# @A310 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.A310-28-2173 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 Configuration definition CONFIGURATION LIST 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A310 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 282173- 832-895-001- INSPECTION TASK SOLUTION UPDATED NOTE UPDATED R Subtask 282173-832-401-001 SUBTASK SOLUTION UPDATED R Subtask 282173-832-403-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

Subtask 282173-832-401-001 SUBTASK SOLUTION UPDATED R Subtask 282173-832-403-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

Subtask 282173-832-404-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED R

TASK 282173- 833-895-001 -REPAIR Subtask 282173-833-401-001 SUBTASK SOLUTION UPDATED NOTE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 282173-833-401-001 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
DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 2 7

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 3 7

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

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DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 4 7

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# @A310 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 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 STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO DEFUEL/VENTILATION YES PRE-ENTRY CHECKLIST YES
DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A310 SERVICE BULLETIN SUMMARY 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) :

18T 19U 52X 58X 82Z 83V 85Z 98W 99Y AFG AIB AIC BAF BBC CFC DAH DEC DGA F2I FDX G8E GAF HFY I2L IRA IRM IYE JAB JAV K1P KAC KYV KZU MGL MWA PIA QAF R1T RJA ROT RZO SBI SGX SUD THY TSC UZB WHT WTJ 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 NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 2 7

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# @A310 SERVICE BULLETIN SUMMARY OBRM NO MANPOWER **CONF 001 Task 282173-832-895-001: INSPECTION TOTAL MANHOURS 9.00 ELAPSED TIME (HOURS) 5.00 Task 282173-833-895-001: REPAIR TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 **CONF 002 Task 282173-832-895-001: INSPECTION TOTAL MANHOURS 12.00 ELAPSED TIME (HOURS) 6.00 Task 282173-833-895-001: REPAIR TOTAL MANHOURS 0.50 ELAPSED TIME (HOURS) 0.50 APPENDICES **CONF ALL Inspection Findings - Reporting Sheet

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 3 7

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# @A310 SERVICE BULLETIN SUMMARY

**CONF 001

B_SB_282173_7_SAAA_01_01 

### B

LH WING SHOWN

RH WING SIMILAR RIB14 RIB2 Z550 (Z650)

TYPICAL Z540 (Z640) 

### A

FR47 FR46 

### C **C C** 

**C**



## C **A** − Z141 Z142



## B

Figure A-USAAA - Sheet 01 FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD - WING AND CENTER TANKS DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 4 7

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# @A310 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 Z319 

### C

**D**

319AB 319BZ

319BB 319AZ

B_SB_282173_7_SAAB_01_01 

### D

**D**



## 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 5 7

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# @A310 SERVICE BULLETIN SUMMARY

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 6 7

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# @A310 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 310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324 310-325 (2) Effectivity by MSN 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0257 0260 0264 0267 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0386 0389-0390 0392 0394 0399-0400 0406-0407 0410 0413 0416 0418-0419 0421-0422 0425 0427-0429 0431 0434 0436-0437 0439 0441 0444-0449 0452 0454 0456-0458 0467 0472-0473 0475-0476 0478 0480-0492 0494-0500 0502-0503 0519-0520 0522-0524 0526-0527 0531 0534 0537-0539 0541-0542 0544-0545 0547 0549-0552 0562 0564-0565 0567-0568 0571 0573-0574 0576 0585-0588 0590-0595 0597 0599-0600 0620 0622 0624 0636 0638 0640 0642 0644 0646-0654 0656 0658 0660-0661 0663 0665 0667 0669 0671-0672 0674 0676 0678 0680 0682 0684 0686-0687 0689 0691 0693 0697 0700 0702 0704 0706

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A310 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 18T 0473 19U 0399 52X 0410 58X 0431 82Z 0550 0551 83V 0427 85Z 0547 98W 0416 0672 99Y 0489 AFG 0496 0497 AIB 0650 0674 0686 AIC 0392 0406 0407 0413 0428 0429 0538 0544 0654 0665 0669 0680 BAF 0367 0372 BBC 0594 0642 0700 CFC 0425 0441 0444 0446 0482 DAH 0291 0293 DEC 0684 0693 0697 DGA 0418 0421 0422 F2I 0309 0419 0487 FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0257 0260 0264 0267 0278 0281 0283 0288 0297 0303 0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346 0353 0355 0356 0359 0360 0362 0364 0369 0378 0394 0400 0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539 0542 0549 0552 0593 0638 G8E 0475 GAF 0434 0484 0498 0499 0503 0522 0523 HFY 0495 0565 I2L 0640 IRA 0338 0370 0375 0379 0389 0390 0436 0671 IRM 0488 0524 0537 0564 0567 0586 0595 0620 IYE 0568 0702 0704 JAB 0320 JAV 0357 0481 K1P 0648 KAC 0647 0649 0663 KYV 0386 KZU 0592 0622 0646 MGL 0526 MWA 0652 DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 2 7

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# @A310 SERVICE BULLETIN
OPERATOR MSN PIA 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689 0691 QAF 0667 R1T 0591 RJA 0445 0490 0491 0531 ROT 0636 0644 RZO 0571 0624 0651 0661 SBI 0486 0520 SGX 0519 0562 SUD 0437 THY 0476 0478 0480 0502 TSC 0447 0472 0483 0485 0527 0541 0545 0588 0597 0599 0600 0658 UZB 0574 0576 0706 WHT 0448 0573 WTJ 0494 (4) Configuration by MSN MSN CONFIGURATION 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0257 0260 0264 0267 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333 0335 0338 0339 0342 0343 0345 0346 0353 0355 0356 0357 0359 0360 0362 0364 0367 0369 0370 0372 0375 0379 0386 0389 0390 0394 0400 0419 0427 0454 0486 0487 001

0378 0392 0399 0406 0407 0410 0413 0416 0418 0421 0422 0425 0428 0429 0431 0434 0436 0437 0439 0441 0444 0445 0446 0447 0448 0449 0452 0456 0457 0458 0467 0472 0473 0475 0476 0478 0480 0481 0482 0483 0484 0485 0488 0489 0490 0491 0492 0494 0495 0496 0497 0498 0499 0500 0502 0503 0519 0520 0522 0523 0524 0526 0527 0531 0534 0537 0538 0539 0541 0542 0544 0545 0547 0549 0550 0551 0552 0562 0564 0565 0567 0568 0571 0573 0574 0576 0585 0586 0587 0588 0590 0591 0592 0593 0594 0595 0597 0599 0600 0620 0622 0624 0636 0638 0640 0642 0644 0646 0647 0648 0649 0650 0651 0652 0653 0654 0656 0658 0660 0661 0663 0665 0667 0669 0671 0672 0674 0676 0678 0680 0682 0684 0686 0687 0689 0691 0693 0697 0700 0702 0704 0706 002

(5) Configuration definition NOTE : This Service Bulletin is only applicable to A310 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 A310-200 aircraft in the effectivity - aircraft without a trim tank.

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 3 7

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# @A310 SERVICE BULLETIN
**CONF 002 Config. 002 is applicable to all A310-300 aircraft in the effectivity - aircraft with a trim tank. (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 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 4 7

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# @A310 SERVICE BULLETIN
**CONF 001 Task 282173-832-895-001: INSPECTION (1) INSPECTION OF THE WING (INNER/OUTER) FUEL PUMP CANISTER HOOD HALVES (2) INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (IF FITTED) Task 282173-833-895-001: REPAIR (1) REPAIR OF THE FUEL PUMP CANISTER HOOD HALVES **CONF 002 Task 282173-832-895-001: INSPECTION (1) INSPECTION OF THE WING (INNER/OUTER) FUEL PUMP CANISTER HOOD HALVES (2) INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (IF FITTED) (3) INSPECTION OF THE TRIM TANK TRANSFER PUMP CANISTER HOODS Task 282173-833-895-001: REPAIR (1) REPAIR OF 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 you receive 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 5 7

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# @A310 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 282173-832-895-001: INSPECTION Get Access 2.00 On Aircraft INSPECTION OF THE WING (INNER/OUTER) FUEL PUMP CANISTER HOOD HALVES 4.00 INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (IF FITTED) 1.00 Tests 0.00 Close-Up 2.00 TOTAL MANHOURS 9.00 ELAPSED TIME (HOURS) 5.00 Task 282173-833-895-001: REPAIR Get Access 0.00 On Aircraft REPAIR OF 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 282173-832-895-001: INSPECTION Get Access 3.00 On Aircraft INSPECTION OF THE WING (INNER/OUTER) FUEL PUMP CANISTER HOOD HALVES 4.00 INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (IF FITTED) 1.00 INSPECTION OF THE TRIM TANK TRANSFER PUMP CANISTER HOODS 1.00

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 6 7

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# @A310 SERVICE BULLETIN

Task 282173-832-895-001: INSPECTION Tests 0.00 Close-Up 3.00 TOTAL MANHOURS 12.00 ELAPSED TIME (HOURS) 6.00 Task 282173-833-895-001: REPAIR Get Access 0.00 On Aircraft REPAIR OF 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 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 28-27-12 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 7 7

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# @A310 SERVICE BULLETIN
L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 8 7

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# @A310 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 As required Lint-Free Cotton Cloth 19-003 As required (2) Components None (3) Equipment Equipment BFEB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 205481 2 HOOD (1) 205481 (1) (2) (1) (2)

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 9 7

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# @A310 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 HOOD (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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 10 7

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# @A310 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 282173-832-895-001 - 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 147AZ 148AZ 540AB 550AB 640AB 650AB 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 147AZ 148AZ 319AZ 319BZ 540AB 550AB 640AB 650AB Manpower TOTAL MANHOURS 12.00
DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 11 7

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# @A310 SERVICE BULLETIN ELAPSED TIME (HOURS) 6.00 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 282173-910-401-001 - STANDARD PRACTICES Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-41-53 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 06-41-57, Page Block 001 and AMM 06-41-53). (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 282173-839-401-001 - 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 282173-910-401-001 - STANDARD PRACTICES Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-41-53 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 06-41-57, Page Block 001 and AMM 06-41-53).
DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 12 7

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# @A310 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 282173-839-401-001 - 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 282173-941-401-001 - JOB SET-UP - WING AND CENTER TANKS (IF FITTED) Work Zones and Access Panels Zone Access/Work location 141 Access Door 147AZ 142 Access Door 148AZ 540 Access Door 540AB 640 Access Door 640AB 550 Access Door 550AB 650 Access Door 650AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 28-11-22, Page Block 401 28-11-29, 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.

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 13 7

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# @A310 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) Put platforms in position to get access to the applicable zones: 1 Wing tanks inner - Zones 540 LH (640 RH) 2 Wing tanks outer - Zones 550 LH (650 RH) 3 Center tank (if fitted) - Zones 141 and 142. (c) Remove the applicable manhole covers: 1 Wing tanks inner 540AB LH (640AB RH) (Refer to AMM 28-11-22, Page Block 401). 2 Wing tanks outer 550AB LH (650AB RH) (Refer to AMM 28-11-22, Page Block 401). 3 Center tank (if fitted) 147AZ LH and 148AZ RH (Refer to AMM 28-11-29, Page Block 401). (d) 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 282173-941-401-001 - JOB SET-UP - WING AND CENTER TANKS (IF FITTED) Work Zones and Access Panels Zone Access/Work location 141 Access Door 147AZ 142 Access Door 148AZ 540 Access Door 540AB 640 Access Door 640AB 550 Access Door 550AB 650 Access Door 650AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 28-11-22, Page Block 401 28-11-29, Page Block 401 Consumable Material List (CML)

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 14 7

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# @A310 SERVICE BULLETIN
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) Put platforms in position to get access to the applicable zones: 1 Wing tanks inner - Zones 540 LH (640 RH) 2 Wing tanks outer - Zones 550 LH (650 RH) 3 Center tank (if fitted) - Zones 141 and 142. (c) Remove the applicable manhole covers: 1 Wing tanks inner 540AB LH (640AB RH) (Refer to AMM 28-11-22, Page Block 401). 2 Wing tanks outer 550AB LH (650AB RH) (Refer to AMM 28-11-22, Page Block 401). 3 Center tank (if fitted) 147AZ LH and 148AZ RH (Refer to AMM 28-11-29, Page Block 401). (d) For the specification of materials (Mat. No.) that you must use in this Service Bulletin refer to Consumable Materials List (CML). (2) Subtask 282173-941-404-001 - JOB SET-UP - TRIM TANK Work Zones and Access Panels Zone Access/Work location 311 Access Door 319AZ 312 Access Door 319BZ Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301 28-27-12, Page Block 401 Consumable Material List (CML)

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 15 7

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# @A310 SERVICE BULLETIN
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). (b) Put platforms in position to get access to the applicable zones: 1 Trim tank - Zones 311 and 312. (c) Remove the applicable manhole covers: 1 Trim tank transfer pump canisters 319AZ and 319BZ (Refer to AMM 28-27-12, Page Block 401). (d) 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. **CONF 001 (1) Subtask 282173-832-401-001 - INSPECTION OF THE WING (INNER/OUTER) FUEL 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

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 16 7

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# @A310 SERVICE BULLETIN
References Fig. A-UAAAA Inspection Flowchart Sheet 01 Fig. A-UCAAA Repair The Fuel Pump Canister Hood Halves - Typical Sheet 01 Fig. A-UBAAA Fuel Pump Canister Hood Halves Inspection - Wing Tanks 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 FIN 280018 and FIN 280020 - Wing tank (RH) - inboard FIN 280015 and FIN 280017 and outboard FIN 280019 and FIN 280021. (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 282173-833-895 001 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 ).

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 17 7

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# @A310 SERVICE BULLETIN (c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings - Reporting Sheet ). (2) Subtask 282173-832-403-001 - INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (IF FITTED) 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
(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 (if fitted) - LH FIN 280022 and RH FIN 280023 (Refer to Fig. A-UAAAA and Fig. A-UBCAA).
DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 18 7

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# @A310 SERVICE BULLETIN
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 282173-833-895 001 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 002 (1) Subtask 282173-832-401-001 - INSPECTION OF THE WING (INNER/OUTER) FUEL 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 Fig. A-UAAAA Inspection Flowchart Sheet 01

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 19 7

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# @A310 SERVICE BULLETIN
References Fig. A-UCAAA Repair The Fuel Pump Canister Hood Halves - Typical Sheet 01 Fig. A-UBAAA Fuel Pump Canister Hood Halves Inspection - Wing Tanks 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 FIN 280018 and FIN 280020 - Wing tank (RH) - inboard FIN 280015 and FIN 280017 and outboard FIN 280019 and FIN 280021. (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 282173-833-895 001 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 20 7

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# @A310 SERVICE BULLETIN (2) Subtask 282173-832-403-001 - INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (IF FITTED) 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
(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 (if fitted) - LH FIN 280022 and RH FIN 280023 (Refer to Fig. A-UAAAA and Fig. A-UBCAA).

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 21 7

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# @A310 SERVICE BULLETIN
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 282173-833-895 001 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 ). (3) Subtask 282173-832-404-001 - INSPECTION OF THE TRIM TANK TRANSFER PUMP CANISTER HOODS 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-UAAAA Inspection Flowchart Sheet 01

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 22 7

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# @A310 SERVICE BULLETIN
References Fig. A-UBEAA Fuel Pump Canister Hood Halves Inspection - Trim Tank 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 ). 2 Cracks are found in 2 Hood Half 205481 Item (1)
a Replace the Hood Halves. (Refer to TASK 282173-833-895 001 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 23 7

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# @A310 SERVICE BULLETIN
**CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 282173-942-401-001 - 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 282173-942-401-001 - 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).

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 24 7

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# @A310 SERVICE BULLETIN
Task 282173-833-895-001 - 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 282173-839-402-001 - 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 25 7

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 282173-839-402-001 - 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 282173-833-401-001 - REPAIR OF 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 HOOD (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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 26 7

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# @A310 SERVICE BULLETIN
Equipment BFEB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 4 3C93-129 2 HOOD (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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 27 7

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# @A310 SERVICE BULLETIN
3 Install the: 2 Hood Half 205481 Item 1 or 2 Hood Half 3C93-129 Item 4 with: 6 Screw Item (2) Retained at removal 6 Washer Item (3) Retained at removal 4 Make sure that all broken parts and unwanted materials are removed from the related tank. **CONF 002 (1) Subtask 282173-833-401-001 - REPAIR OF 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 HOOD (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 HOOD (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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 28 7

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# @A310 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 2 Hood Half 3C93-129 Item 4 with:

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 29 7

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# @A310 SERVICE BULLETIN
6 Screw Item (2) Retained at removal 6 Washer Item (3) Retained at removal 4 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 282173-942-402-001 - 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 282173-942-402-001 - 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 30 7

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# @A310 SERVICE BULLETIN

**CONF ALL

B_SB_282173_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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 31 7

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# @A310 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 B_SB_282173_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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 32 7

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# @A310 SERVICE BULLETIN

**CONF ALL

TYPICAL DAMAGE TYPICAL FR47 FR46

FUEL PUMP CANISTER

HOOD HALF HOOD HALF SCREW AND

WASHER (6 OFF) FILTER 

### B

**B**



## A

**B**

**C C**  − Z141 Z142 

### A

B_SB_282173_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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 33 7

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# @A310 SERVICE BULLETIN

**CONF 002

PUMP 2 CANISTER

VAPOR SEAL

PUMP 1 CANISTER 

### A

TYPICAL 319AB 319BZ

319BB 319AZ − Z311 Z312

FUEL PUMP CANISTER

HOOD HALF HOOD HALF SCREW AND

WASHER (6 OFF) FILTER 

### C

TYPICAL DAMAGE 

### B

**B**



## A

**B**

**C** B_SB_282173_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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 34 7

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# @A310 SERVICE BULLETIN

**CONF ALL

FUEL PUMP CANISTER



### A **A**



## A TYPICAL B_SB_282173_7_CAAA_01_01 

### (1) **1 (4)**  **4 (3)**  **(2)**

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

Figure A-UCAAA - Sheet 01 Repair The Fuel Pump Canister Hood Halves - Typical
DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 35 7

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# @A310 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 36 7

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# @A310 SERVICE BULLETIN Inspection Findings - Reporting Sheet **CONF 001 Complete the Table below by ticking the appropriate finding for each inspection location: SERVICE BULLETIN NO. A310-28-2173 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 Complete the Table below by ticking the appropriate finding for each inspection location: SERVICE BULLETIN NO. A310-28-2173 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A310 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 1 7

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# @A310 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.: A310-28-2173 REVISION No.: 01 - Apr 15/11 Page: 1 7

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