@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.

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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 533202-832-848-001: Inspection

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

APPENDICES

None

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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

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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

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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 - 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

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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, 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.

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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 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.

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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

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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

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SERVICE BULLETIN

This Page Intentionally Left Blank

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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 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.

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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.

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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.

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(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

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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

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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.

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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

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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

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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

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@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

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@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

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@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

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@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

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@A330

SERVICE BULLETIN

**CONF ALL

NO YES

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

NO DEFORMATIONS YES

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

NO YES

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

NO YES

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

NO YES

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

NO YES 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

NO YES

FR37.3, FR37.4 STGR41 − STGR42RH

THE REPORT SHEET

TO AIRBUS

COMPLETE AND SEND

INSPECTION OF THE

ADJACENT FASTENER

ROWS

DO A DETAILED

NO YES 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

YES NO

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

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@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

YES NO

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

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@A330

SERVICE BULLETIN

**CONF ALL

A

A

Z130 FR19

B

STGR52LH

STGR53LH

STGR52LH

STGR53LH

DETAILED INSPECTION FOR MISSING FASTENERS.

NOTE:

01

02 DETAILED INSPECTION OF ADJACENT FASTENER CONDITION.

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

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@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

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@A330

SERVICE BULLETIN

**CONF ALL

FR20

STGR43LH

STGR44LH

NOTE:

01

03

C

VIEW LOOKING FWD

02 DETAILED INSPECTION OF ADJACENT FASTENER CONDITION.

03 DETAILED INSPECTION TO IDENTIFY DAMAGE ON THE FRAME INNER FLANGE.

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

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@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

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@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

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@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

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@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

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@A330

SERVICE BULLETIN

**CONF ALL

STGR41RH

STGR42RH

STGR43RH

C

FR

STGR43RH STGR42RH STGR41RH

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:

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

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

FINDINGS: YES

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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