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@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET 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
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 28 TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL NEW FUEL PUMPS
WITH IMPROVED THERMAL PROTECTION MODIFICATION No.: 13765H5761 This page transmits Revision No.01 of Service Bulletin No.A300-28-6111
ADDITIONAL WORK **CONF ALL REASON Revision No. 01 issued to update the tables in paragraph 1.A.(4) Configuration by MSN.
CHANGES
FRONT MATTER
FUEL - MAIN FUEL PUMP SYSTEM -
INSTALL NEW FUEL PUMPS WITH
IMPROVED THERMAL PROTECTION
CONFIGURATION UPDATED R
SUMMARY
EFFECTIVITY
OPERATOR LIST UPDATED R
PLANNING INFORMATION
EFFECTIVITY
EFFECTIVITY RELATED INFORMATION
UPDATED R Configuration definition CONF 001
CONFIGURATION DEFINITION UPDATED R CONF 002
CONFIGURATION DEFINITION 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.
DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
HISTORY OF PREVIOUS REVISIONS No previous revision
REVISION SEQUENCE ORIGINAL: Dec 15/15 REVISION No. : 01 - Feb 29/16 DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 2 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 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.
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 28 TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL NEW FUEL PUMPS
WITH IMPROVED THERMAL PROTECTION **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR 13765H5761 MINOR None 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.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES As a result of vendor testing, it has been shown that under specific circumstances, with the combination of conditions the fuel pump thermal fuses may not open in time to prevent fuel pump overheat and subsequent in tank ignition. As a result a new standard of fuel pump motor has been developed with improved thermal protection. The new standard restores compliance with the SFAR88 policy.
This Service Bulletin is published to advise all operators of A300-600 series aircraft of the issue of ZODIAC Service Bulletin No. 2052C23-28-02.
This Service Bulletin installs the new standard of fuel pump to all positions.
Fuel pumps can be modified to the latest standard by two means:
- Return to vendor for exchange or modification
- Modify in accordance with ZODIAC Service Bulletin No. 2052C23-28-02.
Accomplishment of this Service Bulletin will improve the fuel pump thermal protection and fully restore compliance to the SFAR88 policy. Full embodiment of this modification is expected to terminate the repeat inspection requirements of AD 2013-0163.
DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY 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 MANDATORY (1)
CANCELS INSPECTION SB NO
POTENTIAL AD YES
A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED YES NOTE
(1) : Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION **CONF 001 No Material **CONF 002 No Material
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
REFERENCES / REPERCUSSIONS TFU
28.21.00.053 OEB None AOT A28W002-13 SIL None ISI None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None OTHER None
NATURE OF THE WORK
AIRCRAFT NO
EQUIPMENT YES DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY HARD NO SOFT NO OBRM NO
MANPOWER **CONF 001 Task 286111-831-895-001: Modification
TOTAL MANHOURS
13.00
ELAPSED TIME (HOURS)
13.00 Additional manhours relat ed to Vendor SB; refer to:
Exchange or Modify the Fuel System Booster Pumps ZODIAC Service Bulletin No.
2052C23-28-02 **CONF 002 Task 286111-831-895-001: Modification
TOTAL MANHOURS
16.50
ELAPSED TIME (HOURS)
16.50 Additional manhours relat ed to Vendor SB; refer to:
Exchange or Modify the Fuel System Booster Pumps ZODIAC Service Bulletin No.
2052C23-28-02
APPENDICES **CONF ALL None DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF 001
LH SHOWN
RH SIMILAR
RH PUMP
LH PUMP FR46 FR47A RIB2 RIB14 Z540 (Z640) No 2 PUMP RH LH No 1 PUMP Z550 (Z650) B 43QA 50QA RH LH 44QA 49QA 280004 280007 280006 280005 No 2 PUMP RH LH280008 280011 45QA 48QA No 1 PUMP RH LH280010 280009 47QA 46QA 280013 280012 82QA 81QA B Z600 Z500 B − Z141 Z142 A D_SB_286111_7_SAAA_01_00 Figure A-USAAA - Sheet 01 DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF 002 B Z600 Z500
LH SHOWN
RH SIMILAR
RH PUMP
LH PUMP FR46 FR47A RIB2 RIB14 Z540 (Z640) No 2 PUMP RH LH No 1 PUMP Z550 (Z650) B B 43QA 50QA RH LH 44QA 49QA 280004 280007 280006 280005 No 2 PUMP RH LH280008 280011 45QA 48QA No 1 PUMP RH LH280010 280009 47QA 46QA 280013 280012 82QA 81QA PUMP 2 280431 14QN PUMP 1 280430 13QN FWDC − Z141 Z142 C A Z319 D_SB_286111_7_SAAB_01_00 Figure A-USAAB - Sheet 01 DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 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: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 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 T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 28 TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL NEW FUEL PUMPS
WITH IMPROVED THERMAL PROTECTION MODIFICATION No.: 13765H5761 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 NOTE : This modification is applicable by Service Bulletin only.
(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: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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 0717 0722 AHK 0683 0770 0855 0856 0857 0858 0859 0860 0870 0871 BCS 0602 0617 0621 0637 0641 0670 0677 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: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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 applicable to all A300-600 aircraft in the effectivity of this Service Bulletin (with no trim tank fitted).
**CONF 002 Config. 002 is applicable to all A300-600R aircraft in the effectivity of this Service Bulletin (with a trim tank fitted).
(6) Material Effectivity
MATERIAL
QTY PER A/C
SEE NOTES Reidentified part set REIDB01 1 B. CONCURRENT REQUIREMENTS None C. REASON
(1) History As a result of vendor testing, it has been shown that under specific circumstances, with the combination of conditions the fuel pump thermal fuses may not open in time to prevent fuel pump overheat and subsequent in tank ignition. As a result a new standard of fuel pump motor has been developed with improved thermal protection. The new standard restores compliance with the SFAR88 policy.
DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
(2) Objective/Action This Service Bulletin is published to advise all operators of A300-600 series aircraft of the issue of ZODIAC Service Bulletin No. 2052C23-28-02.
This Service Bulletin installs the new standard of fuel pump to all positions.
Fuel pumps can be modified to the latest standard by two means:
- Return to vendor for exchange or modification
- Modify in accordance with ZODIAC Service Bulletin No. 2052C23-28-02.
(3) Advantages Accomplishment of this Service Bulletin will improve the fuel pump thermal protection and fully restore compliance to the SFAR88 policy. Full embodiment of this modification is expected to terminate the repeat inspection requirements of AD 2013-0163.
(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 286111-831-895-001: Modification
(1) Remove the LH Wing Inner Tank Booster Pumps
(2) Remove the LH Wing Outer Tank Booster Pumps
(3) Remove the Center Tank Booster Pumps
(4) Remove the RH Wing Inner Tank Booster Pumps
(5) Remove the RH Wing Outer Tank Booster Pumps
(6) Exchange or Modify the Fuel System Booster Pumps
(7) Install the LH Wing Inner Tank Booster Pumps
(8) Install the LH Wing Outer Tank Booster Pumps
(9) Install the Center Tank Booster Pumps
(10) Install the RH Wing Inner Tank Booster Pumps
(11) Install the RH Wing Outer Tank Booster Pumps DATE: Dec 15/15 SERVICE BULLETIN No.: A300-28-6111 REVISION No.: 01 - Feb 29/16 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.