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This text is OCR from a scan. OCR can misread letters and numbers. © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-0465; AD 2016-20-13 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
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GA340
SERVICE BULLETIN AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex: AIRBU 530526F Fax : (33) 5 61 93 42 51
MANDATORY MANDATORY MANDATORY ATA SYSTEM: 53 TITLE: FUSELAGE - INSPECTION OF SKIN DOUBLER REPAIR AT STRINGER 9 JUNCTION BETWEEN FR 10 AND FR13 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
1. PLANNING INFORMATION **CONF ALL
EFFECTIVITY
(1) Models 340-211 340-212 340-213 340-311 340-312 340-313
(2) Effectivity by MSN 0002 0004 0006 0009 0014 0020 0022-0026 0029 0031-0035 0038 0041 0043-0044 0046-0047 0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085 0089-0091 0093-0094 0101 0104 0117 0123 0125-0126 0128 0131 0134-0137 0139 0141-0142 0145-0 0166-0170 0173-0176 0178-0180 0196-0197 0199 0201-0202 0207-0208 0210 0212 28 0233 0236-0237 0242-0243 0245-0246 0252 0257 0260 -0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0319 0321 0325 0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0429-0430 0433-0435 0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 1 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
GA340
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 06Y 0139 0149 15R 0151 151 0009 31V 0093 0257 36V 0024 0052 56W 0006 74W 0047 0051 83V 0216 0280 0292 98X 6Z70 ABD AFR AIB 0131 0141 0161 0182 0192 0199 ALD 0156 0159 0178 ALK 0032 0033 0034 0367 0374 0381 ARG 0085 0094 0123 0126 0128 0170 0193 0373 BOE 0554 CAL 0402 0406 0411 0415 0433 0541 CCA 0201 0242 0243 0264 CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 DGA 0075 0081 DLH 0035 0053 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447 0063 0074 0080 0058 0168 0174 0835 0844 0921 0938 0274 0355 0117 0190 0202 0164 0125 0134 0145 0146 0217 0221 0329 0483 0002 0020 0056 0282 0089 0090 0101 0104 0359 0363 0442 0061 0076 0152 0194 0268 0793 0800 0319 0173 0176 0187 0196 0302 0318 0332 0387 0459 0474 0212 0215 0026 0528 0014 0022 0038 0043 S3R 0004 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 2 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
DA340
SERVICE BULLETIN
OPERATOR MSN SAA 0197 0378 0544 0582 0590 0643 0646 0651 SAS 0167 0413 0424 0430 0435 0450 0467 0470 SFB 0046 SLM 0049 SVW 0955 SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0562 0585 0598 TAP 0041 0044 0079 0091 THT 0385 0395 0438 0446 0668 THY 0023 0025 0057 0115 0180 0270 0331 UAE 0163 0166 0185 0236 VCV 0031 VIR 0114 0214 XAX 0273 0278
(4) Configuration by MSN
MSN CONFIGURATION 0002 0004 0006 0009 0014 0020 0022 0023 0024 0025 0026 001 0029 0031 0032 0033 0034 0035 0038 0041 0043 0044 0046 0047 0049 0051 0052 0053 0056 0057 0058 0061 0063 0074 0075 0076 0078 0079 0080 0081 0084 0085 0089 0090 0091 0093 0094 0101 0104 0114 0115 0117 0123 0125 0126 0128 0131 0134 0135 0136 0137 0139 0141 0142 0145 0146 0147 0149 0150 0151 0152 0154 0156 0157 0158 0159 0160 0161 0163 0164 0166 0167 0168 0169 0170 0173 0174 0175 0176 0178 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214 0215 0216 0217 0218 0220 0221 0227 0228 0233 0236 0237 0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270 0273 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352 0354 0355 0359 0363 0367 0373 0374 0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0429 0430 0433 0434 0435 0438 0442 0446 0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0544 0545 0546 0554 0556 0559 0561 0562 0582 0585 0590 0598 0643 0646 0651
(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 No Material Set 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 3 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
GA340
SERVICE BULLETIN B. CONCURRENT REQUIREMENTS None C. REASON
(1) History Following changes in Apr-2013 revision and Temporary Revision 53-001 (dated Nov 28/14) of SRM A340-200/-300, and with regards to previously embodied SRM repairs, Airbus is requiring the operators to apply specific actions defined in this Service Bulletin.
(2) Objective/Action This Service Bulletin requires the operators to identify records of SRM skin doubler repairs at stringer 9 longitudinal panel junction between Frame 10 and Frame 13.
In case of an existing SRM repair, recorded prior to SRM Temporary Revision 53-001 (dated Nov 28/14), is located in excluded area of SRM Temporary Revision 53-001 (dated Nov 28/14) or subsequent SRM revision, please contact AIRBUS Repair Support (SEOE) for further instructions.
In case of an existing SRM repair, recorded prior to SRM Temporary Revision 53-001 (dated Nov 28/14), is not located in excluded area of SRM Temporary Revision 53-001 (dated Nov 28/14) or subsequent SRM revision, please update recorded inspection instructions in line with the current SRM requirements.
(3) Advantages Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of skin doubler repairs of the longitudinal panel junction at stringer 9 between Frame 10 and Frame 13.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
Task 534225-832-801-001: Inspection
(1) Check if Skin Repairs on Longitudinal Junction at Stringer 9, between Frames 10 and 13, LH and RH Sides, have been accomplished Task 534225-832-802-001: ADDITIONAL WORK for Aircraft on which Service Bulletin No.
A330-53-4225 Revision No. 00 has already been embodied
(1) Check if Skin Repairs on Longitudinal Junction at Stringer 9, between Frames 10 and 13, LH and RH Sides, have been accomplished 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 4 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
GA340
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 Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds given but reference should be made to the AD for confirmation of the mandated accomplishment timescale.
Table 1, Config. 001 - Inspection of SRM skin repair records at stringer 9 longitudinal panel junction between Frame 10 and Frame 13 Condition Action Compliance time Repetitive interval Threshold Grace period All aircraft Check the aircraft Before Sep-2015 None None maintenance program documentation for existing repairs, in accordance with the Subtask 534225-832-001-001 No existing repair No further action None None None covered by a SRM necessary within version prior to this Service Temporary Bulletin Revision 53-001 (Nov 28/14) Existing repair Contact AIRBUS As soon as None None covered by a SRM with detailed repair possible Before version prior to report for specific Sep-2015 Temporary assessment and See NOTE (*) Revision 53-001 tollow their (Nov 28/14) and instructions repair located in an excluded area of Temporary Revision 53-001 (Nov 28/14) or subsequent SRM revision 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
GA340
SERVICE BULLETIN Table 1, Config. 001 - Inspection of SRM skin repair records at stringer 9 longitudinal panel junction between Frame 10 and Frame 13 Condition Action Compliance time Repetitive interval Threshold Grace period Existing repair Update recorded During None None covered by a SRM inspection accomplishment of version prior to instructions in line this Service Temporary with the current Bulletin Revision 53-001 SRM requirements (Nov 28/14) and repair not located in an excluded area of Temporary Revision 53-001 (Nov 28/14) or subsequent SRM revision NOTE (*): It is recommended to contact Airbus 6 months before the end of the Compliance Time.
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 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 Task 534225-832-801-001: Inspection On Bench Check if Skin Repairs on Longitudinal Junction at 2.00 Stringer 9, between Frames 10 and 13, LH and RH Sides, have been accomplished TOTAL MANHOURS 2.00 Task 534225-832-802-001: ADDITIONAL WORK for Aircraft on which Service Bulletin No.
A330-53-4225 Revision No. 00 has already been embodied On Bench 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved
©A340
SERVICE BULLETIN Task 534225-832-802-001: ADDITIONAL WORK for Aircraft on which Service Bulletin No.
A330-53-4225 Revision No. 00 has already been embodied Check if Skin Repairs on Longitudinal Junction at 2.00 Stringer 9, between Frames 10 and 13, LH and RH Sides, have been accomplished TOTAL MANHOURS 2.00 H. WEIGHT AND BALANCE Not Changed
ELECTRICAL LOAD DATA Not Changed J. REFERENCES Elec. Std. Practices Manual (ESPM) 20-55-00 Structural Repair Manual (SRM) 53-11-11 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
©A340
SERVICE BULLETIN This Page Intentionally Left Blank 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 8 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
GA340
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 the Service Bulletin.
C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 9 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
©A340
SERVICE BULLETIN This Page Intentionally Left Blank 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 10 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
©A340
SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 534225-832-801-001 - Inspection WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: 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: The purpose of flow charts is to supplement the information given in the Procedure and Compliance paragraphs and not to serve as the primary source for tasks or compliance times given in this Service Bulletin.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition.
5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 11 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
GA340
SERVICE BULLETIN Task Associated Data Manpower TOTAL MANHOURS 2.00 A. GENERAL
(1) Subtask 534225-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.
B. PREPARATION None C. PROCEDURE
(1) Subtask 534225-832-001-001 - Check if Skin Repairs on Longitudinal Junction at Stringer 9, between Frames 10 and 13, LH and RH Sides, have been accomplished Manpower Resources Manhours 2.00 Minimum number of person Subtask elapsed time 2.00 Skills NON SPECIFIC References Structural Repair Manual (SRM) 53-11-11, Page Block 201 Fig. A-FFAAA Sheet 01 Flow Chart NOTE: For the accomplishment timescale, refer to 1.E. (2).
(a) Check in the aircraft maintenance program documentation if skin repairs on longitudinal junction at stringer 9, between frames 10 and 13, have been accomplished in accordance with any of the following SRM references:
SRM 53-11-11, Page Block 201, paragraph 5.D (Figure 204) SRM 53-11-11, Page Block 201, paragraph 5.E (Figure 205) SRM 53-11-11, Page Block 201, paragraph 5.I (Figure 209)
- SRM 53-11-11, Page Block 201, paragraph 5.J (Figure 210) Refer to Flow Chart Fig. A-FFAAA 5 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4225 REVISION No.: 01 - Jan 14/15 Page: 12 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.