On this page
ADs that cite it · 1
Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.
Also cited in 1 proposed AD.
Text · 27
From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document. © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-9051; AD 2017-06-04 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '29c28f7462d19ff2e8476033d14ed2035727aaa8d6293aaa019b9e172938ed27' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '29c28f7462d19ff2e8476033d14ed2035727aaa8d6293aaa019b9e172938ed27' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
@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 - REAR FUSELAGE - INSPECT SKIN LAP JOINT BELOW STGR 28 BETWEEN FR72 AND FR76, LH AND RH.
**CONF ALL
MODIFICATIONS None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During a routine check on an A300 A/C a damage was initially noticed above the right MID passenger/crew door. After removal of the insulation blankets on the area, a crack was found in the door surrounding panel.
The crack spread longitudinally from Frame(FR) 29 to FR30 approximately, along the radius of the skin panel step. It was not visible from the outside of the A/C because it spreads along a line that is always covered by a sealant bead at the junction of two panels.
A Fatigue and Damage Tolerance (F & DT) analysis was done for the A300-600 A/C fleet for a potential similar issue.
It was concluded that the same kind of longitudinal crack could develop on this fleet in similar area in terms of stress loading and design, which are located at joint between FR72 and FR76 described in this Service Bulletin.
The objective of this Service Bulletin is to provide the necessary instructions, the intervals and the appropriate actions for the inspection of the affected area on A300-600 aircrafts.
Accomplishment of this Service Bulletin will support detection of possible cracks at an early stage, which will contribute to avoid any extensive repair and aircraft down time. Undetected cracks could affect the structural integrity of the area concerned.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1)
CANCELS INSPECTION SB NO
POTENTIAL AD YES
A/C OPERATION AFFECTED NO DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO NOTE
(1) : Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION No Material
EFFECTIVITY 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 UQA URS UTP
CONCURRENT REQUIREMENTS None
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 NO HARD NO SOFT NO OBRM NO
MANPOWER Task 536184-832-848-001: Inspection
TOTAL MANHOURS
6.00
ELAPSED TIME (HOURS)
5.00
APPENDICES Appendix 01 - Elapsed Time Assumption DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF ALL Z170 A FR76 FR75A FR75 FR74 FR73A FR73A
LH SHOWN RH SYMMETRICAL FR72 STGR28 STGR29
INSPECTION OF SKIN LAP JOINT D_SB_536184_6_SAAA_01_01 Figure A-G SAAA - S heet 01 Inspection of the Skin Lap Joint. Affected area DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY This Page Intentionally Left Blank DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 4 6 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 - REAR FUSELAGE - INSPECT SKIN LAP JOINT BELOW STGR 28 BETWEEN FR72 AND FR76, LH AND RH.
MODIFICATION No.: None This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent.
1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY
(1) Models B4-603 B4-605R B4-605RF B4-622F B4-622R B4-622RF C4-605R/F C4-620
(2) Effectivity by MSN 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 0721-0725 0727 0729-0730 0732-0734 0737 0739-0741 0743-0744 0746 0749-0750 0753-0756 0758 0762-0764 0770 0773 0775 0782-0788 0797 0836-0838
(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.
DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
OPERATOR MSN 67Q 0584 0603 0744 0749 0764 ABR 0557 0717 0722 AHK 0683 0770 BCS 0529 0602 0617 0621 0637 0641 0670 0677 0679 0703 0711 0724 0729 0730 0737 0740 0743 0753 0783 0797 0836 0837 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 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 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 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 0727 0729 0730 0732 0733 0734 0737 0739 0740 0741 0743 0744 0746 0749 0750 0753 0754 0755 0756 0758 0762 0763 0764 0770 0773 0775 0782 0783 0784 0785 0786 0787 0788 0797 0836 0837 0838 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 Consumable CMLD01 1 DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN B. CONCURRENT REQUIREMENTS None C. REASON
(1) History During a routine check on an A300 A/C a damage was initially noticed above the right MID passenger/crew door. After removal of the insulation blankets on the area, a crack was found in the door surrounding panel.
The crack spread longitudinally from Frame(FR) 29 to FR30 approximately, along the radius of the skin panel step. It was not visible from the outside of the A/C because it spreads along a line that is always covered by a sealant bead at the junction of two panels.
A Fatigue and Damage Tolerance (F & DT) analysis was done for the A300-600 A/C fleet for a potential similar issue.
It was concluded that the same kind of longitudinal crack could develop on this fleet in similar area in terms of stress loading and design, which are located at joint between FR72 and FR76 described in this Service Bulletin.
(2) Objective/Action The objective of this Service Bulletin is to provide the necessary instructions, the intervals and the appropriate actions for the inspection of the affected area on A300-600 aircrafts.
(3) Advantages Accomplishment of this Service Bulletin will support detection of possible cracks at an early stage, which will contribute to avoid any extensive repair and aircraft down time.
Undetected cracks could affect the structural integrity of the area concerned.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
Task 536184-832-848-001: Inspection
(1) Inspect the Skin Lap Joint below STGR 28 between FR72 and FR76, LH
(2) Inspect the Skin Lap Joint below STGR 28 between FR72 and FR76, RH DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the (thresholds and/or intervals and/or date) given but reference should be made to the AD for confirmation of the mandated accomplishment timescale.
Table 01, Config 001 - Do a Special Detailed Inspection (SDI) of the skin lap joint below STGR 28 between FR72 and FR76
COMPLIANCE TIME
CONDITION ACTION Threshold Grace Period
REPETITIVE
INTERVAL All aircraft Do a Special Detailed Inspection (SDI) of skin lap joint below STGR 28 between FR72 and FR76 29500 FC from the aircraft Entry In Service date 2000 FC from AD effective date None No cracks found Repeat the inspection None None Within 5400 FC Crack found Contact AIRBUS and follow their instructions Before next flight None None F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approv al 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.
Task 536184-832-848-001: Inspection Get Access
1.50 On Aircraft DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN Task 536184-832-848-001: Inspection Inspect the Skin Lap Joint below STGR 28 between FR72 and FR76, LH
1.00 Inspect the Skin Lap Joint below STGR 28 between FR72 and FR76, RH
1.00 Close-Up
2.50
TOTAL MANHOURS
6.00
ELAPSED TIME (HOURS)
5.00 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-GAAAA given in Appendix 01.
H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES Aircraft Maintenance Manual (AMM) 06-21-00 06-31-53 20-21-12 24-00-00 25-22-11 28-26-15 36-12-00 52-34-00 53-17-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 Non Destructive Test Manual (NTM) 53-18-02 Structural Repair Manual (SRM) 51-21-00 51-23-20 K. PUBLICATION AFFECTED Non Destructive Test Manual (NTM) 53-18-02 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN This Page Intentionally Left Blank DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 6 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses None
(2) Price and Availability None B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin.
C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials Consumable CMLD01 ITEM
DESCRIPTION
REFERENCE TO CML MAT. No.
QTY PER A/C SEE NOTES Non Aqueous Cleaner-General 08BAA9 As required Textile-Lint Free Cotton 14SBA1 As required
(2) Components None
(3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 7 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN This Page Intentionally Left Blank DATE: Nov 12/15 SERVICE BULLETIN No.: A300-53-6184 REVISION No.: 00 - Nov 12/15 Page: 8 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.