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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: 53 TITLE: FUSELAGE - CENTER FUSELAGE - REINFORCE UPPER FRAME FEET FITTINGS.
MODIFICATION No.: 12168S21823 12977S22524 This page transmits Revision No.04 of Service Bulletin No.A300-53-6125
ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue.
REASON Revision No. 04 issued to:
- update the threshold for the accomplishment timescale,
- remove cross-references to Service Bulletin No. A300-53-6122 in order to replace them by the Task Airworthiness Limitation Items (ALI) 53-15-58 which cancel Service Bulletin No.
A300-53-6122.
CHANGES The main changes of this revision are:
- Task Airworthiness Limitation Items (ALI) 53-15-58 added,
- Service Bulletin No. A300-53-6122 deleted,
- Threshold updated.
SUMMARY
REASON/DESCRIPTION/OPERATIONAL
CONSEQUENCES
REASON UPDATED R
GENERAL EVALUATION
GENERAL EVALUATION TABLE UPDATED R
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
UPDATED R DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
EFFECTIVITY
OPERATOR LIST UPDATED R
REFERENCES / REPERCUSSIONS
REFERENCES/REPERCUSSIONS TABLE
UPDATED R
PLANNING INFORMATION
EFFECTIVITY
EFFECTIVITY RELATED INFORMATION
UPDATED R Configuration definition
CONFIGURATION LIST UPDATED R CONF 001
CONFIGURATION DEFINITION UPDATED R Material Effectivity
MATERIAL EFFECTIVITY UPDATED R REASON
REASON UPDATED R History
HISTORY UPDATED R Objective/Action
OBJECTIVE/ACTION UPDATED R Advantages
ADVANTAGES UPDATED R
COMPLIANCE Accomplishment Timescale
ACCOMPLISHMENT TIMESCALE UPDATED R
REFERENCES
REFERENCES UPDATED R
REFERENCED DOCUMENTATION UPDATED R
PUBLICATION AFFECTED
PUBLICATIONS AFFECTED UPDATED R
PUBLICATIONS AFFECTED ADDED N
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY
MATERIAL - PRICE AND AVAI LABILITY UPDATED R Procurement Addresses
PROCUREMENT ADDRESSES UPDATED R Price and Availability
PRICE AND AVAILABILITY UPDATED
MATERIAL AVAILABILITY UPDATED
MATERIAL PRICE UPDATED
MATERIAL SET UPDATED R
LIST OF COMPONENTS Kit 536125A01R01
PART MATERIAL SET UPDATED
QUANTITY UPDATED R
LIST OF MATERIALS - OPERATOR
SUPPLIED Consumable Materials Consumable CMLA01
CONSUMABLE MATERIAL SET UPDATED
CONSUMABLE UPDATED R Components
COMPONENTS UPDATED R Component COMPA01
PART MATERIAL SET UPDATED R
TOOLING Tools
TOOLS UPDATED R
ACCOMPLISHMENT INSTRUCTIONS TASK 536125- 831-801-001-
MODIFICATION
TASK SOLUTION UPDATED
NOTE UPDATED
CAUTION UPDATED R Subtask 536125-910-001-001
SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
REFERENCED DOCUMENTATION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED R DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Subtask 536125-839-002-001
SUBTASK SOLUTION ADDED N Subtask 536125-839-001-001
SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN D Subtask 536125-941-002-001
SUBTASK SOLUTION UPDATED
NOTE UPDATED
REFERENCED DOCUMENTATION UPDATED
PANEL UPDATED
ZONE UPDATED R Subtask 536125-831-004-001
SUBTASK SOLUTION UPDATED R Subtask 536125-831-005-001
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 536125-831-006-001
SUBTASK SOLUTION UPDATED R Subtask 536125-831-007-001
SUBTASK SOLUTION UPDATED R Subtask 536125-831-008-001
SUBTASK SOLUTION UPDATED R Subtask 536125-831-009-001
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 536125-831-010-001
SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED R Subtask 536125-942-019-001
SUBTASK SOLUTION UPDATED
PANEL UPDATED
REFERENCED DOCUMENTATION UPDATED R Fig. A-FCAAA Fig. A-FCAAA Sheet 02
SHEET UPDATED R Fig. A-FCAAA Sheet 03
SHEET UPDATED R Fig. A-FCBAA Fig. A-FCBAA Sheet 01
SHEET UPDATED R
FILING 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 Revision No. 01 issued to update the thresholds and modify the content following validation on aircraft MSN 0521 and to inform that this Service Bulletin is anticipated to be rendered mandatory.
This Service Bulletin has been validated on A300-600 aircraft MSN 0521.
Revision No. 02 issued to inform the operators that this Service Bulletin is rendered mandatory and to take into account the different configurations from repair solution currently given in ISB A300-53-6122 and modification No. 12977S22524 (CENTER FUSELAGE - REINFORCE FRAME BASE/ARCHJUNCTIONS).
Revision No. 03 issued to :
modify the thresholds value and the grace period, DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET delete the Config. 002 and Kit 536125A02R00 (MSN 0252 scrapped), update the effectivity.
REVISION SEQUENCE ORIGINAL: Nov 08/00 REVISION No.: 02 - Feb 25/05 REVISION No. : 03 - Sep 13/11 REVISION No. : 04 - Mar 17/15 DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 4 5 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: 53 TITLE: FUSELAGE - CENTER FUSELAGE - REINFORCE UPPER FRAME FEET FITTINGS.
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR 12168S21823 MINOR 12977S22524 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 During inspection in accordance with Airworthiness Limitation Items (ALI) 53-15-54 on A300-600 aircraft, Frame 43, Frame 44, Frame 45 and Frame 46 were found cracked between stringers 24 to 30 on the aircraft right hand side and Frame 45 was found cracked on the aircraft left hand side. At the time of inspection, the aircraft had accumulated 26,100 Flight Cycles (FC) and 32,160 Flight Hours (FH).
On in-service aircraft, undetected cracks can lead to the rupture of the frame foot and subsequent cracking of the adjacent frames and fuselage skin which would require an extensive repair and could have an impact on pressure loading strength capacity of the structure.
This Service Bulletin requires performing expansion of the most fatigue sensitive fastener holes between Frame 41 and Frame 46 on the center box, upper fuselage bent sections, to improve the fatigue life of the area.
For information, when this Service Bulletin No. A300-53-6125 is not accomplished, inspections are required as per Airworthiness Limitation Items (ALI) 53-15-58. Previous inspections from Service Bulletin No.
A300-53-6122 are cancelled and superseded by Airworthiness Limitation Items (ALI) 53-15-58 .
DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1)
CANCELS INSPECTION SB NO
POTENTIAL AD YES
A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO
VALIDATION ON AIRCRAFT YES NOTE
(1) : Service Bulletin must be accomplished.
NOTE : This Service Bulletin has been validated at original issue on A300-600 aircraft with Manufacturer Serial Number (MSN) 0521.
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 536125A01R01 2 28,100.00 Bolt, Pin, Collar, Nut Supplementary kit 536125A01S01 2 17,500.00 Bolt, Pin, Collar, Nut TOTAL 45,600.00 Component COMPA01 2 See SB Nut
EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :
06P 67Q ABR AHK BCS F2I FDX IRA IRM KAC MNB MRJ MSR
SUD TAR THA UQA URS UTP UZB
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL 51-012
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT NO HARD NO DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY SOFT NO OBRM NO
MANPOWER Task 536125-831-801-001: MODIFICATION
TOTAL MANHOURS
83.50
ELAPSED TIME (HOURS)
49.00
APPENDICES None DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF ALL A A FR41 FR46 D_SB_536125_5_SAAA_01_00 Figure A-FSAAA - Sheet 01 DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 4 5 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: 53 TITLE: FUSELAGE - CENTER FUSELAGE - REINFORCE UPPER FRAME FEET FITTINGS.
MODIFICATION No.: 12168S21823 12977S22524 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 : Modification No. 12168S21823 is embodied before delivery on aircraft with Manufacturer Serial Number (MSN) 0805 and subsequent.
NOTE : Modification No. 12977S22524 is applicable by Service Bulletin only.
(1) Models B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/F C4-620 F4-605R
(2) Effectivity by MSN 0294 0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0477 0479 0505 0521 0525 0529-0530 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 0799-0804 DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 1 5 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 06P 0788 67Q 0584 0603 0744 0749 0764 ABR 0677 0743 AHK 0683 0770 BCS 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730 0737 0740 0753 0783 0797 F2I 0294 0529 0557 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 IRA 0632 0696 0723 0727 IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701 0773 KAC 0344 0673 0694 0699 0719 0721 MNB 0521 0525 0532 0734 0739 0755 0756 0758 MRJ 0750 0762 MSR 0561 0607 SUD 0666 0775 TAR 0505 0558 0563 THA 0629 0782 0784 0785 0786 0787 UQA 0626 0643 URS 0733 UTP 0707 0725 0732 0741 0746 0754 0763 UZB 0717 0722 DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
(4) Configuration by MSN MSN
CONFIGURATION 0294 0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0477 0479 0505 0521 0525 0529 0530 0532 0536 0543 0546 0553 0555 0557 0558 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 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 001
(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration.
(6) Material Effectivity
MATERIAL
QTY PER A/C
SEE NOTES Kit 536125A01R01 2 Supplementary kit 536125A01S01 2 Component COMPA01 2 Consumable CMLA01 1 This table shows the supplemental kits (S kits) needed to update the kits already held in your stock to the latest status.
Kit Held by Operator Supplementary Kits Required Latest Status of Kit 536125A01R00 536125A01S01 536125A01R01 536125A01R01 NONE 536125A01R01 B. CONCURRENT REQUIREMENTS None DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN C. REASON
(1) History During inspection in accordance with Airworthiness Limitation Items (ALI) 53-15-54 on A300-600 aircraft, Frame 43, Frame 44, Frame 45 and Frame 46 were found cracked between stringers 24 to 30 on the aircraft right hand side and Frame 45 was found cracked on the aircraft left hand side. At the time of inspection, the aircraft had accumulated 26,100 Flight Cycles (FC) and 32,160 Flight Hours (FH).
On in-service aircraft, undetected cracks can lead to the rupture of the frame foot and subsequent cracking of the adjacent frames and fuselage skin which would require an extensive repair and could have an impact on pressure loading strength capacity of the structure.
(2) Objective/Action This Service Bulletin requires performing expansion of the most fatigue sensitive fastener holes between Frame 41 and Frame 46 on the center box, upper fuselage bent sections, to improve the fatigue life of the area.
(3) Advantages For information, when this Service Bulletin No. A300-53-6125 is not accomplished, inspections are required as per Airworthiness Limitation Items (ALI) 53-15-58. Previous inspections from Service Bulletin No.
A300-53-6122 are cancelled and superseded by Airworthiness Limitation Items (ALI) 53-15-58 .
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
Task 536125-831-801-001: MODIFICATION
(1) Do the Cold Expansion of the Holes on FR41.
(2) Do the Cold Expansion of the Holes on FR42.
(3) Do the Cold Expansion of the Holes on FR43.
(4) Do the Cold Expansion of the Holes on FR44.
(5) Do the Cold Expansion of the Holes on FR45.
(6) Do the Cold Expansion of the Holes on FR46.
(7) Repair the Hole H1 on FR41 thru FR46.
(8) ADDITIONAL KIT (introduced by revision 02 of this Service Bulletin) DATE: Nov 08/00 SERVICE BULLETIN No.: A300-53-6125 REVISION No.: 04 - Mar 17/15 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.