# @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 - FORWARD FUSELAGE - INSPECTION FOR SUSPECTED MISSING/NON - CONFORMING FASTENERS AT SECTION 13 AND 14 FR19 TO FR37.4 **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 forward fuselage at Section 13 and 14, from Frame (FR)19 to FR22 and from FR26/28 to FR37.4. 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. A330-53-3216. 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.: A330-53-3202 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 533202-832-848-001: Inspection TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 10.00 APPENDICES None

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 2 6

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# @A330 SERVICE BULLETIN SUMMARY
**CONF ALL

FR20 FR37.3 FR37.4 

## A FR19

Z130 STGR52LH STGR53LH

STGR43RH

STGR43LH 

## D FR21

FR21 FR22 Y1456
Y1959 Y−1456
Y−953



## B

**C** FR22

G_SB_533202_6_SAAA_01_01 

### F Z240



### A **B C** 

**D E**  **G**

Figure A-GSAAA - Sheet 01 Location of the Inspection Areas DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 3 6

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# @A330 SERVICE BULLETIN SUMMARY
**CONF ALL

FR34 FR35 FR36 FR37

STGR25RH

FR30 FR31 FR32 FR33 FR35 FR36 FR37 FR37.1 FR37.2 FR37.4 FR38 FR37.3

FR30 FR29 FR28

STGR26LH

STGR33LH STGR34LH FR34

STGR24RH 

## E

**F G**  STGR41RH STGR42RH

G_SB_533202_6_SAAA_02_02 Figure A-GSAAA - Sheet 02 Location of the Inspection Areas DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 4 6

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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 - FORWARD FUSELAGE - INSPECTION FOR SUSPECTED MISSING/NON - CONFORMING FASTENERS AT SECTION 13 AND 14 FR19 TO FR37.4 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.: A330-53-3202 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 forward fuselage at Section 13 and 14, from Frame (FR)19 to FR22 and from FR26/28 to FR37.4. (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. A330-53-3216. (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.: A330-53-3202 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 533202-832-848-001: Inspection (1) At FR19, STGR52/STGR53 LH, do a Detailed Inspection for Missing Fasteners (2) At FR20 and STGR43 LH, do a Detailed Inspection for the Installation of Fasteners (3) At FR21 and FR22 LH, do a Detailed Inspection for Missing Fasteners (4) At FR21 and FR22 RH, do a Detailed Inspection for Missing Fasteners (5) At FR26/28 and STGR26 LH, do a Detailed Inspection for Missing Fasteners (6) At FR30, between STGR33/STGR34 LH, do a Detailed Inspection for Missing Fasteners (7) At FR30 to FR37.1, FR37.3 and FR37.4 between STGR41/STGR42 RH, do a Detailed Inspection for Missing Fasteners (8) At FR35 between STGR24/STGR25 RH, do a Detailed Inspection for Missing Fasteners (9) At FR37.3 and STGR44 RH, do a Detailed Inspection for the Installation of 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 and/or intervals and/or date) 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 Organization Approval No. EASA.21J.031. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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 533202-832-848-001: Inspection Get Access 3.50 On Aircraft At FR19, STGR52/STGR53 LH, do a Detailed Inspection for Missing Fasteners 0.50 At FR20 and STGR43 LH, do a Detailed Inspection for the Installation of Fasteners 0.50 At FR21 and FR22 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR21 and FR22 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR26/28 and STGR26 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR30, between STGR33/STGR34 LH, do a Detailed Inspection for Missing Fasteners 0.25 At FR30 to FR37.1, FR37.3 and FR37.4 between STGR41/STGR42 RH, do a Detailed Inspection for Missing Fasteners 0.50 At FR35 between STGR24/STGR25 RH, do a Detailed Inspection for Missing Fasteners 0.25 At FR37.3 and STGR44 RH, do a Detailed Inspection for the Installation of Fasteners 0.25 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. H. WEIGHT AND BALANCE Not Changed

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 4 6

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# @A330 SERVICE BULLETIN 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 25-23-43 25-52-00 25-80-00 52-31-00 52-80-00 53-00-00 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-53-3216 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.: A330-53-3202 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.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 7 6

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# @A330 SERVICE BULLETIN

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DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 8 6

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# @A330 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 533202-832-848-001 - 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 ELECTRICAL 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.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 9 6

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# @A330 SERVICE BULLETIN Task Associated Data Zone 130 240 Access Door 821 831 Panel 131DF 131NG 132DF 132FG 132HG 132KG 132MC 132NX 242DW 242EW 242FW 242GW Manpower TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 10.00 A. GENERAL (1) Subtask 533202-910-201-001 - 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 533202-839-201-001 - 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.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 10 6

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# @A330 SERVICE BULLETIN B. PREPARATION (1) Subtask 533202-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 131NG, Panel 132KG, Panel 131DF, Panel 132DF, Panel 132HG, Panel 132NX, Panel 132FG 240 Access Door 831 Panel 242DW, Panel 242EW, Panel 242FW, Panel 242GW Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-23-43-000-802 Task 25-52-00-000-801 Task 25-80-00-000-801 52-31-00, Page Block 001 Task 53-00-00-000-802 (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 FWD cargo compartment door 821. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 11 6

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# @A330 SERVICE BULLETIN (d) Open the FWD cargo-compartment door 821, refer to AMM 52-31-00, Page Block 001. (e) In the Main-Deck Cargo Compartment, at Frame 35 RH, remove the lining panels 242DW, 242EW, 242FW and 242GW, refer to AMM Task 25-23-43-000-802. (f) In the FWD cargo-compartment, remove floor panels 131NG, 131DF, 132DF, 132FG, 132HG and 132KG, refer to AMM Task 53-00-00-000-802. (g) In the FWD cargo-compartment, remove the sidewall panels 132NX, refer to AMM Task 25-52-00-000-801. (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 533202-832-204-001 - At FR19, STGR52/STGR53 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 131NG Work location Frame 19 from Stringer 52LH to Stringer 53LH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Service Bulletin (SB) A330-53-3216 Fig. A-GCAAA Inspection of the fasteners at Frame 19 between STGR52/STGR53 LH Sheet 01 Fig. A-GFAAA Inspection Flowchart for missing fasteners at Frame 19 between STGR52/53 LH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 12 6

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# @A330 SERVICE BULLETIN (a) At Frame 19 between STGR52/STGR53 LH, 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, Part Number (PN) DAN6-6-4, are installed at the locations as shown in Fig. A-GCAAA 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 533202-832-201 001 At FR20 and STGR43 LH, do a Detailed Inspection for the Installation of Fasteners . 2 If the 4.8 mm (0.189 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GCAAA 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-GCAAA Sheet 01 , View B: <1> If you find damage or cracks at the adjacent fasteners, contact AIRBUS for further instructions before the next flight. <2> If you do not find damage or cracks at the adjacent fasteners, accomplish Modification Service Bulletin No. A330-53-3216 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 533202-832-201-001 - At FR20 and STGR43 LH, do a Detailed Inspection for the Installation of Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 131NG Work location Frame 20 Stringer 43LH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Service Bulletin (SB) A330-53-3216 Structural Repair Manual (SRM) 51-42-00 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 13 6

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# @A330 SERVICE BULLETIN
References Fig. A-GCBAA Inspection of the fasteners at Frame 20 and STGR43 LH Sheet 01 Sheet 02 Fig. A-GFBAA Inspection Flowchart for the installation of fasteners at Frame 20 and STGR43 LH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 20 and STGR43 LH, do a detailed inspection for the installation of fasteners, refer to Fig. A-GFBAA Sheet 01 : 1 If the correct 4.8 mm (0.189 in.) diameter fasteners, PN EN6081D6, are installed at the locations shown in Fig. A-GCBAA Sheet 01 and Fig. A-GCBAA Sheet 02, 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 533202-832-205 001 At FR21 and FR22 LH, do a Detailed Inspection for Missing Fasteners . 2 If there are fasteners of 4.0 mm (0.157 in.) diameter installed (dural rivets) at the locations as shown in Fig. A-GCBAA Sheet 01 and Fig. A-GCBAA Sheet 02, View C, do the worksteps which follow: a Refer to Fig. A-GCBAA Sheet 02, View C, remove and discard the 4.0 mm (0.157 in.) diameter fasteners and accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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 If no fasteners are installed at the locations shown in Fig. A-GCBAA Sheet 01 and Fig. A-GCBAA Sheet 02, View C, do the worksteps which follow: a Do a detailed inspection for damage to the surface protection of the inner frame flange and the condition of the adjacent fasteners (possible sheared fastener(s) or damaged surface protection), as shown in Fig. AGCBAA Sheet 02, View C. <1> If you find damage to the surface protection of the inner frame flange and/or at the adjacent fasteners, contact AIRBUS for further instructions before the next flight.

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 14 6

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# @A330 SERVICE BULLETIN <2> If you do not find damage at the inner frame flange or adjacent fasteners, accomplish Modification Service Bulletin A330-53-3216 at this location before the 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
. (3) Subtask 533202-832-205-001 - At FR21 and FR22 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 131DF Work location from Frame 21 to Frame 22 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3216 Fig. A-GCCAA Inspection of the fasteners between Frame 21 and Frame 22 LH and RH Sheet 01 Fig. A-GFCAA Inspection Flowchart for missing fasteners between Frames 21 and 22 LH and RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 21 and Frame 22 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFCAA Sheet 01 : 1 If the 3.2 mm (0.125 in.) diameter fasteners, PN EN6081D4, are installed at the locations as shown in Fig. A-GCCAA Sheet 01 , View D, 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 533202-832-209 001 At FR21 and FR22 RH, do a Detailed Inspection for Missing Fasteners . DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 15 6

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# @A330 SERVICE BULLETIN
2 If the 3.2 mm (0.125 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GCCAA Sheet 01 , View D, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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
. (4) Subtask 533202-832-209-001 - At FR21 and FR22 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 132DF Work location from Frame 21 to Frame 22 Manpower Resources Manhours 0.25 Minimum number of person 1 Skills References Service Bulletin (SB) A330-53-3216 Fig. A-GCCAA Inspection of the fasteners between Frame 21 and Frame 22 LH and RH Sheet 01 Fig. A-GFCAA Inspection Flowchart for missing fasteners between Frames 21 and 22 LH and RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 21 and Frame 22 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFCAA Sheet 01 : 1 If the 3.2 mm (0.125 in.) diameter fasteners, PN EN6081D4, are installed at the locations as shown in Fig. A-GCCAA Sheet 01 , View D, 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 533202-832-206 001 At FR26/28 and STGR26 LH, do a Detailed Inspection for Missing Fasteners . DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 16 6

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# @A330 SERVICE BULLETIN
2 If the 3.2 mm (0.125 in.) diameter fasteners are not installed at the locations as shown in Fig. A-GCCAA Sheet 01 , View D, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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 533202-832-206-001 - At FR26/28 and STGR26 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Work location Frame 26/28 Stringer 26LH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3216 Fig. A-GFDAA Inspection Flowchart for missing fasteners at Frame 26/28 and STGR26 LH Sheet 01 Fig. A-GCDAA Inspection of the fasteners at Frame 26/28 and STGR26 LH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 26/28 and STGR26 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFDAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fastener, PN DAN6-6-4, is installed at the location as shown in Fig. A-GCDAA 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
. DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 17 6

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

# @A330 SERVICE BULLETIN b Go to SUBTASK 533202-832-207 001 At FR30, between STGR33/STGR34 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-GCDAA Sheet 01 , View B, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3216 at this location before the next flight. NOTE : The fastener hole exists in the seat rail plate. 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
. (6) Subtask 533202-832-207-001 - At FR30, between STGR33/STGR34 LH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 132NX Work location Frame 30 from Stringer 33LH to Stringer 34LH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3216 Fig. A-GCEAA Inspection of the fasteners at Frame 30 between STGR33/STGR34 Sheet 01 Fig. A-GFEAA Inspection Flowchart for missing fasteners at Frame 30 between STGR33/STGR34 LH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 18 6

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

# @A330 SERVICE BULLETIN (a) At Frame 30 and STGR33/STGR34 LH, do a detailed inspection for missing fasteners, refer to Fig. A-GFEAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fasteners, PN DAN6-6-3, are installed at the locations as shown in Fig. A-GCEAA 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 533202-832-208 001 At FR30 to FR37.1, FR37.3 and FR37.4 between STGR41/STGR42 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 as shown in Fig. A-GCEAA Sheet 01 , View B, do the worksteps which follow: a Do a detailed inspection of the adjacent fasteners for damage, deformations or cracks. <1> If you find damage or cracks at the adjacent fasteners, contact AIRBUS for further instructions before the next flight. <2> If you do not find damage or cracks at the adjacent fasteners, accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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
. (7) Subtask 533202-832-208-001 - At FR30 to FR37.1, FR37.3 and FR37.4 between STGR41/STGR42 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 132FG, Panel 132HG, Panel 132KG Work location from Frame 30 to Frame 37.1 Frame 37.3 Frame 37.4 from Stringer 41RH to Stringer 42RH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 19 6

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

# @A330 SERVICE BULLETIN
References Service Bulletin (SB) A330-53-3216 Fig. A-GCFAA Inspection of the fasteners at Frames 30 thru 37.1, Frame 37.3 and Frame 37.4 between STGR41/STGR42 RH Sheet 01 Sheet 02 Fig. A-GFFAA Inspection Flowchart for missing fasteners at Frames 30 thru 37.1, Frame 37.3 and Frame 37.4 between STGR41/STGR42 RH Sheet 01
Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 30 thru Frame 37.1, Frame 37.3 and Frame 37.4 at STGR41/STGR42 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFFAA Sheet 01 : 1 If the 4.8 mm (0.189 in.) diameter fasteners, PN DAN5-6-4, are installed at the locations as shown in Fig. A-GCFAA Sheet 01 and Fig. A-GCFAA Sheet 02, 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 533202-832-202 001 At FR35 between STGR24/STGR25 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 as shown in Fig. A-GCFAA Sheet 01 and Fig. A-GCFAA Sheet 02, View C, do the worksteps which follow: a Do a detailed inspection of the adjacent fasteners for damage, deformations or cracks. <1> If you find damage or cracks at the adjacent fasteners, contact AIRBUS for further instructions before the next flight. <2> If you do not find damage or cracks at the adjacent fasteners, accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 20 6

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

# @A330 SERVICE BULLETIN (8) Subtask 533202-832-202-001 - At FR35 between STGR24/STGR25 RH, do a Detailed Inspection for Missing Fasteners Work Zones and Access Panels Zone Access/Work location 240 Access Door 831 Panel 242DW, Panel 242EW, Panel 242FW, Panel 242GW Work location Frame 35 from Stringer 24RH to Stringer 25RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3216 Fig. A-GCGAA Inspection of the fasteners at Frame 35 between STGR24/STGR25 RH Sheet 01 Sheet 02 Fig. A-GFGAA Inspection Flowchart for missing fasteners at Frame 35 between STGR24/STGR25 RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01 (a) At Frame 35 between STGR24/STGR25 RH, do a detailed inspection for missing fasteners, refer to Fig. A-GFGAA Sheet 01 : 1 If the 4.0 mm (0.157 in.) diameter fasteners, PN EN6081D5, are installed at the locations as shown in Fig. A-GCGAA Sheet 01 and Fig. A-GCGAA Sheet 02, 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 533202-832-203 001 At FR37.3 and STGR44 RH, do a Detailed Inspection for the Installation of Fasteners .

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 21 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 as shown in Fig. A-GCGAA Sheet 01 and Fig. A-GCGAA Sheet 02, View C, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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 533202-832-203-001 - At FR37.3 and STGR44 RH, do a Detailed Inspection for the Installation of Fasteners Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 132KG Work location Frame 37.3 Stringer 44RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Service Bulletin (SB) A330-53-3216 Fig. A-GCHAA Inspection of the fasteners at Frame 37.3 and STGR44 RH Sheet 01 Sheet 02 Fig. A-GFHAA Inspection Flowchart for the installation of fasteners at Frame 37.3 and STGR44 RH Sheet 01 Fig. A-GRAAA Inspection Report Sheet 01

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 22 6

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

# @A330 SERVICE BULLETIN (a) At Frame 37.3 and STGR44 RH, do a detailed inspection for the installation of fasteners, refer to Fig. A-GFHAA Sheet 01 : 1 If the correct 4.0 mm (0.157 in.) diameter fasteners, PN EN6081D5 or DAN5-5, are installed at the locations as shown in Fig. A-GCHAA Sheet 01 and Fig. A-GCHAA Sheet 02, 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
. 2 If there are fasteners of 3.2 mm (0.125 in.) diameter installed (dural rivets) at the locations as shown in Fig. A-GCHAA Sheet 02, do the worksteps which follow: a Refer to Fig. A-GCHAA Sheet 01 and Fig. A-GCHAA Sheet 02, remove and discard the 3.2 mm (0.125 in.) diameter fasteners and accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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 If no fasteners are installed at the locations as shown in Fig. A-GCHAA Sheet 01 and Fig. A-GCHAA Sheet 02, View C, do the worksteps which follow: a Accomplish Modification Service Bulletin No. A330-53-3216 at this location before the 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 E. CLOSE-UP (1) Subtask 533202-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 821 Panel 131NG, Panel 132KG, Panel 132MC, Panel 132NX, Panel 131DF, Panel 132DF, Panel 132FG, Panel 132HG
DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 23 6

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

# @A330 SERVICE BULLETIN
240 Access Door 831 Panel 242DW, Panel 242EW, Panel 242FW, Panel 242GW Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 25-23-43-400-802 Task 25-52-00-400-801 52-31-00, Page Block 001 Task 52-80-00-400-801 Task 53-00-00-400-802 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the insulation blankets that you removed to get access to the work areas, refer to AMM Task 52-80-00-400-801. (c) In the Main Deck Cargo Compartment (MDCC), at Frame 35 RH, install the lining panels 242DW, 242EW, 242FW and 242GW, refer to AMM Task 25-23-43-400-802. (d) In the FWD cargo-compartment, install the sidewall panel 132NX, refer to AMM Task 25-52-00-400-801. (e) In the FWD cargo-compartment, install floor panels 131NG, 131DF, 132DF, 132FG, 132HG and 132KG, refer to AMM Task 53-00-00-400-802. (f) Close the FWD cargo-compartment door 821, refer to AMM 52-31-00, Page Block 001. (g) Remove the access platform(s).

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

YES NO

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 DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR19 STGR52 − STGR53LH

INSPECTION OF THE ADJACENT FASTENER ROWS DO A DETAILED

YES NO DEFORMATIONS OR CRACKS? ANY

NO FURTHER ACTION

AT THIS LOCATION CONTACT AIRBUS BEFORE NEXT FLIGHT FOR FURTHER INSTRUCTIONS

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND ARE FASTENERS INSTALLED?

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533202_6_FAAA_01_07 Figure A-GFAAA - Sheet 01 Inspection Flowchart for missing fasteners at Frame 19 between STGR52/53 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

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 DO A DETAILED INSPECTION FOR THE INSTALLATION OF FASTENERS AT FR20 STGR43LH

DO A DETAILED INSPECTION OF THE

INNER FLANGE FOR ANY DAMAGE

TO THE SURFACE PROTECTION OR SHEARED FASTENERS

FINDINGS

NO FURTHER ACTION

AT THIS LOCATION COMPLETE AND SEND THE REPORT SHEET TO AIRBUS
FOR FURTHER INSTRUCTIONS YES

YES NO

BEFORE THE NEXT FLIGHT CONTACT AIRBUS INSTALLED CORRECT FASTENERS INSTALLED? ARE

NO FASTENERS NO

INSTALLED INCORRECT FASTENERS

FASTENERS REMOVE INCORRECT OR

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533202_6_FBAA_01_08 Figure A-GFBAA - Sheet 01 Inspection Flowchart for the installation of fasteners at Frame 20 and STGR43 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

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 YES NO

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND

NO FURTHER ACTION

AT THIS LOCATION DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR21 AND FR22LH/RH

ARE FASTENERS INSTALLED?

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533202_6_FCAA_01_08 Figure A-GFCAA - Sheet 01 Inspection Flowchart for missing fasteners between Frames 21 and 22 LH and RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

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 YES NO

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND

NO FURTHER ACTION

AT THIS LOCATION DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR26/28 STGR26LH

ARE FASTENERS INSTALLED?

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533202_6_FDAA_01_08 Figure A-GFDAA - Sheet 01 Inspection Flowchart for missing fasteners at Frame 26/28 and STGR26 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

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 YES NO DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR30 STGR33 − STGR34LH

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND INSPECTION OF THE ADJACENT FASTENER ROWS DO A DETAILED

YES NO DEFORMATIONS OR CRACKS? ANY

NO FURTHER ACTION AT THIS LOCATION THE REPORT SHEET TO AIRBUS COMPLETE AND SEND ARE FASTENERS INSTALLED?

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT FOR FURTHER INSTRUCTIONS BEFORE THE NEXT FLIGHT CONTACT AIRBUS

G_SB_533202_6_FEAA_01_09 Figure A-GFEAA - Sheet 01 Inspection Flowchart for missing fasteners at Frame 30 between STGR33/STGR34 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

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 YES NO FR37.3, FR37.4 STGR41 − STGR42RH

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND INSPECTION OF THE ADJACENT FASTENER ROWS DO A DETAILED

YES NO DEFORMATIONS OR CRACKS? ANY

NO FURTHER ACTION AT THIS LOCATION CONTACT AIRBUS BEFORE NEXT FLIGHT FOR FURTHER

THE REPORT SHEET TO AIRBUS COMPLETE AND SEND INSTRUCTIONS DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR30 − FR37, FR37.1,

ARE FASTENERS INSTALLED?

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533202_6_FFAA_01_08 Figure A-GFFAA - Sheet 01 Inspection Flowchart for missing fasteners at Frames 30 thru 37.1, Frame 37.3 and Frame 37.4 between STGR41/STGR42 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

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 DO A DETAILED INSPECTION FOR MISSING FASTENERS AT FR35 STGR24 − STGR25RH

NO FURTHER ACTION

AT THIS LOCATION COMPLETE AND SEND THE REPORT SHEET TO AIRBUS NO YES ARE FASTENERS INSTALLED?

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533202_6_FGAA_01_07 Figure A-GFGAA - Sheet 01 Inspection Flowchart for missing fasteners at Frame 35 between STGR24/STGR25 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

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 DO A DETAILED INSPECTION FOR THE INSTALLATION OF FASTENERS AT FR37.3 STGR44RH

COMPLETE AND SEND

THE REPORT SHEET TO AIRBUS
NO FURTHER ACTION

AT THIS LOCATION NO YES CORRECT FASTENERS INSTALLED? ARE

INCORRECT FASTENERS INSTALLED NO FASTENERS INSTALLED OR

FASTENERS REMOVE INCORRECT

SERVICE BULLETIN A330−53−3216 AT THIS LOCATION ACCOMPLISH MODIFICATION BEFORE NEXT FLIGHT

G_SB_533202_6_FHAA_01_07 Figure A-GFHAA - Sheet 01 Inspection Flowchart for the installation of fasteners at Frame 37.3 and STGR44 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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



### A



## A FR19 Z130 

### B

STGR52LH

STGR53LH STGR52LH

STGR53LH

DETAILED INSPECTION FOR MISSING FASTENERS. **NOTE:** 01 DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. 02 STGR54LH 01

01 02

**FWD**



## B FR19

G_SB_533202_6_CAAA_01_06 Figure A-GCAAA - Sheet 01 Inspection of the fasteners at Frame 19 between STGR52/STGR53 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

Z130

FR20 FR25 

### A

**B**


## A

STGR44LH STGR43LH

STGR50LH FR20



## B **C**

G_SB_533202_6_CBAA_01_00 Figure A-GCBAA - Sheet 01 Inspection of the fasteners at Frame 20 and STGR43 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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

FR20

STGR43LH

STGR44LH

**NOTE:** 01 03



## C VIEW LOOKING FWD

DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. 02 DETAILED INSPECTION TO IDENTIFY DAMAGE ON THE FRAME INNER FLANGE. 03 02

01 01

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST).
G_SB_533202_6_CBAA_02_04 Figure A-GCBAA - Sheet 02 Inspection of the fasteners at Frame 20 and STGR43 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 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 

### B **C A** 

Z130

**NOTE:** 01 TYPICAL 01 FR20 FR21 FR22

FR21 FR22

FR21 FR22 Y1456
Y1959 Y−1456
Y−953 

## A

**B**

**C D** 

**D D** 

**D**



## D

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). G_SB_533202_6_CCAA_01_04 Figure A-GCCAA - Sheet 01 Inspection of the fasteners between Frame 21 and Frame 22 LH and RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 36 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

**NOTE:** 01 (THE FASTENER HOLE FOR DAN6−6 EXISTS IN SEAT RAIL PLATE). Z130



## B Y2244 Y2462 Y2525.5

FR29 **FWD** 01 FR30 FR29 STGR26LH 

### B



## A **A**

FR26/28

FR26/28

DETAILED INSPECTION FOR MISSING FASTENERS G_SB_533202_6_CDAA_01_04 Figure A-GCDAA - Sheet 01 Inspection of the fasteners at Frame 26/28 and STGR26 LH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 37 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



## A FR32 FR31 FR30 FR29

STGR33LH Z130 

### A

STGR34LH 

### B

FR30
STGR33LH

STGR34LH

STGR35LH

**NOTE:** 01 02 01 02 02

VIEW LOOKING ON OUTER SKIN **FWD** 

## B

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. G_SB_533202_6_CEAA_01_05 Figure A-GCEAA - Sheet 01 Inspection of the fasteners at Frame 30 between STGR33/STGR34 DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 38 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z130 

### A

FR30 FR31 FR32 FR33 FR34 FR35 FR36 FR37 FR37.1 FR37.2 FR37.4 FR38 FR37.3



## A **B**

**B B**  **B B**  **B** STGR41RH STGR42RH

G_SB_533202_6_CFAA_01_03 Figure A-GCFAA - Sheet 01 Inspection of the fasteners at Frames 30 thru 37.1, Frame 37.3 and Frame 37.4 between STGR41/STGR42 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 39 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

STGR41RH

STGR42RH

STGR43RH 

### C

FR STGR41RH STGR42RH STGR43RH

**NOTE:** 01 02 02 01 **F W**  **D** 

## C TYPICAL 

## B VIEW LOOKING FWD

DETAILED INSPECTION FOR MISSING FASTENERS (PILOT HOLES EXIST). DETAILED INSPECTION OF ADJACENT FASTENER CONDITION. G_SB_533202_6_CFAA_02_04 Figure A-GCFAA - Sheet 02 Inspection of the fasteners at Frames 30 thru 37.1, Frame 37.3 and Frame 37.4 between STGR41/STGR42 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 40 6

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# @A330 SERVICE BULLETIN

**CONF ALL

Z240

FR32 FR33 FR34 FR35 FR36 FR37

STGR11RH

STGR24RH STGR25RH FR32 FR37
STGR11RH STGR31RH 

### B

**C**



## B **A**

STGR31RH 

### A

G_SB_533202_6_CGAA_01_00 Figure A-GCGAA - Sheet 01 Inspection of the fasteners at Frame 35 between STGR24/STGR25 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 41 6

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# @A330 SERVICE BULLETIN

**CONF ALL

FR35

STGR24RH



## C

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

G_SB_533202_6_CGAA_02_02 Figure A-GCGAA - Sheet 02 Inspection of the fasteners at Frame 35 between STGR24/STGR25 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 42 6

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# @A330 SERVICE BULLETIN

**CONF ALL

Z130 

### A



## A FR36 FR37.3 FR37.4 

### B

STGR44RH

STGR50RH FR37.3


### C



## B

G_SB_533202_6_CHAA_01_00 Figure A-GCHAA - Sheet 01 Inspection of the fasteners at Frame 37.3 and STGR44 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 43 6

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# @A330 SERVICE BULLETIN

**CONF ALL

FR37.3

STGR44RH

VIEW LOOKING FWD 

## C

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

G_SB_533202_6_CHAA_02_04 Figure A-GCHAA - Sheet 02 Inspection of the fasteners at Frame 37.3 and STGR44 RH DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 44 6

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# @A330 SERVICE BULLETIN

**CONF ALL

YES FINDINGS: DATE OF INSPECTION: INSPECTION METHOD:

LOCATION FLIGHT HOURS: NO

INSPECTION ACTIONS: FASTENER(S) INSTALLED?
YES NO YES NO YES NO FR19, STGR52LH AND STGR53LH FR20, STGR43LH FR21 AND FR22 LH AND RH FR26/28, STGR26LH FR30, STGR33 AND STGR34LH FR30−37.1, FR37.3 AND FR37.4 STGR41 AND STGR42RH FR35, STGR24 AND STGR25RH FR37.3, STGR44RH 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.: A330−53−3202 A/C MSN: INSPECTION REPORT

FLIGHT CYCLES: RETURN TO: AIRBUS

DETAILED INSPECTION FOLLOW−UP ACTIONS: AIRBUS CONTACTED?
YES NO YES NO ACCOMPLISHED? BULLETIN No. A330−53−3216 SERVICE DAMAGE FASTENER FOUND AT ADJACENT LOCATIONS?

N/A N/A N/A N/A

N/A N/A N/A N/A INSTALLED? CORRECT FASTENER(S) WAS INSTALLED: IF A FASTENER

N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A

G_SB_533202_6_RAAA_01_04 Figure A-GRAAA - Sheet 01 Inspection Report DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 45 6

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - FORWARD FUSELAGE - INSPECTION FOR SUSPECTED MISSING/NON - CONFORMING FASTENERS AT SECTION 13 AND 14 FR19 TO FR37.4 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.: A330-53-3202 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.: A330-53-3202 REVISION No.: 00 - May 06/14 Page: 1 6

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