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 · 26
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-2016-0465; AD 2016-20-13 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 = 'fcbd6d52952d8877ed0de03316a22529a07448479611441d986f0ef4a5a5bc12' 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 = 'fcbd6d52952d8877ed0de03316a22529a07448479611441d986f0ef4a5a5bc12' 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.
@A340
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 - INSPECTION OF FUSELAGE SKIN PANELS **CONF ALL
MODIFICATIONS None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following changes in the Apr 01/13 revision of the Structural Repair Manual (SRM) for A340 aircraft, and with regards to previously embodied SRM Repairs, AIRBUS now requires operators to apply specific actions listed in this Service Bulletin.
This Service Bulletin is issued to instruct operators to examine their records and take the applicable corrective action when necessary.
Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the fuselage skin panels.
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
LROPS 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) :
DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY 06Y 15R 15T 31V 36V 56W 74W 83V 98X ABD AFR AIB ALD ALK ARG BOE CAL CCA CPA DGA DLH F2I FIN GAF HFY I2L IBE IRM KAC LAN M3R MAU MDG MSR PAL PUE QAF RJA S3R
SAA SAS SFB SLM SVW SWR TAP THT THY UAE VCV VIR XAX
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL 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 **CONF 001 Task 534224-832-848-001: Inspection
TOTAL MANHOURS
1.00
ELAPSED TIME (HOURS)
1.00 **CONF 002 Task 534224-832-848-001: Inspection
TOTAL MANHOURS
1.00
ELAPSED TIME (HOURS)
1.00
APPENDICES **CONF ALL None DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
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 - INSPECTION OF FUSELAGE SKIN PANELS 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 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 0114-0115 0117 0123 0125-0126 0128 0131 0134-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164 0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199 0201-0202 0207-0208 0210 0212-0218 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 0377-0379 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 DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
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 15T 0009 31V 0093 36V 0024 0052 56W 0006 74W 0047 0051 83V 0216 0280 0292 98X 0429 ABD 0210 AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377 0399 AIB 0131 0141 0161 0182 0192 0199 ALD 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 F2I 0063 0074 0080 0257 FIN 0058 0168 0174 0835 0844 0921 0938 GAF 0274 0355 HFY 0117 0190 0202 I2L 0164 IBE 0125 0134 0145 0146 0217 0221 0329 0483 IRM 0002 0020 0056 0282 KAC 0089 0090 0101 0104 LAN 0359 0363 0442 M3R 0061 MAU 0076 0152 0194 0268 0793 0800 MDG 0319 MSR 0156 PAL 0173 0176 0187 0196 0302 0318 0332 0387 0459 0474 PUE 0212 0215 QAF 0026 0528 RJA 0014 0022 0038 0043 DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
OPERATOR MSN S3R 0004 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 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 0545 0546 0554 0556 0559 0561 0562 001 0544 0582 0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955 002
(5) Configuration definition **CONF 001 Config. 001 is valid for aircraft in the effectivity of this Service Bulletin that have not embodied Modification No. 49144S16279.
**CONF 002 Config. 002 is valid for aircraft in the effectivity of this Service Bulletin that have embodied Modification No. 49144S16279.
DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
(6) Material Effectivity None B. CONCURRENT REQUIREMENTS None C. REASON
(1) History Following changes in the Apr 01/13 revision of the Structural Repair Manual (SRM) for A340 aircraft, and with regards to previously embodied SRM Repairs, AIRBUS now requires operators to apply specific actions listed in this Service Bulletin.
(2) Objective/Action This Service Bulletin is issued to instruct operators to examine their records and take the applicable corrective action when necessary.
(3) Advantages Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the fuselage skin panels.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
**CONF 001 Task 534224-832-848-001: Inspection
(1) Do a check of the Aircraft Records **CONF 002 Task 534224-832-848-001: Inspection
(1) Do a check of the Aircraft Records **CONF ALL E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
(2) Accomplishment Timescale Table 01, Config. 001 - A340-200 and A340-300 SRM Update of the Fuselage Skin Doubler Repairs Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval All Aircraft Check the Aircraft records and identify the skin repairs performed as per the Structural Repair Manual (SRM) in the following areas:
Nose forward fuselage (Section 11/12)
- lower shell panels below stringers 31 LH and 31 RH
- lateral and upper panels between Frame (FR) 10 and 18 except panel junction at stringer 9 between FR 10 and 13
- skin panels between FR 18 and 19, below stringers 43 LH/RH Center fuselage (Section
15):
- skin panels between FR 38 and 53.3
- skin panels between FR
53.3 and 54 below stringers 31 LH/RH Forward and rear fuselage (Sections 13, 14, 14A, 15A and 16 thru 18):
- skin panels between FR 18 and 19 above Stringer 43 LH/RH
- skin panels between FR 19 and 38
- skin panels between FR
53.3 and 54 above stringer 31 LH/RH
- skin panels between FR 54 and 80 For repairs in the Nose forward and center fuselage:
- 24 months from September 2014.
See Note (*) For repairs in the forward and rear fuselage:
- 12 months from September 2014 (applicable for aircraft WVs000 series only) or
- 24 months from September 2014 (applicable for aircraft WVs020 series only) See Note (*) None None DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN Table 01, Config. 001 - A340-200 and A340-300 SRM Update of the Fuselage Skin Doubler Repairs Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval Existing repair is covered by a SRM version prior to April 2013 revision and l o c a t e do nn o s e forward fuselage or center fuselage Update the recorded inspection threshold and interval in line with the value given in the April 2013 or subsequent SRM revisions As soon as possible before September 2016. See Note (***) None None Existing repairs covered by a SRM version prior to April 2013 revision, located on the forward and rear fuselage but no longer covered in the current SRM (i.e.:
SRM Figure inactivated or the repair in an excluded area) Contact Airbus with a detailed repair report for specific assessment As soon as possible before September 2015 or September 2016 (for aircraft WVs 020 series only) See note (**) None None Existing repair covered by a SRM version prior to April 2013 revision, located on the forward and rear fuselage and still covered in the current SRM (i.e.: SRM Figure not inactive and the repair is not in an excluded area) Check if the structure underneath the skin (frames or stringers) has been repaired As soon as possible before September 2015 or September 2016 (for aircraft WVs 020 series only) See note (***) None None DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 6 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN Table 01, Config. 001 - A340-200 and A340-300 SRM Update of the Fuselage Skin Doubler Repairs Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval Existing repairs covered by a SRM version prior to April 2013 revision, located on the forward and rear fuselage, still covered in the current SRM (i.e.:
SRM Figure not inactive and the repair not in an excluded area) and without any structural repair underneath the skin.
Update the recorded inspection threshold and intervals in line with the values given in the April 2013 or subsequent SRM revisions As soon as possible before September 2015 or September 2016 (for aircraft WVs 020 series only) See note (***) None None Existing Repairs covered by a SRM version prior to April 2013 revision, located on the forward and rear fuselage, still covered in the current SRM (i.e.:
SRM Figure not inactive and the repair not in an excluded area) and with a structural repair underneath the skin Contact Airbus with a detailed repair report for specific assessment As soon as possible before September 2015 or September 2016 (for aircraft WVs 020 series only) See note (**) None None No existing repair covered by an SRM version prior to April 2013 revision No further action necessary within this Service Bulletin None None None NOTE : (*): It is recommended to check records within 6 months after SB issue date.
NOTE : (**): It is recommended to contact AIRBUS 6 months before end of the compliance time.
NOTE : (***): Any new repair inspection instruction following this update can be achieved at the customers convenience:
DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 7 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
- at anytime within the SB compliance time but no later than any existing repair inspection already scheduled before update
- as per the new inspection instruction updated following this SB Only the schedule of the updated inspection instruction is required to close the SB, not the inspection itself.
Table 01, Config. 002 - A340-300 SRM Update of the Fuselage Skin Doubler Repairs Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval All Aircraft Check the Aircraft records and identify the skin repairs performed as per the Structural Repair Manual (SRM) in the following areas:
Nose forward fuselage (Section 11/12)
- lower shell panels below stringers 31 LH and 31 RH
- lateral and upper panels between FR 10 and 18 except panel junction at stringer 9 between FR 10 and 13
- skin panels between FR 18 and 19, below stringers 43 LH/RH Center fuselage (Section
15):
- skin panels between FR 38 and 53.3
- skin panels between FR
53.3 and 54 below stringers 31 LH/RH 24 months from September 2014.
See Note (*) None None Existing repair is covered by a SRM version prior to April 2013 revision and l o c a t e do nt h e nose forward fuselage or center fuselage Update the recorded inspection threshold and interval in line with the value given in the April 2013 or subsequent SRM revisions.
As soon as possible before September 2016. See Note (**) None None DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 8 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN Table 01, Config. 002 - A340-300 SRM Update of the Fuselage Skin Doubler Repairs Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval No existing repair covered by an SRM version prior to April 2013 revision No further action necessary within this Service Bulletin None None None NOTE : (*): It is recommended to check records within 6 months after SB issue date.
NOTE : (**): Any new repair inspection instruction following this update can be achieved at the customers convenience:
- at anytime within the SB compliance time but no later than any existing repair inspection already scheduled before update
- as per the new inspection instruction updated following this SB Only the schedule of the updated inspection instruction is required to close the SB, not the inspection itself.
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 date given but reference should be made to the AD for confirmation of the mandated accomplishment timescale.
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.
**CONF 001 Task 534224-832-848-001: Inspection On Aircraft DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 9 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN Task 534224-832-848-001: Inspection Do a check of the Aircraft Records
1.00
TOTAL MANHOURS
1.00
ELAPSED TIME (HOURS)
1.00 **CONF 002 Task 534224-832-848-001: Inspection On Aircraft Do a check of the Aircraft Records
1.00
TOTAL MANHOURS
1.00
ELAPSED TIME (HOURS)
1.00 **CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Structural Repair Manual (SRM) 53-00-11 53-11-11 53-31-11 **CONF 002 Structural Repair Manual (SRM) 53-11-11 53-31-11 **CONF ALL K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Dec 15/14 SERVICE BULLETIN No.: A340-53-4224 REVISION No.: 00 - Dec 15/14 Page: 10 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.