@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

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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

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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

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173

REVISION No.: 01 - Apr 15/11 Page: 4

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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

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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

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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

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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

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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

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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

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

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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

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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

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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

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**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.

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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

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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

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SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jan 13/11 SERVICE BULLETIN No.: A310-28-2173

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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SERVICE BULLETIN

**CONF ALL

B_SB_282173_7_AAAA_01_03

NO YES

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

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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-UBAAA - 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

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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

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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-UBEAA - 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

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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

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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

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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

LOCATION FIN FINDING

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

LOCATION FIN FINDING

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

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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

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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

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