# @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: 28 

### TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD MODIFICATION No.: None This page transmits Revision No.01 of Service Bulletin No.A300-28-6106 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 add the Equipment BFEB02 for the Canister Hood PN 3C93-129 (part of Fuel Pump Canister PN C93R51-601). CHANGES SUMMARY REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES REASON UPDATED R MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE UPDATED R MATERIAL PRICE INFORMATION TABLE UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Material Effectivity MATERIAL EFFECTIVITY UPDATED R MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED MATERIAL SET UPDATED R
REASON Objective/Action OBJECTIVE/ACTION UPDATED R

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED R LIST OF MATERIALS - OPERATOR SUPPLIED Equipment EQUIPMENT UPDATED R Equipement BFEB01 PART MATERIAL SET UPDATED NOTE UPDATED R Equipement BFEB02 PART MATERIAL SET ADDED N ACCOMPLISHMENT INSTRUCTIONS TASK 286106- 832-895-001- INSPECTION TASK SOLUTION UPDATED NOTE UPDATED R Subtask 286106-941-402-001 SUBTASK SOLUTION UPDATED R Subtask 286106-832-401-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

Subtask 286106-832-402-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

Subtask 286106-832-401-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

Subtask 286106-832-402-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

Subtask 286106-832-403-002 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

TASK 286106- 833-895-001 -REPAIR Subtask 286106-833-401-001 SUBTASK SOLUTION UPDATED NOTE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 2 7

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 286106-833-401-001 SUBTASK SOLUTION UPDATED NOTE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Fig. A-UAAAA Fig. A-UAAAA Sheet 01 SHEET UPDATED R Fig. A-UBAAA Fig. A-UBAAA Sheet 01 SHEET UPDATED R Fig. A-UBCAA Fig. A-UBCAA Sheet 01 SHEET UPDATED R Fig. A-UBEAA Fig. A-UBEAA Sheet 01 SHEET UPDATED R Fig. A-UCAAA Fig. A-UCAAA 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: Jan 13/11 REVISION No. : 01 - Apr 15/11

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 3 7

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 4 7

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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. 

# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 28 

### TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Some operators have reported cases of cracking on the hood of the inboard and outboard fuel pump canisters located in the inner fuel tanks. The hood is part of the fuel pump canister and forms a surface between the pump inlet mesh and the canister body. The hood is fabricated from thin aluminium alloy in two halves. On one aircraft the detached parts were reported as consisting of two separate pieces. One annular section was subsequently found inside the fuel tank. This Inspection Service Bulletin (ISB) introduces a repetitive Detailed Visual Inspection (DVI) of all fuel pump locations (center, wing inner, wing outer and trim tank). The inspection will also assess which locations are subject to such cracking, and which hoods must be replaced. The Inspection must be done not more than 30 months after the issue date of this Service Bulletin and repeated every 30 months. Replacement of failed hood halves will prevent possible contamination issues and establish which locations are subject to cracking. Replace both hood halves if cracks are found in one of the two halves. You must find and remove all broken pieces from the fuel tanks.

GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A300-600 SERVICE BULLETIN SUMMARY EVALUATION TABLE STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO DEFUEL/VENTILATION YES PRE-ENTRY CHECKLIST YES NOTE (1) : Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEB01 1 See SB Hood Halves Equipment BFEB02 1 See SB Hood Halves **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEB01 1 See SB Hood Halves Equipment BFEB02 1 See SB Hood Halves EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

30T 83V 98W AAL AAW ABD AHK AMU CES CSN F2I FDX G8E IRA IRM JAL KAC KAL LAA MNB MON MSR MXU OHY QTR SUD TAR THA TMA UPS UZB
CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU 28.21.13.001 OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 2 7

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# @A300-600 SERVICE BULLETIN SUMMARY NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 286106-832-895-001: INSPECTION TOTAL MANHOURS 9.00 ELAPSED TIME (HOURS) 5.00 Task 286106-833-895-001: REPAIR TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 **CONF 002 Task 286106-832-895-001: INSPECTION TOTAL MANHOURS 12.00 ELAPSED TIME (HOURS) 6.00 Task 286106-833-895-001: REPAIR TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 APPENDICES **CONF ALL Inspection Findings - Reporting Sheet

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 3 7

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# @A300-600 SERVICE BULLETIN SUMMARY

**CONF 001

LH WING SHOWN RH WING SIMILAR RIB14 RIB2 Z550 (Z650)

TYPICAL Z540 (Z640) FR47 FR46 

### C **C C** 

**C**



## C **A**

**B B**  **A**

− Z141 Z142

D_SB_286106_7_SAAA_01_00 Figure A-USAAA - Sheet 01 FUEL - FUEL PUMP SY STEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD - WING AND CENTER TANKS DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 4 7

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# @A300-600 SERVICE BULLETIN SUMMARY

**CONF 002



### B

PUMP 2 CANISTER

PUMP 1 CANISTER LH WING SHOWN RH WING SIMILAR RIB14 RIB2 Z550 (Z650)

TYPICAL Z540 (Z640) 

### A

FR47 FR46 

## A − Z141 Z142



## B **D**

**D D** 



## D **D**

319AB 319BZ

319BB 319AZ 

### D

**D**



## C

D_SB_286106_7_SAAB_01_01 Z319 

### C

Figure A-USAAB - Sheet 01 FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD - WING, CENTER AND TRIM TANKS DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 5 7

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# @A300-600 SERVICE BULLETIN SUMMARY

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DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 6 7

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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



# MANDATORY MANDATORY MANDATORY ATA SYSTEM: 28 

### TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD 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/FC4-620 F4-605R F4-622R (2) Effectivity by MSN 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0354 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0470 0474 0477 0479 0505-0518 0521 0525 0529-0530 0532 0536 0540 0543 0546 0553-0561 0563 0566 0569 0572 0575 0577 0579 0581-0582 0584 0601-0618 0621 0623 0625-0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721-0750 0752-0764 0766-0775 0777-0794 0797 0799-0841 0845-0878

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A300-600 SERVICE BULLETIN (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. OPERATOR MSN 30T 0626 0643 83V 0423 0459 0460 0463 0466 0470 0474 0510 0511 0512 0615 0639 0675 98W 0740 AAL 0506 0507 0508 0513 0515 0517 0612 AAW 0354 ABD 0529 0557 AHK 0855 0856 0857 0858 0859 0860 0870 0871 AMU 0677 0743 CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763 CSN 0733 0734 0739 0756 F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0461 0606 0610 0637 0645 0711 0724 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 0873 0874 0875 0876 0877 0878 G8E 0462 0465 0469 0509 0514 0516 IRA 0632 0696 0723 0727 IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701 0750 0762 0773 JAL 0602 0617 0621 0641 0670 0679 0683 0703 0729 0730 0737 0753 0770 0783 0797 0836 0837 0838 KAC 0344 0673 0694 0699 0719 0721 KAL 0582 0609 0627 0631 0662 0685 0692 0731 LAA 0601 0616 MNB 0755 0758 MON 0540 0556 0604 0605 MSR 0561 0607 MXU 0767 0788 OHY 0584 0603 0744 0747 0749 0764 QTR 0554 0560 0614 SUD 0666 0775 TAR 0505 0558 0563 THA 0464 0518 0566 0569 0577 0628 0629 0635 0681 0705 0782 0784 0785 0786 0787 TMA 0872

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 2 7

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# @A300-600 SERVICE BULLETIN
OPERATOR MSN UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830 0831 0832 0833 0834 0835 0839 0840 0841 0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864 0865 0866 0867 0868 0869 UZB 0717 0722 (4) Configuration by MSN MSN CONFIGURATION 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0354 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0546 0553 0618 0623 001
0423 0459 0460 0461 0462 0463 0464 0465 0466 0469 0470 0474 0477 0479 0505 0506 0507 0508 0509 0510 0511 0512 0513 0514 0515 0516 0517 0518 0521 0525 0529 0530 0532 0536 0540 0543 0554 0555 0556 0557 0558 0559 0560 0561 0563 0566 0569 0572 0575 0577 0579 0581 0582 0584 0601 0602 0603 0604 0605 0606 0607 0608 0609 0610 0611 0612 0613 0614 0615 0616 0617 0621 0625 0626 0627 0628 0629 0630 0631 0632 0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721 0722 0723 0724 0725 0726 0727 0728 0729 0730 0731 0732 0733 0734 0735 0736 0737 0738 0739 0740 0741 0742 0743 0744 0745 0746 0747 0748 0749 0750 0752 0753 0754 0755 0756 0757 0758 0759 0760 0761 0762 0763 0764 0766 0767 0768 0769 0770 0771 0772 0773 0774 0775 0777 0778 0779 0780 0781 0782 0783 0784 0785 0786 0787 0788 0789 0790 0791 0792 0793 0794 0797 0799 0800 0801 0802 0803 0804 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830 0831 0832 0833 0834 0835 0836 0837 0838 0839 0840 0841 0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0855 0856 0857 0858 0859 0860 0861 0862 0863 0864 0865 0866 0867 0868 0869 0870 0871 0872 0873 0874 0875 0876 0877 0878 002

(5) Configuration definition NOTE : This Service Bulletin is only applicable to A300-600 aircraft that have Fuel Pump Canister Hood PN 205481 (part of Fuel Pump Canister PN 2052C11 or PN 2052C12) or PN 3C93-129 (part of Fuel Pump Canister PN C93R51-601) installed **CONF 001 Config. 001 is applicable to all A300-600 aircraft - aircraft without a trim tank. **CONF 002 Config. 002 is applicable to all A300-600R aircraft - aircraft with a trim tank.
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 3 7

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# @A300-600 SERVICE BULLETIN (6) Material Effectivity NOTE : One BFEB01 or BFEB02 is required for each Fuel Pump Canister. The total quantity of BFE kits will be determined by the result of the inspection requirements of this Service Bulletin. MATERIAL QTY PER A/C SEE NOTES Equipment BFEB01 1 Equipment BFEB02 1 Consumable CMLB01 As required B. CONCURRENT REQUIREMENTS None C. REASON (1) History Some operators have reported cases of cracking on the hood of the inboard and outboard fuel pump canisters located in the inner fuel tanks. The hood is part of the fuel pump canister and forms a surface between the pump inlet mesh and the canister body. The hood is fabricated from thin aluminium alloy in two halves. On one aircraft the detached parts were reported as consisting of two separate pieces. One annular section was subsequently found inside the fuel tank. (2) Objective/Action This Inspection Service Bulletin (ISB) introduces a repetitive Detailed Visual Inspection (DVI) of all fuel pump locations (center, wing inner, wing outer and trim tank). The inspection will also assess which locations are subject to such cracking, and which hoods must be replaced. The Inspection must be done not more than 30 months after the issue date of this Service Bulletin and repeated every 30 months. (3) Advantages Replacement of failed hood halves will prevent possible contamination issues and establish which locations are subject to cracking. Replace both hood halves if cracks are found in one of the two halves. You must find and remove all broken pieces from the fuel tanks. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 4 7

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# @A300-600 SERVICE BULLETIN
**CONF 001 Task 286106-832-895-001: INSPECTION (1) INSPECTION OF THE WING TANKS ( INNER/OUTER) PUMP CANISTER HOOD HALVES (2) INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES Task 286106-833-895-001: REPAIR (1) REPAIR THE FUEL PUMP CANISTER HOOD HALVES **CONF 002 Task 286106-832-895-001: INSPECTION (1) INSPECTION OF THE WING TANKS ( INNER/OUTER) PUMP CANISTER HOOD HALVES (2) INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (3) INSPECTION OF THE TRIM TANK TRANSFER PUMP CANISTER HOOD HALVES Task 286106-833-895-001: REPAIR (1) REPAIR THE FUEL PUMP CANISTER HOOD HALVES **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale Do this Inspection not more than 30 months after the date of issue of this Service Bulletin and repeat every 30 months. Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency ( EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals and/or date) given above but reference should be made to the AD for confirmation of the mandated accomplishment timescale. F. APPROVAL Approved under EASA Design Organisation Approval No. EASA 21J.031.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 5 7

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# @A300-600 SERVICE BULLETIN 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. **CONF 001 Task 286106-832-895-001: INSPECTION Get Access 2.00 On Aircraft INSPECTION OF THE WING TANKS (INNER/OUTER) PUMP CANISTER HOOD HALVES 4.00 INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES 1.00 Tests 0.00 Close-Up 2.00 TOTAL MANHOURS 9.00 ELAPSED TIME (HOURS) 5.00 Task 286106-833-895-001: REPAIR Get Access 0.00 On Aircraft REPAIR THE FUEL PUMP CANISTER HOOD HALVES 0.50 Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 **CONF 002 Task 286106-832-895-001: INSPECTION Get Access 3.00 On Aircraft INSPECTION OF THE WING TANKS (INNER/OUTER) PUMP CANISTER HOOD HALVES 4.00 INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES 1.00 INSPECTION OF THE TRIM TANK TRANSFER PUMP CANISTER HOOD HALVES 1.00 Tests 0.00 DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 6 7

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# @A300-600 SERVICE BULLETIN
Task 286106-832-895-001: INSPECTION Close-Up 3.00 TOTAL MANHOURS 12.00 ELAPSED TIME (HOURS) 6.00 Task 286106-833-895-001: REPAIR Get Access 0.00 On Aircraft REPAIR THE FUEL PUMP CANISTER HOOD HALVES 0.50 Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 **CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-21-00 06-41-53 06-41-57 28-00-00 28-10-00 28-11-22 28-11-29 28-25-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 **CONF 002 Aircraft Maintenance Manual (AMM) 06-21-00 06-41-53 06-41-57 28-00-00 28-10-00 28-11-22 28-11-29 28-25-00 28-27-12 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 **CONF ALL K. PUBLICATION AFFECTED None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 7 7

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# @A300-600 SERVICE BULLETIN
L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 8 7

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# @A300-600 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Vendor parts are to be procured from: Equipment BFEB01 Equipment BFEB02 INTERTECHNIQUE M. Jean_Pierre Michel Bd Sagnat BP3 4220 ROCHE-LA-MOLIERE, FRANCE (2) Price and Availability Procurement terms for the equipment must be negotiated with the equipment supplier. (MATERIAL INFORMATION). B. INDUSTRY SUPPORT INFORMATION Refer to the paragraph: ’Price and Availability’. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 0 Lint-Free Cotton Cloth 19-003 0 (2) Components None (3) Equipment Equipment BFEB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 205481 2 HOODHALF (1) 205481 (1) (2) (1) (2)

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 9 7

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# @A300-600 SERVICE BULLETIN
NOTE (1) : One BFEB01 is required for each Fuel Pump Canister. The total quantity of BFE kits will be determined by the result of the inspection requirements of this Service Bulletin. NOTE (2) : Canister Hood PN 205481 for Fuel Pump Canister PN 2052C11 or PN 2052C12. Equipment BFEB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 4 3C93-129 2 HOODHALF (4) 3C93-129 (1 ) (2) (1 ) (2) NOTE (1) : One BFEB02 is required for each Fuel Pump Canister. The total quantity of BFE kits will be determined by the result of the inspection requirements of this Service Bulletin. NOTE (2) : Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601. E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 10 7

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# @A300-600 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 286106-832-895-001 - INSPECTION 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, CLEANING. Task Associated Data **CONF 001 Zone 141 142 540 550 640 650 Modified FIN 280014 280015 280016 280017 280018 280019 280020 280021 280022 280023 Access Door 142AZ 147AZ 542CB 550BB 642CB 650BB Manpower TOTAL MANHOURS 9.00 ELAPSED TIME (HOURS) 5.00 **CONF 002 Zone 141 142 311 312 540 550 640 650 Modified FIN 280014 280015 280016 280017 280018 280019 280020 280021 280022 280023 280432 280433 Access Door 142AZ 147AZ 319AZ 319BZ 542CB 550BB 642CB 650BB Manpower TOTAL MANHOURS 12.00
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 11 7

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# @A300-600 SERVICE BULLETIN ELAPSED TIME (HOURS) 6.00 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 286106-910-401-001 - STANDARD PRACTICES Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-41-53, Page Block 001 06-41-57, Page Block 001 28-00-00, Page Block 301 28-10-00, Page Block 301 (a) For the identification of Access Panels (Refer to AMM 06-41-53, Page Block 001 and AMM 06-41-57, Page Block 001). (b) For the identification of Zones (Refer to AMM 06-21-00, Page Block 001). (c) Obey the safety procedures when you do work in a fuel tank (Refer to AMM 28-10-00, Page Block 301 and AMM 28-00-00, Page Block 301). (2) Subtask 286106-839-401-001 - ADMINISTRATIVE Manpower Resources Skills AIRFRAME Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 286106-910-401-001 - STANDARD PRACTICES Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-41-53, Page Block 001 06-41-57, Page Block 001 28-00-00, Page Block 301 28-10-00, Page Block 301 (a) For the identification of Access Panels (Refer to AMM 06-41-53, Page Block 001 and AMM 06-41-57, Page Block 001).
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 12 7

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# @A300-600 SERVICE BULLETIN (b) For the identification of Zones (Refer to AMM 06-21-00, Page Block 001). (c) Obey the safety procedures when you do work in a fuel tank (Refer to AMM 28-10-00, Page Block 301 and AMM 28-00-00, Page Block 301). (2) Subtask 286106-839-401-001 - ADMINISTRATIVE Manpower Resources Skills AIRFRAME 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 286106-941-401-001 - JOB SET-UP - WING AND CENTER TANK Work Zones and Access Panels Zone Access/Work location 141 Access Door 147AZ 142 Access Door 142AZ 540 Access Door 542CB 640 Access Door 642CB 550 Access Door 550BB 650 Access Door 650BB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 28-10-00, Page Block 301 28-11-22, Page Block 401 28-11-29, Page Block 401 28-25-00, Page Block 301 Consumable Material List (CML) WARNING : YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO WORK IN OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE SAFETY PROCEDURES, THERE IS A RISK OF: - DEATH OR INJURY TO PERSONS - DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 13 7

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# @A300-600 SERVICE BULLETIN (a) Prepare the aircraft as specified in AMM Task ’STORAGE - SERVICING (Fuel Tank Draining, Venting and Entry)’ (Refer to AMM 28-10-00, Page Block 301). 1 Before you go into a fuel tank you must complete the Pre-Entry Checklist (Refer to AMM 28-10-00, Page Block 301). (b) Defuel all of the aircraft fuel tanks (Refer to AMM 28-25-00, Page Block 301). (c) Put platforms in position to get access to the applicable zones (Refer to AMM 06-21-00, Page Block 001): 1 Wing tanks inner - Zones 540 LH (640 RH) 2 Wing tanks outer - Zones 550 LH (650 RH) 3 Center tank - Zones 141 and 142 (d) Remove the applicable manhole covers: 1 Wing tanks inner 542CB LH (642CB RH) (Refer to AMM 28-11-22, Page Block 401) 2 Wing tanks outer 550BB LH (650BB RH) (Refer to AMM 28-11-22, Page Block 401) 3 Center tank canisters 147AZ LH and 148AZ RH (Refer to AMM 28-11-29, Page Block 401). (e) For the specification of materials (Mat. No.) that you must use in this Service Bulletin refer to Consumable Materials List (CML). **CONF 002 (1) Subtask 286106-941-401-001 - JOB SET-UP - WING AND CENTER TANK Work Zones and Access Panels Zone Access/Work location 141 Access Door 147AZ 142 Access Door 142AZ 540 Access Door 542CB 640 Access Door 642CB 550 Access Door 550BB 650 Access Door 650BB Manpower Resources Skills AIRFRAME

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 14 7

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# @A300-600 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 28-10-00, Page Block 301 28-11-22, Page Block 401 28-11-29, Page Block 401 28-25-00, Page Block 301 Consumable Material List (CML) WARNING : YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO WORK IN OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE SAFETY PROCEDURES, THERE IS A RISK OF: - DEATH OR INJURY TO PERSONS - DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT. (a) Prepare the aircraft as specified in AMM Task ’STORAGE - SERVICING (Fuel Tank Draining, Venting and Entry)’ (Refer to AMM 28-10-00, Page Block 301). 1 Before you go into a fuel tank you must complete the Pre-Entry Checklist (Refer to AMM 28-10-00, Page Block 301). (b) Defuel all of the aircraft fuel tanks (Refer to AMM 28-25-00, Page Block 301). (c) Put platforms in position to get access to the applicable zones (Refer to AMM 06-21-00, Page Block 001): 1 Wing tanks inner - Zones 540 LH (640 RH) 2 Wing tanks outer - Zones 550 LH (650 RH) 3 Center tank - Zones 141 and 142 (d) Remove the applicable manhole covers: 1 Wing tanks inner 542CB LH (642CB RH) (Refer to AMM 28-11-22, Page Block 401) 2 Wing tanks outer 550BB LH (650BB RH) (Refer to AMM 28-11-22, Page Block 401) 3 Center tank canisters 147AZ LH and 148AZ RH (Refer to AMM 28-11-29, Page Block 401). (e) For the specification of materials (Mat. No.) that you must use in this Service Bulletin refer to Consumable Materials List (CML). (2) Subtask 286106-941-402-001 - JOB SET-UP - TRIM TANK Work Zones and Access Panels Zone Access/Work location 311 Access Door 319AZ 312 Access Door 319BZ DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 15 7

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# @A300-600 SERVICE BULLETIN Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 28-25-00, Page Block 301 28-27-12, Page Block 401 Consumable Material List (CML) WARNING : YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO WORK IN OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE SAFETY PROCEDURES, THERE IS A RISK OF: - DEATH OR INJURY TO PERSONS - DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT. (a) Prepare the aircraft as specified in AMM Task ’STORAGE - SERVICING (Fuel Tank Draining, Venting and Entry)’ (Refer to AMM 28-10-00, Page Block 301). 1 Before you go into a fuel tank you must complete the Pre-Entry Checklist (Refer to AMM 28-10-00, Page Block 301). (b) Defuel all of the aircraft fuel tanks (Refer to AMM 28-25-00, Page Block 301). (c) Put platforms in position to get access to the applicable zones: 1 Trim tank - Zones 311 and 312. (d) Remove the applicable manhole covers: 1 Trim tank transfer pump canisters 319AZ and 319BZ (Refer to AMM 28-27-12, Page Block 401). (e) For the specification of materials (Mat. No.) that you must use in this Service Bulletin refer to Consumable Materials List (CML). **CONF ALL C. PROCEDURE NOTE : Operators can have the Fuel Pump Canister Hood PN 205481 (part of Fuel Pump Canister PN 2052C11 or PN 2052C12) or PN 3C93-129 (part of Fuel Pump Canister PN C93R51-601) installed.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 16 7

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# @A300-600 SERVICE BULLETIN
**CONF 001 (1) Subtask 286106-832-401-001 - INSPECTION OF THE WING TANKS (INNER/OUTER) PUMP CANISTER HOOD HALVES Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 As required Lint-Free Cotton Cloth 19-003 As required References Consumable Material List (CML) Fig. A-UAAAA Inspection Flowchart Sheet 01 Fig. A-UBAAA Fuel Pump Canister Hood Halves Inspection - Wing Tanks Sheet 01 Fig. A-UCAAA Repair the Fuel Pump Canister Hood Halves - Typical Sheet 01
(a) Clean the 2 Hood Half 205481 Item (1) with a Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent 11-583 As required (b) Do a Detailed Visual Inspection (DVI) of the fuel pump canister hood halves in the wing tanks: - Wing tank (LH) - inboard FIN 280014 and FIN 280016 and outboard FIN280018 and FIN 280020. - Wing tank (RH) - inboard FIN 280015 and FIN 280017 and outboard FIN 280019 and FIN 280021. DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 17 7

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# @A300-600 SERVICE BULLETIN (Refer to Fig. A-UAAAA and Fig. A-UBAAA). 1 No cracks found in 2 Hood Half 205481 Item (1)
a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). 2 Cracks are found in 2 Hood Half 205481 Item (1)
a Replace the Hood Halves. (Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA). b Make sure that all broken parts and unwanted materials are removed from the related tank.
c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). (c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings - Reporting Sheet ). (2) Subtask 286106-832-402-001 - INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES Manpower Resources Manhours 1.00 Minimum number of person 2 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBCAA Fuel Pump Canister Hood Halves Inspection - Center Tank Sheet 01 Fig. A-UAAAA Inspection Flowchart Sheet 01 Fig. A-UCAAA Repair the Fuel Pump Canister Hood Halves - Typical Sheet 01

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 18 7

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# @A300-600 SERVICE BULLETIN (a) Clean the 2 Hood Half 205481 Item (1) or 2 Hood Half 3C93-129 Item (4) with a Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent 11-583 As required (b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the center tank - LH FIN 280022 and RH FIN 280023 (Refer to Fig. A-UAAAA and Fig. A-UBCAA). 1 No cracks found in 2 Hood Half 205481 Item (1) or 2 Hood Half 3C93-129 Item (4)
a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). 2 Cracks are found in 2 Hood Half 205481 Item (1) or 2 Hood Half 3C93-129 Item (4)
a Replace the Hood Halves. (Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA). b Make sure that all broken parts and unwanted materials are removed from the related tank.
c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). (c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings - Reporting Sheet ).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 19 7

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# @A300-600 SERVICE BULLETIN
**CONF 002 (1) Subtask 286106-832-401-001 - INSPECTION OF THE WING TANKS (INNER/OUTER) PUMP CANISTER HOOD HALVES Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 As required Lint-Free Cotton Cloth 19-003 As required References Consumable Material List (CML) Fig. A-UAAAA Inspection Flowchart Sheet 01 Fig. A-UBAAA Fuel Pump Canister Hood Halves Inspection - Wing Tanks Sheet 01 Fig. A-UCAAA Repair the Fuel Pump Canister Hood Halves - Typical Sheet 01
(a) Clean the 2 Hood Half 205481 Item (1) with a Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent 11-583 As required (b) Do a Detailed Visual Inspection (DVI) of the fuel pump canister hood halves in the wing tanks: - Wing tank (LH) - inboard FIN 280014 and FIN 280016 and outboard FIN280018 and FIN 280020. - Wing tank (RH) - inboard FIN 280015 and FIN 280017 and outboard FIN 280019 and FIN 280021. DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 20 7

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# @A300-600 SERVICE BULLETIN (Refer to Fig. A-UAAAA and Fig. A-UBAAA). 1 No cracks found in 2 Hood Half 205481 Item (1)
a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). 2 Cracks are found in 2 Hood Half 205481 Item (1)
a Replace the Hood Halves. (Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA). b Make sure that all broken parts and unwanted materials are removed from the related tank.
c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). (c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings - Reporting Sheet ). (2) Subtask 286106-832-402-001 - INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES Manpower Resources Manhours 1.00 Minimum number of person 2 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBCAA Fuel Pump Canister Hood Halves Inspection - Center Tank Sheet 01 Fig. A-UAAAA Inspection Flowchart Sheet 01 Fig. A-UCAAA Repair the Fuel Pump Canister Hood Halves - Typical Sheet 01

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 21 7

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# @A300-600 SERVICE BULLETIN (a) Clean the 2 Hood Half 205481 Item (1) or 2 Hood Half 3C93-129 Item (4) with a Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent 11-583 As required (b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the center tank - LH FIN 280022 and RH FIN 280023 (Refer to Fig. A-UAAAA and Fig. A-UBCAA). 1 No cracks found in 2 Hood Half 205481 Item (1) or 2 Hood Half 3C93-129 Item (4)
a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). 2 Cracks are found in 2 Hood Half 205481 Item (1) or 2 Hood Half 3C93-129 Item (4)
a Replace the Hood Halves. (Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA). b Make sure that all broken parts and unwanted materials are removed from the related tank.
c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). (c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings - Reporting Sheet ).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 22 7

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# @A300-600 SERVICE BULLETIN (3) Subtask 286106-832-403-002 - INSPECTION OF THE TRIM TANK TRANSFER PUMP CANISTER HOOD HALVES Manpower Resources Manhours 1.00 Minimum number of person 2 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBEAA Fuel Pump Canister Hood Halves Inspection - Trim Tank Sheet 01 Fig. A-UAAAA Inspection Flowchart Sheet 01 Fig. A-UCAAA Repair the Fuel Pump Canister Hood Halves - Typical Sheet 01
(a) Clean the 2 Hood Half 205481 Item (1) with a Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent 11-583 As required (b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the trim tank - FIN 280432 and FIN 280433 (Refer to Fig. A-UAAAA and Fig. A-UBEAA). 1 No cracks found in 2 Hood Half 205481 Item (1)
a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 23 7

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# @A300-600 SERVICE BULLETIN
2 Cracks are found in 2 Hood Half 205481 Item (1)
a Replace the Hood Halves. (Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA). b Make sure that all broken parts and unwanted materials are removed from the related tank.
c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ). (c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings - Reporting Sheet ). **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 286106-942-401-001 - CLOSE-UP Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 (a) Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING (Fuel Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM 28-10-00, Page Block 301). **CONF 002 (1) Subtask 286106-942-401-001 - CLOSE-UP Manpower Resources Skills AIRFRAME

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 24 7

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# @A300-600 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 (a) Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING (Fuel Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM 28-10-00, Page Block 301).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 25 7

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# @A300-600 SERVICE BULLETIN

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DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 26 7

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# @A300-600 SERVICE BULLETIN
Task 286106-833-895-001 - REPAIR **CONF ALL 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. Task Associated Data **CONF 001 Manpower TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 **CONF 002 Manpower TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 286106-839-402-001 - ADMINISTRATIVE Manpower Resources Skills AIRFRAME Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 27 7

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# @A300-600 SERVICE BULLETIN
**CONF 002 (1) Subtask 286106-839-402-001 - ADMINISTRATIVE Manpower Resources Skills AIRFRAME Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 None **CONF 002 None **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 286106-833-401-001 - REPAIR THE FUEL PUMP CANISTER HOOD HALVES Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Equipment BFEB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 205481 2 HOODHALF (1) (2) NOTE (1) : One BFEB01 is required for each Fuel Pump Canister. The total quantity of BFE kits will be determined by the result of the inspection requirements of this Service Bulletin. NOTE (2) : Canister Hood PN 205481 for Fuel Pump Canister PN 2052C11 or PN 2052C12.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 28 7

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# @A300-600 SERVICE BULLETIN Equipment BFEB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 4 3C93-129 2 HOODHALF (1 ) (2) NOTE (1) : One BFEB02 is required for each Fuel Pump Canister. The total quantity of BFE kits will be determined by the result of the inspection requirements of this Service Bulletin. NOTE (2) : Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UCAAA Repair the Fuel Pump Canister Hood Halves - Typical Sheet 01
(a) Replace the fuel pump canister hood halves, do the steps that follow (Refer to Fig. A-UCAAA): 1 Clean the surface area of the fuel pump canister with a Lint-Free Cotton Cloth 19-003 As required
made moist with Solvent 11-583 As required

2 Remove: 6 Screw Item (2) Retain 6 Washer Item (3) Retain 2 Hood Half 205481 Item (1) Discard or 2 Hood Half 3C93-129 Item (4) Discard NOTE : If there are defective parts they must be replaced (Refer to the Vendor Intertechnique for replacement parts). NOTE : The discarded hood halves have to be replaced with a new ones with the same Part Number.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 29 7

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# @A300-600 SERVICE BULLETIN
3 Install the: 2 Hood Half 205481 Item 1 or with: 2 Hood Half 3C93-129 Item 4 6 Screw Item (2) Retained at removal 6 Washer Item (3) Retained at removal (b) Make sure that all broken parts and unwanted materials are removed from the related tank. **CONF 002 (1) Subtask 286106-833-401-001 - REPAIR THE FUEL PUMP CANISTER HOOD HALVES Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Equipment BFEB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 205481 2 HOODHALF (1) (2) NOTE (1) : One BFEB01 is required for each Fuel Pump Canister. The total quantity of BFE kits will be determined by the result of the inspection requirements of this Service Bulletin. NOTE (2) : Canister Hood PN 205481 for Fuel Pump Canister PN 2052C11 or PN 2052C12. Equipment BFEB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 4 3C93-129 2 HOODHALF (1 ) (2) NOTE (1) : One BFEB02 is required for each Fuel Pump Canister. The total quantity of BFE kits will be determined by the result of the inspection requirements of this Service Bulletin. DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 30 7

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# @A300-600 SERVICE BULLETIN
NOTE (2) : Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent 11-583 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UCAAA Repair the Fuel Pump Canister Hood Halves - Typical Sheet 01
(a) Replace the fuel pump canister hood halves, do the steps that follow (Refer to Fig. A-UCAAA): 1 Clean the surface area of the fuel pump canister with a Lint-Free Cotton Cloth 19-003 As required
made moist with Solvent 11-583 As required

2 Remove: 6 Screw Item (2) Retain 6 Washer Item (3) Retain 2 Hood Half 205481 Item (1) Discard or 2 Hood Half 3C93-129 Item (4) Discard NOTE : If there are defective parts they must be replaced (Refer to the Vendor Intertechnique for replacement parts). NOTE : The discarded hood halves have to be replaced with a new ones with the same Part Number. 3 Install the: 2 Hood Half 205481 Item 1 or with: 2 Hood Half 3C93-129 Item 4

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 31 7

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# @A300-600 SERVICE BULLETIN
6 Screw Item (2) Retained at removal 6 Washer Item (3) Retained at removal (b) Make sure that all broken parts and unwanted materials are removed from the related tank. **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 286106-942-402-001 - CLOSE-UP Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING (Fuel Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM 28-10-00, Page Block 301). **CONF 002 (1) Subtask 286106-942-402-001 - CLOSE-UP Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING (Fuel Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM 28-10-00, Page Block 301).
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 32 7

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# @A300-600 SERVICE BULLETIN

**CONF ALL

D_SB_286106_7_AAAA_01_03 YES NO INSPECTION OF CANISTER HOODS INSTALLED ON FUEL PUMP CANISTER P/Ns 2052C11

OR 2052C12 OR C93R51−601

REPORT

TO AIRBUS IS THE CANISTER

HOOD CRACKED?

REPLACE CANISTER

HOOD

RECORD LOCATION (FIN)

REPORT LOCATION (FIN)

TO AIRBUS

PERFORM REPEAT INSPECTION WITHIN

30 MONTHS OF

PREVIOUS INSPECTION PERFORM REPEAT INSPECTION WITHIN

30 MONTHS OF

PREVIOUS INSPECTION

Figure A-UAAAA - Sheet 01 Inspection Flowchart
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 33 7

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# @A300-600 SERVICE BULLETIN

**CONF ALL

LH WING SHOWN RH WING SIMILAR

FUEL PUMP CANISTER

TYPICAL DAMAGE HOOD HALF HOOD HALF SCREW AND

WASHER (6 OFF) 

### B **A**

RIB14 RIB2 Z550 (Z650) 

### A

TYPICAL 

## A FILTER Z540 (Z640)



## B D_SB_286106_7_BAAA_01_03 HOOD HALF

Figure A-U BAAA - Sheet 01 Fuel Pump Canister Hood Halves Inspection - Wing Tanks
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 34 7

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# @A300-600 SERVICE BULLETIN

**CONF ALL

− Z141 Z142 

### A

TYPICAL DAMAGE TYPICAL FR47 FR46

FUEL PUMP CANISTER

HOOD HALF HOOD HALF SCREW AND

WASHER (6 OFF) FILTER 

### B

**B**



## A

**B**

**C C** 

D_SB_286106_7_BCAA_01_02 HOOD HALF

Figure A-UBCAA - Sheet 01 Fuel Pump Canister Hood Halves Inspection - Center Tank
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 35 7

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# @A300-600 SERVICE BULLETIN

**CONF 002



### A − Z311 Z312 PUMP 2 CANISTER

VAPOR SEAL
PUMP 1 CANISTER

TYPICAL 319AB 319BZ

319BB 319AZ

FUEL PUMP CANISTER

HOOD HALF HOOD HALF SCREW AND

WASHER (6 OFF) FILTER 

### C

TYPICAL DAMAGE 

### B

**B**



## A

**B**

**C** D_SB_286106_7_BEAA_01_02 HOOD HALF

Figure A-U BEAA - Sheet 01 Fuel Pump Canister Hood Halves Inspection - Trim Tank
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 36 7

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# @A300-600 SERVICE BULLETIN

**CONF ALL

FUEL PUMP CANISTER



### A **A**



## A TYPICAL D_SB_286106_7_CAAA_01_01 

### (1) **1 (4)**  **4**

**(3) (2)**  **(3) (2)**  **(3) (2)** 

Figure A-UCAAA - Sheet 01 Repair the Fuel Pump Canister Hood Halves - Typical
DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 37 7

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# @A300-600 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 38 7

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# @A300-600 SERVICE BULLETIN Inspection Findings - Reporting Sheet **CONF 001 Complete the Table below by ticking the appropriate finding for each inspection location: SERVICE BULLETIN NO. A300-28-6106 A/C MSN: DATE OF INSPECTION FLIGHT HOURS: FLIGHT CYCLES FINDING LOCATION FIN YES NO 280014 280015 280016 280017 280018 280019 280020 280021 280022 280023 **CONF 002 SERVICE BULLETIN NO. A300-28-6106 A/C MSN: DATE OF INSPECTION FLIGHT HOURS: FLIGHT CYCLES FINDING LOCATION FIN YES NO 280014 280015 280016 280017 280018 280019 280020 280021 280022 280023 280432 280433

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A300-600 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD 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: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 1 7

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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 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - 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: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106 REVISION No.: 01 - Apr 15/11 Page: 1 7

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