# @A330 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 - REAR FUSELAG E - INSPECTION FOR SUSPECTED MISSING/NON-CONFORMING FASTENERS AT VARIOUS FUSELAGE FRAME AREAS AT SECTION 17 FROM FR68 TO FR72 **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Prior to delivery of an A330-200F aircraft, fasteners were found missing at some locations in the rear fuselage at Section 17 from Frame (FR)68 to FR72. This Service Bulletin describes a detailed inspection of the fastener installation and condition at the affected locations. In the event that fasteners are missing, damaged or incorrectly installed, this Service Bulletin details the procedure to restore the structure to the approved design intent, with the application of Modification Service Bulletin No. A330-53-3219. Accomplishment of this Service Bulletin will make sure that the aircraft will be restored to the original approved design integrity. The inspection should be scheduled during an extended grounding time of the aircraft, because an evaluation of the inspection results by AIRBUS may be required before next flight. 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 NOTE (1) : Service Bulletin must be accomplished. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 1 6

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# @A330 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION No Material EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

CRK ETD MAS MNB QTR THY TPA YZR 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 Task 533214-832-848-001: Inspection TOTAL MANHOURS 10.25 ELAPSED TIME (HOURS) 10.25 APPENDICES None

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 2 6

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# @A330 SERVICE BULLETIN SUMMARY
**CONF ALL



### B

FR67 STGR30RH FR68 FR69 STGR26RH STGR27RH

**NOTE:** INSPECTION AREAS Z260

STGR14LH FR72 FR71 FR70

FR72 FR71 STGR43LH STGR4LH STGR5LH

STGR4RH STGR5RH

FR72 FR70 FR71 

## A Z160



## B
**C**

**D** STGR33RH

FR72 

### A **C D** 

STGR47RH STGR46RH

G_SB_533214_6_SAAA_01_01 Figure A-GSAAA - Sheet 01 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 3 6

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# @A330 SERVICE BULLETIN SUMMARY

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# @A330 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 - REAR FUSELAG E - INSPECTION FOR SUSPECTED MISSING/NON-CONFORMING FASTENERS AT VARIOUS FUSELAGE FRAME AREAS AT SECTION 17 FROM FR68 TO FR72 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 330-223F 330-243F (2) Effectivity by MSN 1004 1032 1051 1062 1070 1092 1115 1136 1148 1164 1175 1180 1320 1332 1344 1350 1368 1380 1386 1406 1414 1418 1428 (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 CRK 1051 1062 1115 1320 ETD 1032 1070 1414 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 1 6

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# @A330 SERVICE BULLETIN
OPERATOR MSN MAS 1136 1148 1164 1180 MNB 1332 QTR 1350 1386 1406 THY 1004 1092 1344 1418 TPA 1368 1380 1428 YZR 1175 (4) Configuration by MSN MSN CONFIGURATION 1004 1032 1051 1062 1070 1092 1115 1136 1148 1164 1175 1180 1320 1332 1344 1350 1368 1380 1386 1406 1414 1418 1428 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 Prior to delivery of an A330-200F aircraft, fasteners were found missing at some locations in the rear fuselage at Section 17 from Frame (FR)68 to FR72. (2) Objective/Action This Service Bulletin describes a detailed inspection of the fastener installation and condition at the affected locations. In the event that fasteners are missing, damaged or incorrectly installed, this Service Bulletin details the procedure to restore the structure to the approved design intent, with the application of Modification Service Bulletin No. A330-53-3219. (3) Advantages Accomplishment of this Service Bulletin will make sure that the aircraft will be restored to the original approved design integrity.

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 2 6

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# @A330 SERVICE BULLETIN (4) Operational/Maintenance Consequences The inspection should be scheduled during an extended grounding time of the aircraft, because an evaluation of the inspection results by AIRBUS may be required before next flight. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 533214-832-848-001: Inspection (1) At FR68, STGR29 RH and STGR30 RH, do a Detailed Inspection for Missing Fasteners (2) At FR69, STGR33 RH, do a Detailed Inspection for Missing Fasteners (3) At FR71, STGR14 LH, do a Detailed Inspection for Missing Fasteners (4) At FR72, STGR26 RH to STGR27 RH, do a Detailed Inspection for Missing Fasteners (5) At FR72, STGR30 RH, do a Detailed Inspection for Missing Fasteners (6) At FR72, STGR43 LH, do a Detailed Inspection for Missing Fasteners (7) At FR72, STGR46 RH and STGR47 RH, do a Detailed Inspection for Missing Fasteners (8) At FR72, STGR5 LH, do a Detailed Inspection for Missing Fasteners (9) At FR72, STGR5 RH, do a Detailed Inspection for Missing Fasteners E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is required within 72 months from Entry Into Service (EIS). 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 above 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 Approval No. EASA.21J.031. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 3 6

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# @A330 SERVICE BULLETIN 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 533214-832-848-001: Inspection Get Access 3.50 On Aircraft At FR68, STGR29 RH and STGR30 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR69, STGR33 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR71, STGR14 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR72, STGR26 RH to STGR27 RH, do a Detailed Inspection for Missing Fasteners 0.50 At FR72, STGR30 RH, do a Detailed Inspection for Missing Fasteners 0.50 At FR72, STGR43 LH, do a Detailed Inspection for Missing Fasteners 0.50 At FR72, STGR46 RH and STGR47 RH, do a Detailed Inspection for Missing Fasteners 0.50 At FR72, STGR5 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR72, STGR5 RH, do a Detailed Inspection for Missing Fasteners 0.25 Close-Up 3.50 TOTAL MANHOURS 10.25 ELAPSED TIME (HOURS) 10.25 NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 4 6

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# @A330 SERVICE BULLETIN J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-21-11 25-54-00 25-55-22 25-80-00 52-30-00 53-00-00 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-53-3219 Structural Repair Manual (SRM) 51-42-00 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 5 6

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# @A330 SERVICE BULLETIN

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# @A330 SERVICE BULLETIN 2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY No Material Set B. INDUSTRY SUPPORT INFORMATION For those aircraft in warranty at the time of such inspection with findings further to inspection as per this Service Bulletin, Airbus will credit the man hours indicated in this Service Bulletin for corrections that are performed on aircraft in warranty at the time of such correction. Credit will be at the agreed inhouse warranty labour rate. Claims for labour allowance should be received not later than 90 days after completion of the last affected warranted aircraft. AIRBUS will credit the man hours indicated in this Service Bulletin for inspections that are performed on aircraft in warranty at the time of such inspection. Credit will be at the agreed inhouse warranty labour rate. Claims for labour allowance should be received not later than 90 days after completion of the last affected warranted aircraft. 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: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 7 6

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# @A330 SERVICE BULLETIN

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# @A330 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 533214-832-848-001 - 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 : 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. NOTE : The accomplishment instructions of this Service Bulletin refer to procedures included in other AIRBUS documents. When the words ’refer to’ are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words ’in accordance with’ are included in the instruction, the procedure in the AIRBUS document must be used. 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.
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 9 6

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# @A330 SERVICE BULLETIN Task Associated Data Zone 160 260 Access Door 823 831 Panel 162EF 162FW 162RW 162VW 162WW 261QQ 261RQ Manpower TOTAL MANHOURS 10.25 ELAPSED TIME (HOURS) 10.25 A. GENERAL (1) Subtask 533214-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-21-11-911-801 Structural Repair Manual (SRM) 51-42-00 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (d) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (e) Remove and install fasteners in accordance with SRM 51-42-00. (f) Tag all the parts you must remove and retain to make the subsequent installation easier. (2) Subtask 533214-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 10 6

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# @A330 SERVICE BULLETIN B. PREPARATION (1) Subtask 533214-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162FW, Panel 162VW, Panel 162WW, Panel 162EF, Panel 162RW 260 Access Door 831 Panel 261QQ, Panel 261RQ Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-54-00-000-001 Task 25-55-22-000-801 Task 25-80-00-000-801 Task 52-30-00-010-803 Task 53-00-00-000-804 (a) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked. - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (b) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (c) Put access platform(s) in position below the bulk cargo-compartment door 823. (d) Open the bulk cargo-compartment door 823, refer to AMM Task 52-30-00-010-803. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 11 6

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# @A330 SERVICE BULLETIN (e) In the Main-Deck Cargo Compartment (MDCC), remove the lining panels 261QQ and 261RQ, refer to AMM Task 25-55-22-000-801. (f) In the bulk cargo-compartment, remove the floor panel 162EF, refer to AMM Task 53-00-00-000-804. (g) In the bulk cargo-compartment, remove the sidewall panel 162FW, 162RW, 162VW and 162WW, refer to AMM Task 25-54-00-000-001. (h) Remove the insulation blankets as necessary to get access to the work areas, refer to AMM Task 25-80-00-000-801. C. PROCEDURE (1) Subtask 533214-832-201-001 - At FR68, STGR29 RH and STGR30 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162FW Work location Frame 68 Stringer 29RH Stringer 30RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFBAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBAAA Inspection of the fasteners at Frame 68, STGR 29RH and STGR 30RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 12 6

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# @A330 SERVICE BULLETIN (a) At Frame 68, STGR29 RH and STGR30 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If 4.0 mm (0.157 in.) diameter fasteners, Part Number (PN) EN6081D5, are installed at the locations as shown in Fig. A-GBAAA Sheet 01 , Views C and D, no repair is necessary at these locations, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-202 001 At FR69, STGR33 RH, do a Detailed Inspection for Missing Fasteners . 2 If 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GBAAA Sheet 01 , Views C and D, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. NOTE : Pilot holes exist. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. (2) Subtask 533214-832-202-001 - At FR69, STGR33 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162FW, Panel 162RW Work location Frame 69 Stringer 33RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFBAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBBAA Inspection of the fasteners at Frame 69, STGR 33RH Sheet 01
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 13 6

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# @A330 SERVICE BULLETIN
References Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 69, STGR33 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fastener, PN EN6069KE6, is installed at the location as shown in Fig. A-GBBAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-203 001 At FR71, STGR14 LH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.8 mm (0.189 in.) diameter fastener is not installed at the location as shown in Fig. A-GBBAA Sheet 01 , View B, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. NOTE : Pilot hole exists. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. (3) Subtask 533214-832-203-001 - At FR71, STGR14 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 260 Access Door 831 Panel 261QQ, Panel 261RQ Work location Frame 71 Stringer 14LH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFBAA Inspection Flowchart for missing fasteners Sheet 01
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 14 6

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# @A330 SERVICE BULLETIN
References Fig. A-GBCAA Inspection of the fasteners at Frame 71, STGR 14LH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 71, STGR14 LH, do a detailed inspection for missing fasteners refer to Fig. A-GFBAA Sheet 01 : 1 If 4.0 mm (0.157 in.) diameter fasteners, PN EN6081D5, are installed at the locations as shown in Fig. A-GBCAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-204 001 At FR72, STGR26 RH to STGR27 RH, do a Detailed Inspection for Missing Fasteners . 2 If 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GBCAA Sheet 01 , View B, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. (4) Subtask 533214-832-204-001 - At FR72, STGR26 RH to STGR27 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162WW Work location Frame 72 from Stringer 26RH to Stringer 27RH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 15 6

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# @A330 SERVICE BULLETIN
References Fig. A-GFAAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBDAA Inspection of the fasteners at Frame 72, STGR 26RH to STGR 27RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 72, STGR26 RH to STGR27 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFAAA: 1 If 4.8 mm (0.189 in.) diameter fasteners, PN DAN6-6-3, are installed at the locations as shown in Fig. A-GBDAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-205 001 At FR72, STGR30 RH, do a Detailed Inspection for Missing Fasteners . 2 If 4.8 mm (0.189 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GBDAA Sheet 01 , View B, do the worksteps which follow: a Do a detailed inspection of the adjacent fasteners for damage, deformations or cracks, as shown in Fig. A-GBDAA Sheet 01 , View B. <1> If you find damage or cracks at the adjacent fasteners, contact AIRBUS for further instructions before next flight. <2> If you do not find damage or cracks at the adjacent fasteners, accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. (5) Subtask 533214-832-205-001 - At FR72, STGR30 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162WW Work location Frame 72 Stringer 30RH
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 16 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFAAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBEAA Inspection of the fasteners at Frame 72, STGR 30RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 72, STGR30 RH, do a detailed inspection for missing fasteners refer to Fig. A-GFAAA Sheet 01 : 1 If 4.0 mm (0.157 in.) diameter fasteners, PN EN6069KE5, are installed at the locations as shown in Fig. A-GBEAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-206 001 At FR72, STGR43 LH, do a Detailed Inspection for Missing Fasteners . 2 If 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GBEAA Sheet 01 , View B, do the worksteps which follow: a Do a detailed inspection of the adjacent fasteners for damage, deformations or cracks, as shown in Fig. A-GBEAA Sheet 01 , View B. <1> If you find damage or cracks at the adjacent fasteners, contact AIRBUS for further instructions before next flight. <2> If you do not find damage or cracks at the adjacent fasteners, accomplish Modification Service Bulletin No.A330-53-3219 at this location before next flight. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
.

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 17 6

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# @A330 SERVICE BULLETIN (6) Subtask 533214-832-206-001 - At FR72, STGR43 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162VW Work location Frame 72 Stringer 43LH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFAAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBFAA Inspection of the fasteners at Frame 72, STGR 43LH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 72, STGR43 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFAAA Sheet 01 : 1 If 4.0 mm (0.157 in.) diameter fasteners, PN EN6069KE5, are installed at the locations as shown in Fig. A-GBFAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-207 001 At FR72, STGR46 RH and STGR47 RH, do a Detailed Inspection for Missing Fasteners . 2 If 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GBFAA Sheet 01 , View B, do the worksteps which follow: a Do a detailed inspection of the adjacent fasteners for an damage, deformations or cracks as shown in Fig. A-GBFAA Sheet 01 , View B. <1> If you find damage or cracks at the adjacent fasteners, contact AIRBUS for further instructions before next flight.
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 18 6

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# @A330 SERVICE BULLETIN <2> If you do not find damage or cracks at the adjacent fasteners, accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. (7) Subtask 533214-832-207-001 - At FR72, STGR46 RH and STGR47 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162EF Work location Frame 72 Stringer 47RH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFAAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBGAA Inspection of the fasteners at Frame 72, STGR 46RH and STGR 47RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 72, STGR46 RH and STGR47 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFAAA Sheet 01 : 1 If 4.0 mm (0.157 in.) diameter fasteners, PN EN6069KE5, are installed at the locations as shown in Fig. A-GBGAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-208 001 At FR72, STGR5 LH, do a Detailed Inspection for Missing Fasteners .

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 19 6

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# @A330 SERVICE BULLETIN
2 If 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GBGAA Sheet 01 , View B, do the worksteps which follow: a Do a detailed inspection of the adjacent fasteners for damage, deformations or cracks as shown in Fig. A-GBGAA Sheet 01 , View B. <1> If you find damage or cracks at the adjacent fasteners, contact AIRBUS for further instructions before next flight. <2> If you do not find damage or cracks at the adjacent fasteners, accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. NOTE : Pilot holes exist. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. (8) Subtask 533214-832-208-001 - At FR72, STGR5 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 260 Access Door 831 Work location Frame 72 Stringer 5LH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFBAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBHAA Inspection of the Fasteners at Frame 72, STGR 5LH and STGR 5RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 20 6

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# @A330 SERVICE BULLETIN (a) At Frame 72, STGR5 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If a 4.8 mm (0.189 in.) diameter fastener, PN EN6081D6, is installed at the location as shown in Fig. A-GBHAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-832-209 001 At FR72, STGR5 RH, do a Detailed Inspection for Missing Fasteners . 2 If a 4.8 mm (0.189 in.) diameter fastener is not installed at the location as shown in Fig. A-GBHAA Sheet 01 , View B, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. NOTE : Pilot hole exists. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. (9) Subtask 533214-832-209-001 - At FR72, STGR5 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 260 Access Door 831 Work location Frame 72 Stringer 5RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3219 Fig. A-GFBAA Inspection Flowchart for missing fasteners Sheet 01 Fig. A-GBHAA Inspection of the Fasteners at Frame 72, STGR 5LH and STGR 5RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 21 6

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# @A330 SERVICE BULLETIN (a) At Frame 72, STGR5 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If a 4.8 mm (0.189 in.) diameter fastener, PN EN6081D6, is installed at the location as shown in Fig. A-GBHAA Sheet 01 , View B, no repair is necessary at this location, do the worksteps which follow: a Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. b Go to SUBTASK 533214-942-201 001 Close-up . 2 If a 4.8 mm (0.189 in.) diameter fastener is not installed at the location as shown in Fig. A-GBHAA Sheet 01 , View B, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3219 at this location before next flight. NOTE : Pilot hole exists. b Write the result of the inspection in the Inspection Report Sheet and send to AIRBUS Customer Services Engineering SEES1, refer to Fig. AGRAAA Sheet 01
. D. TEST None E. CLOSE-UP (1) Subtask 533214-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Panel 162FW, Panel 162VW, Panel 162WW, Panel 162EF, Panel 162RW 260 Access Door 831 Panel 261QQ, Panel 261RQ Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 25-54-00-400-001 Task 25-55-22-400-801 Task 25-80-00-400-801 Task 52-30-00-410-803 Task 53-00-00-400-804
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 22 6

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# @A330 SERVICE BULLETIN (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the insulation blankets which you removed to get access to the work areas, refer to AMM Task 25-80-00-400-801. (c) In the bulk cargo-compartment, install the sidewall panels 162FW, 162RW, 162VW and 162WW, refer to AMM Task 25-54-00-400-001. (d) In the bulk cargo-compartment, install the floor panel 162EF, refer to AMM Task 53-00-00-400-804. (e) In the Main-Deck Cargo Compartment (MDCC), install the lining panels 261QQ and 261RQ, refer to AMM Task 25-55-22-400-801. (f) Close the bulk cargo-compartment door 823, refer to AMM Task 52-30-00-410-803. (g) Remove the access platform(s).

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 23 6

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# @A330 SERVICE BULLETIN

**CONF ALL

**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 YES DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR72 − STGR26−27RH, FR72 − STGR30RH, FR72 − STGR43LH, FR72 − STGR46RH AND STGR47RH

FASTENERS INSTALLED? ARE

DO A DETAILED INSPECTION OF THE ADJACENT FASTENER ROWS

CONTACT AIRBUS FOR FURTHER INSTRUCTIONS

BEFORE NEXT FLIGHT YES

NO DEFORMATIONS

OR CRACKS? ANY

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND

NO FURTHER ACTION AT THIS/THESE LOCATIONS SERVICE BULLETIN A330−53−3219 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533214_6_FAAA_01_04 Figure A-GFAAA - Sheet 01 Inspection Flowchart for missing fasteners DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 24 6

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# @A330 SERVICE BULLETIN

**CONF ALL

**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 YES DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR68 − STGR29−30RH, FR69 − STGR33RH, FR71 − STGR14LH, FR72 − STGR5LH/RH

FASTENERS INSTALLED? ARE

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND

NO FURTHER ACTION AT THIS/THESE LOCATIONS SERVICE BULLETIN A330−53−3219 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533214_6_FBAA_01_03 Figure A-GFBAA - Sheet 01 Inspection Flowchart for missing fasteners DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 25 6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A330 SERVICE BULLETIN

**CONF ALL

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). **NOTE:** 01 VIEW LOOKING AFT Z160 

### A

FR68 FR68

**F W**  **D F**  **W D**  FR68 

### C

**D** STGR29RH

STGR30RH

STGR29RH STGR30RH

01 01 

## B

**C D**  FR72

FR67 STGR29RH STGR30RH FR68



### B


## A

G_SB_533214_6_BAAA_01_03 Figure A-GBAAA - Sheet 01 Inspection of the fasteners at Frame 68, STGR 29RH and STGR 30RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 26 6

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# @A330 SERVICE BULLETIN

**CONF ALL

DETAILED INSPECTION FOR MISSING FASTENER (PILOT HOLE EXISTS). **NOTE:** 01 FR69 STGR32RH

STGR33RH

STGR34RH

VIEW LOOKING ON OUTER SKIN **FWD** 01



## B FR72

FR67 

### B



## A STGR33RH FR69

Z160 

### A

G_SB_533214_6_BBAA_01_03 Figure A-GBBAA - Sheet 01 Inspection of the fasteners at Frame 69, STGR 33RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 27 6

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# @A330 SERVICE BULLETIN

**CONF ALL

DETAILED INSPECTION FOR MISSING FASTENERS. **NOTE:** 01 FR71 VIEW LOOKING FWD STGR14LH STGR13LH

01



## B **A** STGR14LH 

### B Z260 

### A FR72 FR71 FR70

STGR13LH

G_SB_533214_6_BCAA_01_02 Figure A-GBCAA - Sheet 01 Inspection of the fasteners at Frame 71, STGR 14LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 28 6

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# @A330 SERVICE BULLETIN

**CONF ALL

**NOTE:** 01 FR72 STGR25RH

STGR26RH

STGR27RH

STGR28RH

02 VIEW LOOKING ON OUTER SKIN **FWD** 01 02 FR67 

## A STGR26RH

STGR27RH 

### B



## B FR72 Z160 

### A

DETAILED INSPECTION FOR MISSING FASTENERS. DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. G_SB_533214_6_BDAA_01_04 Figure A-GBDAA - Sheet 01 Inspection of the fasteners at Frame 72, STGR 26RH to STGR 27RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 29 6

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# @A330 SERVICE BULLETIN

**CONF ALL

STGR29RH

STGR30RH

STGR31RH FR72 FR71

**NOTE:** 01 02 VIEW LOOKING ON OUTER SKIN **FWD** 03 01 02 FR67 

### B STGR30RH



## B **A** FR72 Z160 

### A

DETAILED INSPECTION FOR MISSING FASTENERS. DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. 02

03 COUPLING IS NOT SHOWN. G_SB_533214_6_BEAA_01_05 Figure A-GBEAA - Sheet 01 Inspection of the fasteners at Frame 72, STGR 30RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 30 6

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# @A330 SERVICE BULLETIN

**CONF ALL

FR72 FR71

**NOTE:** 01 02 VIEW LOOKING ON OUTER SKIN **FWD** 02 01 02 

## B FR72 FR71

STGR43LH 

### B 

## A

STGR41LH

STGR42LH

STGR43LH Z160 

### A

DETAILED INSPECTION FOR MISSING FASTENERS. DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. 03

03 COUPLING IS NOT SHOWN. G_SB_533214_6_BFAA_01_05 Figure A-GBFAA - Sheet 01 Inspection of the fasteners at Frame 72, STGR 43LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 31 6

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# @A330 SERVICE BULLETIN

**CONF ALL

STGR45RH

STGR46RH

STGR47RH FR72 FR71

**NOTE:** 01 02 VIEW LOOKING ON OUTER SKIN **FWD** 02 01 02 

## B FR67 

### B FR72 

## A STGR47RH Z160 

### A

DETAILED INSPECTION FOR MISSING DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. 03 COUPLING IS NOT SHOWN. 03 FASTENERS (PILOT HOLES EXIST). G_SB_533214_6_BGAA_01_04 Figure A-GBGAA - Sheet 01 Inspection of the fasteners at Frame 72, STGR 46RH and STGR 47RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 32 6

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# @A330 SERVICE BULLETIN

**CONF ALL

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). **NOTE:** 01 STGR4

STGR5

FR72

LH SHOWN RH SYMMETRICAL VIEW LOOKING AFT 01 Z260



## B **A** STGR4LH STGR5LH

STGR4RH STGR5RH

FR72 FR70 FR71 

### B **B**



## A

G_SB_533214_6_BHAA_01_03 Figure A-GBHAA - Sheet 01 Inspection of the Fasteners at Frame 72, STGR 5LH and STGR 5RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 33 6

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# @A330 SERVICE BULLETIN

**CONF ALL

SERVICE BULLETIN No. : A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : A330−53−3214 **INSPECTION REPORT**

FINDINGS : YES NO DATE OF INSPECTION : RETURN TO : AIRBUS CUSTOMER SERVICES ENGINEERING − SEES1 FUSELAGE (WB/LR) − VERTICAL TAIL PLANE − CENTER WING BOX (WB/LR) 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 36 14 E−mail: Structure.sbinspectionresult@airbus.com

LOCATION INSPECTION ACTIONS FASTENER(S) INSTALLED? DAMAGE FOUND AT ADJACENT

FASTENER FOLLOW−UP ACTIONS AIRBUS CONTACTED? LOCATIONS? YES NO YES NO YES NO YES NO N/A N/A FR68, STGR29RH − STGR30RH FR69, STGR33RH FR71, STGR14LH FR72, STGR26RH − STGR27RH FR72, STGR30RH FR72, STGR43LH

FR72, STGR5LH N/A N/A
N/A N/A

N/A N/A AND STGR5RH

INSPECTION METHOD: DETAILED INSPECTION

ACCOMPLISHED? BULLETIN No. A330−53−3219 SERVICE

FR72, STGR46RH AND STGR47RH

G_SB_533214_6_RAAA_01_01 Figure A-GRAAA - Sheet 01 Inspection Report DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 34 6

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - REAR FUSELAG E - INSPECTION FOR SUSPECTED MISSING/NON-CONFORMING FASTENERS AT VARIOUS FUSELAGE FRAME AREAS AT SECTION 17 FROM FR68 TO FR72 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: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 1 6

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# @A330 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: May 06/14 SERVICE BULLETIN No.: A330-53-3214 REVISION No.: 00 - May 06/14 Page: 1 6

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