# @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 FUSELAGE - INSPECTION FOR SUSPECTED MISSING/NON-CONFORMING FASTENERS AT SECTION 16 AND SECTION 17 FROM FR57 TO FR59 **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Prior to delivery of an A330-200F aircraft, some fasteners were found missing at some locations in the rear fuselage area at Section 16 and Section 17, from Frame (FR)57 to FR59. 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 accomplishment of Modification Service Bulletin No. A330-53-3217. 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.: A330-53-3212 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 533212-832-848-001: Inspection TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 10.00 APPENDICES None

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 2 6

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# @A330 SERVICE BULLETIN SUMMARY
**CONF ALL


### A **C**

**NOTE:** INSPECTION AREAS LH SHOWN RH SYMMETRICAL

FR60 FR59 FR58 FR57 FR56

STGR26
FR57 FR58 FR59 FR58 

## A FR60 STGR23RH STGR25RH
Z150

FR59



## B

**C** STGR40RH STGR38RH

FR58A STGR30RH STGR32RH

FR59 

### B

STGR41RH

STGR41LH Z260

G_SB_533212_6_SAAA_01_01 Figure A-GSAAA - Sheet 01 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 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 FUSELAGE - INSPECTION FOR SUSPECTED MISSING/NON-CONFORMING FASTENERS AT SECTION 16 AND SECTION 17 FROM FR57 TO FR59 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.: A330-53-3212 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, some fasteners were found missing at some locations in the rear fuselage area at Section 16 and Section 17, from Frame (FR)57 to FR59. (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 accomplishment of Modification Service Bulletin No. A330-53-3217. (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.: A330-53-3212 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 533212-832-848-001: Inspection (1) At FR57, STGR26 LH, do a Detailed Inspection for Missing Fasteners (2) At FR57, STGR26 RH, do a Detailed Inspection for Missing Fasteners (3) At FR58 to FR59, STGR38 RH, do a Detailed Inspection for Missing Fasteners (4) At FR58, STGR41 LH, do a Detailed Inspection for Missing Fasteners (5) At FR58, STGR41 RH, do a Detailed Inspection for Missing Fasteners (6) At FR58A, STGR29 RH to STGR30 RH, do a Detailed Inspection for Missing Fasteners (7) At FR58A, STGR31 RH to STGR33 RH, do a Detailed Inspection for Missing Fasteners (8) At FR59, STGR23 RH, STGR24 RH and STGR25 RH, do a Detailed Inspection for Missing Fasteners (9) At FR59, STGR26 LH, do a Detailed Inspection for Missing Fasteners (10) At FR59, STGR40 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.
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 3 6

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# @A330 SERVICE BULLETIN 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. 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 533212-832-848-001: Inspection Get Access 3.50 On Aircraft At FR57, STGR26 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR57, STGR26 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR58 to FR59, STGR38 RH, do a Detailed Inspection for Missing Fasteners 0.50 At FR58, STGR41 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR58, STGR41 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR58A, STGR29 RH to STGR30 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR58A, STGR31 RH to STGR33 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR59, STGR23 RH, STGR24 RH and STGR25 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR59, STGR26 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR59, STGR40 RH, do a Detailed Inspection for Missing Fasteners 0.50 Close-Up 3.50 TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 10.00 NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 4 6

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# @A330 SERVICE BULLETIN H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-21-11 25-53-00 25-55-22 25-80-00 52-10-00 52-30-00 53-00-00 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-53-3217 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.: A330-53-3212 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.: A330-53-3212 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 533212-832-848-001 - 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.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 9 6

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# @A330 SERVICE BULLETIN Task Associated Data Zone 150 260 Access Door 822 831 Panel 151FC 151HW 151JW 151QW 151RW 152FC 152HW 152JW 152MW 152NW 152VK 152WK 262WW 262XW Manpower TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 10.00 A. GENERAL (1) Subtask 533212-910-201-001 - 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) Remove and install fasteners in accordance with SRM 51-42-00. (e) Tag all the parts you must remove and retain to make the subsequent installation easier. (f) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (2) Subtask 533212-839-202-001 - 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.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 10 6

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# @A330 SERVICE BULLETIN B. PREPARATION (1) Subtask 533212-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152VK, Panel 152WK, Panel 151HW, Panel 151JW, Panel 151QW, Panel 151RW, Panel 152HW, Panel 152JW, Panel 152MW, Panel 152NW, Panel 151FC, Panel 152FC 260 Access Door 831 Panel 262WW, Panel 262XW Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-53-00-000-801 Task 25-55-22-000-801 Task 25-80-00-000-801 Task 52-30-00-010-801 Task 53-00-00-000-803 (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 platforms in position below the AFT cargo-compartment door 822. (d) Open the AFT cargo-compartment door 822, refer to AMM Task 52-30-00-010-801. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 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 sidewall panels 262WW and 262XW, refer to AMM Task 25-55-22-000-801. (f) In the AFT cargo-compartment, remove the floor panels 152VK and 152WK, refer to AMM Task 53-00-00-000-803. (g) In the AFT cargo-compartment, remove the sidewall panels 151HW, 151JW, 151QW, 151RW, 152HW, 152JW, 152MW and 152NW, refer to AMM Task 25-53-00-000-801. (h) In the AFT cargo-compartment, remove the ceiling panels 151FC and 152FC, refer to AMM Task 25-53-00-000-801. (i) 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 533212-832-201-001 - At FR57, STGR26 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 151JW, Panel 151FC Work location Frame 57 Stringer 26LH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFBAA Inspection Flowchart for missing fasteners at Frame 57 to Frame 59 Sheet 01 Fig. A-GBAAA Inspection of the fasteners at Frame 57, STGR26 LH and RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 12 6

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# @A330 SERVICE BULLETIN (a) At Frame 57, STGR26 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fasteners, Part Number (PN) EN6069KE6, are installed at the locations shown in Fig. A-GBAAA 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 533212-832-210 001 At FR57, STGR26 RH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.8 mm (0.189 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBAAA Sheet 01 , View B, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3217 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
. (2) Subtask 533212-832-210-001 - At FR57, STGR26 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152JW, Panel 152FC Work location Frame 57 Stringer 26RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFBAA Inspection Flowchart for missing fasteners at Frame 57 to Frame 59 Sheet 01 Fig. A-GBAAA Inspection of the fasteners at Frame 57, STGR26 LH and RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 13 6

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# @A330 SERVICE BULLETIN (a) At Frame 57, STGR26 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 fasteners, PN EN6069KE6, are installed at the locations shown in Fig. A-GBAAA 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 533212-832-202 001 At FR58 to FR59, STGR38 RH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.8 mm (0.189 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBAAA Sheet 01 , View B, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3217 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
. (3) Subtask 533212-832-202-001 - At FR58 to FR59, STGR38 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152WK Work location from Frame 58 to Frame 59 Stringer 38RH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFAAA Inspection Flowchart for missing fasteners at Frame 58 to Frame 59 Sheet 01 Fig. A-GBBAA Inspection of the fasteners at Frame 58 to Frame 59, STGR38 RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 14 6

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# @A330 SERVICE BULLETIN (a) At Frame 58 to Frame 59, STGR38 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFAAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fasteners, PN MBBN4481-0503, are installed at the locations 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 533212-832-203 001 At FR58, STGR41 LH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.8 mm (0.189 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBBAA 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-GBBAA 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. A330-53-3217 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 533212-832-203-001 - At FR58, STGR41 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 151HW, Panel 151QW Work location Frame 58 Stringer 41LH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 15 6

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# @A330 SERVICE BULLETIN
References Fig. A-GBCAA Inspection of the fasteners at Frame 58, STGR41 LH and RH Sheet 01 Fig. A-GFCAA Inspection Flowchart for missing fasteners at Frame 58 and Frame 59 Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 58, STGR41 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFCAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fasteners, PN DAN5-6-3, are installed at the locations 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 533212-832-211 001 At FR58, STGR41 RH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.8 mm (0.189 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBCAA 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-GBCAA 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. A330-53-3217 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
. (5) Subtask 533212-832-211-001 - At FR58, STGR41 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152HW, Panel 152MW Work location Frame 58 Stringer 41RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 16 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFCAA Inspection Flowchart for missing fasteners at Frame 58 and Frame 59 Sheet 01 Fig. A-GBCAA Inspection of the fasteners at Frame 58, STGR41 LH and RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 58, STGR41 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFCAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fasteners, PN DAN5-6-3, are installed at the locations 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 533212-832-204 001 At FR58A, STGR29 RH to STGR30 RH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.8 mm (0.189 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBCAA 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-GBCAA 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. A330-53-3217 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
.
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 17 6

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

# @A330 SERVICE BULLETIN (6) Subtask 533212-832-204-001 - At FR58A, STGR29 RH to STGR30 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152MW, Panel 152NW Work location Frame 58A from Stringer 29RH to Stringer 30RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFBAA Inspection Flowchart for missing fasteners at Frame 57 to Frame 59 Sheet 01 Fig. A-GBDAA Inspection of the fasteners at Frame 58A, STGR29 RH to STGR30 RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 58A, STGR29 RH to STGR30 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If the 4.0 mm (0.157 in.) diameter fasteners, PN EN6081D5, are installed at the locations shown in Fig. A-GBDAA Sheet 01 , View C, 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 533212-832-205 001 At FR58A, STGR31 RH to STGR33 RH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBDAA Sheet 01 , View C, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3217 at this location before next flight. NOTE : Pilot holes exist.
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 18 6

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

# @A330 SERVICE BULLETIN 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 533212-832-205-001 - At FR58A, STGR31 RH to STGR33 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152MW, Panel 152NW Work location Frame 58A from Stringer 31RH to Stringer 33RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFBAA Inspection Flowchart for missing fasteners at Frame 57 to Frame 59 Sheet 01 Fig. A-GBEAA Inspection of the fasteners at Frame 58A, STGR31 RH to STGR33 RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 58A, STGR31 RH to STGR33 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If the 4.0 mm (0.157 in.) diameter fasteners, PN EN6081D5, are installed at the locations shown in Fig. A-GBEAA Sheet 01 , View C, 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 533212-832-206 001 At FR59, STGR23 RH, STGR24 RH and STGR25 RH, do a Detailed Inspection for Missing Fasteners .

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 19 6

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

# @A330 SERVICE BULLETIN
2 If the 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBEAA Sheet 01 , View C, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3217 at this location before next flight. NOTE : 6 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 533212-832-206-001 - At FR59, STGR23 RH, STGR24 RH and STGR25 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 260 Access Door 831 Panel 262WW, Panel 262XW Work location Frame 59 Stringer 23RH Stringer 24RH Stringer 25RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFBAA Inspection Flowchart for missing fasteners at Frame 57 to Frame 59 Sheet 01 Fig. A-GBFAA Inspection of the fasteners at Frame 59, STGR23 RH, STGR24 RH and STGR25 RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 20 6

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

# @A330 SERVICE BULLETIN (a) At Frame 59, STGR23 RH, STGR24 RH and STGR25 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If the 4.0 mm (0.157 in.) diameter fasteners, PN EN6081D5, are installed at the locations shown in Fig. A-GBFAA Sheet 01 , View C, 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 533212-832-207 001 At FR59, STGR26 LH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBFAA Sheet 01 , View C, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3217 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
. (9) Subtask 533212-832-207-001 - At FR59, STGR26 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 151RW Work location Frame 59 Stringer 26LH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3217 Fig. A-GFAAA Inspection Flowchart for missing fasteners at Frame 58 to Frame 59 Sheet 01 Fig. A-GBGAA Inspection of the fasteners at Frame 59, STGR26 LH Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 21 6

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

# @A330 SERVICE BULLETIN
References Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 59, STGR26 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFAAA Sheet 01 : 1 If the 4.0 mm (0.157 in.) diameter fasteners, PN EN6069KE5, are installed at the locations 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 533212-832-208 001 At FR59, STGR40 RH, do a Detailed Inspection for Missing Fasteners . 2 If the 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations 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. A330-53-3217 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
. (10) Subtask 533212-832-208-001 - At FR59, STGR40 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152VK Work location Frame 59 Stringer 40RH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 22 6

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

# @A330 SERVICE BULLETIN
References Service Bulletin (SB) A330-53-3217 Fig. A-GBHAA Inspection of the fasteners at Frame 59, STGR40 RH Sheet 01 Fig. A-GFCAA Inspection Flowchart for missing fasteners at Frame 58 and Frame 59 Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 59, STGR40 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFCAA Sheet 01 : 1 If the 4.0 mm (0.157 in.) diameter fasteners, PN EN6081D5, are installed at the locations shown in Fig. A-GBHAA Sheet 01 , Section A-A, 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 533212-942-201 001 Close-up . 2 If the 4.0 mm (0.157 in.) diameter fasteners are not installed at the locations shown in Fig. A-GBHAA Sheet 01 , Section A-A, do the worksteps which follow: a Do a detailed inspection of the adjacent fasteners for damage, deformations or cracks as shown in Fig. A-GBHAA 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. A330-53-3217 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
. D. TEST None

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 23 6

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

# @A330 SERVICE BULLETIN E. CLOSE-UP (1) Subtask 533212-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 150 Access Door 822 Panel 152VK, Panel 152WK, Panel 151HW, Panel 151JW, Panel 151QW, Panel 151RW, Panel 152HW, Panel 152JW, Panel 152MW, Panel 152NW, Panel 151FC, Panel 152FC 260 Access Door 831 Panel 262WW, Panel 262XW Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801 Task 25-55-22-400-801 Task 25-80-00-400-001 Task 52-10-00-410-801 Task 52-30-00-410-801 Task 53-00-00-400-803 (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 25-80-00-400-001. (c) In the AFT cargo-compartment, install the ceiling panels 151FC and 152FC, refer to AMM Task 25-53-00-400-801. (d) In the AFT cargo-compartment, install the sidewall panels 151HW, 151JW, 151QW, 151RW, 152HW, 152JW, 152MW and 152NW, refer to AMM Task 25-53-00-400-801. (e) In the AFT cargo-compartment, install the floor panels 152VK and 152WK, refer to AMM Task 53-00-00-400-803. (f) In the Main-Deck Cargo Compartment (MDCC), install the lining panel 262WW and 262XW, refer to AMM Task 25-55-22-400-801. (g) Close the AFT cargo-compartment door 822, refer to AMM Task 52-30-00-410-801. (h) Remove the access platforms.

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 24 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

NO YES

**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. DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR58 TO FR59 − STGR38RH, FR59 − STGR26LH

FASTENERS INSTALLED?
DO A DETAILED INSPECTION OF THE ADJACENT FASTENER ROWS

CONTACT AIRBUS FOR FURTHER INSTRUCTIONS

BEFORE NEXT FLIGHT YES

NO ARE

DEFORMATIONS OR CRACKS? ANY

SERVICE BULLETIN A330−53−3217 AT THIS LOCATION ACCOMPLISH MODIFICATION THE REPORT SHEET TO AIRBUS COMPLETE AND SEND

NO FURTHER ACTION AT THIS/THESE LOCATIONS BEFORE NEXT FLIGHT

G_SB_533212_6_FAAA_01_02 Figure A-GFAAA - Sheet 01 Inspection Flowchart for missing fasteners at Frame 58 to Frame 59 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 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

NO YES

**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. DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR57 − STGR26 LH AND RH, FR58A − STGR29RH TO STGR30RH, FR58A − STGR31RH TO STGR33RH, FR59 − STGR23RH, STGR24RH AND STGR25RH

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND

NO FURTHER ACTION AT THIS/THESE LOCATIONS ARE FASTENERS INSTALLED?

SERVICE BULLETIN A330−53−3217 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533212_6_FBAA_01_02 Figure A-GFBAA - Sheet 01 Inspection Flowchart for missing fasteners at Frame 57 to Frame 59 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 26 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

NO YES DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR59 − STGR40RH AND FR58 − STGR41 LH AND RH

ARE FASTENERS INSTALLED? 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 A330−53−3217 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN. AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR **NOTE:** THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE G_SB_533212_6_FCAA_01_03 Figure A-GFCAA - Sheet 01 Inspection Flowchart for missing fasteners at Frame 58 and Frame 59 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 27 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z150

DETAILED INSPECTION FOR MISSING FASTENERS. **NOTE:** 01 LH SHOWN RH SYMMETRICAL 

## A FR58 FR57 FR56 FR55 FR54



### B STGR26 

### A

FR57

VIEW LOOKING ON OUTBOARD SKIN 

## B STGR25

STGR26

STGR27

**FWD** 01

G_SB_533212_6_BAAA_01_02 Figure A-GBAAA - Sheet 01 Inspection of the fasteners at Frame 57, STGR26 LH and RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 28 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z150 

### A

**NOTE:** 01 02 FR58 FR59 STGR38RH 

### B

FR58

STGR38RH

01 02 02 **FWD** 

## B **A**

DETAILED INSPECTION FOR MISSING FASTENERS. DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. G_SB_533212_6_BBAA_01_02 Figure A-GBBAA - Sheet 01 Inspection of the fasteners at Frame 58 to Frame 59, STGR38 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 29 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z150 

### A

**NOTE:** 01 02 FR57 FR58 FR59



## A

STGR41

STGR42

STGR43

STGR44

STGR45 FR58

LH SHOWN RH SYMMETRICAL 

### B



## B 02

01 02

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. STGR41RH

STGR41LH

G_SB_533212_6_BCAA_01_04 Figure A-GBCAA - Sheet 01 Inspection of the fasteners at Frame 58, STGR41 LH and RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 30 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z150 

### A

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). **NOTE:** 01 FR58 FR59 STGR30RH 

### B

VIEW LOOKING FORWARD STGR29RH

STGR30RH

STGR31RH

STGR32RH

STGR33RH FR58A 

## B **C**

01 FR58A

**FWD** 

## C **A** FR58A

G_SB_533212_6_BDAA_01_03 Figure A-GBDAA - Sheet 01 Inspection of the fasteners at Frame 58A, STGR29 RH to STGR30 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 31 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z150 

### A

DETAILED INSPECTION FOR MISSING FASTENERS (6 PILOT HOLES EXIST). **NOTE:** 01 FR58 FR59 STGR32RH 

### B

VIEW LOOKING FORWARD STGR29RH

STGR30RH

STGR31RH

STGR32RH

STGR33RH FR58A 

## B **C** FR58A

**FWD** 

## C **A** FR58A

STGR32RH 01

G_SB_533212_6_BEAA_01_03 Figure A-GBEAA - Sheet 01 Inspection of the fasteners at Frame 58A, STGR31 RH to STGR33 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 32 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 FORWARD 

## B FR59 

## C TYPICAL INSTALLATION 

## A **A** FR59 FR60 STGR23RH STGR25RH 

### B

STGR23RH

STGR24RH

STGR25RH 

### C **C C** 

**F W**  **D** 01 Z260

G_SB_533212_6_BFAA_01_04 Figure A-GBFAA - Sheet 01 Inspection of the fasteners at Frame 59, STGR23 RH, STGR24 RH and STGR25 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 33 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z150



## A FR62 FR61 FR60 FR59 FR58



### B STGR26LH 

### A

**NOTE:** 02 VIEW LOOKING ON OUTBOARD SKIN 

## B STGR27LH

**FWD** STGR26LH STGR25LH FR59

01 02

01

DETAILED INSPECTION FOR MISSING FASTENERS. DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. G_SB_533212_6_BGAA_01_04 Figure A-GBGAA - Sheet 01 Inspection of the fasteners at Frame 59, STGR26 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 34 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z150 

### A

**NOTE:** 01 02 FR58 FR59 

### B



## A FR59 STGR40RH

**FWD** 

### A

**A** 02 02



## B 01



## A **A** VIEW LOOKING FORWARD ON STGR40RH STGR40RH DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. G_SB_533212_6_BHAA_01_04 Figure A-GBHAA - Sheet 01 Inspection of the fasteners at Frame 59, STGR40 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 35 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

YES FINDINGS: DATE OF INSPECTION: INSPECTION METHOD:

LOCATION FLIGHT HOURS: NO

INSPECTION ACTIONS: FOLLOW−UP ACTIONS: FASTENER(S) AIRBUS CONTACTED? INSTALLED? DAMAGE FASTENER FOUND AT ADJACENT LOCATIONS? YES NO YES NO YES NO YES NO FR57, STGR 26 LH AND RH FR58 − FR59, STGR 38RH FR58, STGR 41 LH AND RH N/A N/A

FR58A, STGR 29RH − STGR 30RH N/A N/A FR58A, STGR 31RH − STGR 33RH N/A N/A FR59, STGR23RH, STGR24RH, N/A N/A STGR25RH FR59, STGR 26LH FR59, STGR 40RH CUSTOMER SERVICE ENGINEERING − SEES1 FUSELAGE (WB/LR) − VERTICAL TAIL PLANE − CENTER WING BOX (WR/LR) 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE E−mail: Structure.sbinspectionresult@airbus.com FAX +33 (0)5 61 93 36 14 SERVICE BULLETIN No.: A330−53−3212 A/C MSN: INSPECTION REPORT

FLIGHT CYCLES: RETURN TO: AIRBUS

DETAILED INSPECTION

ACCOMPLISHED? BULLETIN No. A330−53−3217 SERVICE

G_SB_533212_6_RAAA_01_00 Figure A-GRAAA - Sheet 01 Inspection Report DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 36 6

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - REAR FUSELAGE - INSPECTION FOR SUSPECTED MISSING/NON-CONFORMING FASTENERS AT SECTION 16 AND SECTION 17 FROM FR57 TO FR59 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.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 1 6

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

# @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.: A330-53-3212 REVISION No.: 00 - May 06/14 Page: 1 6

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