@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - NOSE SECTION - INSPECT THE FWD PAX/CREW DOOR

SURROUNDING SKIN PANELS.

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A300-53-6173

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to update the inspection requirements.

CHANGES

The main changes of this revision are:

- Update the flowcharts and accomplishment Timescale Table

- Update the inspection paragraph

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

CONF 002 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

REASON

Objective/Action OBJECTIVE/ACTION UPDATED R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED

CONFIGURATION UPDATED

R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED

CONFIGURATION UPDATED

R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MATERIAL INFORMATION

TOOLING

Tooling - Price and Availability TOOLING - PRICE AND AVAILABILITY UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 536173- 832-801-001-Inspection of

FWD passenger/crew door surrounding

skin panels

TASK SOLUTION UPDATED

TASK TITLE UPDATED

CAUTION UPDATED

R

Subtask 536173-832-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 536173-832-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 536173-832-001-002 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 536173-832-002-002 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Fig. A-FCAAA FIGURE SOLUTION ADDED N

Fig. A-FCAAA Sheet 01 SHEET ADDED N

Fig. A-FCAAB FIGURE SOLUTION ADDED N

Fig. A-FCAAB Sheet 01 SHEET ADDED N

Fig. A-FDAAA FIGURE SOLUTION ADDED N

Fig. A-FDAAA Sheet 01 SHEET ADDED N

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-FFAAA FIGURE SOLUTION UPDATED R

Fig. A-FFAAA Sheet 01 SHEET UPDATED R

Fig. A-FFAAA Sheet 02 SHEET ADDED N

Fig. A-FFAAB FIGURE SOLUTION UPDATED R

Fig. A-FFAAB Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Aug 01/13

REVISION No. : 01 - Feb 28/14

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - NOSE SECTION - INSPECT THE FWD PAX/CREW DOOR

SURROUNDING SKIN PANELS.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

In the frame of AASR (Aging Airplane Safety Rule), new Fatigue and Damage Tolerance (FDT) studies

were launched.

This Inspection Service Bulletin (ISB) requires to perform a one-time detailed inspection of the area

surrounding the forward passenger/crew door and the fail safe ring. The operators will have to report

the observed rework values to Airbus, via the Inspection Report Sheet of this Service Bulletin.

The reporting to Airbus has to be done only for those aircraft on which rework values exceed the new

authorized values (given in the Structural Repair Manual (SRM) 53-12-00 and 53-12-81 chapters).

The inspection reports collected will ensure the monitoring of impacted aircraft and will give appropriate

actions to affected operators for maintaining the continued airworthiness of their aircraft.

This Service Bulletin supersedes and replaces Inspection Service Bulletin A300-53-6126 (FUSELAGENOSE SECTION-INSPECT THE FWD PAX/CREW DOOR SURROUNDING SKIN PANELS).

None

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB YES

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

This Service Bulletin is applicable to this (these) operator(s) :

67Q ABD ABR BCS CES F2I FDX GBG I2L IRA IRM KAC MGC

MNB MON MSR MXU SUD TAR THA URS UZB

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 536173-832-801-001: Inspection of FWD passenger/crew door surrounding skin panels

TOTAL MANHOURS 120.00

ELAPSED TIME (HOURS) 30.00

**CONF 002

Task 536173-832-801-001: Inspection of FWD passenger/crew door surrounding skin panels

TOTAL MANHOURS 120.00

ELAPSED TIME (HOURS) 30.00

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

APPENDICES

**CONF ALL

Appendix 01 : Elapsed Time Assumption

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

**CONF ALL

A

FR13

FR18

STGR9

A

Z220

STGR30

AREA TO BE INSPECTED (BOTH SIDES OF AIRCRAFT)

D_SB_536173_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - NOSE SECTION - INSPECT THE FWD PAX/CREW DOOR

SURROUNDING SKIN PANELS.

MODIFICATION No.: None

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/F C4-620 F4-605R

(2) Effectivity by MSN

0294 0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0477 0479

0505 0521 0525 0529-0530 0532 0536 0543 0546 0553 0555 0557-0559 0561 0563

0572 0575 0577 0579 0581 0584 0602-0605 0607-0608 0611 0613 0617-0618 0621

0623 0625-0626 0629-0630 0632-0633 0637 0641 0643 0657 0659 0664 0666 0668

0670 0673 0677 0679 0681 0683 0688 0694 0696 0699 0701 0703 0705 0707 0709

0711 0713 0715 0717 0719 0721-0730 0732-0746 0748-0750 0752-0764 0766-0775

0777-0794 0797 0799-0804 0836-0838

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

OPERATOR MSN

67Q 0584 0603 0744 0749 0764

ABD 0557

ABR 0683 0770

BCS 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730

0737 0740 0753 0783 0797 0836 0837

CES 0707 0725 0732 0741 0746 0754 0763

F2I 0294 0529

FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559

0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664

0668 0688 0709 0713 0715 0726 0728 0735 0736 0738 0742 0745

0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774

0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799

0800 0801 0802 0803 0804

GBG 0626 0643

I2L 0677

IRA 0632 0696 0723 0727

IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701

0750 0762 0773 0838

KAC 0344 0673 0694 0699 0719 0721

MGC 0743

MNB 0521 0525 0532 0734 0739 0755 0756 0758

MON 0604 0605

MSR 0561 0607

MXU 0767 0788

SUD 0666 0775

TAR 0505 0558 0563

THA 0577 0629 0681 0705 0782 0784 0785 0786 0787

URS 0733

UZB 0717 0722

(4) Configuration by MSN

MSN CONFIGURATION

0294 0344 0358 0361 0365 0380 0388 0401 0405 0408 0411

0414 0417 0477 0479 0505 0521 0525 0529 0530 0532 0536

0543 0546 0553 0555 0557 0558 0559 0561 0563 0572 0575

0577 0579 0581 0584 0602 0603 0604 0605 0607 0608 0611

0613 0617 0618 0621 0623 0625 0626 0629 0630 0632 0633

0637 0641 0643 0657 0659 0664 0666 0668 0670 0673 0677

0679 0681 0683 0688 0694 0696 0699 0701 0703 0705 0707

0709 0711 0713 0715 0717 0719 0721 0722 0723 0724 0725

0727 0729 0730 0732 0733 0734 0737 0739 0740 0741 0743

0744 0746 0749 0750 0753 0754 0755 0756 0758 0762 0763

0764 0767 0770 0773 0775 0782 0783 0784 0785 0786 0787

0788 0797 0836 0837 0838

001

0726 0728 0735 0736 0738 0742 0745 0748 0752 0757 0759

0760 0761 0766 0768 0769 0771 0772 0774 0777 0778 0779

0780 0781 0789 0790 0791 0792 0793 0794 0799 0800 0801

0802 0803 0804

002

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for passenger aircraft.

**CONF 002

Config. 002 is valid for freighter aircraft model F4-605R on which Mod No. 12699S22372

is not embodied.

(6) Material Effectivity

No Material Set

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

In the frame of AASR (Aging Airplane Safety Rule), new Fatigue and Damage Tolerance

(FDT) studies were launched.

(2) Objective/Action

This Inspection Service Bulletin (ISB) requires to perform a one-time detailed inspection

of the area surrounding the forward passenger/crew door and the fail safe ring. The

operators will have to report the observed rework values to Airbus, via the Inspection

Report Sheet of this Service Bulletin.

The reporting to Airbus has to be done only for those aircraft on which rework values

exceed the new authorized values (given in the Structural Repair Manual (SRM)

53-12-00 and 53-12-81 chapters).

(3) Advantages

The inspection reports collected will ensure the monitoring of impacted aircraft and will

give appropriate actions to affected operators for maintaining the continued airworthiness

of their aircraft.

This Service Bulletin supersedes and replaces Inspection Service Bulletin

A300-53-6126 (FUSELAGE-NOSE SECTION-INSPECT THE FWD PAX/CREW DOOR

SURROUNDING SKIN PANELS).

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

Task 536173-832-801-001: Inspection of FWD passenger/crew door surrounding skin panels

(1) Inspect the FWD Passenger/Crew Door surrounding skin panels at LH Side

(2) Inspect the FWD Passenger/Crew Door surrounding skin panels at RH Side

**CONF 002

Task 536173-832-801-001: Inspection of FWD passenger/crew door surrounding skin panels

(1) Inspect the FWD Passenger/Crew Door surrounding skin panels at LH Side

(2) Inspect the FWD Passenger/Crew Door surrounding skin panels at RH Side

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the (thresholds

and/or intervals and/or date) given below but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

Table 1, Config 001 - Do a check of the aircraft status

Condition Action Compliance Time

(whichever occurs

later)

Repetitive interval

All aircraft Do a check of the aircraft status

regarding SB No. A300-53-6126

embodiment, refer to TASK

536173-832-801 001 Inspection of FWD

passenger/crew door surrounding skin

panels

36 months from SB

No. A300-53-6173

REV00 issuance

date

or

Aircraft DSG

(whichever value in

FC or FH reached

first)

None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Table 1, Config 001 - Do a check of the aircraft status

Condition Action Compliance Time

(whichever occurs

later)

Repetitive interval

SB

No.A300-53-6126

is not

accomplished

Do SUBTASK

536173-832-001

001 Inspect the

FWD

Passenger/Crew

Door surrounding

skin panels at LH

Side and

SUBTASK

536173-832-002

001 Inspect the

FWD

Passenger/Crew

Door surrounding

skin panels at RH

Side

Refer to Table 2

SB

No.A300-53-6126

is accomplished

and area described

in Fig. A-FCAAA

was repaired

before A300-600

SRM 53-12-81-101

June 2001 revision

Do SUBTASK

536173-832-001

001 Inspect the

FWD

Passenger/Crew

Door surrounding

skin panels at LH

Side and

SUBTASK

536173-832-002

001 Inspect the

FWD

Passenger/Crew

Door surrounding

skin panels at RH

Side

Refer to Table 2

Update Maintenance Program to be in

accordance with Structural Repair

Inspection (SRI) requirements: SRM

53-12-12-101 Figure 108 (sheet 9) for

skin panel and SRM 53-12-81-101

Figure 101 (sheet 2) for Fail Safe Ring,

refer to SUBTASK 536173-832-001 001

Inspect the FWD Passenger/Crew Door

surrounding skin panels at LH Side

and refer to SUBTASK 536173-832-002

001 Inspect the FWD Passenger/Crew

Door surrounding skin panels at RH

Side

SB Before Next Flight None

No.A300-53-6126

is accomplished

and area described

in Fig. A-FCAAA

was not repaired

before A300-600

SRM 53-12-81-101

June 2001 revision

No further action None None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 5

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Table 2, Config 001 - One time detailed inspection of existing rework on the FWD passenger/crew

door surrounding panels.

Condition Action Compliance Time

(whichever occurs later)

Repetitive interval

Aircraft with SB No

A300-53-6126 not

accomplished

Do TASK

536173-832-801 001

Inspection of FWD

passenger/crew door

surrounding skin panels

(See Note(*))

Before Next Flight None

SB No.A300-53-6126

accomplished and area

described in Fig. AFCAAA repaired before

A300-600 SRM

53-12-81-101 June 2001

revision

Do TASK

536173-832-801 001

Inspection of FWD

passenger/crew door

surrounding skin panels

only in areas described

in Fig. A-FCAAA

Before Next Flight None

No rework found No further action. None None

Rework found Identify the rework area,

the percentage of

rework and the rework

limits, refer to

SUBTASK

536173-832-001 001

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at LH Side and

SUBTASK

536173-832-002 001

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at RH Side

Before Next Flight None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 6

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Table 2, Config 001 - One time detailed inspection of existing rework on the FWD passenger/crew

door surrounding panels.

Condition Action Compliance Time

(whichever occurs later)

Repetitive interval

Update Maintenance

Program to be in

accordance with SRI

requirements: SRM

53-12-12-101 Figure

108 (sheet 9) for skin

panel and SRM

53-12-81-101 Figure

101 (sheet 2) for Fail

Safe Ring, refer to

SUBTASK

536173-832-001 001

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at LH Side and refer to

SUBTASK

536173-832-002 001

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at RH Side

No rework found out of Before Next Flight None

SRM permanent limits

No further action. None None

Rework found out of

SRM permanent limits

Send damage report to

AIRBUS structure repair

support.

Before next flight None

NOTE (*): - All areas covered by a RDAS (issued since aircraft first flight),

or repaired in accordance with A300-600 SRM 53-12-12/81 from

Dec-2008 revision and subsequent, do not have to be inspected as

per this SB.

- For all areas repaired in accordance with A300-600 SRM

53-12-12/81 from Jun-2001 and before Dec-2008 revision:

. Maintenance program to be updated to be in accordance with

SRI requirements:

- Skin panel: SRM 53-12-12-101 Figure 108 (sheet 9)

- Fail Safe Ring: SRM 53-12-81-101 Figure 101 (sheet 2)

. No further action

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 7

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the (thresholds

and/or intervals and/or date) given below but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

Table 1, Config 002 - One time detailed inspection of existing rework on the FWD passenger/crew

door surrounding panels.

Condition Action Compliance Time

(whichever occurs later)

Repetitive interval

All aircraft Do TASK

536173-832-801 001

Inspection of FWD

passenger/crew door

surrounding skin panels

(See Note(**))

36 months from SB No.

A300-53-6173 REV00

issuance date

or

Aircraft DSG (whichever

value in FC or FH

reached first)

None

No rework found No further action. None None

Rework found Identify the rework area,

the percentage of

rework and the rework

limits, refer to

SUBTASK

536173-832-001 002

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at LH Side and

SUBTASK

536173-832-002 002

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at RH Side

Before Next Flight None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 8

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Table 1, Config 002 - One time detailed inspection of existing rework on the FWD passenger/crew

door surrounding panels.

Condition Action Compliance Time

(whichever occurs later)

Repetitive interval

Update Maintenance

Program to be in

accordance with SRI

requirements: SRM

53-12-12-101 Figure

107 (sheet 6-10) for skin

panel and SRM

53-12-81-101-C2 Figure

102 for Fail Safe Ring,

refer to SUBTASK

536173-832-001 002

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at LH Side and refer to

SUBTASK

536173-832-002 002

Inspect the FWD

Passenger/Crew Door

surrounding skin panels

at RH Side

No rework found out of Before Next Flight None

SRM permanent limits

No further action. None None

Rework found out of

SRM permanent limits

Send damage report to

AIRBUS structure repair

support.

Before next flight None

NOTE (**): - All areas covered by a RDAS (issued since aircraft first flight), or

repaired in accordance with A300-600F SRM 53-12-12/81 from

Dec-2009 revision and subsequent, do not have to be inspected as

per this SB.

- For all areas repaired in accordance with A300-600F SRM

53-12-12/81 from Dec-2002 and before Dec-2009 revision, with the

exception of areas described in Fig. A-FCAAB and A-FDAAA:

. Maintenance program to be updated to be in accordance with

SRI requirements:

- Skin panel: A300-600F SRM 53-12-12-101-C2 Figure 107

(sheet 6-10)

- Fail Safe Ring: A300-600F SRM 53-12-81-101-C2 Figure 102

. No further action

- Excluded areas defined in Fig. A-FCAAB and A-FDAAA:

. Detailed inspection is required as per this SB

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 9

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organization Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

For an explanation of the manhours and elapsed time, refer to the Gantt Chart given in

Appendix 01.

**CONF 001

Task 536173-832-801-001: Inspection of FWD passenger/crew door surrounding skin panels

Get Access 8.00

On Aircraft

Inspect the FWD Passenger/Crew Door surrounding

skin panels at LH Side

8.00

Inspect the FWD Passenger/Crew Door surrounding

skin panels at RH Side

8.00

Close-Up 96.00

TOTAL MANHOURS 120.00

ELAPSED TIME (HOURS) 30.00

NOTE: The scuff plate installation time is 48.00 hours (for one side of the aircraft) if

the ambient temperature is 18 Degree Celsius (64.5 Fahreinheit) but can be

reduced to 30.00 hours if the ambient temperature is 20 Degree Celsius

(68 Fahreinheit) or to 24.00 hours if the ambient temperature is 23 Degree

Celsius (73.5 Fahreinheit).

**CONF 002

Task 536173-832-801-001: Inspection of FWD passenger/crew door surrounding skin panels

Get Access 8.00

On Aircraft

Inspect the FWD Passenger/Crew Door surrounding

skin panels at LH Side

8.00

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 10

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task 536173-832-801-001: Inspection of FWD passenger/crew door surrounding skin panels

Inspect the FWD Passenger/Crew Door surrounding

skin panels at RH Side

8.00

Close-Up 96.00

TOTAL MANHOURS 120.00

ELAPSED TIME (HOURS) 30.00

NOTE: The scuff plate installation time is 48.00 hours (for one side of the aircraft) if

the ambient temperature is 18 Degree Celsius (64.5 Fahreinheit) but can be

reduced to 30.00 hours if the ambient temperature is 20 Degree Celsius

(68 Fahreinheit) or to 24.00 hours if the ambient temperature is 23 Degree

Celsius (73.5 Fahreinheit).

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-21-00 24-00-00

25-23-41 52-11-11 53-10-18

Elec. Std. Practices Manual (ESPM) 20-55-00

Illustrated Parts Catalog (IPC) 53-12-22

Non Destructive Test Manual (NTM) 51-10-04

Service Bulletin (SB) A300-53-6126

Structural Repair Manual (SRM) 53-12-12 53-12-81

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-21-00 24-00-00

25-23-41 52-11-11 53-10-18

Elec. Std. Practices Manual (ESPM) 20-55-00

Illustrated Parts Catalog (IPC) 53-12-22

Non Destructive Test Manual (NTM) 51-10-04

Service Bulletin (SB) A300-53-6126

Structural Repair Manual (SRM) 53-12-12 53-12-81

**CONF ALL

K. PUBLICATION AFFECTED

None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 11

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 12

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

None

(2) Price and Availability

None

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Refer to AMM 53-10-18 and IPC 53-12-22.

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

To accomplish this Service Bulletin it is necessary to use the tools listed in the

subsequent referenced AMM tasks:

AMM 53-10-18, Page Block 401

(2) Tools

None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 13

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(3) Special Tools

None

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 14

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 536173-832-801-001 - Inspection of FWD passenger/crew door surrounding skin panels

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 15

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

830 840

Access

Door 831 841

Manpower

TOTAL MANHOURS 120.00

ELAPSED TIME (HOURS) 30.00

**CONF 002

Zone

830 840

Access

Door 831 841

Manpower

TOTAL MANHOURS 120.00

ELAPSED TIME (HOURS) 30.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 536173-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

(a) For identification of zones, refer to AMM 06-20-00, Page Block 001.

(2) Subtask 536173-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

(a) Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 16

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

(1) Subtask 536173-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

(a) For identification of zones, refer to AMM 06-20-00, Page Block 001.

(2) Subtask 536173-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

(a) Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 536173-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

24-00-00, Page Block 301

25-23-41, Page Block 401

52-11-11, Page Block 401

53-10-18, Page Block 401

(a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page

Block 301.

(b) Put access platform(s) in position.

(c) Open the FWD passenger/crew doors Z831 and Z841, refer to AMM 06-21-00,

Page Block 001 and AMM 52-11-11, Page Block 401.

(d) Remove the scuff plates, refer to AMM 53-10-18, Page Block 401.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 17

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

(1) Subtask 536173-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

24-00-00, Page Block 301

25-23-41, Page Block 401

52-11-11, Page Block 401

53-10-18, Page Block 401

(a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page

Block 301.

(b) Put access platform(s) in position.

(c) Open the FWD passenger/crew doors Z831 and Z841, refer to AMM 06-21-00,

Page Block 001 and AMM 52-11-11, Page Block 401.

(d) Remove the scuff plates, refer to AMM 53-10-18, Page Block 401.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 536173-832-001-001 - Inspect the FWD Passenger/Crew Door surrounding

skin panels at LH Side

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Non Destructive Test Manual (NTM) 51-10-04

Structural Repair Manual (SRM) 53-12-12

53-12-81

Fig. A-FBAAA

Areas to be inspected.

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 18

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

References

Fig. A-FRAAA

Inspection Report

Sheet 01

Sheet 02

Fig. A-FCAAA

Areas to be concerned.

Sheet 01

(a) At the threshold given in the PLANNING INFORMATION paragraph E.(2):

1 Do a check of the aircraft status regarding SB No. A300-53-6126 embodiment.

Refer to Fig. A-FBAAA Sheet 01

Refer to Fig. A-FFAAA Sheet 01

a If SB No.A300-53-6126 is not accomplished:

<1> Do a detailed inspection of the passenger/crew door surrounding

skin panels to evaluate the existing rework.

NOTE: - All areas covered by a RDAS (issued since

aircraft first flight), or repaired in accordance

with A300-600 SRM 53-12-12/81 from Dec-2008

revision and subsequent, do not have to be

inspected as per this SB.

- For all areas repaired in accordance with

A300-600 SRM 53-12-12/81 from Jun-2001 and

before Dec-2008 revision:

. Maintenance program to be updated to be

in accordance with SRI requirements:

- Skin panel: SRM 53-12-12-101 Figure 108

(sheet 9)

- Fail Safe Ring: SRM 53-12-81-101 Figure

101 (sheet 2)

. No further action

<a> If no rework is found:

[1] No further action.

<b> If rework is found:

[1] Identify the rework area:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

1 to 5 for zone identification for skin panels,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for zone identification for fail Safe Ring.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 19

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

[2] Determine the percentage of rework:

- in accordance with NTM 51-10-04 (ultrasonic

inspection) for remaining thickness measurement.

- in accordance with SRM 53-12-12-001 Fig. 1 sheet 6

for thickness panel,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for fail safe ring thickness data.

[3] Determine the rework limit of skin panel and fail safe ring:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

6 to 8 for skin panels,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

2 for fail safe ring.

[4] If rework is not out of SRM permanent limits:

[a] Update Maintenance Program to be in accordance

with SRI (Structural Repair Inspection) requirements,

in accordance with SRM 53-12-12-101 Figure 108

(sheet 9) for skin panel and SRM 53-12-81-101

Figure 101 (sheet 2) for Fail Safe Ring.

and

No further action.

[5] If rework is out of SRM permanent limits:

[a] Send the Inspection Report to AIRBUS structure

repair support before next flight, refer to Fig. AFRAAA Sheet 01 and Fig. A-FRAAA Sheet 02.

[b] Send the Damage Report to AIRBUS structure repair

support for damage assessment before next flight.

b If SB No.A300-53-6126 is accomplished and areas described in Fig. AFCAAA Sheet 01 was repaired before A300-600 SRM 53-12-81-101 June

2001 revision:

<1> Do a detailed inspection of the passenger/crew door surrounding

skin panels to evaluate the existing rework only in areas described

in Fig. A-FCAAA Sheet 01.

<a> If no rework is found:

[1] No further action.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 20

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

<b> If rework is found:

[1] Identify the rework area:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

1 to 5 for zone identification for skin panels,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for zone identification for fail Safe Ring.

[2] Determine the percentage of rework:

- in accordance with NTM 51-10-04 (ultrasonic

inspection) for remaining thickness measurement.

- in accordance with SRM 53-12-12-001 Fig. 1 sheet 6

for thickness panel,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for fail safe ring thickness data.

[3] Determine the rework limit of skin panel and fail safe ring:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

6 to 8 for skin panels,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

2 for fail safe ring.

[4] If rework is not out of SRM permanent limits:

[a] Update Maintenance Program to be in accordance

with SRI (Structural Repair Inspection) requirements,

in accordance with SRM 53-12-12-101 Figure 108

(sheet 9) for skin panel and SRM 53-12-81-101

Figure 101 (sheet 2) for Fail Safe Ring.

and

No further action.

[5] If rework is out of SRM permanent limits:

[a] Send the Inspection Report to AIRBUS structure

repair support before next flight, refer to Fig. AFRAAA Sheet 01 and Fig. A-FRAAA Sheet 02.

[b] Send the Damage Report to AIRBUS structure repair

support for damage assessment before next flight.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 21

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

c If SB No.A300-53-6126 is accomplished and area described in Fig. AFCAAA Sheet 01 was not repaired before A300-600 SRM 53-12-81-101

June 2001 revision:

<1> Update Maintenance Program to be in accordance with SRI

(Structural Repair Inspection) requirements, in accordance with SRM

53-12-12-101 Figure 108 (sheet 9) for skin panel and SRM

53-12-81-101 Figure 101 (sheet 2) for Fail Safe Ring.

and

No further action.

(2) Subtask 536173-832-002-001 - Inspect the FWD Passenger/Crew Door surrounding

skin panels at RH Side

Work Zones and Access Panels

Zone Access/Work location

840 Access Door 841

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Non Destructive Test Manual (NTM) 51-10-04

Structural Repair Manual (SRM) 53-12-12

53-12-81

Fig. A-FBAAA

Areas to be inspected.

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Fig. A-FRAAA

Inspection Report

Sheet 01

Sheet 02

Fig. A-FCAAA

Areas to be concerned.

Sheet 01

(a) At the threshold given in the PLANNING INFORMATION paragraph E.(2):

1 Do a check of the aircraft status regarding SB No. A300-53-6126 embodiment.

Refer to Fig. A-FBAAA Sheet 01

Refer to Fig. A-FFAAA Sheet 01

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 22

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

a If SB No.A300-53-6126 is not accomplished:

<1> Do a detailed inspection of the passenger/crew door surrounding

skin panels to evaluate the existing rework.

NOTE: - All areas covered by a RDAS (issued since

aircraft first flight), or repaired in accordance

with A300-600 SRM 53-12-12/81 from Dec-2008

revision and subsequent, do not have to be

inspected as per this SB.

- For all areas repaired in accordance with

A300-600 SRM 53-12-12/81 from Jun-2001 and

before Dec-2008 revision:

. Maintenance program to be updated to be

in accordance with SRI requirements:

- Skin panel: SRM 53-12-12-101 Figure 108

(sheet 9)

- Fail Safe Ring: SRM 53-12-81-101 Figure

101 (sheet 2)

. No further action

<a> If no rework is found:

[1] No further action.

<b> If rework is found:

[1] Identify the rework area:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

1 to 5 for zone identification for skin panels,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for zone identification for fail Safe Ring.

[2] Determine the percentage of rework:

- in accordance with NTM 51-10-04 (ultrasonic

inspection) for remaining thickness measurement.

- in accordance with SRM 53-12-12-001 Fig. 1 sheet 6

for thickness panel,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for fail safe ring thickness data.

[3] Determine the rework limit of skin panel and fail safe ring:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

6 to 8 for skin panels,

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 23

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

2 for fail safe ring.

[4] If rework is not out of SRM permanent limits:

[a] Update Maintenance Program to be in accordance

with SRI (Structural Repair Inspection) requirements,

in accordance with SRM 53-12-12-101 Figure 108

(sheet 9) for skin panel and SRM 53-12-81-101

Figure 101 (sheet 2) for Fail Safe Ring.

and

No further action.

[5] If rework is out of SRM permanent limits:

[a] Send the Inspection Report to AIRBUS structure

repair support before next flight, refer to Fig. AFRAAA Sheet 01 and Fig. A-FRAAA Sheet 02.

[b] Send the Damage Report to AIRBUS structure repair

support for damage assessment before next flight.

b If SB No.A300-53-6126 is accomplished and area described in Fig. AFCAAA Sheet 01 was repaired before A300-600 SRM 53-12-81-101 June

2001 revision:

<1> Do a detailed inspection of the passenger/crew door surrounding

skin panels to evaluate the existing rework only in areas described

in Fig. A-FCAAA Sheet 01.

<a> If no rework is found:

[1] No further action.

<b> If rework is found:

[1] Identify the rework area:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

1 to 5 for zone identification for skin panels,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for zone identification for fail Safe Ring.

[2] Determine the percentage of rework:

- in accordance with NTM 51-10-04 (ultrasonic

inspection) for remaining thickness measurement.

- in accordance with SRM 53-12-12-001 Fig. 1 sheet 6

for thickness panel,

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 24

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

1 for fail safe ring thickness data.

[3] Determine the rework limit of skin panel and fail safe ring:

- in accordance with SRM 53-12-12-101 Fig. 108 sheet

6 to 8 for skin panels,

- in accordance with SRM 53-12-81-101 Fig. 101 sheet

2 for fail safe ring.

[4] If rework is not out of SRM permanent limits:

[a] Update Maintenance Program to be in accordance

with SRI (Structural Repair Inspection) requirements,

in accordance with SRM 53-12-12-101 Figure 108

(sheet 9) for skin panel and SRM 53-12-81-101

Figure 101 (sheet 2) for Fail Safe Ring.

and

No further action.

[5] If rework is out of SRM permanent limits:

[a] Send the Inspection Report to AIRBUS structure

repair support before next flight, refer to Fig. AFRAAA Sheet 01 and Fig. A-FRAAA Sheet 02.

[b] Send the Damage Report to AIRBUS structure repair

support for damage assessment before next flight.

c If SB No.A300-53-6126 is accomplished and area described in Fig. AFCAAA Sheet 01 was not repaired before A300-600 SRM 53-12-81-101

June 2001 revision:

<1> Update Maintenance Program to be in accordance with SRI

(Structural Repair Inspection) requirements, in accordance with SRM

53-12-12-101 Figure 108 (sheet 9) for skin panel and SRM

53-12-81-101 Figure 101 (sheet 2) for Fail Safe Ring.

and

No further action.

**CONF 002

(1) Subtask 536173-832-001-002 - Inspect the FWD Passenger/Crew Door surrounding

skin panels at LH Side

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 25

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Non Destructive Test Manual (NTM) 51-10-04

Structural Repair Manual (SRM) 53-12-12

53-12-81

Fig. A-FFAAB

Flow Chart

Sheet 01

Fig. A-FRAAB

Inspection Report

Sheet 01

Sheet 02

Fig. A-FBAAA

Areas to be inspected.

Sheet 01

Fig. A-FCAAB

Areas to be concerned.

Sheet 01

Fig. A-FDAAA

Areas to be concerned.

Sheet 01

(a) At the threshold given in the PLANNING INFORMATION paragraph E.(2):

1 Do a detailed inspection of the passenger/crew door surrounding skin panels

to evaluate the existing rework.

Refer to Fig. A-FBAAA Sheet 01

Refer to Fig. A-FFAAB Sheet 01

NOTE: - All areas covered by a RDAS (issued since aircraft first

flight), or repaired in accordance with A300-600F SRM

53-12-12/81 from Dec-2009 revision and subsequent, do

not have to be inspected as per this SB.

- For all areas repaired in accordance with A300-600F SRM

53-12-12/81 from Dec-2002 and before Dec-2009 revision,

with the exception of areas defined in Fig. A-FCAAB

Sheet 01 and Fig. A-FDAAA Sheet 01:

. Maintenance program to be updated to be in

accordance with SRI requirements:

- Skin panel: A300-600F SRM 53-12-12-101-C2

Figure 107 (sheet 6-10)

- Fail Safe Ring: A300-600F SRM 53-12-81-101-C2

Figure 102

. No further action

- Excluded areas defined in Fig. A-FCAAB Sheet 01 and

Fig. A-FDAAA Sheet 01:

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 26

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

. Detailed inspection is required as per this SB

a If no rework is found:

<1> No further action.

b If rework is found:

<1> Identify the rework area:

- in accordance with SRM 53-12-12-101-C2 Fig. 107 sheet 1 to 5

for skin panels,

- in accordance with SRM 53-12-81-101-C2 Fig. 102 for fail Safe

Ring.

<2> Determine the percentage of rework:

- in accordance with NTM 51-10-04 (ultrasonic inspection) for

remaining thickness measurement.

- in accordance with SRM 53-12-12-001-C2 Fig. 5 sheet 1&2 for

thickness panels,

- in accordance with SRM 53-12-81-101-C2 Fig. 102 for fail safe

ring thickness data.

<3> Determine the rework limit of skin panel and fail safe ring:

- in accordance with SRM 53-12-12-101-C2 Fig. 107 sheet 6 to

10 for skin panels,

- in accordance with SRM 53-12-81-101-C2 Fig. 102 for fail safe

ring.

<4> If rework is not out of SRM permanent limits:

<a> Update Maintenance Program to be in accordance with SRI

(Structural Repair Inspection) requirements, in accordance with

SRM 53-12-12-101-C2 Fig 107 sheet 6 to 10 for skin panel and

SRM 53-12-81-101-C2 Fig 102 for Fail Safe Ring.

and

No further action.

<5> If rework is out of SRM permanent limits:

<a> Send the Inspection Report to AIRBUS structure repair support

before next flight, refer to Fig. A-FRAAB Sheet 01 and Fig. AFRAAB Sheet 02.

<b> Send the Damage Report to AIRBUS structure repair support

for damage assessment before next flight.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 27

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(2) Subtask 536173-832-002-002 - Inspect the FWD Passenger/Crew Door surrounding

skin panels at RH Side

Work Zones and Access Panels

Zone Access/Work location

840 Access Door 841

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Non Destructive Test Manual (NTM) 51-10-04

Structural Repair Manual (SRM) 53-12-12

53-12-81

Fig. A-FBAAA

Areas to be inspected.

Sheet 01

Fig. A-FFAAB

Flow Chart

Sheet 01

Fig. A-FRAAB

Inspection Report

Sheet 01

Sheet 02

Fig. A-FCAAB

Areas to be concerned.

Sheet 01

Fig. A-FDAAA

Areas to be concerned.

Sheet 01

(a) At the threshold given in the PLANNING INFORMATION paragraph E.(2):

1 Do a detailed inspection of the passenger/crew door surrounding skin panels

to evaluate the existing rework.

Refer to Fig. A-FBAAA Sheet 01

Refer to Fig. A-FFAAB Sheet 01

NOTE: - All areas covered by a RDAS (issued since aircraft first

flight), or repaired in accordance with A300-600F SRM

53-12-12/81 from Dec-2009 revision and subsequent, do

not have to be inspected as per this SB.

- For all areas repaired in accordance with A300-600F SRM

53-12-12/81 from Dec-2002 and before Dec-2009 revision,

with the exception of areas defined in Fig. A-FCAAB

Sheet 01 and Fig. A-FDAAA Sheet 01:

. Maintenance program to be updated to be in

accordance with SRI requirements:

- Skin panel: A300-600F SRM 53-12-12-101-C2

Figure 107 (sheet 6-10)

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 28

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

- Fail Safe Ring: A300-600F SRM 53-12-81-101-C2

Figure 102

. No further action

- Excluded areas defined in Fig. A-FCAAB Sheet 01 and

Fig. A-FDAAA Sheet 01:

. Detailed inspection is required as per this SB

- Excluded areas defined in SRM 53-12-12 Figure 110

(sheet 1 and sheet 2) and SRM 53-12-81 Figure 102

(sheet 2):

. Detailed inspection is required as per this SB

a If no rework is found:

<1> No further action.

b If rework is found:

<1> Identify the rework area:

- in accordance with SRM 53-12-12-101-C2 Fig. 107 sheet 1 to 5

for skin panels,

- in accordance with SRM 53-12-81-101-C2 Fig. 102 for fail Safe

Ring.

<2> Determine the percentage of rework:

- in accordance with NTM 51-10-04 (ultrasonic inspection) for

remaining thickness measurement.

- in accordance with SRM 53-12-12-001-C2 Fig. 5 sheet 1&2 for

thickness panels,

- in accordance with SRM 53-12-81-101-C2 Fig. 102 for fail safe

ring thickness data.

<3> Determine the rework limit of skin panel and fail safe ring:

- in accordance with SRM 53-12-12-101-C2 Fig. 107 sheet 6 to

10 for skin panels,

- in accordance with SRM 53-12-81-101-C2 Fig. 102 for fail safe

ring.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 29

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

<4> If rework is not out of SRM permanent limits:

<a> Update Maintenance Program to be in accordance with SRI

(Structural Repair Inspection) requirements, in accordance with

SRM 53-12-12-101-C2 Fig 107 sheet 6 to 10 for skin panel and

SRM 53-12-81-101-C2 Fig 102 for Fail Safe Ring.

and

No further action.

<5> If rework is out of SRM permanent limits:

<a> Send the Inspection Report to AIRBUS structure repair support

before next flight, refer to Fig. A-FRAAB Sheet 01 and Fig. AFRAAB Sheet 02.

<b> Send the Damage Report to AIRBUS structure repair support

for damage assessment before next flight.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 536173-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

52-11-11, Page Block 401

53-10-18, Page Block 401

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) Install the scuff plates, refer to AMM 53-10-18, Page Block 401.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 30

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(c) Close the FWD passenger/crew doors Z831 and Z841, refer to AMM 06-21-00,

Page Block 001 and AMM 52-11-11, Page Block 401.

(d) Remove the access platforms.

(e) Restore the systems and the aircraft to normal operating condition.

**CONF 002

(1) Subtask 536173-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

52-11-11, Page Block 401

53-10-18, Page Block 401

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) Install the scuff plates, refer to AMM 53-10-18, Page Block 401.

(c) Close the FWD passenger/crew doors Z831 and Z841, refer to AMM 06-21-00,

Page Block 001 and AMM 52-11-11, Page Block 401.

(d) Remove the access platforms.

(e) Restore the systems and the aircraft to normal operating condition.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 31

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

A

FR13

FR18

STGR9

A

Z220

STGR30

AREA TO BE INSPECTED (BOTH SIDES OF AIRCRAFT)

D_SB_536173_5_BAAA_01_02

Figure A-FBAAA - Sheet 01

Areas to be inspected.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 32

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

A

Z220

STGR12LH

STGR26LH

A

FR13

FR18

B

BEAM 6

BEAM 7

BEAM 5

BEAM 2

BEAM 3

BEAM 4

BEAM 1

BEAM 6

BEAM 7

BEAM 8

BEAM 4

BEAM 5

BEAM 3

LH SHOWN

RH SYMMETRICAL

FR14 FR14A FR15 FR15A FR16 FR16A

FR16A

FR15C FR14B FR14C FR14

BEAM 1

BEAM 2

FWD B

01

01

BEAM 8

NOTE:

01 AREAS EXCLUDED SINCE SRM JUNE 2001 REVISION D_SB_536173_5_CAAA_01_02

Figure A-FCAAA - Sheet 01

Areas to be concerned.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 33

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

A

Z220

STGR12LH

STGR26LH

A

FR13

FR18

B

BEAM 6

BEAM 5

BEAM 2

BEAM 3

BEAM 4

BEAM 6

BEAM 4

BEAM 5

BEAM 3

LH SHOWN

RH SYMMETRICAL

FR14 FR14A FR15 FR15A FR16 FR16A

FR16A

FR15C

FR14C FR15B FR14 FR14B

BEAM 2

FWD B

01

BEAM 7

BEAM 8

BEAM 1

BEAM 7

BEAM 8

BEAM 1

NOTE:

01 AREAS WITH NEW ADL SINCE SRM DEC 2009 REVISION D_SB_536173_5_CAAB_01_01

Figure A-FCAAB - Sheet 01

Areas to be concerned.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 34

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

FR18 FR17

FR16A

FR15C FR15B FR14C FR14B FR14 FR13B FR13A FR13

STGR9LH

STGR10LH

STGR11LH

STGR12LH

STGR13LH

STGR14LH

STGR15LH

STGR16LH

STGR17LH

STGR18LH

STGR19LH

STGR20LH

STGR20LH

STGR21LH

STGR22LH

STGR23LH

STGR24LH

STGR25LH

STGR26LH

STGR27LH

STGR28LH

STGR29LH

STGR30LH

FR18 FR13

BEAM8

BEAM7

BEAM6

BEAM5

BEAM8

BEAM7

BEAM6

BEAM5

BEAM4

BEAM3

BEAM2

BEAM1

BEAM4

BEAM3

BEAM2

BEAM1

A

Z220

STGR12LH

STGR26LH

A

FR13

FR18

B

STGR20LH

C

NOTE: FWD FWD

01 AREAS EXCLUDED SINCE DEC 2009 REVISION

01

01

01

01 B C

D_SB_536173_5_DAAA_01_01

Figure A-FDAAA - Sheet 01

Areas to be concerned.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 35

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

DO A CHECK OF THE AIRCRAFT STATUS REGARDING SB No

A300−53−6126 EMBODIMENT AT THE THRESHOLD GIVEN IN

THE PLANNING INFORMATION PARAGRAPH E.(2)

SEE FIGURE A−FFAAA

SHEET 02

JUNE 2001

NO

NO FURTHER ACTION

REVISION

REFER TO TASK 536173−832−801−001

QUESTION

ACTION

FINDING

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE

PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY

SOURCE FOR TASKS OR COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN

YES

NO

UPDATE MAINTENANCE PROGRAM TO BE IN

ACCORDANCE WITH STRUCTURAL 

REPAIR INSPECTION (SRI) REQUIREMENT

SRM 53−12−12−101

FIGURE 108 (SHEET 9) FOR SKIN PANEL AND

SRM 53−12−81−101 FIGURE 101 (SHEET 2)

FOR FAIL SAFE RING

REFER TO SUBTASK 536173−832−001−001

REFER TO SUBTASK 536173−832−002−001

FOR LH SIDE

FOR RH SIDE

No A300−53−6126

ACCOMPLISHED

SEE FIGURE A−FFAAA

SHEET 02

YES

AREA

REPAIRED BEFORE

A300−600 SRM 53−12−81−101

SB

D_SB_536173_5_FAAA_01_07

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 36

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

DO A ONE TIME DETAILED INSPECTION

TO EVALUATE THE EXISTING REWORK ON THE

FWD PASSENGER/CREW DOOR SURROUNDING PANELS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION

PARAGRAPH E.(2)

REWORK

IDENTIFY THE REWORK AREA AND REWORK LIMITS

DETERMINE % OF REWORK LIMITS BY US INSPECTION

REFER TO SUBTASK 536173−832−001−001 FOR LH SIDE

NO

FURTHER

ACTION

REWORK OUT

NO

SEND A DAMAGE REPORT TO AIRBUS

STRUCTURE REPAIR SUPPORT

AND AN INSPECTION REPORT TO

OF SRM LIMITS

REFER TO SUBTASK 536173−832−002−001 FOR RH SIDE

REFER TO TASK 536173−832−801−001

QUESTION

ACTION

FINDING

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE

PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY

SOURCE FOR TASKS OR COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN

YES

YES NO

NO FURTHER ACTION

UPDATE MAINTENANCE PROGRAM TO BE IN

ACCORDANCE WITH STRUCTURAL REPAIR

INSPECTION (SRI) REQUIREMENT

SRM 53−12−12−101

FIGURE 108 (SHEET 9) FOR SKIN PANEL AND

SRM 53−12−81−101 FIGURE 101 (SHEET 2)

FOR FAIL SAFE RING

REFER TO SUBTASK 536173−832−001−001

REFER TO SUBTASK 536173−832−002−001

FOR LH SIDE

FOR RH SIDE

SEE FIG A−FFAAA SHEET 01

AIRBUS BEFORE NEXT FLIGHT

D_SB_536173_5_FAAA_02_03

Figure A-FFAAA - Sheet 02

Flow Chart

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 37

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

DO A ONE TIME DETAILED INSPECTION

TO EVALUATE THE EXISTING REWORK ON THE

FWD PASSENGER/CREW DOOR SURROUNDING PANELS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION

PARAGRAPH E.(2)

REWORK

IDENTIFY THE REWORK AREA AND DETERMINE % OF

VALUES REWORK AND REWORK LIMITS BY US INSPECTION

REFER TO SUBTASK 536173−832−001−002 FOR LH SIDE

NO

FURTHER

ACTION

REWORK OUT

NO

NO FURTHER ACTION

OF SRM LIMITS

REFER TO SUBTASK 536173−832−002−002 FOR RH SIDE

REFER TO TASK 536173−832−801−001

QUESTION

ACTION

FINDING

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE

PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY

SOURCE FOR TASKS OR COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN

YES

YES NO

UPDATE MAINTENANCE PROGRAM TO BE IN

ACCORDANCE WITH STRUCTURAL 

REPAIR INSPECTION (SRI) REQUIREMENT

SRM 53−12−12−101−C2

FIGURE 107 (SHEET 6 TO 10) FOR SKIN PANEL AND

SRM 53−12−81−101−C2 FIGURE 102

FOR FAIL SAFE RING

REFER TO SUBTASK 536173−832−001−002

REFER TO SUBTASK 536173−832−002−002

FOR LH SIDE

FOR RH SIDE

SEND A DAMAGE REPORT TO AIRBUS

STRUCTURE REPAIR SUPPORT

AND AN INSPECTION REPORT TO

AIRBUS BEFORE NEXT FLIGHT

D_SB_536173_5_FAAB_01_06

Figure A-FFAAB - Sheet 01

Flow Chart

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 38

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

% REWORK

LH SIDE

F/C WHEN REWORK % REWORK

RH SIDE

F/C WHEN REWORK REMARKS

INSPECTION REPORT

SERVICE BULLETIN No :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−53−6173

DATE OF INSPECTION :

RETURN TO :

AIRBUS

FUSELAGE (WB/LR) − VERTICAL TAIL PLANE −

CENTER − WING BOX (WB/LR)

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: structure.sbinspectionresult@airbus.com DETAILED

INSPECTION FAX +33 (0)5 61 93 36 14

CUSTOMER SERVICES ENGINEERING − SEES1

REPORT HERE OBSERVED REWORK VALUE FOR FWD PASSENGER DOOR SURROUDING PANELS:

REFER TO SRM 53−12−12 FIG. 108 SHEET 1 TO 5 FOR FWD PASSENGER DOOR FRAME

NOTE:

DEFINITION ZONES

DOOR SURROUNDING

ZONE

REFERENCES)

(AS PER SRM

D_SB_536173_5_RAAA_01_03

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 39

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

% REWORK

LH SIDE

F/C WHEN REWORK % REWORK

RH SIDE

F/C WHEN REWORK REMARKS

INSPECTION REPORT

SERVICE BULLETIN No :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−53−6173

DATE OF INSPECTION :

RETURN TO :

AIRBUS

FUSELAGE (WB/LR) − VERTICAL TAIL PLANE −

CENTER − WING BOX (WB/LR)

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: structure.sbinspectionresult@airbus.com DETAILED

INSPECTION FAX +33 (0)5 61 93 36 14

CUSTOMER SERVICES ENGINEERING − SEES1

REPORT HERE OBSERVED REWORK VALUE FOR FAIL SAFE RING:

REFER TO SRM 53−12−81−101 FIG. 101 FOR IDENTIFICATION OF FAIL SAFE RING ZONES.

NOTE:

DOOR SURROUNDING

ZONE

REFERENCES)

(AS PER SRM

D_SB_536173_5_RAAA_02_03

Figure A-FRAAA - Sheet 02

Inspection Report

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 40

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

% REWORK

LH SIDE

F/C WHEN REWORK % REWORK

RH SIDE

F/C WHEN REWORK REMARKS

INSPECTION REPORT

SERVICE BULLETIN No :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−53−6173

DATE OF INSPECTION :

RETURN TO :

AIRBUS

FUSELAGE (WB/LR) − VERTICAL TAIL PLANE −

CENTER − WING BOX (WB/LR)

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: structure.sbinspectionresult@airbus.com DETAILED

INSPECTION FAX +33 (0)5 61 93 36 14

CUSTOMER SERVICES ENGINEERING − SEES1

REPORT HERE OBSERVED REWORK VALUE FOR FWD PASSENGER DOOR SURROUDING PANELS:

REFER TO SRM 53−12−12−101−C2 FIG. 107 SHEETS 1 TO 5 FOR FWD PASSENGER DOOR FRAME

NOTE:

DEFINITION ZONES.

DOOR SURROUNDING

ZONE

REFERENCES)

(AS PER SRM

D_SB_536173_5_RAAB_01_02

Figure A-FRAAB - Sheet 01

Inspection Report

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 41

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

DOOR SURROUNDING

ZONE

% REWORK

LH SIDE

F/C WHEN REWORK % REWORK

RH SIDE

F/C WHEN REWORK REMARKS

INSPECTION REPORT

SERVICE BULLETIN No :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−53−6173

DATE OF INSPECTION :

RETURN TO :

AIRBUS

FUSELAGE (WB/LR) − VERTICAL TAIL PLANE −

CENTER − WING BOX (WB/LR)

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: structure.sbinspectionresult@airbus.com DETAILED

INSPECTION FAX +33 (0)5 61 93 36 14

CUSTOMER SERVICES ENGINEERING − SEES1

REPORT HERE OBSERVED REWORK VALUE FOR FAIL SAFE RING:

REFER TO SRM 53−12−81−101−C2 FIG. 102 FOR IDENTIFICATION OF FAIL SAFE RING ZONES.

NOTE:

REFERENCES)

(AS PER SRM

D_SB_536173_5_RAAB_02_02

Figure A-FRAAB - Sheet 02

Inspection Report

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 42

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Appendix 01 : Elapsed Time Assumption

**CONF ALL

Refer to the Gantt Chart on the next page for details about the inspection elapsed time assumptions.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Appendix 01 : Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−53−6173

SB ELAPSED TIME

(HOURS)

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

120.00

30.00

STEPS

0 10 15 20 25 30

INSPECTION OF FWD PASSENGER/CREW 8.00 4.00

8.00 4.00

CLOSE−UP 96.00 24.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

PER

2

2

4

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

DOOR SURROUNDING PANELS OF LHS

INSPECTION OF FWD PASSENGER/CREW

DOOR SURROUNDING PANELS OF RHS

5

GET ACCESS 8.00 2.00 4

D_SB_536173_5_AAAA_01_01

Figure A-FAAAA - Sheet 01

Gantt Chart

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - NOSE SECTION - INSPECT THE FWD PAX/CREW DOOR

SURROUNDING SKIN PANELS.

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Aug 01/13 SERVICE BULLETIN No.: A300-53-6173

REVISION No.: 01 - Feb 28/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.