# @A340 SERVICE BULLETIN SUMMARY 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 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 FORWARD PASSENGER DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following changes in Apr-2013 revision of SRM A340-200/-300 and with regards to previously embodied SRM ADL (allowable damage limits), Airbus is requiring the operators to apply specific actions defined in this Service Bulletin. This Service Bulletin requires the operators to identify records of SRM ADL (allowable damage limits) at corners of skin surrounding forward PAX door cutout. It is recommended to check records in the specified areas within 6 months after SB issue date. In case of existing SRM ADL recorded prior to Apr-2013 SRM revision, please contact AIRBUS Repair Support (SEOE) for further instructions. Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the skin surrounding forward PAX door cutout. 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.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 1 5

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# @A340 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION No Material EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

06Y 15R 83V 98X ABD AFR AIB ALK ARG BOE CAL CCA CPA DLH F2I FIN G8E GAF HFY I2L IBE IRM KAC LAN MAU MDG MSR OAL PAL PUE QAF SAA SAS SVW SWR THT THY UAE 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 NO EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 534223-832-801-001: Inspection TOTAL MANHOURS 2.00 APPENDICES None

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 2 5

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# @A340 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 FORWARD PASSENGER DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS 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 NOTE: This Service Bulletin is only applicable to aircraft on which Mod. No.40347S10187 (FUSELAGE - NOSE FORWARD FUSELAGE MODIFY DOOR NR 1 SURROUND) is embodied. (1) Models 340-212 340-213 340-311 340-312 340-313 (2) Effectivity by MSN 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 0225 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: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 1 5

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# @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 83V 0216 98X 0429 ABD 0210 AFR 0186 0207 0237 0245 0246 0260 0307 0310 0377 0399 AIB 0131 0141 0161 0182 ALK 0367 0374 0381 ARG 0123 0126 0128 0170 0193 0373 BOE 0554 CAL 0402 0406 0411 0415 0433 0541 CCA 0192 0199 0201 0242 0243 0264 CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 DLH 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447 F2I 0257 FIN 0168 0174 0835 0844 0921 0938 G8E 0414 GAF 0274 0355 HFY 0117 0190 0202 I2L 0164 IBE 0125 0134 0145 0146 0217 0221 0329 0483 IRM 0282 KAC 0101 0104 LAN 0359 0363 0442 MAU 0152 0194 0268 0793 0800 MDG 0319 MSR 0156 0159 0178 OAL 0280 0292 PAL 0173 0176 0187 0196 0302 0318 0332 0387 0459 0474 PUE 0212 0215 QAF 0528 SAA 0197 0378 0544 0582 0590 0643 0646 0651 SAS 0167 0413 0424 0430 0435 0450 0467 0470 SVW 0955 SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0562 0585 0598 THT 0385 0395 0438 0446 0668 THY 0115 0180 0270 0331 UAE 0163 0166 0185 0236 DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 2 5

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# @A340 SERVICE BULLETIN

OPERATOR MSN VIR 0114 0214 0225 XAX 0273 0278 (4) Configuration by MSN MSN CONFIGURATION 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 0225 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 0414 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 0668 0793 0800 0835 0844 0921 0938 0955 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 No Material Set B. CONCURRENT REQUIREMENTS None C. REASON (1) History Following changes in Apr-2013 revision of SRM A340-200/-300 and with regards to previously embodied SRM ADL (allowable damage limits), 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 ADL (allowable damage limits) at corners of skin surrounding forward PAX door cutout.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 3 5

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# @A340 SERVICE BULLETIN It is recommended to check records in the specified areas within 6 months after SB issue date. In case of existing SRM ADL recorded prior to Apr-2013 SRM revision, please contact AIRBUS Repair Support (SEOE) for further instructions. (3) Advantages Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the skin surrounding forward PAX door cutout. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 534223-832-801-001: Inspection (1) Check if ADL have been recorded at Corners of Skin Surrounding Forward PAX Doors, LH and RH Side 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.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 4 5

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# @A340 SERVICE BULLETIN
Table 1, Config. 001 - Inspection of SRM allowable damage limits records at corners of skin surrounding forward PAX door Compliance time (whichever occurs later) Condition Action Threshold (whichever occurs fist) Grace period (whichever occurs fist) Repetitive interval

All aircraft Check the aircraft maintenance program documentation for existing ADL in the related sections in accordance with the Subtask 534223-832-001-001 Before Sep-2015 for ADL with a Temporary Life Limit and Before Sep-2016 for ADL with a Permanent Acceptance See NOTE (*) None None

No existing ADL covered by a SRM version prior to Apr-2013 revision No further action necessary within this Service Bulletin None None None

ADL detected with a temporary life limit and covered by a SRM version prior to Apr-2013 revision Contact AIRBUS with detailed repair report for specific assessment and follow their instructions As soon as possible before Sep-2015 See NOTE (**) None None

ADL detected with a permanent acceptance and covered by a SRM version prior to Apr-2013 revision Contact AIRBUS with detailed repair report for specific assessment and follow their instructions As soon as possible before Sep-2016 See NOTE (**) 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 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 before incorporation of the Service Bulletin.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 5 5

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# @A340 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 534223-832-801-001: Inspection On Aircraft Check if ADL have been recorded at Corners of Skin Surrounding Forward PAX Doors, LH and RH Side 2.00 TOTAL MANHOURS 2.00 H. WEIGHT AND BALANCE Not Changed I. 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

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 6 5

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# @A340 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

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 7 5

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# @A340 SERVICE BULLETIN

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DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 8 5

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# @A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 534223-832-801-001 - Inspection WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS 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.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 9 5

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# @A340 SERVICE BULLETIN
Task Associated Data Manpower TOTAL MANHOURS 2.00 A. GENERAL (1) Subtask 534223-839-001-001 - 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 534223-832-001-001 - Check if ADL have been recorded at Corners of Skin Surrounding Forward PAX Doors, LH and RH Side Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Structural Repair Manual (SRM) 53-11-11, Page Block 101 Fig. A-FBAAA Area with ADL submitted to assessment Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01
NOTE: For the accomplishment timescale, refer to 1.E.(2). (a) Check in the aircraft maintenance program documentation if ADL have been recorded at corners of skin surrounding forward PAX doors, LH and RH side, according to SRM 53-11-11, Page Block 101 paragraph 4.D. Refer to Fig. A-FBAAA and Flow Chart Fig. A-FFAAA 1 If some ADL covered by a SRM version prior to Apr-2013 revision are found, contact AIRBUS with detailed repair report for specific assessment and follow their instructions. 2 If no ADL covered by a SRM version prior to Apr-2013 revision is found, no further action is required.
DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 10 5

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# @A340 SERVICE BULLETIN
D. TEST None E. CLOSE-UP None

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 11 5

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# @A340 SERVICE BULLETIN

**CONF ALL

350 mm (13.779 in) 60 mm (2.362 in)

260 mm (10.236 in) FR1 FR17 

### A

TYPICAL Z831

AREA ON WHICH ADL ARE SUBMITTED TO ASSESSMENT 01 NOTE:01 Z841 Z220 

### A

LH SIDE SHOWN RH SIDE SYMMETRICAL



## B A FR13 FR17 

### B

B

F_SB_534223_5_BAAA_01_00 Figure A-FBAAA - Sheet 01 Area with ADL submitted to assessment DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 12 5

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# @A340 SERVICE BULLETIN

**CONF ALL

CHECK THE AIRCRAFT MAINTENANCE PROGRAM DOCUMENTATION FOR EXISTING ADL AT CORNERS OF SKIN SURROUNDING

YES COVERED BY A SRM VERSION PRIOR TO EXISTING ADL

CONTACT AIRBUS WITH DETAILED REPAIR

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 NO FURTHER ACTION WITHIN THIS SERVICE BULLETIN

FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARA 1.E.(2) 01 01 FORWARD PAX DOORS, LH AND RH SIDE, IN ACCORDANCE WITH

APR

−2013 REVISION ? 01

REPORT FOR SPECIFIC

ASSESSMENT AND

QUESTION
ACTION FINDING SUBTASK 534223

−832

−001

−001

FOLLOW THEIR INSTRUCTIONS NO

F_SB_534223_5_FAAA_01_00 Figure A-FFAAA - Sheet 01 Flow Chart DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 13 5

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - INSPECTION OF FORWARD PASSENGER DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS MODIFICATION No.: None Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 1 5

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# @A340 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223 REVISION No.: 00 - Sep 26/14 Page: 1 5

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