTALLATIONS BEHIND 171AZ. (PRIOR TO REMOVAL OF  INSULATION)  02. INSPECT FUSELAGE INTERNAL STRUCTURE BELOW CABIN  FLOOR 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 LOWER  FORWARD FACE.  03. REMOVE INSULATION.  04. INSPECT STRUCTURE FOR GENERAL CONDITION.  05. REINSTALL INSULATION.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1 AND  TYPE 2 AFTER INSPECTION.  NOTE: TPS TO BE APPLIED ON BILGE AREAS FROM STRINGER  40 LH/RH TO BOTTOM CENTER LINE FROM FRAME  70 TO 80.  PREP.: REMOVE FLOOR PANELS AND INSULATION.  ACCESS: 171AF 171AZ  162AZ 172AF 172BF  ZL-200-0402-1 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 1 C MRB Z MRB REFERENC ZL-200  GENERAL VISUAL INSPECTION OF:  - SKIN AND STRUCTURE SURROUNDING FWD, MID, AFT  PASSENGER/CREW DOOR AND EMERGENCY EXITS INCLUDING  SCUFF PLATES, DOOR STOPS AND HOOK ATTACHMENT  FITTINGS. (DOORS TO BE OPENED)  - WINDOWS (ZONE 200).  - FLIGHT DECK AREA (ZONE 211/212).  ACCESS: 831 832 833 834 841 842  843 844  ZL-200-0402-2 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 5 YE CPCP MRB REFERENC MRB Z ZL-200  GENERAL VISUAL INSPECTION OF EXTERNAL SKIN OF UPPER 533140-C602- HALF OF FUSELAGE FROM FRAME 1 TO FRAME 80 WITH  PARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINAL  LAP JOINTS FOR SEALING AND CORROSION  ZL-200-0402-3 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 30 MO CPCP MRB REFERENC 533140-C602- GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 WITH  PARTICULAR ATTENTION TO PAINT PEELING, LONGITUDINAL  LAP JOINTS FOR SEALING AND CORROSION  ZL-200-0402-4 200 UPPER HALF OF FUSELAGE-EXTERNAL MEC GVI I: 1 C MRB Z MRB REFERENC ZL-200  GENERAL VISUAL INSPECTION OF:  - SKIN AND STRUCTURE SURROUNDING FWD PASSENGER/CREW  DOORS 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  ZL-210-0403-1 210 FLIGHT COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENC ZL-210  GENERAL VISUAL INSPECTION OF FLIGHT COMPARTMENT  INCLUDING CONTROLS INSTALLATIONS AND OXYGEN PIPES AS  FAR AS VISIBLE.  ZL-210-0403-2 210 FLIGHT COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENC ZL-210  GENERAL VISUAL INSPECTION OF ZONE INSTALLATIONS  INCLUDING LANDING GEAR EMERGENCY EXTENSION, ENGINE  CONTROLS, FLIGHT CONTROLS.  NOTE: THE FOLLOWING PANELS HAVE NOT TO BE REMOVED:  8VU, 9VU, 11VU, 20VU, 21VU, 22VU, 50VU, 130VU  PREP.: REMOVE SEATS, FLOOR PANELS AND LININGS.  ZL-210-0403-3 210 FLIGHT COMPARTMENT MEC GVI T: 15 YE CPCP MRB REFERENC I: 9 YE MRB Z ZL-210  GENERAL VISUAL INSPECTION OF FUSELAGE UPPER LOBE 531140-C603- INTERNAL STRUCTURE INCLUDING FLOOR STRUCTURE.  NOTE: NO REMOVAL OF FLIGHT CONTROL PANEL, CONSOLES OR  ELECTRICAL PANELS. INSULATION TO BE LIFTED  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FOLLOWING  PANELS HAVE NOT TO BE REMOVED: 8VU, 11VU, 20VU,  21VU, 22VU, 50VU, 130VU).  PREP.: REMOVE SEATS, FLOOR PANEL  REMOVE SIDE WALL AND CEILING PANELS OR  ELECTRICAL PANELS  FLOOR PANELS AND LIFT INSULATION ENOUGH TO  INSPECT THE STRUCTURE.  ZL-220-0403-1 220 PASSENGER COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENC ZL-220  GENERAL VISUAL INSPECTION OF CABIN INCLUDING SEAT  BELTS, BACK RESTS, OVERHEAD STOWAGE COMPARTMENT,  GALLEYS AND TOILETS FOR GENERAL CONDITION (AND  BARRIER NET ATTACHMENTS FOR C4-203) IN ZONES 221/222,  231/232, 241/242, 251/252, 261/262  ZL-220-0403-2 220 PASSENGER COMPARTMENT MEC GVI I: 5 YE MRB Z MRB REFERENC ZL-220  GENERAL VISUAL INSPECTION OF:  - LOWER DOOR FRAME  - ZONE 220 INCL. INSTALLATIONS AND AIR DISTRIBUTION.  PREP.: REMOVE LOWER SIDE PANELS, LOWER DOOR FRAME  PANELS AND INSULATION,  ZL-220-0403-5 220 PASSENGER COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENC 230 I: 5 YE MRB Z ZL-220  240 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE 532120-C603- 250 BELOW GALLEYS AND TOILETS AND DOOR ENTRANCE AREAS.  260  PREP: REMOVE GALLEYS AND TOILETS AND FLOOR PANELS  NOTE: 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 REFERENC 230 I: 9 YE MRB Z ZL-220  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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- 250 INTERNAL STRUCTURE FROM FRAME 11/11.1 TO REAR 533240-C603- 260 PRESSURE BULKHEAD FORWARD FACE AND FLOOR STRUCTURE,  UP TO STRINGER 15 EXCLUDING SEAT TRACKS AND FROM  STRINGER 15 LH/RH TO CROWN CENTER LINE.  THIS TASK CAN BE PERFORMED AT THE SAME TIME AS  SB 53-0229 REQUIRING SIMILAR ACCESS.  PREP.: REMOVE TOILET, GALLEY, FLOOR PANELS  REMOVE 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 REFERENC 230 ZL-220  240 GENERAL VISUAL INSPECTION OF ZONES 223/224,  250 233/234,243/244,253/254,263/264 INCLUDING  260 INSTALLATIONS.  NOTE: INSPECTION TO BE PERFORMED FROM LATERAL HATRACK  INSTALLATION TO CENTRAL HATRACK INSTALLATION  PREP.: REMOVE CEILING PANELS.  ZL-220-0403-9 220 PASSENGER COMPARTMENT MEC GVI T: 5 YE CPCP MRB REFERENC 230 I: 5 YE 534101-C603- 240 GENERAL VISUAL INSPECTION OF SEAT TRACKS 534110-C603- 250 BETWEEN FRAME 15A AND FRAME 80, EXCEPT 534120-C603- 260 BELOW GALLEY, TOILETS AND DOOR AREA. 534130-C603- PREP.: REMOVE PASSENGER SEAT. (WITHOUT FLOOR PANELS) 534140-C603- ZL-221-0403-1 220 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 1 C MRB Z MRB REFERENC ZL-221  GENERAL VISUAL INSPECTION OF UPPER (MAIN) DECK CARGO  COMPARTMENT (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 REFERENC I: 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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- BELOW 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 REFERENC 230 I: 9 YE MRB Z ZL-221  240 GENERAL VISUAL INSPECTION FUSELAGE UPPER LOBE 533250-C603- 250 INTERNAL STRUCTURE FROM FRAME 11/11.1 TO REAR 533260-C603- 260 PRESSURE BULKHEAD FORWARD FACE AND FLOOR STRUCTURE,  UP TO STRINGER 15 EXCLUDING SEAT TRACKS AND FROM  STRINGER 15 LH/RH TO CROWN CENTER LINE.  THIS TASK CAN BE PERFORMED AT THE SAME TIME AS  SB 53-0229 REQUIRING SIMILAR ACCESS.  PREP.: REMOVE TOILET, GALLEY, FLOOR PANELS  REMOVE 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 REFERENC ZL-221  GENERAL 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 REFERENC ZL-221  GENERAL VISUAL INSPECTION OF SKIN AND STRUCTURE  SURROUNDING 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 ZL-230-0403-1 230 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC MRB Z ZL-230  GENERAL VISUAL INSPECTION OF ZONE 231/232 INCLUDING 534110-C603- INSTALLATIONS,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 REFERENC MRB Z C53-220-01-0 GENERAL VISUAL INSPECTION OF ZONE 231/232 INCLUDING ZL-230  INSTALLATIONS, AIR DISTRIBUTION DUCTS.  PREP.: REMOVE SIDEWALL PANELS AND INSULATION.  ZL-240-0403-1 240 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC MRB Z ZL-240  GENERAL VISUAL INSPECTION OF ZONES 241/242, 145/146 534120-C603- INCLUDING INSTALLATIONS, AIR DISTRIBUTION DUCTS AND  SEAT TRACKS.  PREP.: REMOVE PAX SEATS, LININGS, LOWER SIDE PANELS,  LOWER DOOR FRAME PANELS AND INSULATION IN AREA  OF 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 ACCESS  TO ZONE 145 AND 146 (ZONES 241/242).  ACCESS: 241AGF 241AKF 241ASF 241ZF 242AAF 242AJF  ZL-240-0403-2 240 UPPER (MAIN) DECK CARGO COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC MRB Z C53-220-01-0 GENERAL VISUAL INSPECTION OF ZONES 241/242, 145/146 ZL-240  INCLUDING INSTALLATIONS, AIR DISTRIBUTION DUCTS.  PREP.: REMOVE LININGS, LOWER SIDE PANELS, LOWER DOOR  FRAME 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  ZL-250-0403-1 250 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC MRB Z ZL-250  GENERAL VISUAL INSPECTION OF ZONE 251/252 INCLUDING 534130-C603- INSTALLATIONS, AIR DISTRIBUTION DUCTS AND SEAT  TRACKS.  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 REFERENC ZL-250  GENERAL VISUAL INSPECTION OF ZONE 251/252 INCLUDING  INSTALLATIONS AND AIR DISTRIBUTION DUCTS.  PREP.: REMOVE SIDEWALL PANELS AND INSULATION.  ZL-260-0403-1 260 PASSENGER COMPARTMENT MEC GVI I: 5 YE CPCP MRB REFERENC MRB Z ZL-260  GENERAL VISUAL INSPECTION OF ZONE 261/262 INCLUDING 534140-C603- INSTALLATIONS, AIR DISTRIBUTION DUCTS AND SEAT  TRACKS.  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 REFERENC ZL-260  GENERAL VISUAL INSPECTION OF ZONE 261/262 INCLUDING  INSTALLATIONS 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 5309 MRB S AMM SSI 5339 * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 5339 - TAIL CONE, AMM SSI 5339 - APU AIR INTAKE AND EXHAUST AREA,  - DRAIN HOLES, MRB REFERENC - LOWER FUSELAGE AT FRAME 80: BETWEEN STRINGERS  34RH AND LH. ZL-300  531940-C602- ZL-300-0402-2 330 EMPENNAGE AND FUSELAGE TAIL MEC GVI I: 1 C CPCP MRB REFERENC 340 MRB Z ZL-300  GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 531940-C602- - HORIZONTAL STABILIZER TRAVEL APRON AREA  AND FAIRINGS,  - HORIZONTAL STABILIZER LEADING EDGE,  - HORIZONTAL STABILIZER TIP,  - ELEVATOR AND DRAIN HOLES,  - FLIGHT CONTROLS AND INSTALLATIONS AS FAR AS VISIBLE  ZL-300-0402-3 320 EMPENNAGE AND FUSELAGE TAIL MEC GVI I: 1 C CPCP MRB REFERENC MRB Z ZL-300  GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 531940-C602- - VERTICAL STABILIZER LEADING EDGE,  - DORSAL FIN,  - VERTICAL STABILIZER TIP,  - RUDDER,  - DRAIN HOLES,  - FLIGHT CONTROLS AND INSTALLATIONS AS FAR AS  VISIBLE.  ZL-300-0402-4 300 EMPENNAGE AND FUSELAGE TAIL MEC GVI T: 9 YE CPCP MRB REFERENC I: 4 YE MRB Z ZL-300  GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 531940-C602- - 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 27-102  SIL  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 VALVE  INCLUDING LOWER PRESSURE DOME AREA FOR CONDITION  ACCESS: 312AR  ZL-310-0403-2 311 TAIL CONE AREA, HORIZONTAL STABILIZER MEC GVI I: 5 YE CPCP MRB REFERENC 312 MRB Z ZL-310  319 GENERAL VISUAL INSPECTION OF FOLLOWING ZONES 531940-C603- INCLUDING STRUCTURE: 551101-C603- - HORIZ. AND VERT. STAB. ATTACHM. AREA,  - HORIZONTAL STABILIZER CENTER SECTION BOX EXTERNAL  STRUCTURE,  - FUSELAGE INTERNAL STRUCTURE BETWEEN FR80 AND 92  INCLUDING REAR PRESSURE BULKHEAD.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION.  ACCESS: 313AL  312AR  ZL-310-0403-3 310 TAIL CONE AREA, HORIZONTAL STABILIZER MEC GVI I: 9 YE CPCP MRB REFERENC MRB Z ZL-310  GENERAL VISUAL INSPECTION OF STRUCTURE IN FOLLOWING 538829-C603- ZONES: 551101-C603- - TAIL CONE-APU AIR INTAKE AREA ZONE 313/314, 551110-C603- - HORIZONTAL STABILIZER CENTER SECTION BOX INTERNAL  STRUCTURE ZONE 319.  NOTE: APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION.  (DO NOT SPRAY TEMPORARY PROTECTION AGAINST  FIRE WALLS. IN CASE OF FIRE THIS COULD CAUSE  AN EXPLOSION.)  ACCESS: 312AR 313AL  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 REFERENC ZL-310  GENERAL 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  ZL-320-0403-1 320 VERTICAL STABILIZER AREA MEC GVI I: 5 YE MRB Z MRB REFERENC ZL-320  GENERAL VISUAL INSPECTION OF STRUCTURE IN FOLLOWING  ZONES:  - 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  322CL 324AT 324BT 325AL 325AR 325BL  325CL 325DL 325EL 325FL 325GL 325HL  325JL 325KL  ZL-320-0403-2 323 VERTICAL STAB.SPAR BOX MEC GVI I: 5 YE CPCP MRB REFERENC MRB Z ZL-320  GENERAL VISUAL INSPECTION OF ZONE INCLUDING 553101-C603- FLIGHT CONTROL INSTALLATIONS FROM RIB 1 TO RIB12.  ACCESS: 311AZ 311BZ 312AR 322AL 322BL 322CL  325AL 325BL 325CL 325DL 325EL 325FL  325GL 325HL 325JL 325KL  ZL-320-0403-3 320 VERT.STAB.TRAIL.EDGE/RUDDER MEC GVI I: 2 C MRB Z MRB REFERENC ZL-320  GENERAL VISUAL INSPECTION OF ZONE INCLUDING FLIGHT  CONTROL INSTALLATIONS AND ATTACHMENTS.  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  326DL 326FL 326HL 326KL  ZL-320-0403-4 326 RUDDER MEC GVI I: 5 YE MRB Z MRB REFERENC ZL-320  GENERAL VISUAL INSPECTION OF ZONE INCLUDING  INTERNAL STRUCTURE.  ACCESS: 325AL 325AR 325BL 325CL 325DL 325EL  325FL 325GL 325HL 325JL 325KL 326AL  326AR 326BL 326BR 326CL 326CR 326DL  326DR 326EL 326ER 326FL 326GL 326HL  326JL 326KL 326LL  ZL-330-0403-1 330 HORIZONTAL STABILIZER MEC GVI I: 5 YE CPCP MRB REFERENC 340 MRB Z ZL-330  GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: 551120-C603- - LEADING EDGE ZONE 331/341, 551130-C603- - STABILIZER TIP ZONE 332/342, 551301-C603- - 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  334CT 334DT 334ET 334FT 334GT 334HT  334JT 334KT 334LT  341AB 341BB 341CB 342AB 344AT 344BT  344CT 344DT 344ET 344FT 344GT 344HT  344JT 344KT 344LT  ZL-330-0403-2 330 HORIZ.STAB.TRLG.EDGE/ELEVATOR MEC GVI I: 2 C MRB Z MRB REFERENC 340 ZL-330  GENERAL 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 AND  ATTACHMENTS.  ACCESS: 334AT 334BT 334CT 334DT 334ET 334FT  334GT 334HT 334JT 334KT 334LT 335AB  335AT 335BB 335BT 335CB 335CT 335DB  335DT 335EB 335ET  344AT 344BT 344CT 344DT 344ET 344FT  344GT 344HT 344JT 344KT 344LT 345AB  345AT 345BB 345BT 345CB 345CT 345DB  345DT 345EB 345ET  ZL-400-0402-1 415 PYLON BOX EXTERNAL SURFACE RIB 1 TO 18 MEC GVI T: 10 YE CPCP MRB REFERENC 416 I: 5 YE MRB Z ZL-400  425 GENERAL VISUAL INSPECTION OF PYLON BOX EXTERNAL 543101-C602- 426 SURFACE FROM RIB 1 TO RIB 18 AND FROM LOWER SPAR TO  473 UPPER SPAR, PYLON AND ENGINE NACELLE STRUCTURE,  474 ACCESS PANELS AND DOORS.  483  484 PREP: COWLS OPENED  ZL-410-0403-1 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 1 C MRB Z MRB REFERENC 420 ZL-410  GENERAL VISUAL INSPECTION OF ZONES, INCLUDING:  - FUEL CONTROLS,  - ENGINE CONTROLS,  - PNEUMATIC INSTALLATIONS,  - HYDRAULIC INSTALLATIONS.  ACCESS: 413AL 413BL 413EL 413FL 414AR 414BR  414CR 414DR 415AL 416AR  423AL 423BL 423EL 423FL 424AR 424BR  424CR 424DR 425AL 426AR  ZL-410-0403-2 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 5 YE MRB Z SIL 54-019  420  GENERAL VISUAL INSPECTION OF ZONE STRUCTURE. MRB REFERENC ZL-410  ACCESS: 413AL 413BL 413EL 413FL 414AR 414BR  414CR 414DR 415AL 416AR  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  424CR 424DR 425AL 426AR  ZL-410-0403-3 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 1 C MRB Z MRB REFERENC 420 ZL-410  GENERAL VISUAL INSPECTION OF ZONES, INCLUDING:  - FUEL CONTROLS,  - ENGINE CONTROLS,  - PNEUMATIC INSTALLATIONS,  - HYDRAULIC INSTALLATIONS.  ACCESS: 413AL 413BL 413FL 413GL 413HL 414AR  414BR 414CR 414DR 414ER 415AL 416AR  423AL 423BL 423FL 423GL 423HL 424AR  424BR 424CR 424DR 424ER 425AL 426AR  ZL-410-0403-4 410 FORWARD PYLON-UPPER/LOWER MEC GVI I: 5 YE MRB Z SIL 54-019  420  GENERAL VISUAL INSPECTION OF ZONES FOR CONDITION OF MRB REFERENC STRUCTURE ZL-410  ACCESS: 413AL 413BL 413FL 413GL 413HL 414AR  414BR 414CR 414DR 414ER 415AL 416AR  423AL 423BL 423FL 423GL 423HL 424AR  424BR 424CR 424DR 424ER 425AL 426AR  ZL-410-0403-5 410 PYLON LEADING EDGE AND LOWER AFT ZONE MEC GVI I: ENG. CHG MRB Z MRB REFERENC 420 ZL-410  470 GENERAL VISUAL INSPECTION OF:  480 - PYLON LEADING EDGE ZONE 411/412 AND 421/422,  - LOWER AFT PYLON ZONE 475/476 AND 485/486.  ACCESS: 411AL  421AL  475AL 475BL 475CL 475DL 476AR 476BR  485AL 485BL 485CL 485DL 486AR 486BR  ZL-410-0403-6 410 PYLON LEADING EDGE AND LOWER AFT ZONE MEC GVI I: ENG. CHG MRB Z MRB REFERENC 420 ZL-410  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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:  480 - PYLON LEADING EDGE ZONE 411/412 AND 421/422,  - LOWER AFT PYLON ZONE 475/476 AND 485/486.  ACCESS: 411AL  421AL  475AL 475BL 475CL 476AR  485AL 485BL 485CL 486AR  ZL-430-0403-1 430 ENGINE MEC GVI I: 1 C MRB Z MRB REFERENC 440 ZL-430  450 GENERAL VISUAL INSPECTION OF COWLING STRUCTURE,  460 LOCKS AND LATCHES IN ZONES 435, 436, 451, 452, 453,  454, 455, 456, 445, 446, 461, 462, 463, 464, 465  AND 466.  ZL-430-0403-2 430 NOSE COWL ENG GVI I: ENGINE MRB Z MRB REFERENC 440 BUILD UP ZL-430  GENERAL VISUAL INSPECTION OF AIR INTAKE RING  (NOSE COWL).  NOTE: RIVETED ACCESS PANELS (PW-ENGINES) NOT TO BE  REMOVED  ACCESS: 433AL 434AR 434BR  443AL 444AR 444BR  ZL-430-0403-3 430 ENGINE ENG GVI I: C MRB Z MRB REFERENC 440 OR ZL-430  GENERAL 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 STARTER  AIR 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 OF  COMPONENTS, PLUMBING, CLAMPS, BRACKETS, LINKAGES AND  ELECTRICAL LEADS ETC.  ZL-450-0403-1 450 FAN REVERSER/ENGINE CORE ENG GVI I: 1 C MRB Z MRB REFERENC 460 ZL-450  GENERAL VISUAL INSPECTION OF FAN REVERSER AND ENGINE  CORE 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  445AL 465AL 466AR  ZL-450-0403-2 450 FAN REVERSER/ENGINE CORE ENG GVI I: 1 C MRB Z MRB REFERENC 460 ZL-450  GENERAL VISUAL INSPECTION OF FAN REVERSER AND ENGINE  CORE 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 REFERENC 480 ZL-470  GENERAL VISUAL INSPECTION OF ZONES, INCLUDING:  - ENGINE CONTROLS,  - FIRE EXTINGUISHER CONTAINER & MOUNTS,  - INDICATING SYSTEM COMPONENTS.  ACCESS: 471AL 471BL 472AR 472BR 473AL 473BL  473DL  481AL 481BL 482AR 482BR 484AR 484BR  484DR  ZL-470-0403-2 470 PYLON/WING LEADING EDGE MEC GVI I: 5 YE MRB Z MRB REFERENC 480 ZL-470  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 FIRE  SHUT-OFF VALVES AND ASSOCIATED CONTROLS.  ACCESS: 471AL 471BL 472AR 472BR 473AL 473BL  473DL  481AL 481BL 482AR 482BR 484AR 484BR  484DR  ZL-500-0402-1 500 EXTERNAL SURFACE OF MAIN WING BOX UPPER MEC GVI I: 2 C CPCP MRB REFERENC 600 AND LOWER SKIN OR MRB Z ZL-500  30 MO 573301-C602- GENERAL VISUAL INSPECTION OF EXTERNAL SURFACE OF MAIN  WING BOX UPPER AND LOWER SKIN SURFACE FROM ROOT TO  TIP (EXCLUDING SKIN PANEL N°2 BETWEEN RIB 1 TO RIB 9)  ZL-500-0402-2 500 WING MEC GVI I: 1 C CPCP ISB 24-073  600 MRB Z SIL 27-022  EXTEND SLATS, FLAPS AND AIRBRAKES AND PERFORM A  GENERAL VISUAL INSPECTION OF THE FOLLOWING AREAS: MRB REFERENC - AREA FORWARD OF FRONT SPAR,INCLUDING WING LEADING ZL-500  EDGE, SLATS, SLAT TRACKS AND SEALS, KRUEGER FLAP 573301-C602- AND MECHANISM, FLIGHT CONTROLS,ANTI-ICE AND FUEL 573330-C603- SYSTEM INSTALLATIONS AND ANTI-ICE EXHAUST HOLES 573401-C602- - WING TIP 578255-C603- - BOTTOM SKIN BETWEEN FRONT AND REAR SPARS 578261-C603- - AREA AFT OF REAR SPAR, INCLUDING INSTALLATIONS AS 578271-C603- VISIBLE IN PARTICULAR AREA FWD OF ALL SPEED AILE- 578281-C603- RON,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 RESPECTIVE  DRAIN HOLES  - SPOILERS AND AIRBRAKES SKIN AND ATTACHMENT LUGS  AND BEARINGS AND THEIR RESPECTIVE DRAIN HOLES  - FLAPS, IN PARTICULAR BOTTOM SKIN AND THEIR  RESPECTIVE DRAIN HOLES  - EXTERNAL SURFACES OF WING LEADING EDGE UPPER AND  LOWER 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 EXTENDED  ZL-500-0402-3 500 EXTERNAL SURFACE OF MAIN WING BOX UPPER MEC GVI I: 2 YE CPCP MRB REFERENC 600 AND LOWER SKIN MRB Z ZL-500  573302-C602- GENERAL VISUAL INSPECTION OF EXTERNAL SURFACE OF MAIN  WING 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 REFERENC 612 MRB Z ZL-510  GENERAL VISUAL INSPECTION OF ZONE, WITH PARTICULAR 578013-C603- ATTENTION TO FLIGHT CONTROLS INCLUDING DRIVE SHAFTS  AND UNIVERSAL JOINTS (GAITERS IN PLACE AND NOT  DAMAGED), ENGINE CONTROL CABLES FOR WEAR AT  FAIRLEADS (4 OFF), ANTI-ICE VALVES AND LOW PRESSURE  FUEL 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  512GB 512HB 512JB 512KB 512LB 513AT  612AB 612BB 612CB 612DB 612EB 612FB  612GB 612HB 612JB 612KB 612LB 613AT  ZL-510-0403-3 512 INBOARD LEADING EDGE MEC GVI I: 5 YE CPCP MRB REFERENC 612 MRB Z ZL-510  GENERAL VISUAL INSPECTION OF INTERNAL STRUCTURE OF 574120-C603- WING LEADING EDGE UPPER AND LOWER SKIN FROM ROOT TO  TIP.  PREP.: EXTEND SLATS.  ACCESS: 512AB 512BB 512CB 512DB 512EB 512FB  512GB 512HB 512JB 512KB 512LB 513AT  612AB 612BB 612CB 612DB 612EB 612FB  612GB 612HB 612JB 612KB 612LB 613AT  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

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THRESHOLD (T) 

INTERVAL (I)

 ZL-520-0403-2 523 FIXED LEADING EDGE MEC GVI I: 1 C CPCP MRB REFERENC 623 MRB Z ZL-520  GENERAL VISUAL INSPECTION OF ZONE, WITH PARTICULAR 578013-C603- ATTENTION TO FLIGHT CONTROLS INCLUDING DRIVE SHAFTS  AND UNIVERSAL JOINTS (GAITERS IN PLACE AND NOT  DAMAGED), ENGINE CONTROLS, ANTI ICE, PNEUMATIC DUCT  AND 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  523GB 523HB 523JB 523KB 523LB 523MB  524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  ZL-520-0403-3 523 FIXED LEADING EDGE MEC GVI I: 5 YE CPCP MRB REFERENC 623 MRB Z ZL-520  GENERAL VISUAL INSPECTION OF ZONE FOR CONDITION OF 578013-C603- INTERNAL 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  523GB 523HB 523JB 523KB 523LB 523MB  524AB 524BB 524CB 524DB 524EB 524FB  524GB 524HB 524JB 524KB  623AB 623BB 623CB 623DB 623EB 623FB  623GB 623HB 623JB 623KB 623LB 623MB  624AB 624BB 624CB 624DB 624EB 624FB  624GB 624HB 624JB 624KB  ZL-530-0403-1 530 FAIRINGS-FLAP TRACKS 2 TO 6 MEC GVI I: 5 YE MRB Z MRB REFERENC 630 ZL-530  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 6  INCLUDING:  - SCREW JACKS, CARRIAGES AND OTHER INSTALLATIONS,  - FLAP TRACK BEAM AND FAIRINGS.  PREP.: EXTEND FLAPS.  ACCESS: 532AF 532AM 533AF 533AM 534AF 534AM  535AF 535AM 536AF 536AM  632AF 632AM 633AF 633AM 634AF 634AM  635AF 635AM 636AF 636AM  ZL-530-0403-2 531 WING TIP MEC GVI I: 5 YE CPCP MRB REFERENC 631 MRB Z ZL-530  GENERAL VISUAL INSPECTION OF ZONE. 572401-C603- ACCESS: 531AB 531AT 531BB  631AB 631AT 631BB  ZL-540-0403-1 540 MAIN FUEL TANK-INBOARD MEC GVI I: 5 YE CPCP MRB REFERENC 550 MRB Z ZL-540  560 GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 571180-C603- 640 - FUEL FEED,REFUEL,DEFUEL,VENTILATION AND JETTISON 571185-C603- 650 SYSTEM PIPES (WHEN FITTED) AND COMPONENTS AND 571190-C603- 660 QUANTITY INDICATION SYSTEM, 573310-C603- - STRUCTURE, 573320-C603- - STRONTIUM CHROMATE CAPSULES (IF INSTALLED) FOR 573330-C603- CORRECT CONTENT.  - OUTBOARD WING LOWER SKIN AT FUEL TANK ACCESS DOORS  AND ASSOCIATED DOORS BETWEEN RIB 01 AND RIB 27.  - WING MAIN BOX INTERNAL STRUCTURE FROM FRONT TO  REAR SPAR BETWWEN RIB 1 AN RIB 27 AND WING TIP  ACCESS: 541AB 541BB 541CB 542CB 542DB 542EB  543AB 543BB 543CB 543DB  550BB 550DB 550EB 550GB 550LB 550QB  560AB  641AB 641BB 641CB 642CB 642DB 642EB  643AB 643BB 643CB 643DB  650BB 650DB 650EB 650GB 650LB 650QB  660AB  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

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THRESHOLD (T) 

INTERVAL (I)

 ZL-550-0403-1 550 FUEL TANK & SURGE TANK MEC GVI I: 5 YE CPCP MRB REFERENC 650 MRB Z ZL-550  GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 571180-C603- - FUEL FEED,REFUEL,DEFUEL,VENTILATION AND JETTISON 571185-C603- SYSTEM (WHEN FITTED), PIPES AND COMPONENTS, 571190-C603- QUANTITY INDICATING SYSTEM, 573310-C603- - VENT HOLES IN RIB 15 (FOR OBSTRUCTION), 573320-C603- - INTERNAL STRUCTURE, INCLUDES ZONE 560 RESPECTIVELY 573330-C603- 660,  - WING MAIN BOX INTERNAL STRUCTURE FROM FRONT TO  REAR SPAR, BETWEEN RIB 27 AND WING TIP.  - OUTBOARD WING LOWER SKIN AT SURGE TANK ACCESS DOORS  AND ASSOCIATED DOORS.  - STRONTIUM CHROMATE CAPSULES (IF INSTALLED) FOR  CORRECT CONTENT.  ACCESS: 550BB 550DB 550EB 550GB 550LB 550QB  560AB  650BB 650DB 650EB 650GB 650LB 650QB  660AB  ZL-570-0402-1 571 MAIN LANDING GEAR BAY MEC GVI I: 1 C MRB Z MRB REFERENC 671 ZL-570  GENERAL 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 REFERENC 672 MRB Z ZL-570  01. GENERAL VISUAL INSPECTION OF: 572201-C603- - WING FIXED TRAILING EDGE INCLUDING REAR SPAR  AFT FACE AND FALSE REAR SPAR RIB 1 TO RIB 9  - WING FIXED TRAILING EDGE INCLUDING REAR SPAR  AFT FACE RIBS 9 TO RIB 25.  - TRAILING EDGE AREA INCLUDING FLIGHT CONTROLS  AND FUEL ISOLATION VALVE  - AFT WING ROOT AREA INCLUDING FLIGHT CONTROLS  INNER FLAP HINGES  - ALL SPEED AILERON HINGE AND ACTUATOR  ATTACHMENTS  - FLAPS DRIVE SYSTEM UNIVERSAL JOINTS (GAITERS IN  PLACE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 NOT  EXCEEDING 9 YEARS  PREP.: FLAPS FULLY EXTENDED  ACCESS: 572AB 572CB 572GB 572LB 575AB 575AT  575BB 575CB 575DB 575EB 575FB 575GB  576AB 576BB 576CB 576DB 576EB 576FB  577AB 577BB 577ET 577FT 577GT  672AB 672CB 672GB 672LB 675AB 675AT  675BB 675CB 675DB 675EB 675FB 675GB  676AB 676BB 676CB 676DB 676EB 676FB  677AB 677BB 677ET 677FT 677GT  ZL-570-0403-2 572 T/E FLAP-ALLSPEED AIL. MEC GVI I: 9 YE CPCP MRB REFERENC 672 MRB Z ZL-570  01. GENERAL VISUAL INSPECTION OF STRUCTURE INCLUDING: 572201-C603- -TRAILING EDGE AREA INTERNAL STRUCTURE, 572210-C603- -INNER FLAP INTERNAL STRUCTURE AS FAR AS VISIBLE, 572220-C603- -ALL SPEED AILERON INTERNAL STRUCTURE, 573301-C602- 02. APPLY TEMPORARY PROTECTION SYSTEMS TYPE 1,  G2 OR G3 AFTER INSPECTION.  PREP.: FLAPS FULLY EXTENDED  ACCESS: 572AB 572CB 572GB 572LB 575AB 575AT  575BB 575CB 575DB 575EB 575FB 575GB  576AB 576BB 576CB 576DB 576EB 576FB  577AB 577BB 577ET 577FT 577GT  672AB 672CB 672GB 672LB 675AB 675AT  675BB 675CB 675DB 675EB 675FB 675GB  676AB 676BB 676CB 676DB 676EB 676FB  677AB 677BB 677ET 677FT 677GT  ZL-570-0403-3 577 AFT WING ROOT MEC GVI I: 5 YE MRB Z MRB REFERENC 677 ZL-570  GENERAL VISUAL INSPECTION OF ZONE FOR CONDITION OF  STRUCTURE INCLUDING FLAP BEAM AND ATTACHMENT  BEARINGS.  PREP.: EXTEND FLAPS.  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  677AB 677AT 677BB 677BT 677CT 677DT  ZL-580-0403-1 580 INTERM/OUTB.FLAP TRAIL.EDGE MEC GVI I: 2 C CPCP MRB REFERENC 680 MRB Z ZL-580  GENERAL VISUAL INSPECTION OF ZONE INCLUDING FLIGHT 572210-C603- CONTROL INSTALLATIONS AND FLAP TAB HINGES AND FLAPS  DRIVE 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 YEARS  PREP.: EXTEND FLAPS.  ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB  581JB 581KB  681CB 681DB 681EB 681FB 681GB 681HB  681JB 681KB  ZL-580-0403-2 580 INTERM/OUTB.FLAP TRAIL.EDGE MEC GVI I: 5 YE MRB Z MRB REFERENC 680 ZL-580  GENERAL VISUAL INSPECTION OF ZONE FOR CONDITION OF  STRUCTURE INCLUDING FLAP INTERNAL STRUCTURE.  PREP.: EXTEND FLAPS.  ACCESS: 581CB 581DB 581EB 581FB 581GB 581HB  581JB 581KB  681CB 681DB 681EB 681FB 681GB 681HB  681JB 681KB  ZL-590-0403-1 590 TRAIL.EDGE-LOWSPEED AIL. MEC GVI I: 2 C CPCP MRB REFERENC 690 MRB Z ZL-590  GENERAL VISUAL INSPECTION OF ZONE INCLUDING FLIGHT 572210-C603- CONTROL INSTALLATIONS AND LOW SPEED AILERON HINGES 572220-C603- AND ACTUATOR ATTACHMENTS AND WING FIXED TRAILING  EDGE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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 YEARS  ACCESS: 591AB 591BB 591CB 591DB 592AB 592BB  592CB 592DB 592EB 592FB 592GB 592HB  691AB 691BB 691CB 691DB 692AB 692BB  692CB 692DB 692EB 692FB 692GB 692HB  ZL-590-0403-2 590 TRAIL.EDGE-LOWSPEED AIL. MEC GVI I: 5 YE MRB Z MRB REFERENC 690 ZL-590  GENERAL VISUAL INSPECTION OF ZONE STRUCTURE  INCLUDING LOW SPEED AILERON STRUCTURE.  ACCESS: 591AB 591BB 591CB 591DB 592AB 592BB  592CB 592DB 592EB 592FB 592GB 592HB  691AB 691BB 691CB 691DB 692AB 692BB  692CB 692DB 692EB 692FB 692GB 692HB  ZL-710-0402-1 711 NOSE GEAR MEC GVI I: 1 C CPCP MRB REFERENC MRB Z C53-100-02-0 GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: ZL-710  NOSE 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 REFERENC MRB Z C53-100-02-0 GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: ZL-710  LOWER HALF OF FUSELAGE ZONE 120  - DOOR HINGE FITTINGS  NOSE 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 ZL-730-0402-1 731 MAIN GEAR MEC GVI I: 1 C MRB Z MRB REFERENC 741 ZL-730  GENERAL VISUAL INSPECTION OF ZONE INCLUDING  LANDING GEAR COMPONENTS AND INSTALLATIONS.  ZL-730-0402-2 730 MAIN GEAR DOORS & AREA MEC GVI I: 1 C CPCP MRB REFERENC 740 MRB Z C53-100-02-0 GENERAL VISUAL INSPECTION OF FOLLOWING ZONES: ZL-730  LOWER HALF OF FUSELAGE ZONE 147/148  - SKIN SURROUNDING MAIN GEAR BAY CUT-OUT  - DOOR HINGE FITTINGS  MAIN 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 REFERENC MRB Z ZL-810  GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 523101-C602- - HOOK FITTINGS,  - SEALS,  - STRUCTURE,  - HYDRAULIC SYSTEM AS APPLICABLE.  ACCESS: 811  ZL-810-0402-2 812 AFT CARGO COMPARTMENT DOOR MEC GVI I: 1 C CPCP MRB REFERENC MRB Z ZL-810  GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 523201-C602- - HOOK FITTINGS,  - SEALS,  - STRUCTURE,  - HYDRAULIC SYSTEM AS APPLICABLE.  ACCESS: 812  ZL-810-0402-3 813 BULK CARGO COMPARTMENT DOOR MEC GVI I: 1 C CPCP MRB REFERENC MRB Z ZL-810  GENERAL VISUAL INSPECTION OF ZONE INCLUDING: 523401-C602- - SEALS,  - OPERATING MECHANISM,  - STRUCTURE.  * * * * * C O N T I N U E D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE THRESHOLD (ST)

SAMPLE INTERVAL (SI) 

THRESHOLD (T) 

INTERVAL (I)

 ZL-810-0402-3 * * * * * C O N T I N U E * * * * *  ACCESS: 813  ZL-830-0402-1 830 PAX/CREW DOORS & EMERG.EXIT MEC GVI I: 1 C CPCP MRB REFERENC 840 MRB Z ZL-830  GENERAL VISUAL INSPECTION OF ALL PAX/CREW AND 521101-C602- EMERGENCY EXIT DOORS INCLUDING: 521110-C602- - SEALS, 521210-C602- - DOOR STOPS, 521301-C602- - HOOK ATTACHMENTS, 522201-C602- - STRUCTURE.  (INCLUDING ZONE 840)  ZL-830-0402-2 835 UDC DOOR MEC GVI I: 1 C CPCP MRB REFERENC MRB Z ZL-830  GENERAL VISUAL INSPECTION OF UPPER (MAIN) DECK CARGO 523601-C602- DOOR INCLUDING:  - HOOK FITTINGS,  - SEALS,  - STRUCTURE,  - HYDRAULIC COMPONENTS AND INSTALLATION.  ACCESS: 835  ZL-830-0402-3 830 FWD PAX/CREW DOOR MEC GVI I: 1 C CPCP MRB REFERENC 840 MRB Z ZL-830  GENERAL VISUAL INSPECTION OF FWD PAX/CREW AND 521101-C602- EMERGENCY EXIT DOORS INCLUDING: 521110-C602- - SEALS, 521210-C602- - DOOR STOPS, 521301-C602- - HOOK ATTACHMENTS, 522201-C602- - STRUCTURE.  (INCLUDING ZONE 840)  ZL-830-0403-2 835 UPPER DECK CARGO DOOR MEC GVI I: 5 YE MRB Z MRB REFERENC ZL-830  01. GENERAL VISUAL INSPECTION OF UDC DOOR FOR GENERAL  CONDITION 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: 
TASK NUMBER ZONE DESCRIPTION SOURCE REFERENCE 

A300 MAINTENANCE PLANNING D

SAMPLE 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  835GR  ZL-830-0403-3 830 PAX/CREW DOORS & EMERG.EXIT MEC GVI I: 5 YE CPCP MRB REFERENC 840 MRB Z ZL-830  GENERAL VISUAL INSPECTION OF MID AND AFT PAX/CREW 521101-C602- DOORS AND EMERG. EXIT, INCLUDING: 521110-C602- - SEALS 521210-C602- - DOOR STOPS 521301-C602- - STRUCTURE FOR CONDITION 522201-C602- (INCLUDING ZONE 840)  PREP.: DOORS REMOVED  * * * * * E N D * * * * *  ZONAL PROGRAM : ZONAL INSPECTIONS REV. DATE: APR 01/10 SECTION: 
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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 

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536513-0606-A 2005/11/18 0027 

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536516-0606-3 2005/11/18 0027 

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536516-0606-7 2005/11/18 0027 

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536577-0606-1 2005/11/18 0027 

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536581-0606-1 2006/10/01 0028 

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536597-0606-D 2005/11/18 0027 

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536598-0606-4 1997/04/15 0021 

536598-0606-7 2006/10/01 0028 

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536598-0606-9 2006/10/01 0028 

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536603-0606-3 2006/10/01 0028 

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536651-0606-1 1997/04/15 0021 

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536651-0606-9 2006/10/01 0028 

536652-0606-1 1997/04/15 0021 

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536702-0606-B 1999/04/23 0024 

536702-0606-C 2005/11/18 0027 
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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 

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536901-0606-G 2005/11/18 0027 

536901-0606-H 2005/11/18 0027 

536901-0606-I 2005/11/18 0027 

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536901-0606-4 2006/10/01 0028 

536901-0606-6 2006/10/01 0028 

536901-0606-7 2006/10/01 0028 

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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 
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538241-0607-1 1993/01/30 0016 

538255-0608-1 1997/04/15 0021 

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538305-0608-1 1997/04/15 0021 

538315-0608-1 1993/01/30 0016 

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538547-0607-1 1993/01/30 0016 

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538561-0608-1 1997/04/15 0021 

538563-0603-1 2005/11/18 0027 

538585-0608-1 1997/04/15 0021 

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538595-0603-1 2002/08/30 0026 

538597-0608-1 1997/04/15 0021 

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538671-0603-1 2002/08/30 0026 
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538759-0608-1 1997/04/15 0021 

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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 

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540011-0604-1 1997/04/15 0021 

541000-0502-2 2002/08/30 0026 

541003-0603-1 1997/04/15 0021 

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548022-0608-1 1993/01/30 0016 

551005-0603-1 1997/04/15 0021 

551007-0603-1 1997/04/15 0021 

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552003-0603-1 1997/04/15 0021 

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555005-0603-1 1997/04/15 0021 

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555009-0604-1 1995/10/30 0019 

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555013-0604-1 1995/10/30 0019 

555015-0603-1 1997/04/15 0021 

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555017-0604-1 1997/04/15 0021 

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555023-0603-1 2009/10/01 0029 

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556002-0606-6 2009/10/01 0029 

558001-0608-1 1997/04/15 0021 

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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 

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571046-0603-2 1993/10/30 0017 

571047-0603-1 1993/01/30 0016 

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571072-0603-2 1997/04/15 0021 

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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 

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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 

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573600-0502-2 1999/04/23 0024 

575021-0604-2 2006/10/01 0028 

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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 

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576002-0606-5 1997/11/18 0022 

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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 
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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 REPERCUSSIONS 

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 

 
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 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 
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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 
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 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 
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 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 
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 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 
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 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

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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 

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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 

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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

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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 
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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 

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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 

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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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 3

RE

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 MAINTENANCE 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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 12

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 13

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 14

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 15

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 16

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 17

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 18

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 19

RE

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 20

RE

V. 

MPD REF. DESIGNAT

ION 

MANUFACT

URER / 

VENDOR 

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 21

RE

V. 

MPD REF. DESIGNAT

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 22

RE

V. 

MPD REF. DESIGNAT

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 

 ISSUE:APR 01/10 APPENDIX 3 — VENDOR RECOMMENDATIONS Page 23

RE

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 

 ISSUE:APR 01/10 APPENDIX 5 — FORMER VOLUME 2 AND 3 CONTENT Page 3

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 manufacturing. 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. 
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(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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'-' : temporary corrosion protection application may be applied at the discretion of the 

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 ()