@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.

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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

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SERVICE BULLETIN

SUMMARY

**CONF ALL

A C

NOTE:

INSPECTION AREAS

LH SHOWN

RH SYMMETRICAL

FR60

FR59

FR58

FR57

FR56

STGR26

FR57

FR58

FR59

A FR58

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

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: May 06/14 SERVICE BULLETIN No.: A330-53-3212

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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

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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.

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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.

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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.

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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

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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

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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.

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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.

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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.

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(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

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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

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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

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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

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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

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@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

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@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

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@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

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@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

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@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

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@A330

SERVICE BULLETIN

**CONF ALL

YES NO

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

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@A330

SERVICE BULLETIN

**CONF ALL

YES NO

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

YES NO

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

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@A330

SERVICE BULLETIN

**CONF ALL

Z150

A

NOTE:

01

02

FR58

FR59

STGR38RH

B

FR58

STGR38RH

02 01 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

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@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

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@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

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@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

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@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

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@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

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@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

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SERVICE BULLETIN

**CONF ALL

FINDINGS: YES

DATE OF INSPECTION:

INSPECTION METHOD:

LOCATION

FLIGHT HOURS:

NO

INSPECTION ACTIONS: FOLLOW−UP ACTIONS:

FASTENER(S) AIRBUS

INSTALLED? CONTACTED?

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

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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

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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.: A330-53-3212

REVISION No.: 00 - May 06/14 Page: 1

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