# Airbus Service Bulletin 28-6114

Copy: No revision named ("SB_28-6114_r00"), 58 pages: PDF https://openairdocs.org/files/sha256/f1/63/f1632380f48ed3b13c99927b8f34a744b9a1d84b4a786fe415c34051948aceb0; text https://openairdocs.org/service-documents/airbus/sb-28-6114/file/f1632380f48e.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2017-0714, the docket of AD 2017-25-09. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: 28-6114
- Page: https://openairdocs.org/service-documents/airbus/sb-28-6114

## Text (58 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2017-0714, the docket of AD 2017-25-09. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A300-600
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
This summary is for information only and is not approved for modification of the aircraft.
ATA SYSTEM: 28
TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL FUEL PUMP CANISTER
WITH NEW HOOD/MESH FOR OUTER AND TRIM TANK POSITIONS
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 None
MINOR
 13643H5740
 13740H5756
NOTE
: As per EASA IR 21, a minor change is one that has no appreciable effect on the
mass, balance, structural strength, reliability, operational characteristics affecting the
airworthiness of the product. All other changes are major changes.
NOTE
: Please ignore the above note (if it is present), this note is auto-generated and does not
apply to this SB.
NOTE
: This modification is related to an airworthiness issue which has been re-classified and
confirmed by EASA as minor in accordance with EU Part 21.A.91. As such, this is
handled by AIRBUS under its D esign Organisation Approval No. EASA.21J.031.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
Fuel pump canisters are located in pairs in all fuel tanks. There is a fabricated aluminium hood (in two
halves) which forms a surface between the fuel pump inlet mesh and the fuel pump canister body.
Some operators have reported cases of cracking on the hood in the inner wing fuel tanks. On one
aircraft, part of the hood detached and was found inside the fuel tank.
Fuel pump canister hoods are currently subject to a mandatory inspection in accordance with Inspection
Service Bulletin No. A300-28-6106.
Following the investigation into in-service failures, this Service Bulletin introduces new canister hoods
for the wing outer tank and the trim tank fuel pumps (where fitted) only. No other fuel pump positions
are affected by this Service Bulletin.
The new design consists of a new two part stainless steel hood assembly that is installed over the
existing inlet mesh as before. To account for tolerances in the inlet mesh diameter and to avoid
installation pre-stress, each hood half has an enlarged central hole, through which a stepped fastener is
installed.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A300-600
SERVICE BULLETIN
SUMMARY
Accomplishment of this Service Bulletin will reduce the scope of the Inspection Service Bulletin No.
A300-28-6106 by canceling the requirement for the repeat inspection of the fuel pump canisters in the
outer wing and trim tanks (only).
The installation of a new fuel pump canister hood changes the part number of the canister assembly.
The Operational/Maintenance Consequences of this Service Bulletin are covered by the update of the
affected publications detailed in ’PLANNING INFORMATION’.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 RECOMMENDED (1)
 CANCELS INSPECTION SB
 YES
POTENTIAL AD
 NO
 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
DE-FUELLING/VENTILATION
 YES
NOTE
 (1)
: Service Bulletin recommended to be accomplished to prevent significant operational
disruptions.
MATERIAL PRICE INFORMATION
**CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEB01
 4
 See SB
 Hood halves and attachments
**CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEB01
 6
 See SB
 Hood halves and attachments
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
67Q ABR AHK BCS FDX IRA IRM KAC MNB MRJ MSR SOP SUD
TAR THA UPS UQA URS UTP
CONCURRENT REQUIREMENTS
None
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A300-600
SERVICE BULLETIN
SUMMARY
REFERENCES / REPERCUSSIONS
TFU
 None
OEB
 None
AOT
 None
SIL
 None
ISI
 None
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 None
NATURE OF THE WORK
AIRCRAFT
 YES
EQUIPMENT
 YES
HARD
 NO
SOFT
 NO
OBRM
 NO
MANPOWER
**CONF 001
Task 286114-831-895-001: Modification
TOTAL MANHOURS
 11.00
ELAPSED TIME (HOURS)
 4.50
**CONF 002
Task 286114-831-895-001: Modification
TOTAL MANHOURS
 15.50
ELAPSED TIME (HOURS)
 4.50
APPENDICES
**CONF ALL
Appendix 01 - Manpower Gantt Chart
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A300-600
SERVICE BULLETIN
SUMMARY
**CONF 001
A
LH WING SHOWN
RH WING SIMILAR
A
A
NOTE:
AREA OF MODIFICATION.
B C
RIB14
Z500
Z600
REAR SPAR
Z650RH
Z550LH
TYPICAL TYPICAL
BEFORE AFTER
FUEL PUMP
CANISTER
HOOD HALF
B C
FUEL PUMP
CANISTER
HOOD HALF
D_SB_286114_7_SAAA_01_01
Figure A-USAAA - Sheet 01
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 4
7
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### Page 5

@A300-600
SERVICE BULLETIN
SUMMARY
**CONF 002
A
A
LH WING SHOWN
RH WING SIMILAR
A
NOTE:
AREA OF MODIFICATION.
RIB14
B
C D
C D
Z319
B
Z500
Z600 REAR SPAR
Z650RH
Z550LH
TYPICAL TYPICAL
BEFORE AFTER
FUEL PUMP
CANISTER
HOOD HALF
C D
FUEL PUMP
CANISTER
HOOD HALF
D_SB_286114_7_SAAB_01_01
Figure A-USAAB - Sheet 01
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 5
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A300-600
SERVICE BULLETIN
SUMMARY
This Page Intentionally Left Blank
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 6
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@A300-600
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
ATA SYSTEM: 28
TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL FUEL PUMP CANISTER
WITH NEW HOOD/MESH FOR OUTER AND TRIM TANK POSITIONS
MODIFICATION No.: 13643H5740 13740H5756
NOTE
: Please ignore the above note (if it is present), this note is auto-generated and does
not apply to this SB.
NOTE
: This modification is related to an airworthiness issue which has been re-classified
and confirmed by EASA as minor in acco rdance with EU Part 21.A.91. As
such, this is handled by AIRBUS under its Design Organisation Approval No.
EASA.21J.031.
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 B4-622 B4-622R C4-605R/FC4-620 F4-605R F4-622R
(2) Effectivity by MSN
0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0477 0479 0505
0521 0525 0530 0532 0536 0543 0546 0553 0555 0557-0559 0561 0563 0572 0575
0579 0581 0584 0602-0603 0607-0608 0611 0613 0617-0618 0621 0623 0625-0626
0629-0630 0632-0633 0637 0641 0643 0657 0659 0664 0666 0668 0670 0673 0677
0679 0683 0688 0694 0696 0699 0701 0703 0707 0709 0711 0713 0715 0717 0719
0721-0730 0732-0746 0748-0750 0752-0764 0766 0768-0775 0777-0794 0797
0799-0840 0845-0878
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 1
7
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### Page 8

@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
67Q
 0584 0603 0744 0749 0764
ABR
 0557 0677 0717 0722
AHK
 0683 0770 0855 0856 0857 0858 0859 0860 0870 0871
BCS
 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730
0737 0740 0743 0753 0783 0797 0836 0837 0872
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
IRA
 0632 0696 0723 0727
IRM
 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701
0773 0838
KAC
 0344 0673 0694 0699 0719 0721
MNB
 0521 0525 0734 0739 0755 0756 0758
MRJ
 0750 0762
MSR
 0561 0607
SOP
 0532
SUD
 0666 0775
TAR
 0505 0558 0563
THA
 0629 0782 0784 0785 0786 0787
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 0845 0846 0847
0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864 0865
0866 0867 0868 0869
UQA
 0626 0643
URS
 0733 0788
UTP
 0707 0725 0732 0741 0746 0754 0763
(4) Configuration by MSN
MSN
 CONFIGURATION
0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414
0417 0546 0553 0618 0623
001
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A300-600
SERVICE BULLETIN
MSN
 CONFIGURATION
0477 0479 0505 0521 0525 0530 0532 0536 0543 0555 0557
0558 0559 0561 0563 0572 0575 0579 0581 0584 0602 0603
0607 0608 0611 0613 0617 0621 0625 0626 0629 0630 0632
0633 0637 0641 0643 0657 0659 0664 0666 0668 0670 0673
0677 0679 0683 0688 0694 0696 0699 0701 0703 0707 0709
0711 0713 0715 0717 0719 0721 0722 0723 0724 0725 0726
0727 0728 0729 0730 0732 0733 0734 0735 0736 0737 0738
0739 0740 0741 0742 0743 0744 0745 0746 0748 0749 0750
0752 0753 0754 0755 0756 0757 0758 0759 0760 0761 0762
0763 0764 0766 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 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
**CONF 001
Config. 001 is valid for A300-600 aircraft given in the effectivity of this Service Bulletin as
a standard configuration.
**CONF 002
Config. 002 is valid for A300-600R aircraft given in the effectivity of this Service Bulletin
as a standard configuration.
(6) Material Effectivity
**CONF 001
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEB01
 4
 (1)
Reidentified part set REIDB01
 1
Consumable CMLB01
 1
NOTE
 (1)
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
**CONF 002
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEB01
 6
 (1)
Reidentified part set REIDB01
 1
Consumable CMLB01
 1
NOTE
 (1)
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A300-600
SERVICE BULLETIN
**CONF ALL
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
Fuel pump canisters are located in pairs in all fuel tanks. There is a fabricated aluminium
hood (in two halves) which forms a surface between the fuel pump inlet mesh and the
fuel pump canister body.
Some operators have reported cases of cracking on the hood in the inner wing fuel
tanks. On one aircraft, part of the hood detached and was found inside the fuel tank.
Fuel pump canister hoods are currently subject to a mandatory inspection in accordance
with Inspection Service Bulletin No. A300-28-6106.
(2) Objective/Action
Following the investigation into in-service failures, this Service Bulletin introduces new
canister hoods for the wing outer tank and the trim tank fuel pumps (where fitted) only.
No other fuel pump positions are affected by this Service Bulletin.
The new design consists of a new two part stainless steel hood assembly that is
installed over the existing inlet mesh as before. To account for tolerances in the inlet
mesh diameter and to avoid installation pre-stress, each hood half has an enlarged
central hole, through which a stepped fastener is installed.
(3) Advantages
Accomplishment of this Service Bulletin will reduce the scope of the Inspection Service
Bulletin No. A300-28-6106 by canceling the requirement for the repeat inspection of the
fuel pump canisters in the outer wing and trim tanks (only).
The installation of a new fuel pump canister hood changes the part number of the
canister assembly.
(4) Operational/Maintenance Consequences
The Operational/Maintenance Consequences of this Service Bulletin are covered by the
update of the affected publications detailed in ’PLANNING INFORMATION’.
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
**CONF 001
Task 286114-831-895-001: Modification
(1) Replace the Hood Halves of the Fuel Pump Canisters in the LH Outer Wing Tank
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 4
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A300-600
SERVICE BULLETIN
(2) Replace the Hood Halves of the Fuel Pump Canisters in the RH Outer Wing Tank
(3) Re-identify the Fuel Pump Canisters in the LH Outer Wing Tank
(4) Re-identify the Fuel Pump Canisters in the RH Outer WingTank
**CONF 002
Task 286114-831-895-001: Modification
(1) Replace the Hood Halves of the Fuel Pump Canisters in the LH Outer Wing Tank
(2) Replace the Hood Halves of the Fuel Pump Canisters in the RH Outer Wing Tank
(3) Replace the Hood Halves of the Fuel Pump Canisters in the Trim Tank
(4) Re-identify the Fuel Pump Canisters in the LH Outer Wing Tank
(5) Re-identify the Fuel Pump Canisters in the RH Outer WingTank
(6) Re-identify the Fuel Pump Canisters in the Trim Tank
**CONF ALL
E. COMPLIANCE
(1) Classification
RECOMMENDED: Service Bulletin recommended to be accomplished to prevent
significant operational disruptions.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin is recommended at the earliest opportunity
where manpower and facilities are available.
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organisation Approval No. EASA.21J.031.
If an aircraft listed in the effectivity has a modification or repair embodied that is not of
AIRBUS origin, and which affects the content of this Service Bulletin, the operator is
responsible for obtaining approval by its airworthiness authority for any adaptation necessary
before incorporation of the Service Bulletin.
G. MANPOWER
The manpower estimates given in this Service Bulletin are based on the direct labor cost to
do the work. These estimates assume that the work will be done by experienced personnel,
and may need to be revised upwards to suit operator’s circumstances. The estimates do not
include the time to prepare, plan or inspect the work. Manufacture and procurement of parts
and tools, drying times for paints, sealants, etc., and general administration work are also not
included.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 5
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A300-600
SERVICE BULLETIN
**CONF 001
Task 286114-831-895-001: Modification
Get Access
 1.00
On Aircraft
Replace the Hood Halves of the Fuel Pump Canisters
in the LH Outer Wing Tank
4.00
Replace the Hood Halves of the Fuel Pump Canisters
in the RH Outer Wing Tank
4.00
Re-identify the Fuel Pump Canisters in the LH Outer
Wing Tank
0.50
Re-identify the Fuel Pump Canisters in the RH Outer
WingTank
0.50
Close-Up
 1.00
TOTAL MANHOURS
 11.00
ELAPSED TIME (HOURS)
 4.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-UAAAA
 given in Appendix 01 - Manpower Gantt Chart .
**CONF 002
Task 286114-831-895-001: Modification
Get Access
 1.00
On Aircraft
Replace the Hood Halves of the Fuel Pump Canisters
in the LH Outer Wing Tank
4.00
Replace the Hood Halves of the Fuel Pump Canisters
in the RH Outer Wing Tank
4.00
Replace the Hood Halves of the Fuel Pump Canisters
in the Trim Tank
4.00
Re-identify the Fuel Pump Canisters in the LH Outer
Wing Tank
0.50
Re-identify the Fuel Pump Canisters in the RH Outer
WingTank
0.50
Re-identify the Fuel Pump Canisters in the Trim Tank
 0.50
Close-Up
 1.00
TOTAL MANHOURS
 15.50
ELAPSED TIME (HOURS)
 4.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-UAAAB
 given in Appendix 01 - Manpower Gantt Chart .
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 6
7
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### Page 13

@A300-600
SERVICE BULLETIN
**CONF ALL
H. WEIGHT AND BALANCE
**CONF 001
The weight and balance estimates given in this Service Bulletin are based on the
Manufacturer’s Empty Weight (MEW) and do not include operator’s items. For the definition of
MEW and operator’s items, refer to the Weight and Balance Manual (WBM) Chapter 1-00-07.
Manufacturers Empty Weight +0.6 KG (+1.3 LB)
Effect on Balance +17.9 KGM (+129.5 LB.FT )
**CONF 002
The weight and balance estimates given in this Service Bulletin are based on the
Manufacturer’s Empty Weight (MEW) and do not include operator’s items. For the definition of
MEW and operator’s items, refer to the Weight and Balance Manual (WBM) Chapter 1-00-07.
Manufacturers Empty Weight +0.9 KG (+2 LB)
Effect on Balance +20.1 KGM (+145.4 LB.FT )
**CONF ALL
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Aircraft Maintenance Manual (AMM)
 06-21-00 06-41-00 20-21-12
24-00-00 28-00-00 28-10-00
28-11-22 28-11-33 28-25-00
Consumable Material List (CML)
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Process and Material Specification (PMS)
 Process and Material Specification
(PMS) 01-06-12
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-30-29 51-40-00
Weight and Balance Manual (WBM)
 Chapter 1-00-07
**CONF 002
Aircraft Maintenance Manual (AMM)
 06-21-00 06-41-00 20-21-12
24-00-00 28-00-00 28-10-00
28-11-22 28-11-33 28-25-00
Consumable Material List (CML)
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 7
7
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@A300-600
SERVICE BULLETIN
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Process and Material Specification (PMS)
 Process and Material Specification
(PMS) 01-06-12
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-30-29 51-40-00
Weight and Balance Manual (WBM)
 Chapter 1-00-07
**CONF ALL
K. PUBLICATION AFFECTED
**CONF 001
Illustrated Parts Catalog (IPC)
 28-21-21
Maintenance Planning Document (MPD)
 282100-05-1
282100-06-1
282100-06-2
**CONF 002
Illustrated Parts Catalog (IPC)
 28-21-21 28-27-12
Maintenance Planning Document (MPD)
 282100-05-1
282100-06-1
282100-06-2
**CONF ALL
L. INTERCHANGEABILITY/MIXABILITY
The interchangeability/mixability possibilities are for new or modified parts introduced by the
accomplishment of this Service Bulletin.
**CONF 001
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Screw
 MS35206-228
 MS35206-228
 01
 Not
Applicable
Screw
 MS35206-228
 C93-463
 01
 Not
Applicable
Washer
 AN935-6L
 G764100
 01
 Not
Applicable
Hood
 205481
 C93-467
 01
 Not
Applicable
Canister-Fuel Booster
Pump
2052C11
 2052C11-5
 01
 Not
Applicable
Canister-Fuel Booster
Pump
2052C12
 2052C12-5
 01
 Not
Applicable
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 8
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### Page 15

@A300-600
SERVICE BULLETIN
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
**CONF 002
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Screw
 MS35206-228
 MS35206-228
 01
 Not
Applicable
Screw
 MS35206-228
 C93-463
 01
 Not
Applicable
Washer
 AN935-6L
 G764100
 01
 Not
Applicable
Hood
 205481
 C93-467
 01
 Not
Applicable
Canister-Fuel Booster
Pump
2052C11
 2052C11-5
 01
 Not
Applicable
Canister-Fuel Booster
Pump
2052C12
 2052C12-5
 01
 Not
Applicable
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
**CONF ALL
M. SPARES
None
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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This Page Intentionally Left Blank
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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
 For Europe, Middle East, Africa
ZODIAC AEROSPACE
61 Rue Pierre Curie CS20001
78373 Plaisir Cedex
FRANCE
Phone: +33 161 34 23 23
Phone AOG: +33 172 02 23 23
Fax:+33 161 34 21 08
For USA
ZODIAC AEROSPACE
4900 St Joe Boulevard
Building 200 Suite 400
College Park
GA 30337
USA
Phone: +1 678 228 8153
Phone AOG: +1 800 879 0411
Fax:+1 404 559 0041
For Asia
ZODIAC AEROSPACE
36 Loyang Drive
Singapore 508949
Phone: +65 6579 2230
Phone AOG: +655 9770 5061
Fax:+65 65579 2231
(2) Price and Availability
No AIRBUS kit will be provided.
Procurement terms for the equipment must be negotiated with the equipment supplier.
B. INDUSTRY SUPPORT INFORMATION
Industry support terms for the equipment must be negotiated with the equipment supplier.
C. LIST OF COMPONENTS
No Kit
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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SERVICE BULLETIN
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
NOTE
: To accomplish this Service Bulletin it is necessary to use the
consumable materials listed i n the subsequent re ferenced tasks:
- AMM 28-11-22, Page Block 401
- AMM 28-11-33, Page Block 401.
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO CML
MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner-- Acetone
 08BBH1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
(2) Components
None
(3) Equipment
Equipment BFEB01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
1
 C93-467
 2
 HOOD
 (1)
 205481
 01
2
 MS35206-228
 4
 SCREW
 (2)
 MS35206-228
 01
3
 G764100
 4
 WASHER
 (3)
 AN935-6L
 01
4
 C93-463
 2
 SCREW
 (2)
 MS35206-228
 01
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s)
which you cannot identify in the LIST OF COMPONENTS of this Service
Bulletin, refer to Standards Manual (SM). The SM will give you the
correct part number to part number relationship.
NOTE
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
Reidentified part set REIDB01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
2052C11-5
 CANISTER
 2052C11
2052C12-5
 CANISTER
 2052C12
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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SERVICE BULLETIN
F. TOOLING
None
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 286114-831-895-001 - Modification
WARNING
: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
WARNING
: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY
KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION
(CDCCL). CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A
POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN
THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A
CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
CAUTION
: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP
ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY
AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE
WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,
COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO
THIS:
- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS
NECESSARY ON WIRING AND COMPONENTS.
- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND
OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION
AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has a procedure accepted by the local authority
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: Discarded parts must be managed at the operator’s discretion.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact AIRBUS for further
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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SERVICE BULLETIN
instructions and approval.
Task Associated Data
**CONF 001
Zone
550 650
Modified FIN
280018 280019 280020 280021
Access
Panel
 550BB 650BB
Manpower
TOTAL MANHOURS
 11.00
ELAPSED TIME (HOURS)
 4.50
**CONF 002
Zone
311 312 319 550 650
Modified FIN
280018 280019 280020 280021 280432 280433
Access
Panel
 319AZ 319BZ 550BB 650BB
Manpower
TOTAL MANHOURS
 15.50
ELAPSED TIME (HOURS)
 4.50
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 286114-910-401-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-21-00, Page Block 001
06-41-00, Page Block 001
20-21-12, Page Block 001
28-00-00, Page Block 301
28-10-00, Page Block 301
Consumable Material List (CML)
Structural Repair Manual (SRM)
 51-30-29
51-40-00
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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SERVICE BULLETIN
(a) For the specification of materials (Mat. No.) that you must use in this Service
Bulletin, refer to Consumable Material List (CML).
(b) Obey the safety procedures when you do work in a fuel tank, refer to AMM
28-00-00, Page Block 301 and AMM 28-10-00, Page Block 301.
(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.
(d) For the identification of zones, refer to AMM 06-21-00, Page Block 001.
(e) Remove and install fasteners in accordance with SRM 51-30-29.
(f) To torque tighten the standard threaded fasteners, refer to AMM 20-21-12, Page
Block 001.
(g) If alternative and substitute fasteners have to be used, you must make sure that the
associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’
column.
(h) If the length of any fastener specified in this Service Bulletin does not meet
installation standards given in SRM Chapter 51, then a fastener of the same
specification, or an approved substitute, with a length which meets the installation
standards given in SRM Chapter 51 may be used. In addition, washers may be
installed for fastener grip length in accordance with SRM Chapter 51.
(2) Subtask 286114-839-401-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF 002
(1) Subtask 286114-910-401-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-21-00, Page Block 001
06-41-00, Page Block 001
20-21-12, Page Block 001
28-00-00, Page Block 301
28-10-00, Page Block 301
Consumable Material List (CML)
Structural Repair Manual (SRM)
 51-30-29
51-40-00
(a) For the specification of materials (Mat. No.) that you must use in this Service
Bulletin, refer to Consumable Material List (CML).
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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SERVICE BULLETIN
(b) Obey the safety procedures when you do work in a fuel tank, refer to AMM
28-00-00, Page Block 301 and AMM 28-10-00, Page Block 301.
(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.
(d) For the identification of zones, refer to AMM 06-21-00, Page Block 001.
(e) Remove and install fasteners in accordance with SRM 51-30-29.
(f) To torque tighten the standard threaded fasteners, refer to AMM 20-21-12, Page
Block 001.
(g) If alternative and substitute fasteners have to be used, you must make sure that the
associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’
column.
(h) If the length of any fastener specified in this Service Bulletin does not meet
installation standards given in SRM Chapter 51, then a fastener of the same
specification, or an approved substitute, with a length which meets the installation
standards given in SRM Chapter 51 may be used. In addition, washers may be
installed for fastener grip length in accordance with SRM Chapter 51.
(2) Subtask 286114-839-401-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
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 286114-941-401-001 - Job Set-Up
Work Zones and Access Panels
Zone
 Access/Work location
550
650
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-21-00, Page Block 001
24-00-00, Page Block 301
28-10-00, Page Block 301
28-25-00, Page Block 301
NOTE
: The items given in this note shall be considered as the basic Aircraft
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page
Block 301.
(b) Defuel the aircraft, refer to AMM 28-25-00, Page Block 301.
(c) 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.
(d) Put platforms in position to get access to the applicable zones, refer to AMM
06-21-00, Page Block 001:
- Wing tanks outer - Zones 550 LH
- Wing tanks outer - Zones 650 RH
(2) Subtask 286114-010-401-001 - Remove the Fuel Tank Access Panel from the LH
Wing
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
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(a) From the LH wing, refer to AMM 28-11-22, Page Block 401, remove the fuel tank
access panel 550BB.
(3) Subtask 286114-010-402-001 - Remove the Fuel Tank Access Panel from the RH
Wing
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
(a) From the RH wing, refer to AMM 28-11-22, Page Block 401, remove the fuel tank
access panel 650BB.
**CONF 002
(1) Subtask 286114-941-401-002 - Job Set-Up
Work Zones and Access Panels
Zone
 Access/Work location
550
650
319
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-21-00, Page Block 001
24-00-00, Page Block 301
28-10-00, Page Block 301
28-25-00, Page Block 301
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 20
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- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page
Block 301.
(b) Defuel the aircraft, refer to AMM 28-25-00, Page Block 301.
(c) 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.
(d) Put platforms in position to get access to the applicable zones, refer to AMM
06-21-00, Page Block 001:
- Wing tanks outer - Zones 550 LH
- Wing tanks outer - Zones 650 RH
- Trim tank - Zones 311 and 312,
(2) Subtask 286114-010-401-001 - Remove the Fuel Tank Access Panel from the LH
Wing
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
(a) From the LH wing, refer to AMM 28-11-22, Page Block 401, remove the fuel tank
access panel 550BB.
(3) Subtask 286114-010-402-001 - Remove the Fuel Tank Access Panel from the RH
Wing
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 21
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SERVICE BULLETIN
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
(a) From the RH wing, refer to AMM 28-11-22, Page Block 401, remove the fuel tank
access panel 650BB.
(4) Subtask 286114-010-403-002 - Remove the Fuel Tank Access Panel from the Trim
Tank
Work Zones and Access Panels
Zone
 Access/Work location
311
 Access
 Panel 319AZ
312
 Access
 Panel 319BZ
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-33, Page Block 401
(a) From the trim tank, refer to AMM 28-11-33, Page Block 401, remove the fuel tank
access panels 319AZ and 319BZ.
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 286114-831-401-001 - Replace the Hood Halves of the Fuel Pump
Canisters in the LH Outer Wing Tank
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Manhours
 4.00
Minimum number of person
 2
Subtask elapsed time
 2.00
Skills
 AIRFRAME
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Material necessary to do the job
Equipment BFEB01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
1
 C93-467
 4
 HOOD
2
 MS35206-228
 8
 SCREW
3
 G764100
 8
 WASHER
4
 C93-463
 4
 SCREW
NOTE
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner--
Acetone
08BBH1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Fig. A-UBAAA
Removal and Installation of the Fuel
Pump Canister Hood Halves in the
Outer Tanks
Sheet 01
Sheet 02
(a) Remove the hood halves from the fuel pump canisters 280018 and 280020 in the
LH wing outer tank.
1
 From the inboard fuel pump canister 280020 in the LH wing outer tank, refer
to Fig. A-UBAAA Sheet 01
 , Views B and C, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
2
 From the outboard fuel pump canister 280018 in the LH wing outer tank, refer
to Fig. A-UBAAA Sheet 01
 , Views B and C, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
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2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
(b) Clean the fuel pump mesh filters, use:
Textile-Lint Free
Cotton
14SBA1 As required
and
Non Aqueous
Cleaner-- Acetone
08BBH1 As required
(c) Visually inspect the fuel pump mesh filters for signs of holes and a satisfactory weld
where it attaches to the top land. If any damage is found, replace mesh.
(d) Install the new hood halves onto the fuel pump canisters 280018 and 280020, in
the LH wing outer tank.
1
 At the inboard fuel pump canister 280020 in the LH wing outer tank, refer to
Fig. A-UBAAA Sheet 02
 , Views D, E and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAA Sheet 02
 ,V i e wE .
2
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
3
 At the outboard fuel pump canister 280018 in the LH wing outer tank, refer to
Fig. A-UBAAA Sheet 02
 , Views D, E and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 24
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4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAA Sheet 02
 ,V i e wE .
4
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
(2) Subtask 286114-831-402-001 - Replace the Hood Halves of the Fuel Pump
Canisters in the RH Outer Wing Tank
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
Manpower Resources
Manhours
 4.00
Minimum number of person
 2
Subtask elapsed time
 2.00
Skills
 AIRFRAME
Material necessary to do the job
Equipment BFEB01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
1
 C93-467
 4
 HOOD
2
 MS35206-228
 8
 SCREW
3
 G764100
 8
 WASHER
4
 C93-463
 4
 SCREW
NOTE
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner--
Acetone
08BBH1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Fig. A-UBAAA
Removal and Installation of the Fuel
Pump Canister Hood Halves in the
Outer Tanks
Sheet 01
Sheet 02
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 25
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(a) Remove the hood halves from the fuel pump canisters 280019 and 280021 in the
RH wing outer tank.
1
 From the inboard fuel pump canister 280021 in the RH wing outer tank, refer
to Fig. A-UBAAA Sheet 01
 , Views B and C, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
2
 From the outboard fuel pump canister 280019 in the RH wing outer tank, refer
to Fig. A-UBAAA Sheet 01
 , Views B and C, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
(b) Clean the fuel pump mesh filters, use:
Textile-Lint Free
Cotton
14SBA1 As required
and
Non Aqueous
Cleaner-- Acetone
08BBH1 As required
(c) Visually inspect the fuel pump mesh filters for signs of holes and a satisfactory weld
where it attaches to the top land. If any damage is found, replace mesh.
(d) Install the new hood halves onto the fuel pump canisters 280018 and 280020, in
the RH wing outer tank.
1
 At the inboard fuel pump canister 280020 in the RH wing outer tank, refer to
Fig. A-UBAAA Sheet 02
 , Views D, E and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 26
7
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### Page 33

@A300-600
SERVICE BULLETIN
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAA Sheet 02
 ,V i e wE .
2
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
3
 At the outboard fuel pump canister 280018 in the RH wing outer tank, refer to
Fig. A-UBAAA Sheet 02
 , Views D, E and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAA Sheet 02
 ,V i e wE .
4
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
(3) Subtask 286114-930-401-001 - Re-identify the Fuel Pump Canisters in the LH Outer
Wing Tank
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 AIRFRAME
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 27
7
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### Page 34

@A300-600
SERVICE BULLETIN
Material necessary to do the job
Reidentified part set REIDB01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
2052C11-5
 CANISTER
 2052C11
2052C12-5
 CANISTER
 2052C12
References
Process and Material Specification
(PMS)
Process and Material Specification (PMS)
01-06-12
(a) Re-identify the pump canisters in the LH wing outer tank, refer to Process and
Material Specification (PMS) 01-06-12.
1
 After modification the PN of the pump canisters in the LH wing outer tank will
change as follows:
2 Canister-Fuel Booster
Pump
2052C11
will become:
2 Canister-Fuel Booster
Pump
2052C11-5
or
2 Canister-Fuel Booster
Pump
2052C12
will become:
2 Canister-Fuel Booster
Pump
2052C12-5
(4) Subtask 286114-930-402-001 - Re-identify the Fuel Pump Canisters in the RH Outer
WingTank
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 AIRFRAME
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 28
7
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### Page 35

@A300-600
SERVICE BULLETIN
Material necessary to do the job
Reidentified part set REIDB01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
2052C11-5
 CANISTER
 2052C11
2052C12-5
 CANISTER
 2052C12
References
Process and Material Specification
(PMS)
Process and Material Specification (PMS)
01-06-12
(a) Re-identify the pump canisters in the RH wing outer tank, refer to Process and
Material Specification (PMS) 01-06-12.
1
 After modification the PN of the pump canisters in the RH wing outer tank will
change as follows:
2 Canister-Fuel Booster
Pump
2052C11
will become:
2 Canister-Fuel Booster
Pump
2052C11-5
or
2 Canister-Fuel Booster
Pump
2052C12
will become:
2 Canister-Fuel Booster
Pump
2052C12-5
**CONF 002
(1) Subtask 286114-831-401-002 - Replace the Hood Halves of the Fuel Pump
Canisters in the LH Outer Wing Tank
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Manhours
 4.00
Minimum number of person
 2
Subtask elapsed time
 2.00
Skills
 AIRFRAME
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 29
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 36

@A300-600
SERVICE BULLETIN
Material necessary to do the job
Equipment BFEB01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
1
 C93-467
 4
 HOOD
2
 MS35206-228
 8
 SCREW
3
 G764100
 8
 WASHER
4
 C93-463
 4
 SCREW
NOTE
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner--
Acetone
08BBH1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Fig. A-UBAAB
Removal and Installation of the Fuel
Pump Canister Hood Halves in the
Outer Tanks and Trim Tank
Sheet 01
Sheet 02
(a) Remove the hood halves from the fuel pump canisters 280018 and 280020 in the
LH wing outer tank.
1
 From the inboard fuel pump canister 280020 in the LH wing outer tank, refer
to Fig. A-UBAAB Sheet 01
 , Views C and D, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
2
 From the outboard fuel pump canister 280018 in the LH wing outer tank, refer
to Fig. A-UBAAB Sheet 01
 , Views C and D, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 30
7
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### Page 37

@A300-600
SERVICE BULLETIN
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
(b) Clean the fuel pump mesh filters, use:
Textile-Lint Free
Cotton
14SBA1 As required
and
Non Aqueous
Cleaner-- Acetone
08BBH1 As required
(c) Visually inspect the fuel pump mesh filters for signs of holes and a satisfactory weld
where it attaches to the top land. If any damage is found, replace mesh.
(d) Install the new hood halves onto the fuel pump canisters 280018 and 280020, in
the LH wing outer tank.
1
 At the inboard fuel pump canister 280020 in the LH wing outer tank, refer to
Fig. A-UBAAB Sheet 02
 , Views E, F and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAB Sheet 02
 ,V i e wF .
2
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
3
 At the outboard fuel pump canister 280018 in the LH wing outer tank, refer to
Fig. A-UBAAB Sheet 02
 , Views E, F and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 31
7
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### Page 38

@A300-600
SERVICE BULLETIN
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAB Sheet 02
 ,V i e wF .
4
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
(2) Subtask 286114-831-402-002 - Replace the Hood Halves of the Fuel Pump
Canisters in the RH Outer Wing Tank
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
Manpower Resources
Manhours
 4.00
Minimum number of person
 2
Subtask elapsed time
 2.00
Skills
 AIRFRAME
Material necessary to do the job
Equipment BFEB01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
1
 C93-467
 4
 HOOD
2
 MS35206-228
 8
 SCREW
3
 G764100
 8
 WASHER
4
 C93-463
 4
 SCREW
NOTE
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner--
Acetone
08BBH1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Fig. A-UBAAB
Removal and Installation of the Fuel
Pump Canister Hood Halves in the
Outer Tanks and Trim Tank
Sheet 01
Sheet 02
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 32
7
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### Page 39

@A300-600
SERVICE BULLETIN
(a) Remove the hood halves from the fuel pump canisters 280019 and 280021 in the
RH wing outer tank.
1
 From the inboard fuel pump canister 280021 in the RH wing outer tank, refer
to Fig. A-UBAAB Sheet 01
 , Views C and D, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
2
 From the outboard fuel pump canister 280019 in the RH wing outer tank, refer
to Fig. A-UBAAB Sheet 01
 , Views C and D, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
(b) Clean the fuel pump mesh filters, use:
Textile-Lint Free
Cotton
14SBA1 As required
and
Non Aqueous
Cleaner-- Acetone
08BBH1 As required
(c) Visually inspect the fuel pump mesh filters for signs of holes and a satisfactory weld
where it attaches to the top land. If any damage is found, replace mesh.
(d) Install the new hood halves onto the fuel pump canisters 280018 and 280020, in
the RH wing outer tank.
1
 At the inboard fuel pump canister 280020 in the RH wing outer tank, refer to
Fig. A-UBAAB Sheet 02
 , Views E, F and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 33
7
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### Page 40

@A300-600
SERVICE BULLETIN
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAB Sheet 02
 ,V i e wF .
2
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
3
 At the outboard fuel pump canister 280018 in the RH wing outer tank, refer to
Fig. A-UBAAB Sheet 02
 , Views E, F and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAB Sheet 02
 ,V i e wF .
4
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
(3) Subtask 286114-831-403-002 - Replace the Hood Halves of the Fuel Pump
Canisters in the Trim Tank
Work Zones and Access Panels
Zone
 Access/Work location
319
 Access
 Panel 319AZ, Panel 319BZ
Manpower Resources
Manhours
 4.00
Minimum number of person
 2
Subtask elapsed time
 2.00
Skills
 AIRFRAME
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 34
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 41

@A300-600
SERVICE BULLETIN
Material necessary to do the job
Equipment BFEB01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
1
 C93-467
 4
 HOOD
2
 MS35206-228
 8
 SCREW
3
 G764100
 8
 WASHER
4
 C93-463
 4
 SCREW
NOTE
: One Kit BFEB01 is required for the modification of each Fuel Pump
Canister.
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner--
Acetone
08BBH1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Fig. A-UBAAB
Removal and Installation of the Fuel
Pump Canister Hood Halves in the
Outer Tanks and Trim Tank
Sheet 01
Sheet 02
(a) Remove the hood halves from the fuel pump canisters 280432 and 280433 in the
trim tank.
1
 From the LH fuel pump canister 280432 in the trim tank, refer to Fig. A-
UBAAB Sheet 01
, Views C and D, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
2
 From the RH fuel pump canister 280433 in the trim tank, refer to Fig. A-
UBAAB Sheet 01
, Views C and D, remove:
6 Screw MS35206-228 Item (2) Discard
6 Washer AN935-6L Item (3) Discard
2 Hood 205481 Item (1) Discard
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 35
7
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### Page 42

@A300-600
SERVICE BULLETIN
NOTE
: Make sure that the canister hood halves (and fasteners) are
removed from the fuel tank in their entirety. If any fragment of
a canister hood is found to be missing, make sure that it is
removed from the fuel tank.
(b) Clean the fuel pump mesh filters, use:
Textile-Lint Free
Cotton
14SBA1 As required
and
Non Aqueous
Cleaner-- Acetone
08BBH1 As required
(c) Visually inspect the fuel pump mesh filters for signs of holes and a satisfactory weld
where it attaches to the top land. If any damage is found, replace mesh.
(d) Install the new hood halves onto the fuel pump canisters 280432 and 280433, in
the trim tank.
1
 At the LH fuel pump canister 280432 in the trim tank, refer to Fig. A-UBAAB
Sheet 02
, Views E, F and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAB Sheet 02
 ,V i e wF .
2
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
3
 At the RH fuel pump canister 280018 in the trim tank, refer to Fig. A-UBAAB
Sheet 02
, Views E, F and Section A-A, install:
2 Hood Half C93-467 Item 1
with:
4 Screw MS35206-228 Item 2
2 Stepped-Screw
Assembly
C93-463 Item 4
4 Washer G764100 Item 3
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 36
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 43

@A300-600
SERVICE BULLETIN
NOTE
: Make sure that the clearance is equal between the hood
halves, refer to Fig. A-UBAAB Sheet 02
 ,V i e wF .
4
 Torque the Screw, Item 2 and the Stepped Screw Assembly, Item 5, to 0.2
m.daN (1.47 lbf ft).
(4) Subtask 286114-930-401-001 - Re-identify the Fuel Pump Canisters in the LH Outer
Wing Tank
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 AIRFRAME
Material necessary to do the job
Reidentified part set REIDB01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
2052C11-5
 CANISTER
 2052C11
2052C12-5
 CANISTER
 2052C12
References
Process and Material Specification
(PMS)
Process and Material Specification (PMS)
01-06-12
(a) Re-identify the pump canisters in the LH wing outer tank, refer to Process and
Material Specification (PMS) 01-06-12.
1
 After modification the PN of the pump canisters in the LH wing outer tank will
change as follows:
2 Canister-Fuel Booster
Pump
2052C11
will become:
2 Canister-Fuel Booster
Pump
2052C11-5
or
2 Canister-Fuel Booster
Pump
2052C12
will become:
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 37
7
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### Page 44

@A300-600
SERVICE BULLETIN
2 Canister-Fuel Booster
Pump
2052C12-5
(5) Subtask 286114-930-402-001 - Re-identify the Fuel Pump Canisters in the RH Outer
WingTank
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 AIRFRAME
Material necessary to do the job
Reidentified part set REIDB01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
2052C11-5
 CANISTER
 2052C11
2052C12-5
 CANISTER
 2052C12
References
Process and Material Specification
(PMS)
Process and Material Specification (PMS)
01-06-12
(a) Re-identify the pump canisters in the RH wing outer tank, refer to Process and
Material Specification (PMS) 01-06-12.
1
 After modification the PN of the pump canisters in the RH wing outer tank will
change as follows:
2 Canister-Fuel Booster
Pump
2052C11
will become:
2 Canister-Fuel Booster
Pump
2052C11-5
or
2 Canister-Fuel Booster
Pump
2052C12
will become:
2 Canister-Fuel Booster
Pump
2052C12-5
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 38
7
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### Page 45

@A300-600
SERVICE BULLETIN
(6) Subtask 286114-930-403-002 - Re-identify the Fuel Pump Canisters in the Trim
Tank
Work Zones and Access Panels
Zone
 Access/Work location
319
 Access
 Panel 319AZ, Panel 319BZ
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 AIRFRAME
Material necessary to do the job
Reidentified part set REIDB01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
2052C11-5
 CANISTER
 2052C11
2052C12-5
 CANISTER
 2052C12
References
Process and Material Specification
(PMS)
Process and Material Specification (PMS)
01-06-12
(a) Re-identify the pump canisters in the trim tank, refer to Process and Material
Specification (PMS) 01-06-12.
1
 After modification the PN of the pump canisters in the trim tank will change as
follows:
2 Canister-Fuel Booster
Pump
2052C11
will become:
2 Canister-Fuel Booster
Pump
2052C11-5
or
2 Canister-Fuel Booster
Pump
2052C12
will become:
2 Canister-Fuel Booster
Pump
2052C12-5
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 39
7
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### Page 46

@A300-600
SERVICE BULLETIN
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 286114-700-401-001 - Testing
Manpower Resources
Skills
 AIRFRAME
NOTE
: The tests that are necessary are included in the Subtasks that follow:
- SUBTASK 286114-410-402 001 Install the Fuel Tank Access Panels
at the LH Wing
- SUBTASK 286114-410-401 001 Install the Fuel Tank Access Panels
at the RH Wing
The manhours for the tests are included in the referenced Service
Bulletin subtasks.
**CONF 002
(1) Subtask 286114-700-401-002 - Testing
Manpower Resources
Skills
 AIRFRAME
NOTE
: The tests that are necessary are included in the Subtasks that follow:
- SUBTASK 286114-410-402 001 Install the Fuel Tank Access Panels
at the LH Wing
- SUBTASK 286114-410-401 001 Install the Fuel Tank Access Panels
at the RH Wing
- SUBTASK 286114-410-403 002 Install the Fuel Tank Access Panels
at the Trim Tank
The manhours for the tests are included in the referenced Service
Bulletin subtasks.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 40
7
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### Page 47

@A300-600
SERVICE BULLETIN
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 286114-410-402-001 - Install the Fuel Tank Access Panels at the LH Wing
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
(a) At the LH wing, refer to AMM 28-11-22, Page Block 401, install the fuel tank
access panel 550BB.
(2) Subtask 286114-410-401-001 - Install the Fuel Tank Access Panels at the RH Wing
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
(a) At the LH wing, refer to AMM 28-11-22, Page Block 401, install the fuel tank
access panel 650BB.
(3) Subtask 286114-942-402-001 - Close-Up
Manpower Resources
Skills
 NON SPECIFIC
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Remove the access platform(s).
(c) Put the aircraft back to its initial configuration.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 41
7
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### Page 48

@A300-600
SERVICE BULLETIN
**CONF 002
(1) Subtask 286114-410-402-001 - Install the Fuel Tank Access Panels at the LH Wing
Work Zones and Access Panels
Zone
 Access/Work location
550
 Access
 Panel 550BB
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
(a) At the LH wing, refer to AMM 28-11-22, Page Block 401, install the fuel tank
access panel 550BB.
(2) Subtask 286114-410-401-001 - Install the Fuel Tank Access Panels at the RH Wing
Work Zones and Access Panels
Zone
 Access/Work location
650
 Access
 Panel 650BB
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-22, Page Block 401
(a) At the LH wing, refer to AMM 28-11-22, Page Block 401, install the fuel tank
access panel 650BB.
(3) Subtask 286114-410-403-002 - Install the Fuel Tank Access Panels at the Trim Tank
Work Zones and Access Panels
Zone
 Access/Work location
311
 Access
 Panel 319AZ
312
 Access
 Panel 319BZ
Manpower Resources
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 28-11-33, Page Block 401
(a) At the trim tank, refer to AMM 28-11-33, Page Block 401, install the fuel tank
access panels 319AZ and 319BZ.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 42
7
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### Page 49

@A300-600
SERVICE BULLETIN
(4) Subtask 286114-942-402-001 - Close-Up
Manpower Resources
Skills
 NON SPECIFIC
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Remove the access platform(s).
(c) Put the aircraft back to its initial configuration.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 43
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 50

@A300-600
SERVICE BULLETIN
**CONF 001
C
BEFORE
TYPICAL
HOOD HALF
FILTER
FUEL PUMP
CANISTER
HOOD HALF
TYPICAL
C
B
C
A
LH WING SHOWN
RH WING SIMILAR
A
A
RIB14
B D
(2)
(3)
(2)
(3)
(1)
(3)
(2)
Z500
Z600
REAR SPAR
Z650RH
Z550LH
D_SB_286114_7_BAAA_01_00
Figure A-UBAAA - Sheet 01
Removal and Installation of the Fuel Pump Canister Hood Halves in the Outer Tanks
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 44
7
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### Page 51

@A300-600
SERVICE BULLETIN
**CONF 001
TYPICAL
MAINTAIN A
CLEARANCE HERE
A A
E
NOTE:
MAKE SURE THAT THE CLEARANCE IS 01
EQUAL BETWEEN THE HOOD HALVES.
4
1
2
3
3
2
A
A
4 01
01
1
E
TYPICAL
D
AFTER
HOOD HALF
FILTER
FUEL PUMP
CANISTER
HOOD HALF
E
D_SB_286114_7_BAAA_02_01
Figure A-UBAAA - Sheet 02
Removal and Installation of the Fuel Pump Canister Hood Halves in the Outer Tanks
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 45
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 52

@A300-600
SERVICE BULLETIN
**CONF 002
D
A
A
LH WING SHOWN
RH WING SIMILAR
A
RIB14
B
Z319
B
BEFORE
TYPICAL
HOOD HALF
FILTER
FUEL PUMP
CANISTER
HOOD HALF
TYPICAL
C E
C E
C
D
D
(2)
(3)
(2)
(3)
(1)
(3)
(2)
Z500
Z600
REAR SPAR
Z650RH
Z550LH
D_SB_286114_7_BAAB_01_00
Figure A-UBAAB - Sheet 01
Removal and Installation of the Fuel Pump Canister Hood Halves in the Outer Tanks and Trim Tank
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 46
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 53

@A300-600
SERVICE BULLETIN
**CONF 002
F
TYPICAL
MAINTAIN A
CLEARANCE HERE
A A
AFTER
TYPICAL
NOTE:
MAKE SURE THAT THE CLEARANCE IS 01
EQUAL BETWEEN THE HOOD HALVES.
E
F
4
1
HOOD HALF
FUEL PUMP
CANISTER
FILTER
HOOD HALF
F
2
3
3
2
A
A
4 01
01
1
D_SB_286114_7_BAAB_02_01
Figure A-UBAAB - Sheet 02
Removal and Installation of the Fuel Pump Canister Hood Halves in the Outer Tanks and Trim Tank
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 47
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 54

@A300-600
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 48
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 55

@A300-600
SERVICE BULLETIN
Appendix 01 - Manpower Gantt Chart
**CONF 001
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−28−6114
GET ACCESS 1.00 1.00
4.00 2.00
4.00 2.00
0.50 0.50
0.50 0.50
1
2
2
1
1
CLOSE−UP 1.00 1.00 1
REPLACE THE HOOD HALVES OF THE FUEL PUMP
CANISTERS IN THE LH OUTER WING TANK
REPLACE THE HOOD HALVES OF THE FUEL PUMP
CANISTERS IN THE RH OUTER WING TANK
RE−IDENTIFY THE FUEL PUMP CANISTERS
IN THE LH OUTER WING TANK
RE−IDENTIFY THE FUEL PUMP CANISTERS
IN THE RH OUTER WING TANK
MH ET/S
TOTAL MANHOURS
SB ELAPSED TIME
11.00
4.50
STEPS
50
MH
ET/S:
PER
MANHOURS
ELAPSED TIME PER STEP
NUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.
OPERATORS MAY DETERMINE THAT ANOTHER WAY
TO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
:
:
SB ELAPSED TIME
(HOURS)
1 2 3 4
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS
ARE NOT REFLECTED IN THIS GANTT CHART.
D_SB_286114_7_AAAA_01_00
Figure A-UAAAA - Sheet 01
Manpower Gantt Chart
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 56

@A300-600
SERVICE BULLETIN
Appendix 01 - Manpower Gantt Chart
**CONF 002
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−28−6114
GET ACCESS 1.00 1.00
4.00 2.00
4.00 2.00
0.50 0.50
0.50 0.50
1
2
2
1
1
CLOSE−UP 1.00 1.00 1
REPLACE THE HOOD HALVES OF THE FUEL PUMP
CANISTERS IN THE LH OUTER WING TANK
REPLACE THE HOOD HALVES OF THE FUEL PUMP
CANISTERS IN THE RH OUTER WING TANK
RE−IDENTIFY THE FUEL PUMP CANISTERS
IN THE LH OUTER WING TANK
RE−IDENTIFY THE FUEL PUMP CANISTERS
IN THE RH OUTER WING TANK
4.00 2.00
0.50 0.50
2
1
REPLACE THE HOOD HALVES OF THE FUEL PUMP
CANISTERS IN THE TRIM TANK
RE−IDENTIFY THE FUEL PUMP CANISTERS
IN THE TRIM TANK
MH ET/S
TOTAL MANHOURS
SB ELAPSED TIME
15.50
4.50
STEPS
50
MH
ET/S:
PER
MANHOURS
ELAPSED TIME PER STEP
NUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.
OPERATORS MAY DETERMINE THAT ANOTHER WAY
TO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
:
:
SB ELAPSED TIME
(HOURS)
1 2 3 4
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS
ARE NOT REFLECTED IN THIS GANTT CHART.
D_SB_286114_7_AAAB_01_00
Figure A-UAAAB - Sheet 01
Manpower Gantt Chart
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 57

@A300-600
SERVICE BULLETIN
Service Bulletin REPORTING
TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL FUEL PUMP CANISTER
WITH NEW HOOD/MESH FOR OUTER AND TRIM TANK POSITIONS
MODIFICATION No.: 13643H5740 13740H5756
NOTE
: Please ignore the above note (if it is present), this note is auto-generated and does
not apply to this SB.
NOTE
: This modification is related to an airworthiness issue which has been re-classified
and confirmed by EASA as minor in acco rdance with EU Part 21.A.91. As
such, this is handled by AIRBUS under its Design Organisation Approval No.
EASA.21J.031.
SB Reporting status
This Service Bulletin will only be incorporated into affected customized Maintenance and Flight
Operations Products if it is duly reported to Airbus.
General information
The SB Reporting policy is published in ISI 00.00.00135. This document provides information regarding:
the SB Reporting means and benefits, the update of customized Maintenance Products and customized
Flight Operations Products.
If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations Products" for
further information on the update of affected Flight Operations Products.
SB Reporting procedure
Standard practice to report SB is to use the online reporting application on AirbusWorld.
Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus. Question 2 "What are the standard
practices for SB reporting?"
- If this SB requires previous or simultaneous accomplishment of other SBs, Question 3 "What about
the reporting of prerequisite Service Bulletin?"
NOTE:
 ISI 00.00.00179 covers all the frequently asked questions about SB Reporting. It is revised on a
regular basis.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 58

@A300-600
SERVICE BULLETIN
QUALITY PERCEPTION FORM
Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data
that you provide us will be used to analyse areas of difficulties and to take corrective action to further
improve the quality of our Service Bulletins.
We thank you for the time you have taken in completing this form.
(Please rate on a scale of 1 to 4, with 4 being the highest score)
- Quality rating of this SB 4321
- Quality rating of the Accomplishment Instructions 4321
- Quality rating of the Illustrations 4321
- Is this SB easy to understand ? Y/N
If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a
short description of the issue.
Planning Material Instructions
X Effectivity X Kit content X Preparation
X Reason X List of Materials Operator Supplied X Mod/Inspection
X Manpower X Industry support X Test
X References X Re-identification X Close-Up
X Publication X Tooling X Illustrations
Comments:
Operator: Date:
Name/Title:
Please return this form to:
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn : SEM4 Service Bulletins Management
F A X:( 3 3 )56 19 34 25 1
Or via your Resident Customer Support Office.
DATE: Jan 09/17 SERVICE BULLETIN No.: A300-28-6114
REVISION No.: 00 - Jan 09/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

---
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