# @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



# MANDATORYMANDATORYMANDATORY
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

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# @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

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# @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

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# @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

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# @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. 

# MANDATORYMANDATORYMANDATORY
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

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# @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

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# @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

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# @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

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# @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



# MANDATORYMANDATORYMANDATORY
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

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# @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

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# @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

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# @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

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# @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 Before Next Flight None SB 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

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# @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 areadescribed 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

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# @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 Before Next Flight None No rework found out of 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

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# @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

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# @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 Before Next Flight None No rework found out of 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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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 FR16A FR16 FR15A FR15 FR14A FR14 FR16A FR15C FR14C FR14B FR14

BEAM 1 BEAM 2



## B **FWD** 01 01

BEAM 8

**NOTE:** AREAS EXCLUDED SINCE SRM JUNE 2001 REVISION 01 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

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# @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 SYMMETRICALFR16A FR16 FR15A FR15 FR14A FR14 FR16A FR15C FR15B FR14C FR14B FR14

BEAM 2



## B **FWD** 01 BEAM 7 BEAM 8

BEAM 1 BEAM 7 BEAM 8

BEAM 1

**NOTE:** AREAS WITH NEW ADL SINCE SRM DEC 2009 REVISION 01 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

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# @A300-600 SERVICE BULLETIN

**CONF 002

FR18 FR17 FR16A FR15C FR15B FR14CFR14B 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

**FWD FWD**  **NOTE:** AREAS EXCLUDED SINCE DEC 2009 REVISION 01 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

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# @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

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# @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 TOOF 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

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# @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

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# @A300-600 SERVICE BULLETIN

**CONF 001

% REWORKLH SIDE F/C WHEN REWORK % REWORKRH 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

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# @A300-600 SERVICE BULLETIN

**CONF 001

% REWORKLH SIDE F/C WHEN REWORK % REWORKRH 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

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# @A300-600 SERVICE BULLETIN

**CONF 002

% REWORKLH SIDE F/C WHEN REWORK % REWORKRH 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

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# @A300-600 SERVICE BULLETIN

**CONF 002

DOOR SURROUNDING ZONE % REWORKLH 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

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# @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

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# @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

10 15 20 25 30 0 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

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# @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

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# @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

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