@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP

CANISTER HOOD

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A300-28-6106

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 01 issued to add the Equipment BFEB02 for the Canister Hood PN 3C93-129 (part of Fuel

Pump Canister PN C93R51-601).

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Material Effectivity MATERIAL EFFECTIVITY UPDATED R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET QUANTITY UPDATED

MATERIAL SET UPDATED

R

REASON

Objective/Action OBJECTIVE/ACTION UPDATED R

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 1

7

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@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Equipment EQUIPMENT UPDATED R

Equipement BFEB01 PART MATERIAL SET UPDATED

NOTE UPDATED

R

Equipement BFEB02 PART MATERIAL SET ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 286106- 832-895-001-INSPECTION TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 286106-941-402-001 SUBTASK SOLUTION UPDATED R

Subtask 286106-832-401-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

Subtask 286106-832-402-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

Subtask 286106-832-401-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

Subtask 286106-832-402-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

Subtask 286106-832-403-002 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

TASK 286106- 833-895-001-REPAIR

Subtask 286106-833-401-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 2

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@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 286106-833-401-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Fig. A-UAAAA

Fig. A-UAAAA Sheet 01 SHEET UPDATED R

Fig. A-UBAAA

Fig. A-UBAAA Sheet 01 SHEET UPDATED R

Fig. A-UBCAA

Fig. A-UBCAA Sheet 01 SHEET UPDATED R

Fig. A-UBEAA

Fig. A-UBEAA Sheet 01 SHEET UPDATED R

Fig. A-UCAAA

Fig. A-UCAAA Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Jan 13/11

REVISION No. : 01 - Apr 15/11

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 3

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@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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

7

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

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP

CANISTER HOOD

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Some operators have reported cases of cracking on the hood of the inboard and outboard fuel pump

canisters located in the inner fuel tanks. The hood is part of the fuel pump canister and forms a surface

between the pump inlet mesh and the canister body. The hood is fabricated from thin aluminium alloy in

two halves.

On one aircraft the detached parts were reported as consisting of two separate pieces. One annular

section was subsequently found inside the fuel tank.

This Inspection Service Bulletin (ISB) introduces a repetitive Detailed Visual Inspection (DVI) of all fuel

pump locations (center, wing inner, wing outer and trim tank). The inspection will also assess which

locations are subject to such cracking, and which hoods must be replaced. The Inspection must be

done not more than 30 months after the issue date of this Service Bulletin and repeated every 30

months.

Replacement of failed hood halves will prevent possible contamination issues and establish which

locations are subject to cracking. Replace both hood halves if cracks are found in one of the two

halves. You must find and remove all broken pieces from the fuel tanks.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 1

7

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

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

DEFUEL/VENTILATION YES PRE-ENTRY CHECKLIST YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEB01 1 See SB Hood Halves

Equipment BFEB02 1 See SB Hood Halves

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEB01 1 See SB Hood Halves

Equipment BFEB02 1 See SB Hood Halves

EFFECTIVITY

**CONF ALL

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

30T 83V 98W AAL AAW ABD AHK AMU CES CSN F2I FDX G8E

IRA IRM JAL KAC KAL LAA MNB MON MSR MXU OHY QTR SUD

TAR THA TMA UPS UZB

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 28.21.13.001

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 2

7

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

SERVICE BULLETIN

SUMMARY

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 286106-832-895-001: INSPECTION

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 5.00

Task 286106-833-895-001: REPAIR

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

**CONF 002

Task 286106-832-895-001: INSPECTION

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Task 286106-833-895-001: REPAIR

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

APPENDICES

**CONF ALL

Inspection Findings - Reporting Sheet

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 3

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

SERVICE BULLETIN

SUMMARY

**CONF 001

LH WING SHOWN

RH WING SIMILAR

RIB14

RIB2

Z550 (Z650)

TYPICAL

Z540 (Z640) FR47

FR46

C

C

C

C

C

A

B

B

A

Z141 Z142 − 

D_SB_286106_7_SAAA_01_00

Figure A-USAAA - Sheet 01

FUEL - FUEL PUMP SY STEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD - WING AND

CENTER TANKS

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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

7

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

SERVICE BULLETIN

SUMMARY

**CONF 002

B

PUMP 2

CANISTER

PUMP 1

CANISTER

LH WING SHOWN

RH WING SIMILAR

RIB14

RIB2

Z550 (Z650)

TYPICAL

Z540 (Z640)

A

FR47

FR46 A

Z141 Z142 − 

B

D

D

D

D

D

319AB

319BZ

319BB

319AZ

D

D

C

D_SB_286106_7_SAAB_01_01

Z319

C

Figure A-USAAB - Sheet 01

FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP CANISTER HOOD - WING,

CENTER AND TRIM TANKS

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 5

7

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

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 6

7

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

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP

CANISTER HOOD

MODIFICATION No.: None

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/FC4-620 F4-605R

F4-622R

(2) Effectivity by MSN

0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0354 0358 0361 0365

0380 0388 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0470 0474 0477

0479 0505-0518 0521 0525 0529-0530 0532 0536 0540 0543 0546 0553-0561 0563

0566 0569 0572 0575 0577 0579 0581-0582 0584 0601-0618 0621 0623 0625-0633

0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670 0673 0675

0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709

0711 0713 0715 0717 0719 0721-0750 0752-0764 0766-0775 0777-0794 0797

0799-0841 0845-0878

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 1

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@A300-600

SERVICE BULLETIN

(3) Effectivity by Operator

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

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

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

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

OPERATOR MSN

30T 0626 0643

83V 0423 0459 0460 0463 0466 0470 0474 0510 0511 0512 0615 0639

0675

98W 0740

AAL 0506 0507 0508 0513 0515 0517 0612

AAW 0354

ABD 0529 0557

AHK 0855 0856 0857 0858 0859 0860 0870 0871

AMU 0677 0743

CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763

CSN 0733 0734 0739 0756

F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0461 0606

0610 0637 0645 0711 0724

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

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

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

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

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

0800 0801 0802 0803 0804 0873 0874 0875 0876 0877 0878

G8E 0462 0465 0469 0509 0514 0516

IRA 0632 0696 0723 0727

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

0750 0762 0773

JAL 0602 0617 0621 0641 0670 0679 0683 0703 0729 0730 0737 0753

0770 0783 0797 0836 0837 0838

KAC 0344 0673 0694 0699 0719 0721

KAL 0582 0609 0627 0631 0662 0685 0692 0731

LAA 0601 0616

MNB 0755 0758

MON 0540 0556 0604 0605

MSR 0561 0607

MXU 0767 0788

OHY 0584 0603 0744 0747 0749 0764

QTR 0554 0560 0614

SUD 0666 0775

TAR 0505 0558 0563

THA 0464 0518 0566 0569 0577 0628 0629 0635 0681 0705 0782 0784

0785 0786 0787

TMA 0872

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 2

7

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@A300-600

SERVICE BULLETIN

OPERATOR MSN

UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816

0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828

0829 0830 0831 0832 0833 0834 0835 0839 0840 0841 0845 0846

0847 0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864

0865 0866 0867 0868 0869

UZB 0717 0722

(4) Configuration by MSN

MSN CONFIGURATION

0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351

0354 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414

0417 0546 0553 0618 0623

001

0423 0459 0460 0461 0462 0463 0464 0465 0466 0469 0470

0474 0477 0479 0505 0506 0507 0508 0509 0510 0511 0512

0513 0514 0515 0516 0517 0518 0521 0525 0529 0530 0532

0536 0540 0543 0554 0555 0556 0557 0558 0559 0560 0561

0563 0566 0569 0572 0575 0577 0579 0581 0582 0584 0601

0602 0603 0604 0605 0606 0607 0608 0609 0610 0611 0612

0613 0614 0615 0616 0617 0621 0625 0626 0627 0628 0629

0630 0631 0632 0633 0635 0637 0639 0641 0643 0645 0657

0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681

0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707

0709 0711 0713 0715 0717 0719 0721 0722 0723 0724 0725

0726 0727 0728 0729 0730 0731 0732 0733 0734 0735 0736

0737 0738 0739 0740 0741 0742 0743 0744 0745 0746 0747

0748 0749 0750 0752 0753 0754 0755 0756 0757 0758 0759

0760 0761 0762 0763 0764 0766 0767 0768 0769 0770 0771

0772 0773 0774 0775 0777 0778 0779 0780 0781 0782 0783

0784 0785 0786 0787 0788 0789 0790 0791 0792 0793 0794

0797 0799 0800 0801 0802 0803 0804 0805 0806 0807 0808

0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819

0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830

0831 0832 0833 0834 0835 0836 0837 0838 0839 0840 0841

0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0855

0856 0857 0858 0859 0860 0861 0862 0863 0864 0865 0866

0867 0868 0869 0870 0871 0872 0873 0874 0875 0876 0877

0878

002

(5) Configuration definition

NOTE: This Service Bulletin is only applicable to A300-600 aircraft that have

Fuel Pump Canister Hood PN 205481 (part of Fuel Pump Canister PN

2052C11 or PN 2052C12) or PN 3C93-129 (part of Fuel Pump Canister

PN C93R51-601) installed

**CONF 001

Config. 001 is applicable to all A300-600 aircraft - aircraft without a trim tank.

**CONF 002

Config. 002 is applicable to all A300-600R aircraft - aircraft with a trim tank.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 3

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@A300-600

SERVICE BULLETIN

(6) Material Effectivity

NOTE: One BFEB01 or BFEB02 is required for each Fuel Pump Canister. The

total quantity of BFE kits will be determined by the result of the

inspection requirements of this Service Bulletin.

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEB01 1

Equipment BFEB02 1

Consumable CMLB01 As required

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Some operators have reported cases of cracking on the hood of the inboard and

outboard fuel pump canisters located in the inner fuel tanks. The hood is part of the fuel

pump canister and forms a surface between the pump inlet mesh and the canister body.

The hood is fabricated from thin aluminium alloy in two halves.

On one aircraft the detached parts were reported as consisting of two separate pieces.

One annular section was subsequently found inside the fuel tank.

(2) Objective/Action

This Inspection Service Bulletin (ISB) introduces a repetitive Detailed Visual Inspection

(DVI) of all fuel pump locations (center, wing inner, wing outer and trim tank). The

inspection will also assess which locations are subject to such cracking, and which

hoods must be replaced. The Inspection must be done not more than 30 months after

the issue date of this Service Bulletin and repeated every 30 months.

(3) Advantages

Replacement of failed hood halves will prevent possible contamination issues and

establish which locations are subject to cracking. Replace both hood halves if cracks are

found in one of the two halves. You must find and remove all broken pieces from the

fuel tanks.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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

7

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

SERVICE BULLETIN

**CONF 001

Task 286106-832-895-001: INSPECTION

(1) INSPECTION OF THE WING TANKS (INNER/OUTER) PUMP CANISTER HOOD

HALVES

(2) INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES

Task 286106-833-895-001: REPAIR

(1) REPAIR THE FUEL PUMP CANISTER HOOD HALVES

**CONF 002

Task 286106-832-895-001: INSPECTION

(1) INSPECTION OF THE WING TANKS (INNER/OUTER) PUMP CANISTER HOOD

HALVES

(2) INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES

(3) INSPECTION OF THE TRIM TANK TRANSFER PUMP CANISTER HOOD HALVES

Task 286106-833-895-001: REPAIR

(1) REPAIR THE FUEL PUMP CANISTER HOOD HALVES

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Do this Inspection not more than 30 months after the date of issue of this Service

Bulletin and repeat every 30 months.

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the

issue of an Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals

and/or date) given above but reference should be made to the AD for confirmation of the

mandated accomplishment timescale.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 21J.031.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 5

7

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

SERVICE BULLETIN

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

**CONF 001

Task 286106-832-895-001: INSPECTION

Get Access 2.00

On Aircraft

INSPECTION OF THE WING TANKS (INNER/OUTER)

PUMP CANISTER HOOD HALVES

4.00

INSPECTION OF THE CENTER TANK PUMP

CANISTER HOOD HALVES

1.00

Tests 0.00

Close-Up 2.00

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 5.00

Task 286106-833-895-001: REPAIR

Get Access 0.00

On Aircraft

REPAIR THE FUEL PUMP CANISTER HOOD

HALVES

0.50

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

**CONF 002

Task 286106-832-895-001: INSPECTION

Get Access 3.00

On Aircraft

INSPECTION OF THE WING TANKS (INNER/OUTER)

PUMP CANISTER HOOD HALVES

4.00

INSPECTION OF THE CENTER TANK PUMP

CANISTER HOOD HALVES

1.00

INSPECTION OF THE TRIM TANK TRANSFER PUMP

CANISTER HOOD HALVES

1.00

Tests 0.00

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 6

7

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

SERVICE BULLETIN

Task 286106-832-895-001: INSPECTION

Close-Up 3.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Task 286106-833-895-001: REPAIR

Get Access 0.00

On Aircraft

REPAIR THE FUEL PUMP CANISTER HOOD

HALVES

0.50

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-21-00 06-41-53 06-41-57

28-00-00 28-10-00 28-11-22

28-11-29 28-25-00

Consumable Material List (CML)

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

**CONF 002

Aircraft Maintenance Manual (AMM) 06-21-00 06-41-53 06-41-57

28-00-00 28-10-00 28-11-22

28-11-29 28-25-00 28-27-12

Consumable Material List (CML)

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

**CONF ALL

K. PUBLICATION AFFECTED

None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 7

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SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 8

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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 0

Lint-Free Cotton Cloth 19-003 0

(2) Components

None

(3) Equipment

Equipment BFEB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 205481 2 HOODHALF (1) 205481 (1) (2) (1)

(2)

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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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 HOODHALF (4) 3C93-129 (1) (2) (1)

(2)

NOTE (1): One BFEB02 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 10

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@A300-600

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 286106-832-895-001 - INSPECTION

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

**CONF 001

Zone

141 142 540 550 640 650

Modified FIN

280014 280015 280016 280017 280018 280019 280020 280021 280022 280023

Access

Door 142AZ 147AZ 542CB 550BB 642CB 650BB

Manpower

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 5.00

**CONF 002

Zone

141 142 311 312 540 550 640 650

Modified FIN

280014 280015 280016 280017 280018 280019 280020 280021 280022 280023

280432 280433

Access

Door 142AZ 147AZ 319AZ 319BZ 542CB 550BB 642CB 650BB

Manpower

TOTAL MANHOURS 12.00

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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SERVICE BULLETIN

ELAPSED TIME (HOURS) 6.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 286106-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

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

06-41-53, Page Block 001

06-41-57, Page Block 001

28-00-00, Page Block 301

28-10-00, Page Block 301

(a) For the identification of Access Panels (Refer to AMM 06-41-53, Page Block 001

and AMM 06-41-57, Page Block 001).

(b) For the identification of Zones (Refer to AMM 06-21-00, Page Block 001).

(c) Obey the safety procedures when you do work in a fuel tank (Refer to AMM

28-10-00, Page Block 301 and AMM 28-00-00, Page Block 301).

(2) Subtask 286106-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

**CONF 002

(1) Subtask 286106-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

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

06-41-53, Page Block 001

06-41-57, Page Block 001

28-00-00, Page Block 301

28-10-00, Page Block 301

(a) For the identification of Access Panels (Refer to AMM 06-41-53, Page Block 001

and AMM 06-41-57, Page Block 001).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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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 286106-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 286106-941-401-001 - JOB SET-UP - WING AND CENTER TANK

Work Zones and Access Panels

Zone Access/Work location

141 Access Door 147AZ

142 Access Door 142AZ

540 Access Door 542CB

640 Access Door 642CB

550 Access Door 550BB

650 Access Door 650BB

Manpower Resources

Skills AIRFRAME

References

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

28-10-00, Page Block 301

28-11-22, Page Block 401

28-11-29, Page Block 401

28-25-00, Page Block 301

Consumable Material List (CML)

WARNING: YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO

WORK IN OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE

SAFETY PROCEDURES, THERE IS A RISK OF:

- DEATH OR INJURY TO PERSONS

- DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 13

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(a) Prepare the aircraft as specified in AMM Task ’STORAGE - SERVICING (Fuel

Tank Draining, Venting and Entry)’ (Refer to AMM 28-10-00, Page Block 301).

1 Before you go into a fuel tank you must complete the Pre-Entry Checklist

(Refer to AMM 28-10-00, Page Block 301).

(b) Defuel all of the aircraft fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(c) Put platforms in position to get access to the applicable zones (Refer to AMM

06-21-00, Page Block 001):

1 Wing tanks inner - Zones 540 LH (640 RH)

2 Wing tanks outer - Zones 550 LH (650 RH)

3 Center tank - Zones 141 and 142

(d) Remove the applicable manhole covers:

1 Wing tanks inner 542CB LH (642CB RH) (Refer to AMM 28-11-22, Page Block

401)

2 Wing tanks outer 550BB LH (650BB RH) (Refer to AMM 28-11-22, Page Block

401)

3 Center tank canisters 147AZ LH and 148AZ RH (Refer to AMM 28-11-29,

Page Block 401).

(e) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

**CONF 002

(1) Subtask 286106-941-401-001 - JOB SET-UP - WING AND CENTER TANK

Work Zones and Access Panels

Zone Access/Work location

141 Access Door 147AZ

142 Access Door 142AZ

540 Access Door 542CB

640 Access Door 642CB

550 Access Door 550BB

650 Access Door 650BB

Manpower Resources

Skills AIRFRAME

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 14

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SERVICE BULLETIN

References

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

28-10-00, Page Block 301

28-11-22, Page Block 401

28-11-29, Page Block 401

28-25-00, Page Block 301

Consumable Material List (CML)

WARNING: YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO

WORK IN OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE

SAFETY PROCEDURES, THERE IS A RISK OF:

- DEATH OR INJURY TO PERSONS

- DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT.

(a) Prepare the aircraft as specified in AMM Task ’STORAGE - SERVICING (Fuel

Tank Draining, Venting and Entry)’ (Refer to AMM 28-10-00, Page Block 301).

1 Before you go into a fuel tank you must complete the Pre-Entry Checklist

(Refer to AMM 28-10-00, Page Block 301).

(b) Defuel all of the aircraft fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(c) Put platforms in position to get access to the applicable zones (Refer to AMM

06-21-00, Page Block 001):

1 Wing tanks inner - Zones 540 LH (640 RH)

2 Wing tanks outer - Zones 550 LH (650 RH)

3 Center tank - Zones 141 and 142

(d) Remove the applicable manhole covers:

1 Wing tanks inner 542CB LH (642CB RH) (Refer to AMM 28-11-22, Page Block

401)

2 Wing tanks outer 550BB LH (650BB RH) (Refer to AMM 28-11-22, Page Block

401)

3 Center tank canisters 147AZ LH and 148AZ RH (Refer to AMM 28-11-29,

Page Block 401).

(e) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(2) Subtask 286106-941-402-001 - JOB SET-UP - TRIM TANK

Work Zones and Access Panels

Zone Access/Work location

311 Access Door 319AZ

312 Access Door 319BZ

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301

28-25-00, Page Block 301

28-27-12, Page Block 401

Consumable Material List (CML)

WARNING: YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO

WORK IN OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE

SAFETY PROCEDURES, THERE IS A RISK OF:

- DEATH OR INJURY TO PERSONS

- DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT.

(a) Prepare the aircraft as specified in AMM Task ’STORAGE - SERVICING (Fuel

Tank Draining, Venting and Entry)’ (Refer to AMM 28-10-00, Page Block 301).

1 Before you go into a fuel tank you must complete the Pre-Entry Checklist

(Refer to AMM 28-10-00, Page Block 301).

(b) Defuel all of the aircraft fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(c) Put platforms in position to get access to the applicable zones:

1 Trim tank - Zones 311 and 312.

(d) Remove the applicable manhole covers:

1 Trim tank transfer pump canisters 319AZ and 319BZ (Refer to AMM 28-27-12,

Page Block 401).

(e) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

**CONF ALL

C. PROCEDURE

NOTE: Operators can have the Fuel Pump Canister Hood PN 205481 (part of Fuel

Pump Canister PN 2052C11 or PN 2052C12) or PN 3C93-129 (part of Fuel

Pump Canister PN C93R51-601) installed.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 16

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**CONF 001

(1) Subtask 286106-832-401-001 - INSPECTION OF THE WING TANKS (INNER/OUTER)

PUMP CANISTER HOOD HALVES

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Consumable Material List (CML)

Fig. A-UAAAA

Inspection Flowchart

Sheet 01

Fig. A-UBAAA

Fuel Pump Canister Hood Halves

Inspection - Wing Tanks

Sheet 01

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

(a) Clean the

2 Hood Half 205481 Item (1)

with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

(b) Do a Detailed Visual Inspection (DVI) of the fuel pump canister hood halves in the

wing tanks:

- Wing tank (LH) - inboard FIN 280014 and FIN 280016 and outboard

FIN280018 and FIN 280020.

- Wing tank (RH) - inboard FIN 280015 and FIN 280017 and outboard FIN

280019 and FIN 280021.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 17

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SERVICE BULLETIN

(Refer to Fig. A-UAAAA and Fig. A-UBAAA).

1 No cracks found in

2 Hood Half 205481 Item (1)

a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

2 Cracks are found in

2 Hood Half 205481 Item (1)

a Replace the Hood Halves.

(Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA).

b Make sure that all broken parts and unwanted materials are removed from the

related tank.

c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

(c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings -

Reporting Sheet ).

(2) Subtask 286106-832-402-001 - INSPECTION OF THE CENTER TANK PUMP

CANISTER HOOD HALVES

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBCAA

Fuel Pump Canister Hood Halves

Inspection - Center Tank

Sheet 01

Fig. A-UAAAA

Inspection Flowchart

Sheet 01

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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SERVICE BULLETIN

(a) Clean the

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

(b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the

center tank - LH FIN 280022 and RH FIN 280023

(Refer to Fig. A-UAAAA and Fig. A-UBCAA).

1 No cracks found in

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

2 Cracks are found in

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

a Replace the Hood Halves.

(Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA).

b Make sure that all broken parts and unwanted materials are removed from the

related tank.

c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

(c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings -

Reporting Sheet ).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 19

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SERVICE BULLETIN

**CONF 002

(1) Subtask 286106-832-401-001 - INSPECTION OF THE WING TANKS (INNER/OUTER)

PUMP CANISTER HOOD HALVES

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Consumable Material List (CML)

Fig. A-UAAAA

Inspection Flowchart

Sheet 01

Fig. A-UBAAA

Fuel Pump Canister Hood Halves

Inspection - Wing Tanks

Sheet 01

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

(a) Clean the

2 Hood Half 205481 Item (1)

with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

(b) Do a Detailed Visual Inspection (DVI) of the fuel pump canister hood halves in the

wing tanks:

- Wing tank (LH) - inboard FIN 280014 and FIN 280016 and outboard

FIN280018 and FIN 280020.

- Wing tank (RH) - inboard FIN 280015 and FIN 280017 and outboard FIN

280019 and FIN 280021.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

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(Refer to Fig. A-UAAAA and Fig. A-UBAAA).

1 No cracks found in

2 Hood Half 205481 Item (1)

a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

2 Cracks are found in

2 Hood Half 205481 Item (1)

a Replace the Hood Halves.

(Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA).

b Make sure that all broken parts and unwanted materials are removed from the

related tank.

c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

(c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings -

Reporting Sheet ).

(2) Subtask 286106-832-402-001 - INSPECTION OF THE CENTER TANK PUMP

CANISTER HOOD HALVES

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBCAA

Fuel Pump Canister Hood Halves

Inspection - Center Tank

Sheet 01

Fig. A-UAAAA

Inspection Flowchart

Sheet 01

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 21

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SERVICE BULLETIN

(a) Clean the

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

(b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the

center tank - LH FIN 280022 and RH FIN 280023

(Refer to Fig. A-UAAAA and Fig. A-UBCAA).

1 No cracks found in

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

2 Cracks are found in

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

a Replace the Hood Halves.

(Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA).

b Make sure that all broken parts and unwanted materials are removed from the

related tank.

c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

(c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings -

Reporting Sheet ).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 22

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SERVICE BULLETIN

(3) Subtask 286106-832-403-002 - INSPECTION OF THE TRIM TANK TRANSFER PUMP

CANISTER HOOD HALVES

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBEAA

Fuel Pump Canister Hood Halves

Inspection - Trim Tank

Sheet 01

Fig. A-UAAAA

Inspection Flowchart

Sheet 01

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

(a) Clean the

2 Hood Half 205481 Item (1)

with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

(b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the

trim tank - FIN 280432 and FIN 280433

(Refer to Fig. A-UAAAA and Fig. A-UBEAA).

1 No cracks found in

2 Hood Half 205481 Item (1)

a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 23

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SERVICE BULLETIN

2 Cracks are found in

2 Hood Half 205481 Item (1)

a Replace the Hood Halves.

(Refer to TASK 286106-833-895 001 REPAIR and Fig. A-UCAAA).

b Make sure that all broken parts and unwanted materials are removed from the

related tank.

c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

(c) Send a record of the inspection results to AIRBUS (Refer to Inspection Findings -

Reporting Sheet ).

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 286106-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301

(a) Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING

(Fuel Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM

28-10-00, Page Block 301).

**CONF 002

(1) Subtask 286106-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 24

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@A300-600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301

(a) Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING

(Fuel Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM

28-10-00, Page Block 301).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 25

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 26

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SERVICE BULLETIN

Task 286106-833-895-001 - REPAIR

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

**CONF 002

Manpower

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 286106-839-402-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 27

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SERVICE BULLETIN

**CONF 002

(1) Subtask 286106-839-402-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

None

**CONF 002

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 286106-833-401-001 - REPAIR THE FUEL PUMP CANISTER HOOD

HALVES

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Equipment BFEB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 205481 2 HOODHALF (1) (2)

NOTE (1): One BFEB01 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 205481 for Fuel Pump Canister PN 2052C11 or PN

2052C12.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 28

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SERVICE BULLETIN

Equipment BFEB02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 3C93-129 2 HOODHALF (1) (2)

NOTE (1): One BFEB02 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601.

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

(a) Replace the fuel pump canister hood halves, do the steps that follow (Refer to Fig.

A-UCAAA):

1 Clean the surface area of the fuel pump canister with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

2 Remove:

6 Screw Item (2) Retain

6 Washer Item (3) Retain

2 Hood Half 205481 Item (1) Discard

or

2 Hood Half 3C93-129 Item (4) Discard

NOTE: If there are defective parts they must be replaced (Refer to the

Vendor Intertechnique for replacement parts).

NOTE: The discarded hood halves have to be replaced with a new

ones with the same Part Number.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 29

7

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SERVICE BULLETIN

3 Install the:

2 Hood Half 205481 Item 1

or

with:

2 Hood Half 3C93-129 Item 4

6 Screw Item (2) Retained at

removal

6 Washer Item (3) Retained at

removal

(b) Make sure that all broken parts and unwanted materials are removed from the

related tank.

**CONF 002

(1) Subtask 286106-833-401-001 - REPAIR THE FUEL PUMP CANISTER HOOD

HALVES

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Equipment BFEB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 205481 2 HOODHALF (1) (2)

NOTE (1): One BFEB01 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 205481 for Fuel Pump Canister PN 2052C11 or PN

2052C12.

Equipment BFEB02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 3C93-129 2 HOODHALF (1) (2)

NOTE (1): One BFEB02 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 30

7

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@A300-600

SERVICE BULLETIN

NOTE (2): Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601.

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

(a) Replace the fuel pump canister hood halves, do the steps that follow (Refer to Fig.

A-UCAAA):

1 Clean the surface area of the fuel pump canister with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

2 Remove:

6 Screw Item (2) Retain

6 Washer Item (3) Retain

2 Hood Half 205481 Item (1) Discard

or

2 Hood Half 3C93-129 Item (4) Discard

NOTE: If there are defective parts they must be replaced (Refer to the

Vendor Intertechnique for replacement parts).

NOTE: The discarded hood halves have to be replaced with a new

ones with the same Part Number.

3 Install the:

2 Hood Half 205481 Item 1

or

with:

2 Hood Half 3C93-129 Item 4

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 31

7

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@A300-600

SERVICE BULLETIN

6 Screw Item (2) Retained at

removal

6 Washer Item (3) Retained at

removal

(b) Make sure that all broken parts and unwanted materials are removed from the

related tank.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 286106-942-402-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301

Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING (Fuel

Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM 28-10-00,

Page Block 301).

**CONF 002

(1) Subtask 286106-942-402-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301

Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING (Fuel

Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM 28-10-00,

Page Block 301).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 32

7

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@A300-600

SERVICE BULLETIN

**CONF ALL

D_SB_286106_7_AAAA_01_03

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.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 33

7

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

SERVICE BULLETIN

**CONF ALL

LH WING SHOWN

RH WING SIMILAR

FUEL PUMP

CANISTER

TYPICAL DAMAGE

HOOD

HALF

HOOD

HALF

SCREW AND

WASHER

(6 OFF)

B

A

RIB14

RIB2

Z550 (Z650)

A

TYPICAL

A

FILTER

Z540 (Z640)

B

D_SB_286106_7_BAAA_01_03

HOOD

HALF

Figure A-UBAAA - Sheet 01

Fuel Pump Canister Hood Halves Inspection - Wing Tanks

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 34

7

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@A300-600

SERVICE BULLETIN

**CONF ALL

Z141 Z142 − 

A

TYPICAL DAMAGE

TYPICAL

FR47

FR46

FUEL PUMP

CANISTER

HOOD

HALF

HOOD

HALF

SCREW AND

WASHER

(6 OFF) FILTER

B

B

A

B

C

C

D_SB_286106_7_BCAA_01_02

HOOD

HALF

Figure A-UBCAA - Sheet 01

Fuel Pump Canister Hood Halves Inspection - Center Tank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 35

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SERVICE BULLETIN

**CONF 002

A

Z311 Z312 − 

PUMP 2

CANISTER

VAPOR SEAL

PUMP 1

CANISTER

TYPICAL

319AB

319BZ

319BB

319AZ

FUEL PUMP

CANISTER

HOOD

HALF

HOOD

HALF

SCREW AND

WASHER

(6 OFF) FILTER

C

TYPICAL DAMAGE

B

B

A

B

C

D_SB_286106_7_BEAA_01_02

HOOD

HALF

Figure A-UBEAA - Sheet 01

Fuel Pump Canister Hood Halves Inspection - Trim Tank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 36

7

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SERVICE BULLETIN

**CONF ALL

FUEL PUMP

CANISTER

A A

A

TYPICAL

D_SB_286106_7_CAAA_01_01

(1) 1

(4) 4

(3)

(2)

(3) (2)

(3) (2)

Figure A-UCAAA - Sheet 01

Repair the Fuel Pump Canister Hood Halves - Typical

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 37

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 38

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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.

A300-28-6106

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

SERVICE BULLETIN NO.

A300-28-6106

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.: A300-28-6106

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.: A300-28-6106

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.: A300-28-6106

REVISION No.: 01 - Apr 15/11 Page: 1

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