@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.

ATA SYSTEM: 36

TITLE: PNEUMATIC - LEAK DETECTION - ADAPT DUAL LOOP AFTER FIRST

RETROFIT

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 58530D46962

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The APU bleed leak detection system detects any ambient overheat in the vicinity of the APU bleed air

ducts. It is made of a single overheat detection loop which runs along the APU bleed air ducts in

section 15/21 and section 16 thru 19.1. The SFAR88 requirements will induce MMEL restrictions on this

system from 2009.

This Service Bulletin details the installation of a second APU bleed leak detection loop (APU LOOP

B) in parallel to the current APU loop (APU LOOP A) in section 15/21 and section 16 thru 19.1.

The Service Bulletin No. A330-36-3032 ’Introduce Adapted Dual-Loop Overheat-Detection APU BleedAir-Duct ’was retrofitted on the first aircraft in May 2008. After a check of the overheat-detectionloop installation, some none compliances to ATA 36-22 installation requirements have been reported.

This Service Bulletin provides design improvements to the Service Bulletin No. A330-36-3032 OHDS

installation.

The accomplishment of this Service Bulletin improves dual-loop overheat-detection of APU Bleed-AirDuct, in accordance to ATA 36-22 installation requirements.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD NO A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational

disruptions.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 363038A01R01 1 27,500.00 Sensing element

Kit 363038A02R01 1 1,800.00 Bundle, Clamp, Hardware

Kit 363038D01R01 1 280.00 Clamp, placards and tie-cables

Kit 363038D10R01 1 55.00 Sleeves, screws, spacers and clamps

Kit 363038D12R00 1 35.00 Sleeves, screw, spacer and clamps

Kit 363038D14R00 1 2,870.00 Sleeves

TOTAL 32,540.00

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 363038A01R01 1 27,500.00 Sensing element

Kit 363038A02R01 1 1,800.00 Bundle, Clamp, Hardware

Kit 363038D01R01 1 280.00 Clamp, placards and tie-cables

Kit 363038D11R01 1 65.00 Sleeves, screws, spacers and clamps

Kit 363038D12R00 1 35.00 Sleeves, screw, spacer and clamps

Kit 363038D14R00 1 2,870.00 Sleeves

TOTAL 32,550.00

EFFECTIVITY

**CONF ALL

This Service Bulletin is applicable to this (these) operator(s) :

AEA QAF QTR

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin(s) or the equivalent production modification(s):

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

SUMMARY

Service Bulletin No. A330-36-3032 Mod. No. 55198D46286

55961D46493

55962D46494

NOTE: The Service Bulletin No. A330-36-3032 introduces the adapted dual loop overheat leak

detection of the APU bleed air duct.

NOTE: The Mod. No. 55198D46286 introduces the adapted dual loop overheat leak detection

of the APU bleed air duct.

NOTE: The Mod. No. 55961D46493 introduces the modification of the dual loop overheat leak

detection in section 19.

NOTE: The Mod. No. 55962D46494 introduces the modification of the dual loop overheat

detection (CFRP-bulkhead).

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER OIT SE999.0063/06

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 363038-831-848-001: Modification

TOTAL MANHOURS 166.00

ELAPSED TIME (HOURS) 88.25

**CONF 002

Task 363038-831-848-001: Modification

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 88.25

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

SUMMARY

APPENDICES

**CONF ALL

Appendix 01: Elapsed Time Assumptions

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

B

A

Z310

Z170

Z150 Z160

Z140

Z130

Z120

FR56

FR39.2

FR39.1

FR37

FR19

FR56

FR65

FR72

FR80

FR95

/82

FR95

800VU

A

B

ADAPTATION OF THE DUAL LOOP

OVERHEAT LEAK DETECTION AFTER

FIRST RETROFIT INSTALLATION

G_SB_363038_6_SAAA_01_00

ADAPTATION OF THE DUAL LOOP

OVERHEAT LEAK DETECTION AFTER

FIRST RETROFIT INSTALLATION

Figure A-GSAAA - Sheet 01

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 6

6

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 36

TITLE: PNEUMATIC - LEAK DETECTION - ADAPT DUAL LOOP AFTER FIRST

RETROFIT

MODIFICATION No.: 58530D46962

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

This modification is applicable by Service Bulletin only.

(1) Models

330-202 330-243

(2) Effectivity by MSN

0473 0489 0551 0597 0605

(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

AEA 0551 0597

QAF 0605

QTR 0473 0489

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0473 0489 0551 0597 001

0605 002

(5) Configuration definition

**CONF 001

Config. 001 is valid for all A330-200 aircraft given in the effectivity of this Service Bulletin

on which the Modification No. 48980D42587 is not embodied and on which the Service

Bulletin No. A330-36-3032 is accomplished.

**CONF 002

Config. 002 is valid for all A330-200 aircraft given in the effectivity of this Service Bulletin

on which the Modification No. 48980D42587 is embodied and the Service Bulletin No.

A330-36-3032 is accomplished.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 363038A01R01 1

Kit 363038A02R01 1

Reidentified part set REIDA01 1

Consumable CMLA01 1

Kit 363038D01R01 1

Kit 363038D10R01 1

Kit 363038D12R00 1

Kit 363038D14R00 1

Consumable CMLD01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 363038A01R01 1

Kit 363038A02R01 1

Reidentified part set REIDA01 1

Consumable CMLA01 1

Kit 363038D01R01 1

Kit 363038D11R01 1

Kit 363038D12R00 1

Kit 363038D14R00 1

Consumable CMLD01 1

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

**CONF ALL

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin(s) or the equivalent production modification(s):

Service Bulletin No. A330-36-3032 Mod. No. 55198D46286

55961D46493

55962D46494

NOTE: The Service Bulletin No. A330-36-3032 introduces the adapted dual loop

overheat leak detection of the APU bleed air duct.

NOTE: The Mod. No. 55198D46286 introduces the adapted dual loop overheat leak

detection of the APU bleed air duct.

NOTE: The Mod. No. 55961D46493 introduces the modification of the dual loop

overheat leak detection in section 19.

NOTE: The Mod. No. 55962D46494 introduces the modification of the dual loop

overheat detection (CFRP-bulkhead).

C. REASON

(1) History

The APU bleed leak detection system detects any ambient overheat in the vicinity of the

APU bleed air ducts. It is made of a single overheat detection loop which runs along

the APU bleed air ducts in section 15/21 and section 16 thru 19.1. The SFAR88

requirements will induce MMEL restrictions on this system from 2009.

(2) Objective/Action

This Service Bulletin details the installation of a second APU bleed leak detection loop

(APU LOOP B) in parallel to the current APU loop (APU LOOP A) in section 15/21

and section 16 thru 19.1. The Service Bulletin No. A330-36-3032 ’Introduce Adapted

Dual-Loop Overheat-Detection APU Bleed-Air-Duct ’was retrofitted on the first aircraft

in May 2008. After a check of the overheat-detection-loop installation, some none

compliances to ATA 36-22 installation requirements have been reported. This Service

Bulletin provides design improvements to the Service Bulletin No. A330-36-3032 OHDS

installation.

(3) Advantages

The accomplishment of this Service Bulletin improves dual-loop overheat-detection of

APU Bleed-Air-Duct, in accordance to ATA 36-22 installation requirements.

(4) Operational/Maintenance Consequences

None

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 363038-831-848-001: Modification

(1) Remove the sensing elements and the supports between FR39 and FR44

(2) Remove the sensing elements and the supports between FR44 and FR53.2

(3) Remove the sensing elements and the supports between FR53.2 and FR53.6

(4) Remove the sensing elements and the supports between FR53.6 and FR55

(5) If necessary, remove the ducts between FR35.5 and FR35.6 for access

(6) Install a New Support for the Routing of the Sensing Elements between FR53.5 and

FR53.6

(7) If removed, Install the Ducts between FR53.5 and FR53.6

(8) If necessary, Remove the Ducts between FR43 and FR45 for access

(9) Install the new Brackets for the Routing of the Sensing Elements at FR44

(10) If removed, install the ducts between FR43 and FR45

(11) Install the Sensing Elements and the Supports between FR39 and FR44

(12) Install the sensing elements and the supports between FR44 and FR50

(13) Install the sensing elements and the supports between FR50 and FR53.6

(14) Install the sensing elements and the supports between FR53.6 and FR55

(15) If necessary, remove the ducts between FR39 and FR40 for access

(16) Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the

sensing elements.

(17) Modify the existing Harness 2SG.

(18) Modify the Wiring between the Avionics Compartment and the Cargo Compartment.

(19) Modify the Wiring in the Main rack 800VU.

(20) If removed, install the ducts between FR39 and FR40.

(21) Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct

(22) Remove the clamp and the attaching parts from the overheat sensing elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

(23) Remove the clamp from the overheat-detection dual loops at Frame 80

(24) Reroute the sensing elements 32HF and 357HF

(25) Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage

(26) Install the clamp and the new attaching parts on the overheat sensing elements in

the rear fuselage

(27) Install the sleeves on the APU bleed-air-duct

**CONF 002

Task 363038-831-848-001: Modification

(1) Remove the sensing elements and the supports between FR39 and FR44

(2) Remove the sensing elements and the supports between FR44 and FR53.2

(3) Remove the sensing elements and the supports between FR53.2 and FR53.6

(4) Remove the sensing elements and the supports between FR53.6 and FR55

(5) If necessary, remove the ducts between FR35.5 and FR35.6 for access

(6) Install a New Support for the Routing of the Sensing Elements between FR53.5 and

FR53.6

(7) If removed, Install the Ducts between FR53.5 and FR53.6

(8) If necessary, Remove the Ducts between FR43 and FR45 for access

(9) Install the new Brackets for the Routing of the Sensing Elements at FR44

(10) If removed, install the ducts between FR43 and FR45

(11) Install the Sensing Elements and the Supports between FR39 and FR44

(12) Install the sensing elements and the supports between FR44 and FR50

(13) Install the sensing elements and the supports between FR50 and FR53.6

(14) Install the sensing elements and the supports between FR53.6 and FR55

(15) If necessary, remove the ducts between FR39 and FR40 for access

(16) Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the

sensing elements.

(17) Modify the existing Harness 2SG.

(18) Modify the Wiring between the Avionics Compartment and the Cargo Compartment.

(19) Modify the Wiring in the Main rack 800VU.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

(20) If removed, install the ducts between FR39 and FR40.

(21) Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct

(22) Remove the clamps and the attaching parts from the overheat sensing elements

(23) Remove the clamp from the overheat-detection dual loops at Frame 80

(24) Reroute the sensing elements 32HF and 357HF

(25) Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage

(26) Install the clamps and the new attaching parts on the overheat sensing elements in

the rear fuselage

(27) Install the sleeves on the APU bleed-air-duct

**CONF ALL

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available.

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.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

SERVICE BULLETIN

**CONF 001

Task 363038-831-848-001: Modification

Get Access 20.75

On Aircraft

Remove the sensing elements and the supports

between FR39 and FR44

4.00

Remove the sensing elements and the supports

between FR44 and FR53.2

4.00

Remove the sensing elements and the supports

between FR53.2 and FR53.6

4.00

Remove the sensing elements and the supports

between FR53.6 and FR55

4.00

If necessary, remove the ducts between FR35.5 and

FR35.6 for access

1.00

Install a New Support for the Routing of the Sensing

Elements between FR53.5 and FR53.6

1.00

If removed, Install the Ducts between FR53.5 and

FR53.6

2.00

If necessary, Remove the Ducts between FR43 and

FR45 for access

1.00

Install the new Brackets for the Routing of the Sensing

Elements at FR44

1.00

If removed, install the ducts between FR43 and FR45 2.00

Install the Sensing Elements and the Supports

between FR39 and FR44

14.00

Install the sensing elements and the supports between

FR44 and FR50

14.00

Install the sensing elements and the supports between

FR50 and FR53.6

21.00

Install the sensing elements and the supports between

FR53.6 and FR55

14.00

If necessary, remove the ducts between FR39 and

FR40 for access

1.00

Modify the Interconnecting Electrical Wire FIN 309HF

and 310HF, between the sensing elements.

3.00

Modify the existing Harness 2SG. 10.00

Modify the Wiring between the Avionics Compartment

and the Cargo Compartment.

1.00

Modify the Wiring in the Main rack 800VU. 2.00

If removed, install the ducts between FR39 and FR40. 2.00

Remove the sleeves from the Auxiliary Power Unit

(APU) bleed-air-duct

1.25

Remove the clamp and the attaching parts from the

overheat sensing elements

1.00

Remove the clamp from the overheat-detection dual

loops at Frame 80

0.25

Reroute the sensing elements 32HF and 357HF 0.25

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SERVICE BULLETIN

Task 363038-831-848-001: Modification

Replace the clamp of the electrical harness 5866VB/2S

in the rear fuselage

1.50

Install the clamp and the new attaching parts on the

overheat sensing elements in the rear fuselage

1.00

Install the sleeves on the APU bleed-air-duct 1.50

Tests 4.00

Close-Up 28.50

TOTAL MANHOURS 166.00

ELAPSED TIME (HOURS) 88.25

**CONF 002

Task 363038-831-848-001: Modification

Get Access 20.75

On Aircraft

Remove the sensing elements and the supports

between FR39 and FR44

4.00

Remove the sensing elements and the supports

between FR44 and FR53.2

4.00

Remove the sensing elements and the supports

between FR53.2 and FR53.6

4.00

Remove the sensing elements and the supports

between FR53.6 and FR55

4.00

If necessary, remove the ducts between FR35.5 and

FR35.6 for access

1.00

Install a New Support for the Routing of the Sensing

Elements between FR53.5 and FR53.6

1.00

If removed, Install the Ducts between FR53.5 and

FR53.6

2.00

If necessary, Remove the Ducts between FR43 and

FR45 for access

1.00

Install the new Brackets for the Routing of the Sensing

Elements at FR44

1.00

If removed, install the ducts between FR43 and FR45 2.00

Install the Sensing Elements and the Supports

between FR39 and FR44

14.00

Install the sensing elements and the supports between

FR44 and FR50

14.00

Install the sensing elements and the supports between

FR50 and FR53.6

21.00

Install the sensing elements and the supports between

FR53.6 and FR55

14.00

If necessary, remove the ducts between FR39 and

FR40 for access

1.00

Modify the Interconnecting Electrical Wire FIN 309HF

and 310HF, between the sensing elements.

3.00

Modify the existing Harness 2SG. 10.00

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

Task 363038-831-848-001: Modification

Modify the Wiring between the Avionics Compartment

and the Cargo Compartment.

1.00

Modify the Wiring in the Main rack 800VU. 2.00

If removed, install the ducts between FR39 and FR40. 2.00

Remove the sleeves from the Auxiliary Power Unit

(APU) bleed-air-duct

1.25

Remove the clamps and the attaching parts from the

overheat sensing elements

1.25

Remove the clamp from the overheat-detection dual

loops at Frame 80

0.25

Reroute the sensing elements 32HF and 357HF 0.25

Replace the clamp of the electrical harness 5866VB/2S

in the rear fuselage

1.50

Install the clamps and the new attaching parts on the

overheat sensing elements in the rear fuselage

1.25

Install the sleeves on the APU bleed-air-duct 1.50

Tests 4.00

Close-Up 28.50

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 88.25

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight +1.508 KG (+3.3245 LB)

Effect on Balance +52.743 KGM (+381.490 LB.FT )

**CONF 002

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight +1.510 KG (+3.3289 LB)

Effect on Balance +52.850 KGM (+382.264 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52

06-41-53 11-00-00 12-34-24

20-21-15 21-20-00 21-26-00

22-96-00 22-97-00 24-41-00

25-52-00 25-53-00 25-75-41

31-50-00 31-60-00 32-12-00

33-13-00 33-14-00 36-11-34

36-12-00 36-12-41 36-22-00

36-22-17 52-10-00 52-30-00

52-41-00 52-52-00 53-00-00

53-35-11 53-35-13

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-43-10 20-48-00 20-52-10

20-55-00

Service Bulletin (SB) A330-36-3032

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52

06-41-53 11-00-00 12-34-24

20-21-15 21-20-00 21-26-00

22-96-00 22-97-00 24-41-00

25-52-00 25-53-00 25-75-41

31-50-00 31-60-00 32-12-00

33-13-00 33-14-00 36-11-34

36-12-00 36-12-41 36-22-00

36-22-17 52-10-00 52-30-00

52-41-00 52-52-00 53-00-00

53-35-11 53-35-13

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-43-10 20-48-00 20-52-10

20-55-00

Service Bulletin (SB) A330-36-3032

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 36-22-00 36-22-17

Aircraft Schematic Manual (ASM) 36-22-00

Aircraft Wiring List (AWL)

Aircraft Wiring Manual (AWM) 36-12-04 36-22-05 91-03-06

91-03-07

Illustrated Parts Catalog (IPC) 24-92-02 24-92-04 25-14-01

25-71-01 25-92-31 36-22-03

36-22-04 53-36-03

Trouble Shooting Manual (TSM) 36-22-00

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Sensing element 35610-2-255 35606-2-255 03 Not

Applicable

Sensing element 35631-2-255 35620-2-255 03 Not

Applicable

Sensing element 35627-2-255 35621-2-255 03 Not

Applicable

Sensing element 35616-2-255 35618-2-255 03 Not

Applicable

Sensing element 35610-2-255 35597-2-255 03 Not

Applicable

Sensing element 35611-2-255 35598-2-255 03 Not

Applicable

Sensing element 35601-2-255 35595-2-255 03 Not

Applicable

Sensing element 35600-2-255 35596-2-255 03 Not

Applicable

Sensing element 35569-2-255 35568-4-255 03 Not

Applicable

Sensing element 35569-2-255 35567-3-255 03 Not

Applicable

Sensing element 35593-3-255 35597-3-255 03 Not

Applicable

Sensing element 35579-2-255 35587-2-255 03 Not

Applicable

Sensing element 35632-2-255 35627-2-255 03 Not

Applicable

Sensing element 35627-2-255 35625-2-255 03 Not

Applicable

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Blanket-Insulation F2581677800000 F0041196500000 03 Not

Applicable

Blanket-Insulation F2581677900000 F0041196600000 03 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Sensing element 35610-2-255 35606-2-255 03 Not

Applicable

Sensing element 35631-2-255 35620-2-255 03 Not

Applicable

Sensing element 35627-2-255 35621-2-255 03 Not

Applicable

Sensing element 35616-2-255 35618-2-255 03 Not

Applicable

Sensing element 35610-2-255 35597-2-255 03 Not

Applicable

Sensing element 35611-2-255 35598-2-255 03 Not

Applicable

Sensing element 35601-2-255 35595-2-255 03 Not

Applicable

Sensing element 35600-2-255 35596-2-255 03 Not

Applicable

Sensing element 35569-2-255 35568-4-255 03 Not

Applicable

Sensing element 35569-2-255 35567-3-255 03 Not

Applicable

Sensing element 35593-3-255 35597-3-255 03 Not

Applicable

Sensing element 35579-2-255 35587-2-255 03 Not

Applicable

Sensing element 35632-2-255 35627-2-255 03 Not

Applicable

Sensing element 35627-2-255 35625-2-255 03 Not

Applicable

Blanket-Insulation F2581677800000 F0041196500000 03 Not

Applicable

Blanket-Insulation F2581677900000 F0041196600000 03 Not

Applicable

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF ALL

M. SPARES

None

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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This Page Intentionally Left Blank

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 363038A01R01

Kit 363038A02R01

Kit 363038D01R01

Kit 363038D10R01

Kit 363038D11R01

Kit 363038D12R00

Kit 363038D14R00

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is:

AIRBUS

Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 2590

For ordering by E-mail: airbus.kit@airbus.com

(2) Price and Availability

Kit 363038A01R01

Cost 27,500.00 USD

Availability 150 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 363038A02R01

Cost 1,800.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 363038D01R01

Cost 280.00 USD

Availability 90 calendar days from receipt of order

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The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 363038D10R01

Cost 55.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 363038D11R01

Cost 65.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 363038D12R00

Cost 35.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 363038D14R00

Cost 2,870.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

10 NSA5543-00 123 CLAMP

11 ASNA0342T04-01 16 BOLT

13 NSA5539S 249 SLEEVE

14 ASNA2397-10L 152 WASHER

15 NSA5542-00 20 NUT

16 NSA5527-03-01 40 SPACER

17 NSA5527-03-10 3 SPACER

18 NSA5527-03-11 17 SPACER

19 NAS6603-24 2 BOLT

20 NAS6603-1 72 BOLT

21 NAS6603-9 33 BOLT

22 NSA5527-03-15 1 SPACER

23 NAS6603-16 3 BOLT

24 NAS6603-15 7 BOLT

25 NSA5545-00 1 ANGLE

26 NAS6603-32 3 BOLT

28 NAS6603-12 1 BOLT

29 NAS6603-2 22 BOLT

30 NSA5546-00 7 ANGLE

32 F1131031621700 2 PLACARD

33 F1131031623700 2 PLACARD

34 F1131031621800 2 PLACARD

35 F1131031623800 2 PLACARD

36 F1131031623900 2 PLACARD

37 F1131031621900 2 PLACARD

38 F1131031624000 2 PLACARD

39 F1131031622000 2 PLACARD

40 F1131031622100 2 PLACARD

41 F1131031624100 2 PLACARD

42 F1131031622200 2 PLACARD

43 F1131031624200 2 PLACARD

44 F1131031620400 2 PLACARD

45 F1131031624300 2 PLACARD

70 F3611548300000 3 SUPPORT

71 F3611548800000 1 SUPPORT

72 F3611548700000 1 SUPPORT

73 F3611548500000 1 SUPPORT

74 F3611548900000 1 SUPPORT

75 F3611548400000 1 SUPPORT

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

76 F3611548200000 1 SUPPORT

77 F3611548600000 1 SUPPORT

78 F3611549700000 1 SUPPORT

79 F3611549100000 9 SUPPORT

80 F3611549500000 1 SUPPORT

81 F3611549600000 1 SUPPORT

82 F3611549400000 1 SUPPORT

83 F3611549800000 1 SUPPORT

84 F3611549300000 1 SUPPORT

85 NSA5549-90 2 CONNECTR

86 NSA5538-00 3 CLAMP

87 NAS6603-17 5 BOLT

88 F1131031620500 1 PLACARD

89 F1131031624400 1 PLACARD

90 F1131031620600 1 PLACARD

91 F1131031624500 1 PLACARD

93 F3611549200000 1 SUPPORT

94 NAS6603-10 5 BOLT

95 F3611549000000 1 SUPPORT

96 F5392059300000 1 SUPPORT

97 ASNA2050DCJ3215 4 RIVET

98 F0041178800000 1 SUPPORT

99 F0041178800100 1 SUPPORT

100 35606-2-255 1 SNSGELEM (1) 35610-2-255 03

101 35621-2-255 1 SNSGELEM (11) 35627-2-255 03

102 35620-2-255 1 SNSGELEM (2) 35631-2-255 03

103 35618-2-255 2 SNSGELEM (12) 35616-2-255 03

104 35567-3-255 1 SNSGELEM (7) 35569-2-255 03

105 35598-2-255 1 SNSGELEM (13) 35611-2-255 03

106 35595-2-255 3 SNSGELEM (5) 35601-2-255 03

107 35596-2-255 1 SNSGELEM (15) 35600-2-255 03

108 35568-4-255 1 SNSGELEM (7) 35569-2-255 03

109 35597-3-255 1 SNSGELEM (8) 35593-3-255 03

110 35587-2-255 1 SNSGELEM (17) 35579-2-255 03

111 35627-2-255 1 SNSGELEM (9) 35632-2-255 03

112 35625-2-255 1 SNSGELEM (11) 35627-2-255 03

113 35610-2-255 1 SNSGELEM (1) 35610-2-255

114 35597-2-255 1 SNSGELEM (1) 35610-2-255 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

14 ASNA2397-10L 1 WASHER

16 NSA5527-03-01 1 SPACER

22 NSA5527-03-15 1 SPACER

131 NSA935808-03 20 WASHER

141 NSA5527-03-02 2 SPACER

150 NSA935807-04 4 CLAMP

151 NSA5159-17 1 STUD

152 NSA5527-03-08 1 SPACER

153 NSA935808-01 8 WASHER

157 NSA5159-10 1 STUD

158 NAS1801-3-9 3 SCREW

169 NSA935401-03 208 TIE

171 NAS1801-3-17 2 SCREW

172 NAS1149F0332P 2 WASHER

174 35301-74 2 CABLE

175 35301-75 2 CABLE

176 NSA5516-21ND 5 CLAMP

177 NSA5516-22ND 5 CLAMP

178 NSA5516-23ND 5 CLAMP

179 NSA5516-07ND 2 CLAMP

180 NSA5516-08ND 2 CLAMP

181 NSA5516-10ND 2 CLAMP

F9000095228595 1 BUNDLE

NSA935401-06 200 TIE

NSA935401-13 200 TIE

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 363038D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

169 NSA935401-03 30 TIE

210 MS21919WCH14 1 CLAMP

211 F9237000207200 8 PLCRDSET

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SERVICE BULLETIN

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 363038D10R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

13 NSA5539S 10 SLEEVE

16 NSA5527-03-01 4 SPACER

86 NSA5538-00 2 CLAMP

207 NAS1802-3-13 4 SCREW

208 NSA5527-03-04 2 SPACER

209 NAS1801-3-8 2 SCREW

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 363038D11R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

13 NSA5539S 12 SLEEVE

16 NSA5527-03-01 4 SPACER

86 NSA5538-00 2 CLAMP

207 NAS1802-3-13 4 SCREW

208 NSA5527-03-04 3 SPACER

209 NAS1801-3-8 3 SCREW

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 363038D12R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

13 NSA5539S 2 SLEEVE

16 NSA5527-03-01 1 SPACER

86 NSA5538-00 2 CLAMP

207 NAS1802-3-13 1 SCREW

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

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Kit 363038D14R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

13 NSA5539S 6 SLEEVE

200 F3617062404000 1 SLEEVE

201 F3617062403800 1 SLEEVE

202 F3617062403600 1 SLEEVE

203 F3617062403400 1 SLEEVE

204 F3617062403200 1 SLEEVE

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Adhesive Tape (Insulation Blanket

Repair)

08-073 As required

Interfay Sealant 09-005 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Adhesive Tape (Insulation Blanket

Repair)

08-073 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

None

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E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

Reidentified part set REIDA01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F0041196500000 BLANKET F2581677800000

F0041196600000 BLANKET F2581677900000

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 363038-831-848-001 - Modification

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: YOU MUST MAKE SURE THAT THE LANDING GEAR GROUND SAFETY

LOCKS ARE INSTALLED AND THE WHEEL CHOCKS ARE IN POSITIONS.

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.

Task Associated Data

**CONF 001

Zone

120 150 190 210 310

Modified FIN

313AL 312AR 22HF 23HF 24HF 25HF 32HF 97HF 98HF 99HF 100HF 101HF 102HF

137HF 138HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF

310HF 311HF 312HF 357HF 3501VS 3503VS 3591VS 3593VS

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 166.00

ELAPSED TIME (HOURS) 88.25

**CONF 002

Zone

120 150 190 210 310

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Modified FIN

313AL 312AR 22HF 23HF 24HF 25HF 32HF 97HF 98HF 99HF 100HF 101HF 102HF

137HF 138HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF

310HF 311HF 312HF 357HF 3501VS 3503VS 3591VS 3593VS

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 88.25

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 363038-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-21-15-912-801

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-43-10

20-48-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12

51-24-00

51-43-00

51-47-00

(a) Use a non metallic spatula to remove the sealant and clean the areas with :

Solvent General

Purpose

11-026 As required

(b) For fasteners spacing and margin (Refer to SRM 51-47-00).

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(c) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(d) Clean the areas where you will install the placards with :

Solvent General

Purpose

11-026 As required

Lint-Free Cotton

Cloth

19-003 As required

and

(e) Apply the sealant (Refer to SRM 51-24-00).

(f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001).

(g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block

001).

(h) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(i) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(j) If you find part numbers of hardware components in the related kit(s) which you

cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the

Standards Manual (SM). The SM will give you the correct part number to part

number relationship.

(k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201).

(l) Apply a special protection on new parts (Refer to SRM 51-23-12).

(m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00).

(n) Obey the instructions of the splices installation (Refer to ESPM 20-43-10).

(o) Make sure that the electrical connectors are serviceable before you connect them

again.

(p) To install new wires, cut them to the necessary length, crimp the terminals and

connect them (Refer to ESPM 20-48-00).

(q) Put blanking plugs on the disconnected line ends.

(2) Subtask 363038-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-44

Fig. A-GBHAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer

to Consumable Material List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM

20-25-51).

(d) For tolerances for waviness and bends in sensing element wires (Refer to Fig. AGBHAA).

(e) Install the SB/MOD identification placards in a position where you can clearly see

them.

(f) If necessary, clean the work areas with:

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(3) Subtask 363038-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 26

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SERVICE BULLETIN

**CONF 002

(1) Subtask 363038-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-21-15-912-801

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-43-10

20-48-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12

51-24-00

51-43-00

51-47-00

(a) Use a non metallic spatula to remove the sealant and clean the areas with :

Solvent General

Purpose

11-026 As required

(b) For fasteners spacing and margin (Refer to SRM 51-47-00).

(c) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(d) Clean the areas where you will install the placards with :

Solvent General

Purpose

11-026 As required

Lint-Free Cotton

Cloth

19-003 As required

and

(e) Apply the sealant (Refer to SRM 51-24-00).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001).

(g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block

001).

(h) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(i) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(j) If you find part numbers of hardware components in the related kit(s) which you

cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the

Standards Manual (SM). The SM will give you the correct part number to part

number relationship.

(k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201).

(l) Apply a special protection on new parts (Refer to SRM 51-23-12).

(m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00).

(n) Obey the instructions of the splices installation (Refer to ESPM 20-43-10).

(o) Make sure that the electrical connectors are serviceable before you connect them

again.

(p) To install new wires, cut them to the necessary length, crimp the terminals and

connect them (Refer to ESPM 20-48-00).

(q) Put blanking plugs on the disconnected line ends.

(2) Subtask 363038-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-44

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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References

Fig. A-GBHAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer

to Consumable Material List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM

20-25-51).

(d) For tolerances for waviness and bends in sensing element wires (Refer to Fig. AGBHAA).

(e) Install the SB/MOD identification placards in a position where you can clearly see

them.

(f) If necessary, clean the work areas with:

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(3) Subtask 363038-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 363038-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 29

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References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 32-12-00-010-801

Task 36-11-34-000-802

Task 36-22-17-000-801

Task 36-22-17-000-802

Task 52-10-00-010-801

52-30-00, Page Block 201

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801).

(d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822

(Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201).

(e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801).

(g) Do the Job Set-up procedure as specified in the removal of the sensing elements

(Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802).

(h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring

Computer (BMC) (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-000-802).

(2) Subtask 363038-010-002-001 - Remove/Open for Access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 25-52-00-000-801

Task 25-53-00-000-801

Task 25-75-41-000-801

Task 53-00-00-000-802

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 53-35-13-000-802

(a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the

floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task

53-00-00-000-802).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer

to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).

(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to

AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).

(d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition

panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM

Task 25-52-00-000-801).

(e) At Frame 20 in the FWD cargo-compartment, remove the partition panels

131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-52-00-000-801).

(f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo

compartment, remove (if necessary) the sidewall panels 151EW, 151GW

and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-53-00-000-801).

(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC

and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-53-00-000-801).

(h) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW

(Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).

(i) On the LH side of the belly fairing, remove (if necessary) the panels 191HB,

191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to

AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task

53-35-13-000-802).

(j) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and

192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802).

(k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM

Task 25-75-41-000-801).

(3) Subtask 363038-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1, GEN 2, APU GEN,

- EXT A (B).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 31

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(b) Open, safety and tags the following circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR),

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector (s).

(4) Subtask 363038-941-202-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001

(a) Put access platform(s) in position at below the access doors 312AR and 313AL.

(b) Open and secure the maintenance door 312AR (Refer to AMM 52-41-00, Page

Block 001).

(c) Open and secure the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

**CONF 002

(1) Subtask 363038-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 32

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 32-12-00-010-801

Task 36-11-34-000-802

Task 36-22-17-000-801

Task 36-22-17-000-802

Task 52-10-00-010-801

52-30-00, Page Block 201

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801).

(d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822

(Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201).

(e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801).

(g) Do the Job Set-up procedure as specified in the removal of the sensing elements

(Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802).

(h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring

Computer (BMC) (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-000-802).

(2) Subtask 363038-010-002-001 - Remove/Open for Access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 25-52-00-000-801

Task 25-53-00-000-801

Task 25-75-41-000-801

Task 53-00-00-000-802

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 53-35-13-000-802

(a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the

floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task

53-00-00-000-802).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 33

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(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer

to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).

(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to

AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).

(d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition

panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM

Task 25-52-00-000-801).

(e) At Frame 20 in the FWD cargo-compartment, remove the partition panels

131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-52-00-000-801).

(f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo

compartment, remove (if necessary) the sidewall panels 151EW, 151GW

and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-53-00-000-801).

(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC

and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-53-00-000-801).

(h) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW

(Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).

(i) On the LH side of the belly fairing, remove (if necessary) the panels 191HB,

191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to

AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task

53-35-13-000-802).

(j) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and

192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802).

(k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM

Task 25-75-41-000-801).

(3) Subtask 363038-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1, GEN 2, APU GEN,

- EXT A (B).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 34

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SERVICE BULLETIN

(b) Open, safety and tags the following circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR),

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector (s).

(4) Subtask 363038-941-202-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001

(a) Put access platform(s) in position at below the access doors 312AR and 313AL.

(b) Open and secure the maintenance door 312AR (Refer to AMM 52-41-00, Page

Block 001).

(c) Open and secure the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 35

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@A330

SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 363038-831-001-001 - Remove the sensing elements and the supports

between FR39 and FR44

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 02, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 97HF

1 Sensing element 35610-2-255 Item (1) Discard

FIN 98HF

1 Sensing element 35631-2-255 Item (2) Discard

FIN 302HF

1 Sensing element 35610-2-255 Item (1) Discard

FIN 303HF

1 Sensing element 35627-2-255 Item (11) Discard

2 Support Item (59) Discard

4 Rivet Item (45) Discard

2 Placard Item (23) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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@A330

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1 Placard Item (24) Discard

2 Placard Item (29) Discard

1 Placard Item (30) Discard

4 Nut Item (57) Discard

14 Screw Item (76) Discard

32 Washer Item (46) Discard

64 Protective sleeve Item (56) Discard

23 Clamp Item (58) Discard

2 Screw Item (47) Discard

18 Clamp Item (82) Discard

9 Spacer Item (55) Discard

1 Screw Item (50) Discard

10 Spacer Item (53) Discard

5 Screw Item (52) Discard

4 Screw Item (52) Discard

6 Screw Item (48) Discard

As

required

Wire-lock Item (100) Discard

(2) Subtask 363038-831-002-001 - Remove the sensing elements and the supports

between FR44 and FR53.2

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 37

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References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 99HF

1 Sensing element 35618-2-255 Item (3) Discard

FIN 100HF

1 Sensing element 35610-2-255 Item (1) Discard

FIN 304HF

1 Sensing element 35616-2-255 Item (12) Discard

FIN 305HF

1 Sensing element 35611-2-255 Item (13) Discard

2 Support Item (59) Discard

4 Rivet Item (45) Discard

1 Placard Item (25) Discard

2 Placard Item (26) Discard

1 Placard Item (27) Discard

1 Placard Item (30) Discard

2 Placard Item (31) Discard

2 Placard Item (32) Discard

1 Placard Item (33) Discard

4 Nut Item (57) Discard

1 Plate assy Item (41) Discard

8 Screw Item (76) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 38

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SERVICE BULLETIN

30 Washer Item (46) Discard

56 Protective sleeve Item (56) Discard

18 Clamp Item (58) Discard

1 Screw Item (47) Discard

20 Clamp Item (82) Discard

10 Spacer Item (55) Discard

5 Screw Item (50) Discard

17 Spacer Item (53) Discard

12 Screw Item (52) Discard

3 Screw Item (48) Discard

1 Screw Item (49) Discard

1 Spacer Item (54) Discard

As

required

Wire-lock Item (100) Discard

(3) Subtask 363038-831-003-001 - Remove the sensing elements and the supports

between FR53.2 and FR53.6

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 04, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 23HF

1 Sensing element 35569-2-255 Item (7) Discard

FIN 101HF

1 Sensing element 35601-2-255 Item (5) Discard

FIN 102HF

1 Sensing element 35601-2-255 Item (5) Discard

FIN 306HF

1 Sensing element 35601-2-255 Item (5) Discard

FIN 307HF

1 Sensing element 35600-2-255 Item (15) Discard

FIN 308HF

1 Sensing element 35569-2-255 Item (7) Discard

3 Support Item (59) Discard

6 Rivet Item (45) Discard

2 Placard Item (20) Discard

1 Placard Item (27) Discard

2 Placard Item (28) Discard

1 Placard Item (33) Discard

2 Placard Item (34) Discard

2 Placard Item (35) Discard

6 Nut Item (57) Discard

1 Plate assy Item (40) Discard

11 Screw Item (76) Discard

38 Washer Item (46) Discard

74 Protective sleeve Item (56) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 40

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SERVICE BULLETIN

29 Clamp Item (58) Discard

2 Screw Item (50) Discard

16 Clamp Item (82) Discard

8 Spacer Item (55) Discard

21 Spacer Item (53) Discard

19 Screw Item (52) Discard

6 Screw Item (48) Discard

As

required

Wire-lock Item (100) Discard

(4) Subtask 363038-831-004-001 - Remove the sensing elements and the supports

between FR53.6 and FR55

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 05, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 24HF

1 Sensing element 35593-3-255 Item (8) Discard

FIN 25HF

1 Sensing element 35632-2-255 Item (9) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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FIN 311HF

1 Sensing element 35579-2-255 Item (17) Discard

FIN 312HF

1 Sensing element 35627-2-255 Item (11) Discard

1 Support Item (59) Discard

2 Rivet Item (45) Discard

1 Placard Item (21) Discard

1 Placard Item (22) Discard

1 Placard Item (36) Discard

1 Placard Item (37) Discard

2 Nut Item (57) Discard

1 Connector Item (61) Discard

14 Screw Item (76) Discard

27 Washer Item (46) Discard

54 Protective sleeve Item (56) Discard

21 Clamp Item (58) Discard

4 Screw Item (52) Discard

14 Spacer Item (53) Discard

2 Screw Item (51) Discard

12 Clamp Item (82) Discard

6 Spacer Item (55) Discard

4 Screw Item (48) Discard

3 Screw Item (77) Discard

As

required

Wire-lock Item (100) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

(5) Subtask 363038-020-001-001 - If necessary, remove the ducts between FR35.5 and

FR35.6 for access

Work Zones and Access Panels

Zone Access/Work location

150

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801

Fig. A-FBBAA

Removal/Installation of the Ducts

between FR53.6 and FR53.7 on the LH

side (for Access)

Sheet 01

(a) Remove :

Fig. A-FBBAA

(Refer to AMM Task 36-12-41-000-801)

1 Duct assy Item (112) Retain

1 Duct assy Item (113) Retain

1 Duct assy Item (114) Retain

(6) Subtask 363038-831-005-001 - Install a New Support for the Routing of the Sensing

Elements between FR53.5 and FR53.6

Work Zones and Access Panels

Zone Access/Work location

150

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 43

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SERVICE BULLETIN

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

96 F5392059300000 1 SUPPORT

97 ASNA2050DCJ3215 2 RIVET

Reidentified part set REIDA01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F0041196500000 BLANKET F2581677800000

F0041196600000 BLANKET F2581677900000

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Adhesive Tape (insulation

Blanket Repair)

08-073 As required

Interfay Sealant 09-005 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

References

Fig. A-FBCAA

Installation of a New Bracket between

FR53.5 and FR53.6

Sheet 01

Sheet 02

(a) Move the insulation blanket to get access to the modification area.

(b) Put the bracket Item 96 in position as shown on Fig. A-FBCAA.

(c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.)

and 3.35mm (0.132in.) to match the holes of the bracket Item 96.

Refer to Fig. A-FBCAA

(d) Cut the insulation blanket to permit the installation of the bracket Item 96.

NOTE: For the repair of the insulation blanket use :

Adhesive Tape

(insulation Blanket

Repair)

08-073 As required

(e) Re-identify the insulation blanket :

1 Blanket-Insulation F2581677800000

becomes :

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

1 Blanket-Insulation F0041196500000

or,

1 Blanket-Insulation F2581677900000

becomes :

1 Blanket-Insulation F0041196600000

(f) Install :

Refer to Fig. A-FBCAA

1 Support F5392059300000 Item 96

2 Rivet ASNA2050DCJ3215 Item 97

NOTE: To the interface of the new bracket and the structure apply :

Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

NOTE: Wet install the fasteners with :

Interfay Sealant 09-005 As required

(g) Install the insulation blanket.

(7) Subtask 363038-420-001-001 - If removed, Install the Ducts between FR53.5 and

FR53.6

Work Zones and Access Panels

Zone Access/Work location

150

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801

Fig. A-FBBAA

Removal/Installation of the Ducts

between FR53.6 and FR53.7 on the LH

side (for Access)

Sheet 01

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

(a) Install :

Refer to Fig. A-FBBAA

(Refer to AMM Task 36-12-41-400-801)

1 Duct assy Item (112) Retained at

removal

1 Duct assy Item (113) Retained at

removal

1 Duct assy Item (114) Retained at

removal

(8) Subtask 363038-020-002-001 - If necessary, Remove the Ducts between FR43 and

FR45 for access

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801

Fig. A-FBDAA

Removal/Installation of the Ducts

between FR44 and FR47 on the LH side

(for Access)

Sheet 01

(a) Remove :

Refer to Fig. A-FBDAA

(Refer to AMM Task 36-12-41-000-801)

1 Duct assy Item (115) Retain

1 Duct assy Item (116) Retain

(9) Subtask 363038-831-006-001 - Install the new Brackets for the Routing of the

Sensing Elements at FR44

Work Zones and Access Panels

Zone Access/Work location

190

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 46

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

97 ASNA2050DCJ3215 2 RIVET

98 F0041178800000 1 SUPPORT

99 F0041178800100 1 SUPPORT

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Interfay Sealant 09-005 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

References

Fig. A-FBKAA

Installation of Two New Brackets at

FR44

Sheet 01

Sheet 02

(a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBKAA

.

(b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm

(0.132in.) as shown on Fig. A-FBKAA.

(c) Install :

1 Support F0041178800000 Item 98

1 Support F0041178800100 Item 99

2 Rivet ASNA2050DCJ3215 Item 97

NOTE: To the interface of the new bracket and the structure apply :

Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 47

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SERVICE BULLETIN

NOTE: Wet install the fasteners with :

Interfay Sealant 09-005 As required

(10) Subtask 363038-410-001-001 - If removed, install the ducts between FR43 and

FR45

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 43 to Frame 45

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801

Fig. A-FBDAA

Removal/Installation of the Ducts

between FR44 and FR47 on the LH side

(for Access)

Sheet 01

(a) Install :

(Refer to AMM Task 36-12-41-400-801)

1 Duct assy Item (115) Retained at

removal

1 Duct assy Item (116) Retained at

removal

(11) Subtask 363038-831-007-001 - Install the Sensing Elements and the Supports

between FR39 and FR44

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 39 to Frame 44

Manpower Resources

Manhours 14.00

Minimum number of person 1

Subtask elapsed time 14.00

Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 48

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SERVICE BULLETIN

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 30 CLAMP

11 ASNA0342T04-01 4 BOLT

13 NSA5539S 62 SLEEVE

14 ASNA2397-10L 34 WASHER

15 NSA5542-00 4 NUT

16 NSA5527-03-01 8 SPACER

18 NSA5527-03-11 6 SPACER

20 NAS6603-1 19 BOLT

21 NAS6603-9 8 BOLT

24 NAS6603-15 6 BOLT

29 NAS6603-2 2 BOLT

30 NSA5546-00 2 ANGLE

32 F1131031621700 2 PLACARD

33 F1131031623700 2 PLACARD

34 F1131031621800 1 PLACARD

35 F1131031623800 1 PLACARD

70 F3611548300000 1 SUPPORT

71 F3611548800000 1 SUPPORT

78 F3611549700000 1 SUPPORT

79 F3611549100000 1 SUPPORT

100 35606-2-255 1 SNSGELEM

101 35621-2-255 1 SNSGELEM

102 35620-2-255 1 SNSGELEM

113 35610-2-255 1 SNSGELEM

References

Fig. A-FBEAA

Installation of the New Sensing

Elements between FR39 and FR44 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR39 and FR40.2.

1 Install the supports between FR39 and FR40 :

1 Angle NSA5546-00 Item 30

2 Rivet-Blind ASNA0342T04-01 Item 11

8 Clamp NSA5543-00 Item 10

6 Spacer NSA5527-03-01 Item 16

2 Spacer NSA5527-03-11 Item 18

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

8 Washer ASNA2397-10L Item 14

6 Bolt NAS6603-9 Item 21

2 Bolt NAS6603-15 Item 24

2 Install the supports between FR40 and FR40.2 :

1 Support F3611549100000 Item 79

1 Support F3611549700000 Item 78

5 Clamp NSA5543-00 Item 10

1 Spacer NSA5527-03-01 Item 16

8 Washer ASNA2397-10L Item 14

1 Bolt NAS6603-9 Item 21

6 Bolt NAS6603-1 Item 20

2 Bolt NAS6603-2 Item 29

1 Angle NSA5546-00 Item 30

2 Rivet-Blind ASNA0342T04-01 Item 11

3 Install the placards between FR39 and FR40.2 :

2 Placard F1131031621700 Item 32

2 Placard F1131031623700 Item 33

1 Placard F1131031621800 Item 34

1 Placard F1131031623800 Item 35

4 Install the sensing elements between FR39 and FR40.2 :

FIN 97HF

1 Sensing Element 35606-2-255 Item 100

FIN 302HF

1 Sensing Element 35610-2-255 Item 113

28 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(b) Install the sensing elements and the supports between FR40.2 and FR44.

1 Install the supports between FR40.2 and FR44 :

1 Support F3611548300000 Item 70

1 Support F3611548800000 Item 71

17 Clamp NSA5543-00 Item 10

4 Spacer NSA5527-03-11 Item 18

1 Spacer NSA5527-03-01 Item 16

18 Washer ASNA2397-10L Item 14

13 Bolt NAS6603-1 Item 20

1 Bolt NAS6603-9 Item 21

4 Bolt NAS6603-15 Item 24

2 Install the sensing elements between FR40.2 and FR44 :

FIN 98HF

1 Sensing Element 35620-2-255 Item 102

FIN 303HF

1 Sensing Element 35621-2-255 Item 101

34 Sleeve-Protective NSA5539S Item 13

(12) Subtask 363038-831-008-001 - Install the sensing elements and the supports

between FR44 and FR50

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 44 to Frame 50

Manpower Resources

Manhours 14.00

Minimum number of person 1

Subtask elapsed time 14.00

Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 51

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SERVICE BULLETIN

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 29 CLAMP

11 ASNA0342T04-01 4 BOLT

13 NSA5539S 58 SLEEVE

14 ASNA2397-10L 35 WASHER

15 NSA5542-00 8 NUT

16 NSA5527-03-01 10 SPACER

17 NSA5527-03-10 1 SPACER

18 NSA5527-03-11 5 SPACER

19 NAS6603-24 2 BOLT

20 NAS6603-1 13 BOLT

21 NAS6603-9 8 BOLT

23 NAS6603-16 3 BOLT

26 NAS6603-32 1 BOLT

29 NAS6603-2 8 BOLT

30 NSA5546-00 2 ANGLE

34 F1131031621800 1 PLACARD

35 F1131031623800 1 PLACARD

36 F1131031623900 2 PLACARD

37 F1131031621900 2 PLACARD

38 F1131031624000 2 PLACARD

39 F1131031622000 2 PLACARD

40 F1131031622100 1 PLACARD

41 F1131031624100 1 PLACARD

79 F3611549100000 4 SUPPORT

80 F3611549500000 1 SUPPORT

81 F3611549600000 1 SUPPORT

103 35618-2-255 2 SNSGELEM

105 35598-2-255 1 SNSGELEM

114 35597-2-255 1 SNSGELEM

References

Fig. A-FBFAA

Installation of the New Sensing

Elements between FR44 and FR50 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR44 and FR46 :

1 Install the supports between FR44 and FR46 :

1 Support F3611549600000 Item 81

17 Clamp NSA5543-00 Item 10

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 52

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SERVICE BULLETIN

8 Spacer NSA5527-03-01 Item 16

5 Spacer NSA5527-03-11 Item 18

21 Washer ASNA2397-10L Item 14

2 Bolt NAS6603-24 Item 19

4 Bolt NAS6603-1 Item 20

6 Bolt NAS6603-9 Item 21

3 Bolt NAS6603-16 Item 23

2 Bolt NAS6603-2 Item 29

2 Install the placards at FR44 :

1 Placard F1131031621800 Item 34

1 Placard F1131031623800 Item 35

1 Placard F1131031623900 Item 36

1 Placard F1131031621900 Item 37

3 Install the sensing elements between FR44 and FR46 :

FIN 99HF

1 Sensing Element 35618-2-255 Item 103

FIN 304HF

1 Sensing Element 35618-2-255 Item 103

34 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(b) Install the sensing elements and the supports between FR46 and FR50.

1 Install the supports between FR46 and FR50 :

2 Angle NSA5546-00 Item 30

4 Rivet-Blind ASNA0342T04-01 Item 11

1 Support F3611549500000 Item 80

4 Support F3611549100000 Item 79

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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12 Clamp NSA5543-00 Item 10

2 Spacer NSA5527-03-01 Item 16

1 Spacer NSA5527-03-10 Item 17

14 Washer ASNA2397-10L Item 14

9 Bolt NAS6603-1 Item 20

2 Bolt NAS6603-9 Item 21

1 Bolt NAS6603-32 Item 26

6 Bolt NAS6603-2 Item 29

2 Install the placards between FR46 and FR50 :

1 Placard F1131031623900 Item 36

1 Placard F1131031621900 Item 37

2 Placard F1131031624000 Item 38

2 Placard F1131031622000 Item 39

1 Placard F1131031622100 Item 40

1 Placard F1131031624100 Item 41

3 Install the sensing elements between FR46 and FR50 :

FIN 100HF

1 Sensing Element 35597-2-255 Item 114

FIN 305HF

1 Sensing Element 35598-2-255 Item 105

24 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(13) Subtask 363038-831-009-001 - Install the sensing elements and the supports

between FR50 and FR53.6

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 50 to Frame 53.6

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 54

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SERVICE BULLETIN

Manpower Resources

Manhours 21.00

Minimum number of person 1

Subtask elapsed time 21.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 37 CLAMP

11 ASNA0342T04-01 6 BOLT

13 NSA5539S 74 SLEEVE

14 ASNA2397-10L 51 WASHER

15 NSA5542-00 6 NUT

16 NSA5527-03-01 16 SPACER

18 NSA5527-03-11 1 SPACER

20 NAS6603-1 23 BOLT

21 NAS6603-9 16 BOLT

22 NSA5527-03-15 1 SPACER

24 NAS6603-15 1 BOLT

25 NSA5545-00 1 ANGLE

28 NAS6603-12 1 BOLT

29 NAS6603-2 10 BOLT

30 NSA5546-00 2 ANGLE

40 F1131031622100 1 PLACARD

41 F1131031624100 1 PLACARD

42 F1131031622200 2 PLACARD

43 F1131031624200 2 PLACARD

44 F1131031620400 2 PLACARD

45 F1131031624300 2 PLACARD

70 F3611548300000 1 SUPPORT

72 F3611548700000 1 SUPPORT

73 F3611548500000 1 SUPPORT

74 F3611548900000 1 SUPPORT

75 F3611548400000 1 SUPPORT

76 F3611548200000 1 SUPPORT

77 F3611548600000 1 SUPPORT

79 F3611549100000 3 SUPPORT

82 F3611549400000 1 SUPPORT

83 F3611549800000 1 SUPPORT

84 F3611549300000 1 SUPPORT

104 35567-3-255 1 SNSGELEM

106 35595-2-255 3 SNSGELEM

107 35596-2-255 1 SNSGELEM

108 35568-4-255 1 SNSGELEM

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 55

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SERVICE BULLETIN

References

Fig. A-FBGAA

Installation of the New Sensing

Elements between FR50 and FR53.6 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR50 and FR53.2.

1 Install the supports between FR50 and FR53.2 :

1 Support F3611548700000 Item 72

1 Support F3611548400000 Item 75

1 Support F3611549400000 Item 82

1 Angle NSA5546-00 Item 30

2 Rivet-Blind ASNA0342T04-01 Item 11

13 Clamp NSA5543-00 Item 10

7 Spacer NSA5527-03-01 Item 16

16 Washer ASNA2397-10L Item 14

9 Bolt NAS6603-1 Item 20

7 Bolt NAS6603-9 Item 21

2 Install the placards between FR50 and FR53.2 :

1 Placard F1131031622100 Item 40

1 Placard F1131031624100 Item 41

1 Placard F1131031622200 Item 42

1 Placard F1131031624200 Item 43

3 Install the sensing elements between FR50 and FR53.2 :

FIN 101HF

1 Sensing Element 35595-2-255 Item 106

FIN 102HF

1 Sensing Element 35595-2-255 Item 106

26 Sleeve-Protective NSA5539S Item 13

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 56

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2 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(b) Install the sensing elements and the supports between FR53.2 and FR53.6.

1 Install the supports between FR53.2 and FR53.6 :

1 Support F3611548300000 Item 70

1 Support F3611548500000 Item 73

1 Support F3611548900000 Item 74

1 Support F3611548200000 Item 76

1 Support F3611548600000 Item 77

3 Support F3611549100000 Item 79

1 Support F3611549800000 Item 83

1 Support F3611549300000 Item 84

1 Angle NSA5545-00 Item 25

1 Angle NSA5546-00 Item 30

4 Rivet-Blind ASNA0342T04-01 Item 11

24 Clamp NSA5543-00 Item 10

9 Spacer NSA5527-03-01 Item 16

1 Spacer NSA5527-03-11 Item 18

1 Spacer NSA5527-03-15 Item 22

35 Washer ASNA2397-10L Item 14

14 Bolt NAS6603-1 Item 20

9 Bolt NAS6603-9 Item 21

1 Bolt NAS6603-15 Item 24

1 Bolt NAS6603-12 Item 28

10 Bolt NAS6603-2 Item 29

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 57

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2 Install the placards between FR53.2 and FR53.6 :

1 Placard F1131031622200 Item 42

1 Placard F1131031624200 Item 43

2 Placard F1131031620400 Item 44

2 Placard F1131031624300 Item 45

3 Install the sensing elements between FR53.2 and FR53.6 :

FIN 102HF

1 Sensing Element 35595-2-255 Item 106

FIN 307HF

1 Sensing Element 35596-2-255 Item 107

FIN 23HF

1 Sensing Element 35568-4-255 Item 108

FIN 308HF

1 Sensing Element 35567-3-255 Item 104

48 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(14) Subtask 363038-831-010-001 - Install the sensing elements and the supports

between FR53.6 and FR55

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 53.6 to Frame 55

Manpower Resources

Manhours 14.00

Minimum number of person 1

Subtask elapsed time 14.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 27 CLAMP

11 ASNA0342T04-01 2 BOLT

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 58

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5539S 55 SLEEVE

14 ASNA2397-10L 32 WASHER

15 NSA5542-00 2 NUT

16 NSA5527-03-01 6 SPACER

17 NSA5527-03-10 2 SPACER

18 NSA5527-03-11 5 SPACER

20 NAS6603-1 17 BOLT

21 NAS6603-9 1 BOLT

26 NAS6603-32 2 BOLT

29 NAS6603-2 2 BOLT

30 NSA5546-00 1 ANGLE

70 F3611548300000 1 SUPPORT

79 F3611549100000 1 SUPPORT

85 NSA5549-90 2 CONNECTR

86 NSA5538-00 3 CLAMP

87 NAS6603-17 5 BOLT

88 F1131031620500 1 PLACARD

89 F1131031624400 1 PLACARD

90 F1131031620600 1 PLACARD

91 F1131031624500 1 PLACARD

93 F3611549200000 1 SUPPORT

94 NAS6603-10 5 BOLT

95 F3611549000000 1 SUPPORT

109 35597-3-255 1 SNSGELEM

110 35587-2-255 1 SNSGELEM

111 35627-2-255 1 SNSGELEM

112 35625-2-255 1 SNSGELEM

References

Fig. A-FBHAA

Installation of the New Sensing

Elements between FR53.6 and FR55 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR53.6 and FR55.

1 Install the supports between FR53.6 and FR55 :

1 Support F3611548300000 Item 70

1 Support F3611549100000 Item 79

1 Support F3611549200000 Item 93

1 Support F3611549000000 Item 95

1 Angle NSA5546-00 Item 30

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2 Rivet-Blind ASNA0342T04-01 Item 11

27 Clamp NSA5543-00 Item 10

3 Clamp NSA5538-00 Item 86

6 Spacer NSA5527-03-01 Item 16

2 Spacer NSA5527-03-10 Item 17

5 Spacer NSA5527-03-11 Item 18

32 Washer ASNA2397-10L Item 14

17 Bolt NAS6603-1 Item 20

1 Bolt NAS6603-9 Item 21

2 Bolt NAS6603-32 Item 26

2 Bolt NAS6603-2 Item 29

5 Bolt NAS6603-17 Item 87

5 Bolt NAS6603-10 Item 94

2 Install the placards between FR53.6 and FR55 :

1 Placard F1131031620500 Item 88

1 Placard F1131031624400 Item 89

1 Placard F1131031620600 Item 90

1 Placard F1131031624500 Item 91

3 Install the sensing elements between FR53.6 and FR55 :

FIN 24HF

1 Sensing Element 35597-3-255 Item 109

FIN 311HF

1 Sensing Element 35587-2-255 Item 110

FIN 25HF

1 Sensing Element 35627-2-255 Item 111

FIN 312HF

1 Sensing Element 35625-2-255 Item 112

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2 Nut NSA5542-00 Item 15

2 Connector NSA5549-90 Item 85

55 Sleeve-Protective NSA5539S Item 13

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(15) Subtask 363038-010-001-001 - If necessary, remove the ducts between FR39 and

FR40 for access

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

Fig. A-FBPAA

Removal/Installation of the Ducts

Between FR39 and FR40 for Access

Sheet 01

(a) Remove :

Fig. A-FBPAA

(Refer to AMM Task 21-20-00-010-801)

1 Duct assy Item (125) Retain

1 Duct assy Item (126) Retain

1 Duct assy Item (127) Retain

(16) Subtask 363038-831-011-001 - Modify the Interconnecting Electrical Wire FIN

309HF and 310HF, between the sensing elements.

Work Zones and Access Panels

Zone Access/Work location

150

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 ASNA2397-10L 1 WASHER

169 NSA935401-03 8 TIE

174 35301-74 1 CABLE

175 35301-75 1 CABLE

F9000095228595 BUNDLE

References

Elec. Std. Practices Manual (ESPM) 20-43-10

Service Bulletin (SB) A330-36-3032

Fig. A-FBJAA

Drilling of a New Hole in the Structure

between FR53.5 and FR53.6 on the LH

side and Installation of Sensing

Elements

Sheet 01

Sheet 02

Sheet 03

Fig. A-FWCAA

Installation of the Wiring of the New

Sensing Elements

Sheet 01

(a) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and

Fig. A-FBJAA Sheet 02, remove without disconnection the FINs 137HF and 138HF

and the FINs 309HF and 310HF attached with :

1 Screw Item (168) Retain

1 Washer Item (14) Discard

2 Clamp Item (155) Retain

1 Spacer Item (18) Retain

(b) Modify the splice FIN 3503VS :

1 Before any disconnection, record the wires number associated to the FIN

137HF and the FIN 138HF.

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2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF :

FIN 3503VS

1 Splice Discard

NOTE: Retain the identification sleeves and the identification label of

the 3503VS and of the wires associated to the FIN 137HF and

the FIN 138HF.

3 Remove :

FIN 137HF

1 Cable-Electrical

Interconnecting

35301-74 Item (174) Discard

4 Maintain in position :

FIN 138HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175)

5 Put in position :

FIN 137HF

1 Cable-Electrical

Interconnecting

35301-75 Item 175

6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN

137HF and the FIN 138HF, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3503VS with the identification sleeves

and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at removal,

identify the wires associated to the FINs 137HF and 138HF

with the retained identification sleeves.

(c) Modify the splice FIN 3593VS :

NOTE: Apply the following modifications only if were not applied with

the embodiment of the Service Bulletin No. A330-36-3032 or the

associated Technical Adaptation.

1 Before any disconnection, record the wires number associated to the FIN

309HF and the FIN 310HF.

2 Remove the splice FIN 3593VS between the FIN 309HF and the FIN 310HF :

FIN 3593VS

1 Splice Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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NOTE: Retain the identification sleeves and the identification label of

the 3593VS and of the wires associated to the FIN 309HF and

the FIN 310HF.

3 Remove :

FIN 309HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175) Discard

4 Maintain in position :

FIN 310HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175)

5 Put in position :

FIN 309HF

1 Cable-Electrical

Interconnecting

35301-74 Item 174

6 Install the new splice FIN 3593VS (PN E0360RK1816) between the FIN

309HF and the FIN 310HF, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3593VS with the identification sleeves

and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at removal,

identify the wires associated to the FINs 309HF and 310HF

with the retained identification sleeves.

(d) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and

Fig. A-FBJAA Sheet 02, install the FINs 137HF and 138HF and the FINs 309HF

and 310HF (spliced previously) with :

1 Spacer Item (18) Retained at

removal

2 Clamp Item (155) Retained at

removal

1 Washer ASNA2397-10L Item 14

1 Screw Item (168) Retained at

removal

and attach it with :

8 Tie-Cable NSA935401-03 Item 169

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NOTE: After connection, secure the FINs 137HF and 138HF and the FINs

309HF and 310HF with Wire-lock MS20995C32 Item 27, (Refer to

Fig. A-FBJAA Sheet 03).

(e) If necessary, secure the nuts (installed on the fuselage) and the FIN 138HF and the

FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBJAA Sheet 03).

(17) Subtask 363038-831-012-001 - Modify the existing Harness 2SG.

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 10.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

16 NSA5527-03-01 1 SPACER

22 NSA5527-03-15 1 SPACER

131 NSA935808-03 20 WASHER

141 NSA5527-03-02 2 SPACER

150 NSA935807-04 4 CLAMP

151 NSA5159-17 1 STUD

152 NSA5527-03-08 1 SPACER

153 NSA935808-01 8 WASHER

157 NSA5159-10 1 STUD

158 NAS1801-3-9 3 SCREW

171 NAS1801-3-17 2 SCREW

172 NAS1149F0332P 2 WASHER

174 35301-74 1 CABLE

175 35301-75 1 CABLE

176 NSA5516-21ND 5 CLAMP

177 NSA5516-22ND 5 CLAMP

178 NSA5516-23ND 5 CLAMP

179 NSA5516-07ND 2 CLAMP

180 NSA5516-08ND 2 CLAMP

181 NSA5516-10ND 2 CLAMP

F9000095228595 BUNDLE

References

Elec. Std. Practices Manual (ESPM) 20-43-10

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References

Service Bulletin (SB) A330-36-3032

Fig. A-FBMAA

Modification of the Existing Harness

2SG

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

Sheet 11

Sheet 12

Sheet 13

Sheet 14

Sheet 15

Sheet 16

Sheet 17

Sheet 18

Sheet 19

Fig. A-FWCAA

Installation of the Wiring of the New

Sensing Elements

Sheet 01

(a) Modify the supports of existing routing between 302HF located on the left hand side

at stringer 36 and Frame 40 and the 3520VP located on the right hand side at

Frame 39.1 :

NOTE: Apply the following modifications only if were not applied with

the embodiment of the Service Bulletin No. A330-36-3032 or the

associated Technical Adaptation.

1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame

39.2, remove :

a For Section A-A :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (152) Retain

1 Clamp Item (150) Retain

1 Stud Item (151) Retain

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b For Section B-B :

6 Nut Item (154) Retain

6 Washer Item (153) Discard

6 Clamp Item (150) Retain

6 Spacer Item (152) Retain

6 Clamp Item (150) Retain

6 Stud Item (151) Retain

c For Section C-C :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (155) Discard

1 Spacer Item (152) Retain

1 Clamp Item (155) Discard

1 Stud Item (151) Retain

2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame

39.2, install :

a For Section D-D :

1 Stud Item (151) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

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b For Section E-E :

6 Stud Item (151) Retained at

removal

6 Clamp Item (150) Retained at

removal

6 Spacer Item (152) Retained at

removal

6 Clamp Item (150) Retained at

removal

6 Washer NSA935808-03 Item 131

6 Nut Item (154) Retained at

removal

c For Section F-F :

1 Stud Item (151) Retained at

removal

1 Clamp NSA935807-04 Item 150

1 Spacer Item (152) Retained at

removal

1 Clamp NSA935807-04 Item 150

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09,

along the Frame 39.1 and between Stringer 39 and 40, remove :

a For Section G-G :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (155) Discard

1 Spacer Item (152) Retain

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1 Clamp Item (150) Retain

1 Stud Item (151) Retain

b For Section H-H :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (155) Discard

1 Spacer Item (152) Retain

1 Clamp Item (155) Retain

1 Stud Item (151) Retain

4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09,

along the Frame 39.1 and between Stringer 39 and 40, install :

a For Section J-J :

1 Stud Item (151) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp NSA935807-04 Item 150

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

b For Section K-K :

1 Stud Item (151) Retained at

removal

1 Clamp Item (155) Retained at

removal

1 Spacer Item (152) Retained at

removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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1 Clamp NSA935807-04 Item 150

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between

Stringer 40 and 43, remove for detail F :

2 Nut Item (154) Retain

2 Washer Item (153) Discard

2 Clamp Item (150) Retain

2 Spacer Item (152) Retain

2 Clamp Item (135) Retain

2 Clamp Item (134) Retain

2 Stud Item (151) Retain

6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between

Stringer 40 and 43, install for detail G :

2 Stud Item (151) Retained at

removal

2 Clamp Item (134) Retained at

removal

2 Clamp Item (135) Retained at

removal

2 Spacer Item (152) Retained at

removal

2 Clamp Item (150) Retained at

removal

2 Washer NSA935808-03 Item 131

2 Nut Item (154) Retained at

removal

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7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the

Frame 39.1 and between Stringers 44 and 45, remove :

a For Section L-L :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Clamp Item (138) Retain

1 Spacer Item (152) Retain

1 Clamp Item (135) Retain

1 Clamp Item (134) Retain

1 Stud Item (151) Retain

b For Section M-M :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (152) Retain

1 Clamp Item (135) Retain

1 Clamp Item (134) Retain

1 Stud Item (151) Retain

8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the

Frame 39.1 and between Stringers 44 and 45, install :

a For Section N-N :

1 Stud Item (151) Retained at

removal

1 Clamp Item (134) Retained at

removal

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1 Clamp Item (135) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (138) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

b For Section P-P :

1 Stud Item (151) Retained at

removal

1 Clamp Item (134) Retained at

removal

1 Clamp Item (135) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the

Frame 39.1 and between Stringers 46 and 48, remove for section Q-Q :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (16) Discard

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1 Clamp Item (139) Retain

1 Spacer Item (152) Retain

1 Clamp Item (135) Retain

1 Clamp Item (134) Retain

1 Stud Item (157) Discard

10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the

Frame 39.1 and between Stringers 46 and 48, install for Section R-R :

1 Stud NSA5159-17 Item 151

1 Clamp Item (134) Retained at

removal

1 Clamp Item (135) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (139) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between

Stringers 49 and 52, remove for detail K :

2 Nut Item (154) Retain

2 Washer Item (153) Discard

2 Clamp Item (150) Retain

2 Spacer Item (152) Retain

2 Clamp Item (138) Retain

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2 Stud Item (151) Retain

12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between

Stringers 49 and 52, install for detail L :

2 Stud Item (151) Retained at

removal

2 Clamp Item (138) Retained at

removal

2 Spacer Item (152) Retained at

removal

2 Clamp Item (150) Retained at

removal

2 Washer NSA935808-03 Item 131

2 Nut Item (154) Retained at

removal

13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between

Stringers 52 and 54, remove for Section S-S :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Clamp Item (138) Retain

1 Spacer Item (141) Retain

1 Clamp Item (138) Retain

1 Stud Item (140) Retain

14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between

Stringers 52 and 54, install for Section T-T :

1 Stud Item (140) Retained at

removal

1 Clamp Item (138) Retained at

removal

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1 Spacer Item (141) Retained at

removal

1 Clamp Item (138) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

15 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the

Stringers 54, remove for detail N :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (152) Retain

1 Clamp Item (138) Retain

1 Stud Item (151) Retain

16 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the

Stringers 54, install for detail P :

1 Stud Item (151) Retained at

removal

1 Clamp Item (138) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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17 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between

Stringers 54 and 48, remove for detail Q :

3 Screw Item (167) Discard

3 Washer Item (153) Discard

3 Clamp Item (138) Retain

3 Clamp Item (150) Retain

18 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between

Stringers 54 and 48, install for detail R :

3 Clamp Item (150) Retained at

removal

3 Clamp Item (138) Retained at

removal

3 Washer NSA935808-01 Item 153

3 Screw NAS1801-3-9 Item 158

19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the

Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, remove :

a For Section U-U :

1 Nut Item (154) Discard

1 Washer Item (153) Discard

1 Clamp Item (135) Discard

1 Spacer Item (18) Discard

1 Clamp Item (134) Discard

1 Stud Item (151) Discard

b For Section V-V :

1 Screw Item (183) Discard

1 Washer Item (153) Discard

1 Clamp Item (184) Discard

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1 Spacer Item (141) Discard

1 Clamp Item (184) Discard

20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the

Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for

Section W-W :

2 Spacer NSA5527-03-02 Item 141

2 Clamp NSA5516-07ND Item 179

or

2 Clamp NSA5516-08ND Item 180

or

2 Clamp NSA5516-10ND Item 181

and

2 Washer NAS1149F0332P Item 172

2 Screw NAS1801-3-17 Item 171

NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND

or NSA5516-08ND or NSA5516-10ND.

21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 47 and 46, remove for detail Y :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (165) Discard

1 Spacer Item (152) Retain

1 Clamp Item (155) Retain

1 Clamp Item (155) Retain

1 Stud Item (163) Retain

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22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 47 and 46, install for detail Z :

1 Stud Item (163) Retained at

removal

1 Clamp Item (155) Retained at

removal

1 Clamp Item (155) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Spacer NSA5527-03-15 Item 22

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 46 and 45, remove for detail W :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (135) Retain

1 Spacer Item (18) Discard

1 Clamp Item (134) Discard

1 Stud Item (151) Discard

24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 46 and 45, install for detail X:

1 Stud NSA5159-10 Item 157

1 Clamp NSA5516-21ND Item 176

or

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

1 Clamp NSA5516-22ND Item 177

or

1 Clamp NSA5516-23ND Item 178

and

1 Spacer NSA5527-03-01 Item 16

1 Spacer NSA5527-03-08 Item 152

1 Clamp Item (135) Retained at

removal

1 Washer NSA935808-01 Item 153

1 Nut Item (154) Retained at

removal

NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND

or NSA5516-22ND or NSA5516-23ND.

25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 44 and 43, remove for detail AA :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (135) Retain

1 Spacer Item (18) Retain

1 Clamp Item (134) Discard

1 Stud Item (151) Retain

26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 44 and 43, install for detail AB :

1 Stud Item (151) Retained at

removal

1 Clamp NSA5516-21ND Item 176

or

1 Clamp NSA5516-22ND Item 177

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

or

1 Clamp NSA5516-23ND Item 178

and

1 Spacer Item (18) Retained at

removal

1 Clamp Item (135) Retained at

removal

1 Washer NSA935808-01 Item 153

1 Nut Item (154) Retained at

removal

NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND

or NSA5516-22ND or NSA5516-23ND.

27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 42 and 38, remove for detail AC :

3 Screw Item (167) Retain

3 Washer Item (153) Discard

3 Clamp Item (135) Retain

3 Clamp Item (134) Discard

28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 42 and 38, install for detail AD :

3 Clamp NSA5516-21ND Item 176

or

3 Clamp NSA5516-22ND Item 177

or

3 Clamp NSA5516-23ND Item 178

and

3 Clamp Item (135) Retained at

removal

3 Washer NSA935808-01 Item 153

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

3 Screw Item (167) Retained at

removal

NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND

or NSA5516-22ND or NSA5516-23ND.

(b) Modify the existing route 2SG between FIN 302HF located on the left hand side at

stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment

:

NOTE: Apply the following modifications only if the Service Bulletin No.

A330-36-3032 and the associated Technical Adaptation were

applied. The following modification consists to restore the aircraft

to the configuration before Service Bulletin No. A330-36-3032 and

associated Technical Adaptation.

1 Modify the Interconnecting Electrical Wire FIN 301HF (Only if aircraft is

equipped with FIN 301HF PN 35301-75) :

Refer to ESPM 20-43-10

a Before any disconnection, record the wires number associated to the FIN

301HF.

b Remove the splice FIN 3591VS between the FIN 301HF and the wire No.

3622-0540 :

FIN 3591VS

1 Splice Discard

NOTE: Retain the identification sleeves and the identification

label of the 3591VS and of the wires associated to the

FIN 301HF.

c Remove :

FIN 301HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175) Discard

d Install :

1 Cable-Electrical

Interconnecting

35301-74 Item 174

e Install the new splice FIN 3591VS (PN NSA936809RG0002) between the

FIN 301HF and the wire No. 3622-0540, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3591VS with the identification

sleeves and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at

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SERVICE BULLETIN

removal, identify the wires associated to the FINs 301HF

with the retained identification sleeves.

NOTE: After connection, Secure the FIN 301HF and FIN 302HF

with Wire-lock MS20995C41 item 133.

2 Modify the Interconnecting Electrical Wire FIN 22HF (If aircraft is equipped

with FIN 22HF PN 35301-74) :

a Before any disconnection, record the wires number associated to the FIN

22HF.

b Remove the splice FIN 3501VS between the FIN 22HF and the wire No.

3622-0082 :

FIN 3501VS

1 Splice Discard

NOTE: Retain the identification sleeves and the identification

label of the 3501VS and of the wires associated to the

FIN 22HF.

c Remove :

FIN 22HF

1 Cable-Electrical

Interconnecting

35301-74 Item (174) Discard

d Install :

1 Cable-Electrical

Interconnecting

35301-75 Item 175

e Install the new splice FIN 3501VS (PN NSA936809RG0002) between the

FIN 22HF and the wire No. 3622-0082, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3501VS with the identification

sleeves and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at

removal, identify the wires associated to the FINs 22HF

with the retained identification sleeves.

NOTE: After connection, Secure the FIN 22HF and FIN 97HF

with Wire-lock MS20995C41 item 133.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

(18) Subtask 363038-831-013-001 - Modify the Wiring between the Avionics

Compartment and the Cargo Compartment.

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095228595 BUNDLE

References

Service Bulletin (SB) A330-36-3032

Fig. A-FBMAA

Modification of the Existing Harness

2SG

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

Sheet 11

Sheet 12

Sheet 13

Sheet 14

Sheet 15

Sheet 16

Sheet 17

Sheet 18

Sheet 19

Fig. A-FWBAA

Modification of the Wiring between the

Cargo Compartment and the Avionics

Compartment

Sheet 01

NOTE: Apply the following modifications only if were not applied with the

embodiment of the Service Bulletin No. A330-36-3032 or the associated

Technical Adaptation.

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SERVICE BULLETIN

(a) Modify the connection of the wire No. 3622-0542 as shown on the wiring diagram,

Fig. A-FWBAA Sheet 01.

NOTE: If necessary use contact PN EN3155-003F2222 supplied in :

Bundle F9000095228595

(19) Subtask 363038-831-014-001 - Modify the Wiring in the Main rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Work location Electrical panel 800VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

169 NSA935401-03 200 TIE

F9000095228595 BUNDLE

NSA935401-06 200 TIE

NSA935401-13 200 TIE

References

Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802

Task 36-11-34-400-802

Service Bulletin (SB) A330-36-3032

Fig. A-FWAAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Fig. A-FHAAA

Hook-Up Chart of the Modification of the

Wiring in the Main Rack 800VU

Sheet 01

NOTE: Apply the following modifications only if were not applied with the

embodiment of the Service Bulletin No. A330-36-3032 or the associated

Technical Adaptation.

(a) Remove and retain the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task

36-11-34-000-802).

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SERVICE BULLETIN

(b) Remove the wire as shown on the wiring diagram Fig. A-FWAAA Sheet 01, and as

given in the Hook-up Chart line :

- 1 (Refer to Fig. A-FHAAA Sheet 01).

(c) Install the wires as shown on the wiring diagram Fig. A-FWAAA Sheet 01 and as

given in the Hook-up Chart lines :

- 4 thru 5 (Refer to Fig. A-FHAAA Sheet 01) supplied in :

Bundle F9000095228595

(d) Attach the wires with :

200 Tie-Cable NSA935401-03 Item 169

200 Tie-Cable NSA935401-06

200 Tie-Cable NSA935401-13

(e) Install the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802).

(20) Subtask 363038-831-015-001 - If removed, install the ducts between FR39 and

FR40.

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

Fig. A-FBPAA

Removal/Installation of the Ducts

Between FR39 and FR40 for Access

Sheet 01

(a) Install :

Refer to Fig. A-FBPAA

(Refer to AMM Task 21-20-00-410-801)

1 Duct assy Item (125) Retained at

removal

1 Duct assy Item (126) Retained at

removal

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SERVICE BULLETIN

1 Duct assy Item (127) Retained at

removal

(21) Subtask 363038-831-201-001 - Remove the sleeves from the Auxiliary Power Unit

(APU) bleed-air-duct

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 313AL, Door 312AR

Work location from Frame 83 to Frame 93

Manpower Resources

Manhours 1.25

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the Sleeves from the APU

Bleed-Air-Duct

Sheet 01

(a) Remove the sleeves from the APU bleed-air-duct in the rear fuselage section.

Refer to Fig. A-GBAAA Sheet 01.

1 Between Frame 83 and Frame 93 remove the sleeves:

1 Sleeve Assy F3617062402000 Item (200) Discard

1 Sleeve Assy F3617062402400 Item (201) Discard

1 Sleeve Assy F3617062402600 Item (202) Discard

1 Sleeve Assy F3617062402800 Item (203) Discard

1 Sleeve Assy F3617062403000 Item (204) Discard

(22) Subtask 363038-831-202-001 - Remove the clamp and the attaching parts from the

overheat sensing elements

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 83 to Frame 88

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801

Fig. A-GBBAA

Removal of the Clamp and the Attaching

Parts from the Overheat Sensing

Elements

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamp and the attaching parts in the rear fuselage.

Refer to Fig. A-GBBAA Sheet 01 thru Fig. A-GBBAA Sheet 04.

Refer to AMM Task 36-22-17-000-801.

1 Between Frame 83 and Frame 84, remove:

Refer to Fig. A-GBBAA Sheet 02, View B and Fig. A-GBBAA Sheet 04, View

F.

2 Sleeve-Protective NSA5539S Item (13) Discard

1 Clamp NSA5543-00 Item (10) Retain

with

1 Screw NAS1096-3-5 Item (205) Discard

2 Between Frame 84 and Frame 85, remove:

Refer to Fig. A-GBBAA Sheet 02, View C and Fig. A-GBBAA Sheet 04, View

F.

4 Sleeve-Protective NSA5539S Item (13) Discard

2 Clamp NSA5543-00 Item (10) Retain

with

2 Screw NAS1096-3-5 Item (205) Discard

3 Between Frame 85 and Frame 86, remove:

Refer to Fig. A-GBBAA Sheet 03, View D and Fig. A-GBBAA Sheet 04, View

F.

2 Sleeve-Protective NSA5539S Item (13) Discard

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SERVICE BULLETIN

1 Clamp NSA5543-00 Item (10) Discard

with

1 Screw NAS1096-3-5 Item (205) Discard

4 Between Frame 86 and Frame 87, remove:

Refer to Fig. A-GBBAA Sheet 03, View E and Fig. A-GBBAA Sheet 04, View

F.

2 Sleeve-Protective NSA5539S Item (13) Discard

1 Clamp NSA5543-00 Item (10) Retain

with

1 Screw NAS1096-3-5 Item (205) Discard

5 From the sensing elements clamp at Frame 88, remove:

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 04, View G.

1 Screw NAS1096-3-5 Item (205) Discard

(23) Subtask 363038-831-204-001 - Remove the clamp from the overheat-detection dual

loops at Frame 80

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location Frame 80

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801

Fig. A-GBCAA

Removal of the Clamps and the

Attaching Parts from the OverheatDetection Dual Loops at Frame 80

Sheet 01

Sheet 02

(a) Remove the clamp from the sensing elements 32HF and 357HF.

Refer to Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02.

Refer to AMM Task 36-22-17-000-801.

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1 From Frame 80, remove:

2 Sleeve-Protective NSA5539S Item (13) Discard

1 Clamp NSA5543-00 Item (10) Discard

with

1 Screw NAS1096-3-5 Item (205) Discard

(24) Subtask 363038-831-205-001 - Reroute the sensing elements 32HF and 357HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location Frame 80

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Kit 363038D12R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5539S 2 SLEEVE

16 NSA5527-03-01 1 SPACER

86 NSA5538-00 2 CLAMP

207 NAS1802-3-13 1 SCREW

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801

Fig. A-GBDAA

Rerouting of the Sensing Elements

32HF and 357HF and Installation of

Clamps

Sheet 01

Sheet 02

Fig. A-GBHAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

(a) Reroute the sensing elements 32HF and 357HF and install the clamps.

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02.

Refer to AMM Task 36-22-17-400-801.

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1 Reroute the sensing elements 32HF and 357HF at Frame 80 from parallel

installation to on-top-of-each-other installation and install:

2 Sleeve-Protective NSA5539S Item 13

1 Spacer NSA5527-03-01 Item 16

2 Clamp NSA5538-00 Item 86

with

1 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

(25) Subtask 363038-831-206-001 - Replace the clamp of the electrical harness

5866VB/2S in the rear fuselage

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 90 to Frame 91

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills AIRFRAME

Material necessary to do the job

Kit 363038D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

169 NSA935401-03 30 TIE

210 MS21919WCH14 1 CLAMP

211 F9237000207200 8 PLCRDSET

References

Fig. A-GBEAA

Replacement of the Clamp between

Frame 90 and Frame 91

Sheet 01

Sheet 02

Sheet 03

(a) Replace the clamp between Frame 90 and Frame 91.

Refer to Fig. A-GBEAA Sheet 01 thru Fig. A-GBEAA Sheet 03.

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SERVICE BULLETIN

1 Between Frame 90 and Frame 91, STGR6RH, remove the clamp:

Refer to Fig. A-GBEAA Sheet 03, View C.

1 Clamp-Loop, Crs ABS0805-09 Item (214) Discard

2 Install the new clamp between Frame 90 and Frame 91, STGR6RH:

Refer to Fig. A-GBEAA Sheet 03, View D.

1 Clamp MS21919WCH14 Item 210

3 Install the Service Bulletin placards along the harness routing of 5866VB/2S:

8 Placard Set F9237000207200 Item 211

and

30 Tie-Cable NSA935401-03 Item 169

(26) Subtask 363038-831-207-001 - Install the clamp and the new attaching parts on the

overheat sensing elements in the rear fuselage

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 83 to Frame 88

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 363038D10R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5539S 10 SLEEVE

16 NSA5527-03-01 4 SPACER

86 NSA5538-00 2 CLAMP

207 NAS1802-3-13 4 SCREW

208 NSA5527-03-04 2 SPACER

209 NAS1801-3-8 2 SCREW

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 91

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References

Fig. A-GBFAA

Installation of the Clamp and the

Attaching Parts in the Rear Fuselage

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GBHAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

(a) Install the clamp and the new attaching parts in the rear fuselage.

Refer to Fig. A-GBFAA Sheet 01 thru Fig. A-GBFAA Sheet 05.

Refer to AMM Task 36-22-17-400-801.

1 Between Frame 83 and Frame 84, install:

Refer to Fig. A-GBFAA Sheet 02.

1 Clamp NSA5543-00 Item (10) Retained at

removal

2 Sleeve-Protective NSA5539S Item 13

with

1 Spacer NSA5527-03-04 Item 208

1 Screw NAS1801-3-8 Item 209

NOTE: The torque value of the screw, Item 209, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

2 Between Frame 84 and Frame 85, install:

Refer to Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA Sheet 04, View F.

2 Clamp NSA5543-00 Item (10) Retained at

removal

4 Sleeve-Protective NSA5539S Item 13

with

2 Spacer NSA5527-03-01 Item 16

2 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 92

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SERVICE BULLETIN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

3 Between Frame 85 and Frame 86, install:

Refer to Fig. A-GBFAA Sheet 05, Views G and H.

2 Sleeve-Protective NSA5539S Item 13

2 Clamp NSA5538-00 Item 86

with

1 Spacer NSA5527-03-01 Item 16

1 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

4 Between Frame 86 and Frame 87, install:

Refer to Fig. A-GBFAA Sheet 04.

1 Clamp NSA5543-00 Item (10) Retained at

removal

2 Sleeve-Protective NSA5539S Item 13

with

1 Spacer NSA5527-03-01 Item 16

1 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

5 On the sensing elements clamp at Frame 88, install:

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 05, View J.

1 Spacer NSA5527-03-04 Item 208

1 Screw NAS1801-3-8 Item 209

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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NOTE: The torque value of the screw, Item 209, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

(27) Subtask 363038-831-209-001 - Install the sleeves on the APU bleed-air-duct

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 313AL, Door 312AR

Work location from Frame 83 to Frame 94

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Kit 363038D14R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5539S 6 SLEEVE

200 F3617062404000 1 SLEEVE

201 F3617062403800 1 SLEEVE

202 F3617062403600 1 SLEEVE

203 F3617062403400 1 SLEEVE

204 F3617062403200 1 SLEEVE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Adhesive Tape (Insulation

Blanket Repair)

08-073 As required

References

Fig. A-GBGAA

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

(a) Install the sleeves on the APU bleed-air-duct in the rear fuselage section.

Refer to Fig. A-GBGAA Sheet 01.

1 Install new sleeves on the sensing elements at Frame 83, Frame 88 and

Frame 91:

Refer to Fig. A-GBGAA Sheet 01, View B.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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6 Sleeve-Protective NSA5539S Item 13

2 Between Frame 83 thru Frame 94, install the sleeves on the APU bleed-airduct and close them with adhesive strips:

1 Sleeve Assy F3617062404000 Item 200

1 Sleeve Assy F3617062403800 Item 201

1 Sleeve Assy F3617062403600 Item 202

1 Sleeve Assy F3617062403400 Item 203

1 Sleeve Assy F3617062403200 Item 204

with

Adhesive Tape

(Insulation Blanket

Repair)

08-073 As required

NOTE: Make sure that the blowout apertures of the blankets are near

(under) the sensing elements.

NOTE: Make sure that there is no contact between the sensing

elements and the sleeves between Frame 86 and Frame 87.

**CONF 002

(1) Subtask 363038-831-001-001 - Remove the sensing elements and the supports

between FR39 and FR44

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 02, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 97HF

1 Sensing element 35610-2-255 Item (1) Discard

FIN 98HF

1 Sensing element 35631-2-255 Item (2) Discard

FIN 302HF

1 Sensing element 35610-2-255 Item (1) Discard

FIN 303HF

1 Sensing element 35627-2-255 Item (11) Discard

2 Support Item (59) Discard

4 Rivet Item (45) Discard

2 Placard Item (23) Discard

1 Placard Item (24) Discard

2 Placard Item (29) Discard

1 Placard Item (30) Discard

4 Nut Item (57) Discard

14 Screw Item (76) Discard

32 Washer Item (46) Discard

64 Protective sleeve Item (56) Discard

23 Clamp Item (58) Discard

2 Screw Item (47) Discard

18 Clamp Item (82) Discard

9 Spacer Item (55) Discard

1 Screw Item (50) Discard

10 Spacer Item (53) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 96

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SERVICE BULLETIN

5 Screw Item (52) Discard

4 Screw Item (52) Discard

6 Screw Item (48) Discard

As

required

Wire-lock Item (100) Discard

(2) Subtask 363038-831-002-001 - Remove the sensing elements and the supports

between FR44 and FR53.2

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 99HF

1 Sensing element 35618-2-255 Item (3) Discard

FIN 100HF

1 Sensing element 35610-2-255 Item (1) Discard

FIN 304HF

1 Sensing element 35616-2-255 Item (12) Discard

FIN 305HF

1 Sensing element 35611-2-255 Item (13) Discard

2 Support Item (59) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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4 Rivet Item (45) Discard

1 Placard Item (25) Discard

2 Placard Item (26) Discard

1 Placard Item (27) Discard

1 Placard Item (30) Discard

2 Placard Item (31) Discard

2 Placard Item (32) Discard

1 Placard Item (33) Discard

4 Nut Item (57) Discard

1 Plate assy Item (41) Discard

8 Screw Item (76) Discard

30 Washer Item (46) Discard

56 Protective sleeve Item (56) Discard

18 Clamp Item (58) Discard

1 Screw Item (47) Discard

20 Clamp Item (82) Discard

10 Spacer Item (55) Discard

5 Screw Item (50) Discard

17 Spacer Item (53) Discard

12 Screw Item (52) Discard

3 Screw Item (48) Discard

1 Screw Item (49) Discard

1 Spacer Item (54) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 98

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SERVICE BULLETIN

As

required

Wire-lock Item (100) Discard

(3) Subtask 363038-831-003-001 - Remove the sensing elements and the supports

between FR53.2 and FR53.6

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 04, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 23HF

1 Sensing element 35569-2-255 Item (7) Discard

FIN 101HF

1 Sensing element 35601-2-255 Item (5) Discard

FIN 102HF

1 Sensing element 35601-2-255 Item (5) Discard

FIN 306HF

1 Sensing element 35601-2-255 Item (5) Discard

FIN 307HF

1 Sensing element 35600-2-255 Item (15) Discard

FIN 308HF

1 Sensing element 35569-2-255 Item (7) Discard

3 Support Item (59) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

6 Rivet Item (45) Discard

2 Placard Item (20) Discard

1 Placard Item (27) Discard

2 Placard Item (28) Discard

1 Placard Item (33) Discard

2 Placard Item (34) Discard

2 Placard Item (35) Discard

6 Nut Item (57) Discard

1 Plate assy Item (40) Discard

11 Screw Item (76) Discard

38 Washer Item (46) Discard

74 Protective sleeve Item (56) Discard

29 Clamp Item (58) Discard

2 Screw Item (50) Discard

16 Clamp Item (82) Discard

8 Spacer Item (55) Discard

21 Spacer Item (53) Discard

19 Screw Item (52) Discard

6 Screw Item (48) Discard

As

required

Wire-lock Item (100) Discard

(4) Subtask 363038-831-004-001 - Remove the sensing elements and the supports

between FR53.6 and FR55

Work Zones and Access Panels

Zone Access/Work location

190

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 100

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Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills NON SPECIFIC

References

Fig. A-FBAAA

Installation of the New Sensing

Elements between FR39 and FR55, on

the LH Side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

(a) Remove :

Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 05, Fig. A-FBAAA Sheet 06

and Fig. A-FBAAA Sheet 07

FIN 24HF

1 Sensing element 35593-3-255 Item (8) Discard

FIN 25HF

1 Sensing element 35632-2-255 Item (9) Discard

FIN 311HF

1 Sensing element 35579-2-255 Item (17) Discard

FIN 312HF

1 Sensing element 35627-2-255 Item (11) Discard

1 Support Item (59) Discard

2 Rivet Item (45) Discard

1 Placard Item (21) Discard

1 Placard Item (22) Discard

1 Placard Item (36) Discard

1 Placard Item (37) Discard

2 Nut Item (57) Discard

1 Connector Item (61) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 101

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SERVICE BULLETIN

14 Screw Item (76) Discard

27 Washer Item (46) Discard

54 Protective sleeve Item (56) Discard

21 Clamp Item (58) Discard

4 Screw Item (52) Discard

14 Spacer Item (53) Discard

2 Screw Item (51) Discard

12 Clamp Item (82) Discard

6 Spacer Item (55) Discard

4 Screw Item (48) Discard

3 Screw Item (77) Discard

As

required

Wire-lock Item (100) Discard

(5) Subtask 363038-020-001-001 - If necessary, remove the ducts between FR35.5 and

FR35.6 for access

Work Zones and Access Panels

Zone Access/Work location

150

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801

Fig. A-FBBAA

Removal/Installation of the Ducts

between FR53.6 and FR53.7 on the LH

side (for Access)

Sheet 01

(a) Remove :

Fig. A-FBBAA

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

(Refer to AMM Task 36-12-41-000-801)

1 Duct assy Item (112) Retain

1 Duct assy Item (113) Retain

1 Duct assy Item (114) Retain

(6) Subtask 363038-831-005-001 - Install a New Support for the Routing of the Sensing

Elements between FR53.5 and FR53.6

Work Zones and Access Panels

Zone Access/Work location

150

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

96 F5392059300000 1 SUPPORT

97 ASNA2050DCJ3215 2 RIVET

Reidentified part set REIDA01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F0041196500000 BLANKET F2581677800000

F0041196600000 BLANKET F2581677900000

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Adhesive Tape (insulation

Blanket Repair)

08-073 As required

Interfay Sealant 09-005 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

References

Fig. A-FBCAA

Installation of a New Bracket between

FR53.5 and FR53.6

Sheet 01

Sheet 02

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 103

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SERVICE BULLETIN

(a) Move the insulation blanket to get access to the modification area.

(b) Put the bracket Item 96 in position as shown on Fig. A-FBCAA.

(c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.)

and 3.35mm (0.132in.) to match the holes of the bracket Item 96.

Refer to Fig. A-FBCAA

(d) Cut the insulation blanket to permit the installation of the bracket Item 96.

NOTE: For the repair of the insulation blanket use :

Adhesive Tape

(insulation Blanket

Repair)

08-073 As required

(e) Re-identify the insulation blanket :

1 Blanket-Insulation F2581677800000

becomes :

1 Blanket-Insulation F0041196500000

or,

1 Blanket-Insulation F2581677900000

becomes :

1 Blanket-Insulation F0041196600000

(f) Install :

Refer to Fig. A-FBCAA

1 Support F5392059300000 Item 96

2 Rivet ASNA2050DCJ3215 Item 97

NOTE: To the interface of the new bracket and the structure apply :

Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

NOTE: Wet install the fasteners with :

Interfay Sealant 09-005 As required

(g) Install the insulation blanket.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

(7) Subtask 363038-420-001-001 - If removed, Install the Ducts between FR53.5 and

FR53.6

Work Zones and Access Panels

Zone Access/Work location

150

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801

Fig. A-FBBAA

Removal/Installation of the Ducts

between FR53.6 and FR53.7 on the LH

side (for Access)

Sheet 01

(a) Install :

Refer to Fig. A-FBBAA

(Refer to AMM Task 36-12-41-400-801)

1 Duct assy Item (112) Retained at

removal

1 Duct assy Item (113) Retained at

removal

1 Duct assy Item (114) Retained at

removal

(8) Subtask 363038-020-002-001 - If necessary, Remove the Ducts between FR43 and

FR45 for access

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 105

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SERVICE BULLETIN

References

Fig. A-FBDAA

Removal/Installation of the Ducts

between FR44 and FR47 on the LH side

(for Access)

Sheet 01

(a) Remove :

Refer to Fig. A-FBDAA

(Refer to AMM Task 36-12-41-000-801)

1 Duct assy Item (115) Retain

1 Duct assy Item (116) Retain

(9) Subtask 363038-831-006-001 - Install the new Brackets for the Routing of the

Sensing Elements at FR44

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

97 ASNA2050DCJ3215 2 RIVET

98 F0041178800000 1 SUPPORT

99 F0041178800100 1 SUPPORT

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Interfay Sealant 09-005 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

References

Fig. A-FBKAA

Installation of Two New Brackets at

FR44

Sheet 01

Sheet 02

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBKAA

.

(b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm

(0.132in.) as shown on Fig. A-FBKAA.

(c) Install :

1 Support F0041178800000 Item 98

1 Support F0041178800100 Item 99

2 Rivet ASNA2050DCJ3215 Item 97

NOTE: To the interface of the new bracket and the structure apply :

Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

NOTE: Wet install the fasteners with :

Interfay Sealant 09-005 As required

(10) Subtask 363038-410-001-001 - If removed, install the ducts between FR43 and

FR45

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 43 to Frame 45

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801

Fig. A-FBDAA

Removal/Installation of the Ducts

between FR44 and FR47 on the LH side

(for Access)

Sheet 01

(a) Install :

(Refer to AMM Task 36-12-41-400-801)

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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1 Duct assy Item (115) Retained at

removal

1 Duct assy Item (116) Retained at

removal

(11) Subtask 363038-831-007-001 - Install the Sensing Elements and the Supports

between FR39 and FR44

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 39 to Frame 44

Manpower Resources

Manhours 14.00

Minimum number of person 1

Subtask elapsed time 14.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 30 CLAMP

11 ASNA0342T04-01 4 BOLT

13 NSA5539S 62 SLEEVE

14 ASNA2397-10L 34 WASHER

15 NSA5542-00 4 NUT

16 NSA5527-03-01 8 SPACER

18 NSA5527-03-11 6 SPACER

20 NAS6603-1 19 BOLT

21 NAS6603-9 8 BOLT

24 NAS6603-15 6 BOLT

29 NAS6603-2 2 BOLT

30 NSA5546-00 2 ANGLE

32 F1131031621700 2 PLACARD

33 F1131031623700 2 PLACARD

34 F1131031621800 1 PLACARD

35 F1131031623800 1 PLACARD

70 F3611548300000 1 SUPPORT

71 F3611548800000 1 SUPPORT

78 F3611549700000 1 SUPPORT

79 F3611549100000 1 SUPPORT

100 35606-2-255 1 SNSGELEM

101 35621-2-255 1 SNSGELEM

102 35620-2-255 1 SNSGELEM

113 35610-2-255 1 SNSGELEM

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 108

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References

Fig. A-FBEAA

Installation of the New Sensing

Elements between FR39 and FR44 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR39 and FR40.2.

1 Install the supports between FR39 and FR40 :

1 Angle NSA5546-00 Item 30

2 Rivet-Blind ASNA0342T04-01 Item 11

8 Clamp NSA5543-00 Item 10

6 Spacer NSA5527-03-01 Item 16

2 Spacer NSA5527-03-11 Item 18

8 Washer ASNA2397-10L Item 14

6 Bolt NAS6603-9 Item 21

2 Bolt NAS6603-15 Item 24

2 Install the supports between FR40 and FR40.2 :

1 Support F3611549100000 Item 79

1 Support F3611549700000 Item 78

5 Clamp NSA5543-00 Item 10

1 Spacer NSA5527-03-01 Item 16

8 Washer ASNA2397-10L Item 14

1 Bolt NAS6603-9 Item 21

6 Bolt NAS6603-1 Item 20

2 Bolt NAS6603-2 Item 29

1 Angle NSA5546-00 Item 30

2 Rivet-Blind ASNA0342T04-01 Item 11

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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3 Install the placards between FR39 and FR40.2 :

2 Placard F1131031621700 Item 32

2 Placard F1131031623700 Item 33

1 Placard F1131031621800 Item 34

1 Placard F1131031623800 Item 35

4 Install the sensing elements between FR39 and FR40.2 :

FIN 97HF

1 Sensing Element 35606-2-255 Item 100

FIN 302HF

1 Sensing Element 35610-2-255 Item 113

28 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(b) Install the sensing elements and the supports between FR40.2 and FR44.

1 Install the supports between FR40.2 and FR44 :

1 Support F3611548300000 Item 70

1 Support F3611548800000 Item 71

17 Clamp NSA5543-00 Item 10

4 Spacer NSA5527-03-11 Item 18

1 Spacer NSA5527-03-01 Item 16

18 Washer ASNA2397-10L Item 14

13 Bolt NAS6603-1 Item 20

1 Bolt NAS6603-9 Item 21

4 Bolt NAS6603-15 Item 24

2 Install the sensing elements between FR40.2 and FR44 :

FIN 98HF

1 Sensing Element 35620-2-255 Item 102

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 110

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FIN 303HF

1 Sensing Element 35621-2-255 Item 101

34 Sleeve-Protective NSA5539S Item 13

(12) Subtask 363038-831-008-001 - Install the sensing elements and the supports

between FR44 and FR50

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 44 to Frame 50

Manpower Resources

Manhours 14.00

Minimum number of person 1

Subtask elapsed time 14.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 29 CLAMP

11 ASNA0342T04-01 4 BOLT

13 NSA5539S 58 SLEEVE

14 ASNA2397-10L 35 WASHER

15 NSA5542-00 8 NUT

16 NSA5527-03-01 10 SPACER

17 NSA5527-03-10 1 SPACER

18 NSA5527-03-11 5 SPACER

19 NAS6603-24 2 BOLT

20 NAS6603-1 13 BOLT

21 NAS6603-9 8 BOLT

23 NAS6603-16 3 BOLT

26 NAS6603-32 1 BOLT

29 NAS6603-2 8 BOLT

30 NSA5546-00 2 ANGLE

34 F1131031621800 1 PLACARD

35 F1131031623800 1 PLACARD

36 F1131031623900 2 PLACARD

37 F1131031621900 2 PLACARD

38 F1131031624000 2 PLACARD

39 F1131031622000 2 PLACARD

40 F1131031622100 1 PLACARD

41 F1131031624100 1 PLACARD

79 F3611549100000 4 SUPPORT

80 F3611549500000 1 SUPPORT

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

81 F3611549600000 1 SUPPORT

103 35618-2-255 2 SNSGELEM

105 35598-2-255 1 SNSGELEM

114 35597-2-255 1 SNSGELEM

References

Fig. A-FBFAA

Installation of the New Sensing

Elements between FR44 and FR50 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR44 and FR46 :

1 Install the supports between FR44 and FR46 :

1 Support F3611549600000 Item 81

17 Clamp NSA5543-00 Item 10

8 Spacer NSA5527-03-01 Item 16

5 Spacer NSA5527-03-11 Item 18

21 Washer ASNA2397-10L Item 14

2 Bolt NAS6603-24 Item 19

4 Bolt NAS6603-1 Item 20

6 Bolt NAS6603-9 Item 21

3 Bolt NAS6603-16 Item 23

2 Bolt NAS6603-2 Item 29

2 Install the placards at FR44 :

1 Placard F1131031621800 Item 34

1 Placard F1131031623800 Item 35

1 Placard F1131031623900 Item 36

1 Placard F1131031621900 Item 37

3 Install the sensing elements between FR44 and FR46 :

FIN 99HF

1 Sensing Element 35618-2-255 Item 103

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FIN 304HF

1 Sensing Element 35618-2-255 Item 103

34 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(b) Install the sensing elements and the supports between FR46 and FR50.

1 Install the supports between FR46 and FR50 :

2 Angle NSA5546-00 Item 30

4 Rivet-Blind ASNA0342T04-01 Item 11

1 Support F3611549500000 Item 80

4 Support F3611549100000 Item 79

12 Clamp NSA5543-00 Item 10

2 Spacer NSA5527-03-01 Item 16

1 Spacer NSA5527-03-10 Item 17

14 Washer ASNA2397-10L Item 14

9 Bolt NAS6603-1 Item 20

2 Bolt NAS6603-9 Item 21

1 Bolt NAS6603-32 Item 26

6 Bolt NAS6603-2 Item 29

2 Install the placards between FR46 and FR50 :

1 Placard F1131031623900 Item 36

1 Placard F1131031621900 Item 37

2 Placard F1131031624000 Item 38

2 Placard F1131031622000 Item 39

1 Placard F1131031622100 Item 40

1 Placard F1131031624100 Item 41

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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3 Install the sensing elements between FR46 and FR50 :

FIN 100HF

1 Sensing Element 35597-2-255 Item 114

FIN 305HF

1 Sensing Element 35598-2-255 Item 105

24 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(13) Subtask 363038-831-009-001 - Install the sensing elements and the supports

between FR50 and FR53.6

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 50 to Frame 53.6

Manpower Resources

Manhours 21.00

Minimum number of person 1

Subtask elapsed time 21.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 37 CLAMP

11 ASNA0342T04-01 6 BOLT

13 NSA5539S 74 SLEEVE

14 ASNA2397-10L 51 WASHER

15 NSA5542-00 6 NUT

16 NSA5527-03-01 16 SPACER

18 NSA5527-03-11 1 SPACER

20 NAS6603-1 23 BOLT

21 NAS6603-9 16 BOLT

22 NSA5527-03-15 1 SPACER

24 NAS6603-15 1 BOLT

25 NSA5545-00 1 ANGLE

28 NAS6603-12 1 BOLT

29 NAS6603-2 10 BOLT

30 NSA5546-00 2 ANGLE

40 F1131031622100 1 PLACARD

41 F1131031624100 1 PLACARD

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

42 F1131031622200 2 PLACARD

43 F1131031624200 2 PLACARD

44 F1131031620400 2 PLACARD

45 F1131031624300 2 PLACARD

70 F3611548300000 1 SUPPORT

72 F3611548700000 1 SUPPORT

73 F3611548500000 1 SUPPORT

74 F3611548900000 1 SUPPORT

75 F3611548400000 1 SUPPORT

76 F3611548200000 1 SUPPORT

77 F3611548600000 1 SUPPORT

79 F3611549100000 3 SUPPORT

82 F3611549400000 1 SUPPORT

83 F3611549800000 1 SUPPORT

84 F3611549300000 1 SUPPORT

104 35567-3-255 1 SNSGELEM

106 35595-2-255 3 SNSGELEM

107 35596-2-255 1 SNSGELEM

108 35568-4-255 1 SNSGELEM

References

Fig. A-FBGAA

Installation of the New Sensing

Elements between FR50 and FR53.6 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR50 and FR53.2.

1 Install the supports between FR50 and FR53.2 :

1 Support F3611548700000 Item 72

1 Support F3611548400000 Item 75

1 Support F3611549400000 Item 82

1 Angle NSA5546-00 Item 30

2 Rivet-Blind ASNA0342T04-01 Item 11

13 Clamp NSA5543-00 Item 10

7 Spacer NSA5527-03-01 Item 16

16 Washer ASNA2397-10L Item 14

9 Bolt NAS6603-1 Item 20

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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7 Bolt NAS6603-9 Item 21

2 Install the placards between FR50 and FR53.2 :

1 Placard F1131031622100 Item 40

1 Placard F1131031624100 Item 41

1 Placard F1131031622200 Item 42

1 Placard F1131031624200 Item 43

3 Install the sensing elements between FR50 and FR53.2 :

FIN 101HF

1 Sensing Element 35595-2-255 Item 106

FIN 102HF

1 Sensing Element 35595-2-255 Item 106

26 Sleeve-Protective NSA5539S Item 13

2 Nut NSA5542-00 Item 15

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(b) Install the sensing elements and the supports between FR53.2 and FR53.6.

1 Install the supports between FR53.2 and FR53.6 :

1 Support F3611548300000 Item 70

1 Support F3611548500000 Item 73

1 Support F3611548900000 Item 74

1 Support F3611548200000 Item 76

1 Support F3611548600000 Item 77

3 Support F3611549100000 Item 79

1 Support F3611549800000 Item 83

1 Support F3611549300000 Item 84

1 Angle NSA5545-00 Item 25

1 Angle NSA5546-00 Item 30

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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4 Rivet-Blind ASNA0342T04-01 Item 11

24 Clamp NSA5543-00 Item 10

9 Spacer NSA5527-03-01 Item 16

1 Spacer NSA5527-03-11 Item 18

1 Spacer NSA5527-03-15 Item 22

35 Washer ASNA2397-10L Item 14

14 Bolt NAS6603-1 Item 20

9 Bolt NAS6603-9 Item 21

1 Bolt NAS6603-15 Item 24

1 Bolt NAS6603-12 Item 28

10 Bolt NAS6603-2 Item 29

2 Install the placards between FR53.2 and FR53.6 :

1 Placard F1131031622200 Item 42

1 Placard F1131031624200 Item 43

2 Placard F1131031620400 Item 44

2 Placard F1131031624300 Item 45

3 Install the sensing elements between FR53.2 and FR53.6 :

FIN 102HF

1 Sensing Element 35595-2-255 Item 106

FIN 307HF

1 Sensing Element 35596-2-255 Item 107

FIN 23HF

1 Sensing Element 35568-4-255 Item 108

FIN 308HF

1 Sensing Element 35567-3-255 Item 104

48 Sleeve-Protective NSA5539S Item 13

4 Nut NSA5542-00 Item 15

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(14) Subtask 363038-831-010-001 - Install the sensing elements and the supports

between FR53.6 and FR55

Work Zones and Access Panels

Zone Access/Work location

190 Work location from Frame 53.6 to Frame 55

Manpower Resources

Manhours 14.00

Minimum number of person 1

Subtask elapsed time 14.00

Skills AIRFRAME

Material necessary to do the job

Kit 363038A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NSA5543-00 27 CLAMP

11 ASNA0342T04-01 2 BOLT

13 NSA5539S 55 SLEEVE

14 ASNA2397-10L 32 WASHER

15 NSA5542-00 2 NUT

16 NSA5527-03-01 6 SPACER

17 NSA5527-03-10 2 SPACER

18 NSA5527-03-11 5 SPACER

20 NAS6603-1 17 BOLT

21 NAS6603-9 1 BOLT

26 NAS6603-32 2 BOLT

29 NAS6603-2 2 BOLT

30 NSA5546-00 1 ANGLE

70 F3611548300000 1 SUPPORT

79 F3611549100000 1 SUPPORT

85 NSA5549-90 2 CONNECTR

86 NSA5538-00 3 CLAMP

87 NAS6603-17 5 BOLT

88 F1131031620500 1 PLACARD

89 F1131031624400 1 PLACARD

90 F1131031620600 1 PLACARD

91 F1131031624500 1 PLACARD

93 F3611549200000 1 SUPPORT

94 NAS6603-10 5 BOLT

95 F3611549000000 1 SUPPORT

109 35597-3-255 1 SNSGELEM

110 35587-2-255 1 SNSGELEM

111 35627-2-255 1 SNSGELEM

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

112 35625-2-255 1 SNSGELEM

References

Fig. A-FBHAA

Installation of the New Sensing

Elements between FR53.6 and FR55 on

LH side

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the sensing elements and the supports between FR53.6 and FR55.

1 Install the supports between FR53.6 and FR55 :

1 Support F3611548300000 Item 70

1 Support F3611549100000 Item 79

1 Support F3611549200000 Item 93

1 Support F3611549000000 Item 95

1 Angle NSA5546-00 Item 30

2 Rivet-Blind ASNA0342T04-01 Item 11

27 Clamp NSA5543-00 Item 10

3 Clamp NSA5538-00 Item 86

6 Spacer NSA5527-03-01 Item 16

2 Spacer NSA5527-03-10 Item 17

5 Spacer NSA5527-03-11 Item 18

32 Washer ASNA2397-10L Item 14

17 Bolt NAS6603-1 Item 20

1 Bolt NAS6603-9 Item 21

2 Bolt NAS6603-32 Item 26

2 Bolt NAS6603-2 Item 29

5 Bolt NAS6603-17 Item 87

5 Bolt NAS6603-10 Item 94

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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2 Install the placards between FR53.6 and FR55 :

1 Placard F1131031620500 Item 88

1 Placard F1131031624400 Item 89

1 Placard F1131031620600 Item 90

1 Placard F1131031624500 Item 91

3 Install the sensing elements between FR53.6 and FR55 :

FIN 24HF

1 Sensing Element 35597-3-255 Item 109

FIN 311HF

1 Sensing Element 35587-2-255 Item 110

FIN 25HF

1 Sensing Element 35627-2-255 Item 111

FIN 312HF

1 Sensing Element 35625-2-255 Item 112

2 Nut NSA5542-00 Item 15

2 Connector NSA5549-90 Item 85

55 Sleeve-Protective NSA5539S Item 13

NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27.

(15) Subtask 363038-010-001-001 - If necessary, remove the ducts between FR39 and

FR40 for access

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

Fig. A-FBPAA

Removal/Installation of the Ducts

Between FR39 and FR40 for Access

Sheet 01

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(a) Remove :

Fig. A-FBPAA

(Refer to AMM Task 21-20-00-010-801)

1 Duct assy Item (125) Retain

1 Duct assy Item (126) Retain

1 Duct assy Item (127) Retain

(16) Subtask 363038-831-011-001 - Modify the Interconnecting Electrical Wire FIN

309HF and 310HF, between the sensing elements.

Work Zones and Access Panels

Zone Access/Work location

150

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 ASNA2397-10L 1 WASHER

169 NSA935401-03 8 TIE

174 35301-74 1 CABLE

175 35301-75 1 CABLE

F9000095228595 BUNDLE

References

Elec. Std. Practices Manual (ESPM) 20-43-10

Service Bulletin (SB) A330-36-3032

Fig. A-FBJAA

Drilling of a New Hole in the Structure

between FR53.5 and FR53.6 on the LH

side and Installation of Sensing

Elements

Sheet 01

Sheet 02

Sheet 03

Fig. A-FWCAA

Installation of the Wiring of the New

Sensing Elements

Sheet 01

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(a) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and

Fig. A-FBJAA Sheet 02, remove without disconnection the FINs 137HF and 138HF

and the FINs 309HF and 310HF attached with :

1 Screw Item (168) Retain

1 Washer Item (14) Discard

2 Clamp Item (155) Retain

1 Spacer Item (18) Retain

(b) Modify the splice FIN 3503VS :

1 Before any disconnection, record the wires number associated to the FIN

137HF and the FIN 138HF.

2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF :

FIN 3503VS

1 Splice Discard

NOTE: Retain the identification sleeves and the identification label of

the 3503VS and of the wires associated to the FIN 137HF and

the FIN 138HF.

3 Remove :

FIN 137HF

1 Cable-Electrical

Interconnecting

35301-74 Item (174) Discard

4 Maintain in position :

FIN 138HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175)

5 Put in position :

FIN 137HF

1 Cable-Electrical

Interconnecting

35301-75 Item 175

6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN

137HF and the FIN 138HF, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3503VS with the identification sleeves

and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at removal,

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identify the wires associated to the FINs 137HF and 138HF

with the retained identification sleeves.

(c) Modify the splice FIN 3593VS :

NOTE: Apply the following modifications only if were not applied with

the embodiment of the Service Bulletin No. A330-36-3032 or the

associated Technical Adaptation.

1 Before any disconnection, record the wires number associated to the FIN

309HF and the FIN 310HF.

2 Remove the splice FIN 3593VS between the FIN 309HF and the FIN 310HF :

FIN 3593VS

1 Splice Discard

NOTE: Retain the identification sleeves and the identification label of

the 3593VS and of the wires associated to the FIN 309HF and

the FIN 310HF.

3 Remove :

FIN 309HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175) Discard

4 Maintain in position :

FIN 310HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175)

5 Put in position :

FIN 309HF

1 Cable-Electrical

Interconnecting

35301-74 Item 174

6 Install the new splice FIN 3593VS (PN E0360RK1816) between the FIN

309HF and the FIN 310HF, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3593VS with the identification sleeves

and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at removal,

identify the wires associated to the FINs 309HF and 310HF

with the retained identification sleeves.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(d) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and

Fig. A-FBJAA Sheet 02, install the FINs 137HF and 138HF and the FINs 309HF

and 310HF (spliced previously) with :

1 Spacer Item (18) Retained at

removal

2 Clamp Item (155) Retained at

removal

1 Washer ASNA2397-10L Item 14

1 Screw Item (168) Retained at

removal

and attach it with :

8 Tie-Cable NSA935401-03 Item 169

NOTE: After connection, secure the FINs 137HF and 138HF and the FINs

309HF and 310HF with Wire-lock MS20995C32 Item 27, (Refer to

Fig. A-FBJAA Sheet 03).

(e) If necessary, secure the nuts (installed on the fuselage) and the FIN 138HF and the

FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBJAA Sheet 03).

(17) Subtask 363038-831-012-001 - Modify the existing Harness 2SG.

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 10.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

16 NSA5527-03-01 1 SPACER

22 NSA5527-03-15 1 SPACER

131 NSA935808-03 20 WASHER

141 NSA5527-03-02 2 SPACER

150 NSA935807-04 4 CLAMP

151 NSA5159-17 1 STUD

152 NSA5527-03-08 1 SPACER

153 NSA935808-01 8 WASHER

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

157 NSA5159-10 1 STUD

158 NAS1801-3-9 3 SCREW

171 NAS1801-3-17 2 SCREW

172 NAS1149F0332P 2 WASHER

174 35301-74 1 CABLE

175 35301-75 1 CABLE

176 NSA5516-21ND 5 CLAMP

177 NSA5516-22ND 5 CLAMP

178 NSA5516-23ND 5 CLAMP

179 NSA5516-07ND 2 CLAMP

180 NSA5516-08ND 2 CLAMP

181 NSA5516-10ND 2 CLAMP

F9000095228595 BUNDLE

References

Elec. Std. Practices Manual (ESPM) 20-43-10

Service Bulletin (SB) A330-36-3032

Fig. A-FBMAA

Modification of the Existing Harness

2SG

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

Sheet 11

Sheet 12

Sheet 13

Sheet 14

Sheet 15

Sheet 16

Sheet 17

Sheet 18

Sheet 19

Fig. A-FWCAA

Installation of the Wiring of the New

Sensing Elements

Sheet 01

(a) Modify the supports of existing routing between 302HF located on the left hand side

at stringer 36 and Frame 40 and the 3520VP located on the right hand side at

Frame 39.1 :

NOTE: Apply the following modifications only if were not applied with

the embodiment of the Service Bulletin No. A330-36-3032 or the

associated Technical Adaptation.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame

39.2, remove :

a For Section A-A :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (152) Retain

1 Clamp Item (150) Retain

1 Stud Item (151) Retain

b For Section B-B :

6 Nut Item (154) Retain

6 Washer Item (153) Discard

6 Clamp Item (150) Retain

6 Spacer Item (152) Retain

6 Clamp Item (150) Retain

6 Stud Item (151) Retain

c For Section C-C :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (155) Discard

1 Spacer Item (152) Retain

1 Clamp Item (155) Discard

1 Stud Item (151) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame

39.2, install :

a For Section D-D :

1 Stud Item (151) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

b For Section E-E :

6 Stud Item (151) Retained at

removal

6 Clamp Item (150) Retained at

removal

6 Spacer Item (152) Retained at

removal

6 Clamp Item (150) Retained at

removal

6 Washer NSA935808-03 Item 131

6 Nut Item (154) Retained at

removal

c For Section F-F :

1 Stud Item (151) Retained at

removal

1 Clamp NSA935807-04 Item 150

1 Spacer Item (152) Retained at

removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 127

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1 Clamp NSA935807-04 Item 150

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09,

along the Frame 39.1 and between Stringer 39 and 40, remove :

a For Section G-G :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (155) Discard

1 Spacer Item (152) Retain

1 Clamp Item (150) Retain

1 Stud Item (151) Retain

b For Section H-H :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (155) Discard

1 Spacer Item (152) Retain

1 Clamp Item (155) Retain

1 Stud Item (151) Retain

4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09,

along the Frame 39.1 and between Stringer 39 and 40, install :

a For Section J-J :

1 Stud Item (151) Retained at

removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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1 Clamp Item (150) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp NSA935807-04 Item 150

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

b For Section K-K :

1 Stud Item (151) Retained at

removal

1 Clamp Item (155) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp NSA935807-04 Item 150

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between

Stringer 40 and 43, remove for detail F :

2 Nut Item (154) Retain

2 Washer Item (153) Discard

2 Clamp Item (150) Retain

2 Spacer Item (152) Retain

2 Clamp Item (135) Retain

2 Clamp Item (134) Retain

2 Stud Item (151) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 129

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SERVICE BULLETIN

6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between

Stringer 40 and 43, install for detail G :

2 Stud Item (151) Retained at

removal

2 Clamp Item (134) Retained at

removal

2 Clamp Item (135) Retained at

removal

2 Spacer Item (152) Retained at

removal

2 Clamp Item (150) Retained at

removal

2 Washer NSA935808-03 Item 131

2 Nut Item (154) Retained at

removal

7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the

Frame 39.1 and between Stringers 44 and 45, remove :

a For Section L-L :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Clamp Item (138) Retain

1 Spacer Item (152) Retain

1 Clamp Item (135) Retain

1 Clamp Item (134) Retain

1 Stud Item (151) Retain

b For Section M-M :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 130

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SERVICE BULLETIN

1 Clamp Item (150) Retain

1 Spacer Item (152) Retain

1 Clamp Item (135) Retain

1 Clamp Item (134) Retain

1 Stud Item (151) Retain

8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the

Frame 39.1 and between Stringers 44 and 45, install :

a For Section N-N :

1 Stud Item (151) Retained at

removal

1 Clamp Item (134) Retained at

removal

1 Clamp Item (135) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (138) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

b For Section P-P :

1 Stud Item (151) Retained at

removal

1 Clamp Item (134) Retained at

removal

1 Clamp Item (135) Retained at

removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 131

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SERVICE BULLETIN

1 Spacer Item (152) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the

Frame 39.1 and between Stringers 46 and 48, remove for section Q-Q :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (16) Discard

1 Clamp Item (139) Retain

1 Spacer Item (152) Retain

1 Clamp Item (135) Retain

1 Clamp Item (134) Retain

1 Stud Item (157) Discard

10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the

Frame 39.1 and between Stringers 46 and 48, install for Section R-R :

1 Stud NSA5159-17 Item 151

1 Clamp Item (134) Retained at

removal

1 Clamp Item (135) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (139) Retained at

removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 132

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SERVICE BULLETIN

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between

Stringers 49 and 52, remove for detail K :

2 Nut Item (154) Retain

2 Washer Item (153) Discard

2 Clamp Item (150) Retain

2 Spacer Item (152) Retain

2 Clamp Item (138) Retain

2 Stud Item (151) Retain

12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between

Stringers 49 and 52, install for detail L :

2 Stud Item (151) Retained at

removal

2 Clamp Item (138) Retained at

removal

2 Spacer Item (152) Retained at

removal

2 Clamp Item (150) Retained at

removal

2 Washer NSA935808-03 Item 131

2 Nut Item (154) Retained at

removal

13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between

Stringers 52 and 54, remove for Section S-S :

1 Nut Item (154) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 133

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SERVICE BULLETIN

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Clamp Item (138) Retain

1 Spacer Item (141) Retain

1 Clamp Item (138) Retain

1 Stud Item (140) Retain

14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between

Stringers 52 and 54, install for Section T-T :

1 Stud Item (140) Retained at

removal

1 Clamp Item (138) Retained at

removal

1 Spacer Item (141) Retained at

removal

1 Clamp Item (138) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

15 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the

Stringers 54, remove for detail N :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (152) Retain

1 Clamp Item (138) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 134

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SERVICE BULLETIN

1 Stud Item (151) Retain

16 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the

Stringers 54, install for detail P :

1 Stud Item (151) Retained at

removal

1 Clamp Item (138) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

17 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between

Stringers 54 and 48, remove for detail Q :

3 Screw Item (167) Discard

3 Washer Item (153) Discard

3 Clamp Item (138) Retain

3 Clamp Item (150) Retain

18 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between

Stringers 54 and 48, install for detail R :

3 Clamp Item (150) Retained at

removal

3 Clamp Item (138) Retained at

removal

3 Washer NSA935808-01 Item 153

3 Screw NAS1801-3-9 Item 158

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 135

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SERVICE BULLETIN

19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the

Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, remove :

a For Section U-U :

1 Nut Item (154) Discard

1 Washer Item (153) Discard

1 Clamp Item (135) Discard

1 Spacer Item (18) Discard

1 Clamp Item (134) Discard

1 Stud Item (151) Discard

b For Section V-V :

1 Screw Item (183) Discard

1 Washer Item (153) Discard

1 Clamp Item (184) Discard

1 Spacer Item (141) Discard

1 Clamp Item (184) Discard

20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the

Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for

Section W-W :

2 Spacer NSA5527-03-02 Item 141

2 Clamp NSA5516-07ND Item 179

or

2 Clamp NSA5516-08ND Item 180

or

2 Clamp NSA5516-10ND Item 181

and

2 Washer NAS1149F0332P Item 172

2 Screw NAS1801-3-17 Item 171

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 136

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@A330

SERVICE BULLETIN

NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND

or NSA5516-08ND or NSA5516-10ND.

21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 47 and 46, remove for detail Y :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (150) Retain

1 Spacer Item (165) Discard

1 Spacer Item (152) Retain

1 Clamp Item (155) Retain

1 Clamp Item (155) Retain

1 Stud Item (163) Retain

22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 47 and 46, install for detail Z :

1 Stud Item (163) Retained at

removal

1 Clamp Item (155) Retained at

removal

1 Clamp Item (155) Retained at

removal

1 Spacer Item (152) Retained at

removal

1 Spacer NSA5527-03-15 Item 22

1 Clamp Item (150) Retained at

removal

1 Washer NSA935808-03 Item 131

1 Nut Item (154) Retained at

removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 137

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SERVICE BULLETIN

23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 46 and 45, remove for detail W :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (135) Retain

1 Spacer Item (18) Discard

1 Clamp Item (134) Discard

1 Stud Item (151) Discard

24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame

39.2 and between Stringers 46 and 45, install for detail X:

1 Stud NSA5159-10 Item 157

1 Clamp NSA5516-21ND Item 176

or

1 Clamp NSA5516-22ND Item 177

or

1 Clamp NSA5516-23ND Item 178

and

1 Spacer NSA5527-03-01 Item 16

1 Spacer NSA5527-03-08 Item 152

1 Clamp Item (135) Retained at

removal

1 Washer NSA935808-01 Item 153

1 Nut Item (154) Retained at

removal

NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND

or NSA5516-22ND or NSA5516-23ND.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 138

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SERVICE BULLETIN

25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 44 and 43, remove for detail AA :

1 Nut Item (154) Retain

1 Washer Item (153) Discard

1 Clamp Item (135) Retain

1 Spacer Item (18) Retain

1 Clamp Item (134) Discard

1 Stud Item (151) Retain

26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 44 and 43, install for detail AB :

1 Stud Item (151) Retained at

removal

1 Clamp NSA5516-21ND Item 176

or

1 Clamp NSA5516-22ND Item 177

or

1 Clamp NSA5516-23ND Item 178

and

1 Spacer Item (18) Retained at

removal

1 Clamp Item (135) Retained at

removal

1 Washer NSA935808-01 Item 153

1 Nut Item (154) Retained at

removal

NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND

or NSA5516-22ND or NSA5516-23ND.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 139

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SERVICE BULLETIN

27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 42 and 38, remove for detail AC :

3 Screw Item (167) Retain

3 Washer Item (153) Discard

3 Clamp Item (135) Retain

3 Clamp Item (134) Discard

28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA

Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame

39.2 and between Stringers 42 and 38, install for detail AD :

3 Clamp NSA5516-21ND Item 176

or

3 Clamp NSA5516-22ND Item 177

or

3 Clamp NSA5516-23ND Item 178

and

3 Clamp Item (135) Retained at

removal

3 Washer NSA935808-01 Item 153

3 Screw Item (167) Retained at

removal

NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND

or NSA5516-22ND or NSA5516-23ND.

(b) Modify the existing route 2SG between FIN 302HF located on the left hand side at

stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment

:

NOTE: Apply the following modifications only if the Service Bulletin No.

A330-36-3032 and the associated Technical Adaptation were

applied. The following modification consists to restore the aircraft

to the configuration before Service Bulletin No. A330-36-3032 and

associated Technical Adaptation.

1 Modify the Interconnecting Electrical Wire FIN 301HF (Only if aircraft is

equipped with FIN 301HF PN 35301-75) :

Refer to ESPM 20-43-10

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 140

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SERVICE BULLETIN

a Before any disconnection, record the wires number associated to the FIN

301HF.

b Remove the splice FIN 3591VS between the FIN 301HF and the wire No.

3622-0540 :

FIN 3591VS

1 Splice Discard

NOTE: Retain the identification sleeves and the identification

label of the 3591VS and of the wires associated to the

FIN 301HF.

c Remove :

FIN 301HF

1 Cable-Electrical

Interconnecting

35301-75 Item (175) Discard

d Install :

1 Cable-Electrical

Interconnecting

35301-74 Item 174

e Install the new splice FIN 3591VS (PN NSA936809RG0002) between the

FIN 301HF and the wire No. 3622-0540, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3591VS with the identification

sleeves and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at

removal, identify the wires associated to the FINs 301HF

with the retained identification sleeves.

NOTE: After connection, Secure the FIN 301HF and FIN 302HF

with Wire-lock MS20995C41 item 133.

2 Modify the Interconnecting Electrical Wire FIN 22HF (If aircraft is equipped

with FIN 22HF PN 35301-74) :

a Before any disconnection, record the wires number associated to the FIN

22HF.

b Remove the splice FIN 3501VS between the FIN 22HF and the wire No.

3622-0082 :

FIN 3501VS

1 Splice Discard

NOTE: Retain the identification sleeves and the identification

label of the 3501VS and of the wires associated to the

FIN 22HF.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 141

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SERVICE BULLETIN

c Remove :

FIN 22HF

1 Cable-Electrical

Interconnecting

35301-74 Item (174) Discard

d Install :

1 Cable-Electrical

Interconnecting

35301-75 Item 175

e Install the new splice FIN 3501VS (PN NSA936809RG0002) between the

FIN 22HF and the wire No. 3622-0082, supplied in :

Bundle F9000095228595

NOTE: Identify the splice FIN 3501VS with the identification

sleeves and the identification label retained at removal.

NOTE: In accordance to the wires connections recorded at

removal, identify the wires associated to the FINs 22HF

with the retained identification sleeves.

NOTE: After connection, Secure the FIN 22HF and FIN 97HF

with Wire-lock MS20995C41 item 133.

(18) Subtask 363038-831-013-001 - Modify the Wiring between the Avionics

Compartment and the Cargo Compartment.

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095228595 BUNDLE

References

Service Bulletin (SB) A330-36-3032

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 142

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SERVICE BULLETIN

References

Fig. A-FBMAA

Modification of the Existing Harness

2SG

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

Sheet 11

Sheet 12

Sheet 13

Sheet 14

Sheet 15

Sheet 16

Sheet 17

Sheet 18

Sheet 19

Fig. A-FWBAA

Modification of the Wiring between the

Cargo Compartment and the Avionics

Compartment

Sheet 01

NOTE: Apply the following modifications only if were not applied with the

embodiment of the Service Bulletin No. A330-36-3032 or the associated

Technical Adaptation.

(a) Modify the connection of the wire No. 3622-0542 as shown on the wiring diagram,

Fig. A-FWBAA Sheet 01.

NOTE: If necessary use contact PN EN3155-003F2222 supplied in :

Bundle F9000095228595

(19) Subtask 363038-831-014-001 - Modify the Wiring in the Main rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Work location Electrical panel 800VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 143

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SERVICE BULLETIN

Material necessary to do the job

Kit 363038A02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

169 NSA935401-03 200 TIE

F9000095228595 BUNDLE

NSA935401-06 200 TIE

NSA935401-13 200 TIE

References

Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802

Task 36-11-34-400-802

Service Bulletin (SB) A330-36-3032

Fig. A-FWAAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Fig. A-FHAAA

Hook-Up Chart of the Modification of the

Wiring in the Main Rack 800VU

Sheet 01

NOTE: Apply the following modifications only if were not applied with the

embodiment of the Service Bulletin No. A330-36-3032 or the associated

Technical Adaptation.

(a) Remove and retain the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task

36-11-34-000-802).

(b) Remove the wire as shown on the wiring diagram Fig. A-FWAAA Sheet 01, and as

given in the Hook-up Chart line :

- 1 (Refer to Fig. A-FHAAA Sheet 01).

(c) Install the wires as shown on the wiring diagram Fig. A-FWAAA Sheet 01 and as

given in the Hook-up Chart lines :

- 4 thru 5 (Refer to Fig. A-FHAAA Sheet 01) supplied in :

Bundle F9000095228595

(d) Attach the wires with :

200 Tie-Cable NSA935401-03 Item 169

200 Tie-Cable NSA935401-06

200 Tie-Cable NSA935401-13

(e) Install the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 144

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SERVICE BULLETIN

(20) Subtask 363038-831-015-001 - If removed, install the ducts between FR39 and

FR40.

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

Fig. A-FBPAA

Removal/Installation of the Ducts

Between FR39 and FR40 for Access

Sheet 01

(a) Install :

Refer to Fig. A-FBPAA

(Refer to AMM Task 21-20-00-410-801)

1 Duct assy Item (125) Retained at

removal

1 Duct assy Item (126) Retained at

removal

1 Duct assy Item (127) Retained at

removal

(21) Subtask 363038-831-201-001 - Remove the sleeves from the Auxiliary Power Unit

(APU) bleed-air-duct

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 313AL, Door 312AR

Work location from Frame 83 to Frame 93

Manpower Resources

Manhours 1.25

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 145

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SERVICE BULLETIN

References

Fig. A-GBAAA

Removal of the Sleeves from the APU

Bleed-Air-Duct

Sheet 01

(a) Remove the sleeves from the APU bleed-air-duct in the rear fuselage section.

Refer to Fig. A-GBAAA Sheet 01.

1 Between Frame 83 and Frame 93 remove the sleeves:

1 Sleeve Assy F3617062402000 Item (200) Discard

1 Sleeve Assy F3617062402400 Item (201) Discard

1 Sleeve Assy F3617062402600 Item (202) Discard

1 Sleeve Assy F3617062402800 Item (203) Discard

1 Sleeve Assy F3617062403000 Item (204) Discard

(22) Subtask 363038-831-203-001 - Remove the clamps and the attaching parts from the

overheat sensing elements

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 83 to Frame 88

Manpower Resources

Manhours 1.25

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801

Fig. A-GBBAB

Removal of the Clamp and the Attaching

Parts from the Overheat Sensing

Elements

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamps and the attaching parts in the rear fuselage.

Refer to Fig. A-GBBAB Sheet 01 thru Fig. A-GBBAB Sheet 04.

Refer to AMM Task 36-22-17-000-801.

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1 Between Frame 83 and Frame 84, remove:

Refer to Fig. A-GBBAB Sheet 02, View B and Fig. A-GBBAB Sheet 04, View

F.

4 Sleeve-Protective NSA5539S Item (13) Discard

2 Clamp NSA5543-00 Item (10) Retain

with

2 Screw NAS1096-3-5 Item (205) Discard

2 Between Frame 84 and Frame 85, remove:

Refer to Fig. A-GBBAB Sheet 02, View C and Fig. A-GBBAB Sheet 04, View

F.

4 Sleeve-Protective NSA5539S Item (13) Discard

2 Clamp NSA5543-00 Item (10) Retain

with

2 Screw NAS1096-3-5 Item (205) Discard

3 Between Frame 85 and Frame 86, remove:

Refer to Fig. A-GBBAB Sheet 03, View D and Fig. A-GBBAB Sheet 04, View

F.

2 Sleeve-Protective NSA5539S Item (13) Discard

1 Clamp NSA5543-00 Item (10) Discard

with

1 Screw NAS1096-3-5 Item (205) Discard

4 Between Frame 86 and Frame 87, remove:

Refer to Fig. A-GBBAB Sheet 03, View E and Fig. A-GBBAB Sheet 04, View

F.

2 Sleeve-Protective NSA5539S Item (13) Discard

1 Clamp NSA5543-00 Item (10) Retain

with

1 Screw NAS1096-3-5 Item (205) Discard

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5 From the sensing elements clamp at Frame 88, remove:

Refer to Fig. A-GBBAB Sheet 01 and Fig. A-GBBAB Sheet 04, View G.

1 Screw NAS1096-3-5 Item (205) Discard

(23) Subtask 363038-831-204-001 - Remove the clamp from the overheat-detection dual

loops at Frame 80

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location Frame 80

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801

Fig. A-GBCAA

Removal of the Clamps and the

Attaching Parts from the OverheatDetection Dual Loops at Frame 80

Sheet 01

Sheet 02

(a) Remove the clamp from the sensing elements 32HF and 357HF.

Refer to Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02.

Refer to AMM Task 36-22-17-000-801.

1 From Frame 80, remove:

2 Sleeve-Protective NSA5539S Item (13) Discard

1 Clamp NSA5543-00 Item (10) Discard

with

1 Screw NAS1096-3-5 Item (205) Discard

(24) Subtask 363038-831-205-001 - Reroute the sensing elements 32HF and 357HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location Frame 80

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Kit 363038D12R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5539S 2 SLEEVE

16 NSA5527-03-01 1 SPACER

86 NSA5538-00 2 CLAMP

207 NAS1802-3-13 1 SCREW

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801

Fig. A-GBDAA

Rerouting of the Sensing Elements

32HF and 357HF and Installation of

Clamps

Sheet 01

Sheet 02

Fig. A-GBHAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

(a) Reroute the sensing elements 32HF and 357HF and install the clamps.

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02.

Refer to AMM Task 36-22-17-400-801.

1 Reroute the sensing elements 32HF and 357HF at Frame 80 from parallel

installation to on-top-of-each-other installation and install:

2 Sleeve-Protective NSA5539S Item 13

1 Spacer NSA5527-03-01 Item 16

2 Clamp NSA5538-00 Item 86

with

1 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(25) Subtask 363038-831-206-001 - Replace the clamp of the electrical harness

5866VB/2S in the rear fuselage

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 90 to Frame 91

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills AIRFRAME

Material necessary to do the job

Kit 363038D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

169 NSA935401-03 30 TIE

210 MS21919WCH14 1 CLAMP

211 F9237000207200 8 PLCRDSET

References

Fig. A-GBEAA

Replacement of the Clamp between

Frame 90 and Frame 91

Sheet 01

Sheet 02

Sheet 03

(a) Replace the clamp between Frame 90 and Frame 91.

Refer to Fig. A-GBEAA Sheet 01 thru Fig. A-GBEAA Sheet 03.

1 Between Frame 90 and Frame 91, STGR6RH, remove the clamp:

Refer to Fig. A-GBEAA Sheet 03, View C.

1 Clamp-Loop, Crs ABS0805-09 Item (214) Discard

2 Install the new clamp between Frame 90 and Frame 91, STGR6RH:

Refer to Fig. A-GBEAA Sheet 03, View D.

1 Clamp MS21919WCH14 Item 210

3 Install the Service Bulletin placards along the harness routing of 5866VB/2S:

8 Placard Set F9237000207200 Item 211

and

30 Tie-Cable NSA935401-03 Item 169

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(26) Subtask 363038-831-208-001 - Install the clamps and the new attaching parts on

the overheat sensing elements in the rear fuselage

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 83 to Frame 88

Manpower Resources

Manhours 1.25

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Kit 363038D11R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5539S 12 SLEEVE

16 NSA5527-03-01 4 SPACER

86 NSA5538-00 2 CLAMP

207 NAS1802-3-13 4 SCREW

208 NSA5527-03-04 3 SPACER

209 NAS1801-3-8 3 SCREW

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801

Fig. A-GBFAB

Installation of the Clamp and the

Attaching Parts in the Rear Fuselage

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GBHAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

(a) Install the clamps and the new attaching parts in the rear fuselage.

Refer to Fig. A-GBFAB Sheet 01 and Fig. A-GBFAB Sheet 05.

Refer to AMM Task 36-22-17-400-801.

1 Between Frame 83 and Frame 84, install:

Refer to Fig. A-GBFAB Sheet 02, Views B and C.

2 Clamp NSA5543-00 Item (10) Retained at

removal

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4 Sleeve-Protective NSA5539S Item 13

with

2 Spacer NSA5527-03-04 Item 208

2 Screw NAS1801-3-8 Item 209

NOTE: The torque value of the screw, Item 209, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

2 Between Frame 84 and Frame 85, install:

Refer to Fig. A-GBFAB Sheet 03 and Fig. A-GBFAB Sheet 04, View F.

2 Clamp NSA5543-00 Item (10) Retained at

removal

4 Sleeve-Protective NSA5539S Item 13

with

2 Spacer NSA5527-03-01 Item 16

2 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

3 Between Frame 85 and Frame 86, install:

Refer to Fig. A-GBFAB Sheet 05, Views G and H.

2 Sleeve-Protective NSA5539S Item 13

2 Clamp NSA5538-00 Item 86

with

1 Spacer NSA5527-03-01 Item 16

1 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

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SERVICE BULLETIN

wires, refer to Fig. A-GBHAA.

4 Between Frame 86 and Frame 87, install:

Refer to Fig. A-GBFAB Sheet 04, View E and F.

1 Clamp NSA5543-00 Item (10) Retained at

removal

2 Sleeve-Protective NSA5539S Item 13

with

1 Spacer NSA5527-03-01 Item 16

1 Screw NAS1802-3-13 Item 207

NOTE: The torque value of the screw, Item 207, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

5 On the sensing elements clamp at Frame 88, install:

Refer to Fig. A-GBFAB Sheet 01 and Fig. A-GBFAB Sheet 05, View J.

1 Spacer NSA5527-03-04 Item 208

1 Screw NAS1801-3-8 Item 209

NOTE: The torque value of the screw, Item 209, is 0.25m.daN

(22.00lbf.in).

NOTE: For tolerances for waviness and bends in sensing element

wires, refer to Fig. A-GBHAA.

(27) Subtask 363038-831-209-001 - Install the sleeves on the APU bleed-air-duct

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 313AL, Door 312AR

Work location from Frame 83 to Frame 94

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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Material necessary to do the job

Kit 363038D14R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5539S 6 SLEEVE

200 F3617062404000 1 SLEEVE

201 F3617062403800 1 SLEEVE

202 F3617062403600 1 SLEEVE

203 F3617062403400 1 SLEEVE

204 F3617062403200 1 SLEEVE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Adhesive Tape (Insulation

Blanket Repair)

08-073 As required

References

Fig. A-GBGAA

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

(a) Install the sleeves on the APU bleed-air-duct in the rear fuselage section.

Refer to Fig. A-GBGAA Sheet 01.

1 Install new sleeves on the sensing elements at Frame 83, Frame 88 and

Frame 91:

Refer to Fig. A-GBGAA Sheet 01, View B.

6 Sleeve-Protective NSA5539S Item 13

2 Between Frame 83 thru Frame 94, install the sleeves on the APU bleed-airduct and close them with adhesive strips:

1 Sleeve Assy F3617062404000 Item 200

1 Sleeve Assy F3617062403800 Item 201

1 Sleeve Assy F3617062403600 Item 202

1 Sleeve Assy F3617062403400 Item 203

1 Sleeve Assy F3617062403200 Item 204

with

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Adhesive Tape

(Insulation Blanket

Repair)

08-073 As required

NOTE: Make sure that the blowout apertures of the blankets are near

(under) the sensing elements.

NOTE: Make sure that there is no contact between the sensing

elements and the sleeves between Frame 86 and Frame 87.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 363038-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1, GEN 2, APU GEN,

- EXT A (B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(d) Remove the safety clips and tags and close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 363038-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 25-75-41-400-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Task 36-11-34-400-802

Task 36-12-00-710-801

Task 36-12-41-400-801

Task 36-22-00-710-806

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Preliminary Tests :

NOTE: If the aircraft is operated in actual CAT III conditions, you must

also do the LAND CAT III capability test (Refer to AMM Task

22-97-00-740-801).

1 On each connector which was disconnected :

- Do the checks as defined by ESPM 20-52-10.

NOTE: The Functional test and/or operational test requested by this

ESPM procedure is given hereafter.

2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to

AMM Task 33-13-00-710-801).

3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801).

4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer

to AMM Task 21-26-00-710-803).

5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM

Task 22-96-00-740-801).

6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring

(ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803).

7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to

AMM Task 31-60-00-710-802).

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(b) Test of the equipments :

1 If applicable, do the test procedure as specified after the installation

of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task

25-75-41-400-801).

2 If ducts removed, do the test procedure as specified after the installation of the

APU bleed air ducts (Refer to AMM Task 36-12-41-400-801).

3 If ducts removed, do the test procedure as specified after the installation of the

air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801).

4 Do the Operational Test of the APU bleed-air supply and crossbleed system

(Refer to AMM Task 36-12-00-710-801).

5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1

and 1HA2) (Refer to AMM Task 36-11-34-400-802).

(c) Test of the connectors :

1 Test of the connectors 3506VC and 3672VC :

a Do the Operational Test of the overheat detection system (Refer to AMM

Task 36-22-00-710-806).

2 Test of the Terminal Block 2901VT :

a None (Covered by the tests of the equipments)

(3) Subtask 363038-710-201-001 - Operational

Work Zones and Access Panels

Zone Access/Work location

210

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806

(a) Do the operational test of the overheat detection system (Refer to AMM Task

36-22-00-710-806).

**CONF 002

(1) Subtask 363038-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1, GEN 2, APU GEN,

- EXT A (B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(d) Remove the safety clips and tags and close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 363038-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 25-75-41-400-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Task 36-11-34-400-802

Task 36-12-00-710-801

Task 36-12-41-400-801

Task 36-22-00-710-806

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Preliminary Tests :

NOTE: If the aircraft is operated in actual CAT III conditions, you must

also do the LAND CAT III capability test (Refer to AMM Task

22-97-00-740-801).

1 On each connector which was disconnected :

- Do the checks as defined by ESPM 20-52-10.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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NOTE: The Functional test and/or operational test requested by this

ESPM procedure is given hereafter.

2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to

AMM Task 33-13-00-710-801).

3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801).

4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer

to AMM Task 21-26-00-710-803).

5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM

Task 22-96-00-740-801).

6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring

(ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803).

7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to

AMM Task 31-60-00-710-802).

(b) Test of the equipments :

1 If applicable, do the test procedure as specified after the installation

of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task

25-75-41-400-801).

2 If ducts removed, do the test procedure as specified after the installation of the

APU bleed air ducts (Refer to AMM Task 36-12-41-400-801).

3 If ducts removed, do the test procedure as specified after the installation of the

air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801).

4 Do the Operational Test of the APU bleed-air supply and crossbleed system

(Refer to AMM Task 36-12-00-710-801).

5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1

and 1HA2) (Refer to AMM Task 36-11-34-400-802).

(c) Test of the connectors :

1 Test of the connectors 3506VC and 3672VC :

a Do the Operational Test of the overheat detection system (Refer to AMM

Task 36-22-00-710-806).

2 Test of the Terminal Block 2901VT :

a None (Covered by the tests of the equipments)

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

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(3) Subtask 363038-710-201-001 - Operational

Work Zones and Access Panels

Zone Access/Work location

210

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806

(a) Do the operational test of the overheat detection system (Refer to AMM Task

36-22-00-710-806).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 363038-410-002-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 25-52-00-400-801

Task 25-53-00-400-801

Task 25-75-41-400-801

Task 53-00-00-400-802

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 53-35-13-400-802

(a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the

floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task

53-00-00-400-802).

(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to

AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).

(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to

AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).

(d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition

panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM

Task 25-52-00-400-801).

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(e) At Frame 20 in the FWD cargo-compartment, install the partition panels

131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-52-00-400-801).

(f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo

compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW

(Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).

(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC

and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-53-00-400-801).

(h) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW

(Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).

(i) On the LH side of the belly fairing, install (if removed) the panels 191HB,

191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to

AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task

53-35-13-400-802)

(j) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and

192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802).

(k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM

Task 25-75-41-400-801).

(2) Subtask 363038-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 32-12-00-410-801

Task 36-11-34-400-802

Task 36-22-17-400-801

Task 36-22-17-400-802

Task 52-10-00-410-801

52-30-00, Page Block 201

52-52-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door

822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block

201).

(c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 161

6

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@A330

SERVICE BULLETIN

(d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801).

(e) Do the close-up procedure as specified in the installation of the sensing elements

(Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802).

(f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1

and 1HA2) (Refer to AMM Task 36-11-34-400-802).

(g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801).

(h) Remove the access platform(s).

(i) Restore the systems and the aircraft to normal operating conditions.

(3) Subtask 363038-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 313AL, Door 312AR

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001

(a) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page

Block 001).

(b) Release and close the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(c) Remove the access platform(s).

**CONF 002

(1) Subtask 363038-410-002-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 25-52-00-400-801

Task 25-53-00-400-801

Task 25-75-41-400-801

Task 53-00-00-400-802

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 53-35-13-400-802

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 162

6

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@A330

SERVICE BULLETIN

(a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the

floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task

53-00-00-400-802).

(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to

AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).

(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to

AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).

(d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition

panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM

Task 25-52-00-400-801).

(e) At Frame 20 in the FWD cargo-compartment, install the partition panels

131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-52-00-400-801).

(f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo

compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW

(Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).

(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC

and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task

25-53-00-400-801).

(h) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW

(Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).

(i) On the LH side of the belly fairing, install (if removed) the panels 191HB,

191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to

AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task

53-35-13-400-802)

(j) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and

192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802).

(k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM

Task 25-75-41-400-801).

(2) Subtask 363038-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 163

6

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 32-12-00-410-801

Task 36-11-34-400-802

Task 36-22-17-400-801

Task 36-22-17-400-802

Task 52-10-00-410-801

52-30-00, Page Block 201

52-52-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door

822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block

201).

(c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801).

(e) Do the close-up procedure as specified in the installation of the sensing elements

(Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802).

(f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1

and 1HA2) (Refer to AMM Task 36-11-34-400-802).

(g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801).

(h) Remove the access platform(s).

(i) Restore the systems and the aircraft to normal operating conditions.

(3) Subtask 363038-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 313AL, Door 312AR

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001

(a) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page

Block 001).

(b) Release and close the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 164

6

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@A330

SERVICE BULLETIN

(c) Remove the access platform(s).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 165

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

B

A

FR39

FR45

FR53.5

FR56

(1)

(2)

97HF

98HF

(9)

(8)

25HF

24HF

(3)

(1)

99HF

100HF

(5)

(5) 102HF

101HF

(7) 23HF

Z190

AFTER

(1) A

(7)

(11)

(11)

(17)

(12)

(13)

(5)

(15)

G_SB_363038_5_BAAA_01_00

302HF

303HF

304HF

305HF

306HF

307HF

311HF

312HF

308HF

C

W

B B

Figure A-FBAAA - Sheet 01

Installation of the New Sensing Elements between FR39 and FR55, on the LH Side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 166

6

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@A330

SERVICE BULLETIN

**CONF ALL

BELLY FAIRING TRACE

FUSELAGE TRACE

G_SB_363038_5_BAAA_02_00

(11)

(1)

(1)

97HF

302HF

(2) 98HF

303HF

FR43

FR42

FR41

FR44

FR43

FR42

FR41

FR40.3

FR40.2

FR40

FR40.1

FR40.3

FR40.2

FR40.1

FR40

(45)

(45)

(24)

(29) (30)

(23)

(59)

(23) (29)

(45)

B

E

D

D

E

J

J

F

G

H

J

F

F

L

K

F

F

K

K K

(59)

K K

Figure A-FBAAA - Sheet 02

Installation of the New Sensing Elements between FR39 and FR55, on the LH Side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 167

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

FR51

FR50

FR49

FR48

FR47

FR46

FR45

FR47 FR48

FR46 FR45

BELLY FAIRING TRACE

FUSELAGE TRACE

(46)

(76)

(46)

(76)

(46)

(52)

(56) (56) (53)

(58)

(30) (31)

(32)

(26)

(59)

(25)

(31)

(45)

(45)

(45)

(32)

(26) (27)

(33)

(59)

G_SB_363038_5_BAAA_03_00

(12)

(3)

(13)

(1) 100HF

305HF

99HF

304HF

C

J

N

R

G

S

U J

F

T

H

F

M

J

V

V

J

S

J

J

M

N

P Q

41

R

K K

K K

H

Q

P

Figure A-FBAAA - Sheet 03

Installation of the New Sensing Elements between FR39 and FR55, on the LH Side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 168

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

G_SB_363038_5_BAAA_04_00

(5)

(5)

(5)

(15)

(7) (7)

23HF

308HF

307HF

102HF

101HF

306HF

FR53.6

FR53.5

FR53.4

FR53.3

FR53.2

FR53.1

FR53

FR52

FR51

FR53.5

FR53.4

FR53.3

FR53.2

FR53.1

FR53

FR52

FUSELAGE TRACE

BELLY FAIRING TRACE

(56)

(58)

(56) (46)

(76) (56)

(40)

(46)

(50)

(46)

(76)

(82)

(20) (35)

(45)

(45)

(59)

(34)

(20)

(35)

(45)

(45)

(59)

(45)

(27)

(33)

(45)

(34)

(28)

(59)

(28)

W

X

Y

Z A A

X

Y A A

Z F

K

J

J

F

H

J

F

F J

J

K K

K K

K

J

(53)

Figure A-FBAAA - Sheet 04

Installation of the New Sensing Elements between FR39 and FR55, on the LH Side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 169

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

55°

55°

FR53.6

FR53.5

(17)

(8)

(9)

(11)

(61)

(100)

(22) (100)

(37)

(45)

(45)

(36)

(21)

(59)

FR55

FR54

FR53.9

FR53.8

FR53.7

FR53.6

311HF

24HF

25HF

312HF

B

B

A

A

G_SB_363038_5_BAAA_05_00

B B

C C

D D A A

B B

C C

D D

E E

G G

F

F

J J

G G

J

F

J

F

F F

K K

H

H

Figure A-FBAAA - Sheet 05

Installation of the New Sensing Elements between FR39 and FR55, on the LH Side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 170

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

G_SB_363038_5_BAAA_06_00

(56)

(56)

(58)

(46)

(76)

(56)

(82)

(55)

(56)

(82)

(46)

(47)

(53)

(55)

(56)

(82)

(56)

(82)

(46)

(50)

(53)

(56)

(56)

(58)

(46)

(52)

(55)

(56)

(82)

(46)

(48)

(56)

(82)

(56)

(82)

(46)

(48)

(55)

(55) (46)

(48)

(56)

(82)

(56)

(82)

(46)

(50)

(55)

(53)

(56)

(82)

(55)

(46)

(48)

(56)

(82)

(46)

(50)

(55)

(53)

(54)

(55) (46)

(49)

(56)

(82)

F

G

H

J

K

L

V S

T U

Figure A-FBAAA - Sheet 06

Installation of the New Sensing Elements between FR39 and FR55, on the LH Side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 171

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

OR

(53)

(55)

(46)

(51)

(56)

(82)

(55)

(56)

(82)

(53)

(46)

(51)

(56)

(82)

(55)

(46)

(48)

(57)

(57)

(100)

(100) (100)

(57)

(57)

(56)

(82)

(56)

(82)

(55)

(46)

(48)

(53)

(56)

(56)

(58)

(46)

(77)

(46) (56)

(76)

(56)

(58)

(56)

(58) (46)

(76)

H H

E E

F F

G G

J J K K

G_SB_363038_5_BAAA_07_00

Figure A-FBAAA - Sheet 07

Installation of the New Sensing Elements between FR39 and FR55, on the LH Side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 172

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

B

(113)

(112)

(114)

FR53.5

FR53.6

A

Z150

B

G_SB_363038_5_BBAA_01_00

Figure A-FBBAA - Sheet 01

Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access)

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 173

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

Z150

FR53.3

FR54

FR53.5

FR53.6

96

C

B

FWD

B

A

STGR32

STGR33

STGR34

STGR36 STGR35

G_SB_363038_5_BCAA_01_00

Figure A-FBCAA - Sheet 01

Installation of a New Bracket between FR53.5 and FR53.6

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 174

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

FR53.5

197 mm

(7.75 in)

96

FR53.6

D

F

W

D

D

C

19.8 mm

(0.78 in)

ASNA2050DCJ3215 3.25 mm

(0.128 in)

3.35 mm

(0.132 in)

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

RIVET

VIEW LOOKING DOWN

STGR23

STGR33

STGR34

01 APPLY MAT. No. 09−005A TO THE INTERFACE

02 SEALANT BEAD WITH MAT No. 09−016B.

03 WET INSTALL THE FASTENERS WITH MAT. No. 09−005A.

NOTE:

OF THE NEW BRACKET AND THE STRUCTURE.

03

96

01

02

97

G_SB_363038_5_BCAA_02_00

Figure A-FBCAA - Sheet 02

Installation of a New Bracket between FR53.5 and FR53.6

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 175

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A Z190

FR47

FR44

FR40.2

(116)

(115)

A

B

B

G_SB_363038_5_BDAA_01_00

Figure A-FBDAA - Sheet 01

Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access)

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 176

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

B

A

FR56

FR53.5

A

FR45

FR39

101

102

113

100

303HF

98HF

302HF

97HF

Z190

G_SB_363038_5_BEAA_01_00

Figure A-FBEAA - Sheet 01

Installation of the New Sensing Elements between FR39 and FR44 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 177

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

FR44

FR43

FR42

FR41

FR40.3

FR40.2

FR40.1

FR40

FR40.2

FR40.3

FR41

FR42

FR43

FR40.1

FR40

BELLY FAIRING TRACE

FUSELAGE TRACE

114 97HF

101 303HF

113 302HF

102 98HF

L

J

C

G

E

30

11

TYPICAL

P

OR

15

27

15

27

27

15

15

B

Q

G_SB_363038_5_BEAA_02_00

Figure A-FBEAA - Sheet 02

Installation of the New Sensing Elements between FR39 and FR44 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 178

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

R

C C

C C

C C

H

D

B

B

P Q

P Q

FWD

FWD

C VIEW LOOKING AFT

C

C

C

C

C

B

B

FR39.2

FR40

C

D

113

114

302HF

F 97HF

E

13

14

20

10

10

13

14

20

14

20

13

14

16

21

10

14

20 13

14

20

10

78

F

33

32

35

34

30

32 33

30

G

H

FR40.2 FR40.1 FR40

G_SB_363038_5_BEAA_03_00

Figure A-FBEAA - Sheet 03

Installation of the New Sensing Elements between FR39 and FR44 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 179

6

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@A330

SERVICE BULLETIN

**CONF ALL

13

10

14

20

18

10

14 13

24

16

13

10

14

21

FR41

FR40.3

FR40.2

K

101 303HF

FWD

D

D

A

A

A

A

A

A

B

B

FR44 FR43 FR42

N

FWD

10 13

14

20

13

14

20

13 10

14

20

14

20

14

13 10

14

16

13

10

70

13 10

14

18

24

18

13

14

24

18

13

10

10

14

24

79

14

29

10

13 14

29

TYPICAL

R

S

N

K

J

L

A A B B C C

D D

10

S

A

A

A

A

A

A

A

A

A

A

102 98HF

21 20

G_SB_363038_5_BEAA_04_00

Figure A-FBEAA - Sheet 04

Installation of the New Sensing Elements between FR39 and FR44 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 180

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

B

Z190

FR56

FR53.5

FR39

AFTER

A

114

103 105

103

100HF

99HF 305HF

304HF

FR45

G_SB_363038_5_BFAA_01_00

Figure A-FBFAA - Sheet 01

Installation of the New Sensing Elements between FR44 and FR50 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 181

6

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@A330

SERVICE BULLETIN

**CONF ALL

FR48

FR47

FR46

FR45

FR51

FR50

FR49

FR48

FR47

FR46

FR45

N

L

F

C

H

K

FUSELAGE TRACE

BELLY FAIRING TRACE

100 100HF

105 305HF

103 99HF

30

11

TYPICAL

B S

OR

27

15

27 15

27

15

15

T

304HF 103

G_SB_363038_5_BFAA_02_00

Figure A-FBFAA - Sheet 02

Installation of the New Sensing Elements between FR44 and FR50 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 182

6

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@A330

SERVICE BULLETIN

**CONF ALL

39

38 36

37

39

38

40

41

C

C

E

E

C

C

E

E

Q

C

C

C

C

FR45

FR44

VIEW LOOKING FORWARD

FR46

VIEW LOOKING FORWARD VIEW LOOKING AFT

FWD

FWD

FWD

FWD

FWD

(2POS)

36

37

103

103

99HF

304HF

E

J

13 13 13 10 13

14

18

23

14

18

23

14

18

23 14

20

14

20

G

F

(2POS)

10

13

14

20

34

35

D E

J

H

D

C

S T

N

Q

Q

30 30

C

C

10 10

81

10

10

13

14

20

T

K

S T

G

C

C

G_SB_363038_5_BFAA_03_00

Figure A-FBFAA - Sheet 03

Installation of the New Sensing Elements between FR44 and FR50 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 183

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

FWD

L

P

R

Q R

TYPICAL

10 13

14

20

14

20

14

20

13 13 10 10

14

20

79

14

29

80

14

29 13

10

13

14

20

10

16

10

13

14

21 17

10

13

14

26

16

18

10

13

14

19

A A C C

E E G G

Q

105 305HP

100 100HP

G

G

A

A A

A

C

C

C

A C

A

A

A

A

A

FR50 FR47 FR48 FR49

P

G_SB_363038_5_BFAA_04_00

Figure A-FBFAA - Sheet 04

Installation of the New Sensing Elements between FR44 and FR50 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 184

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

B

Z190

FR56

FR53.5

FR45

FR39

AFTER

106

107

102HF

307HF

106

106

101HF

306HF

108

104

23HF

308HF

A

G_SB_363038_5_BGAA_01_00

Figure A-FBGAA - Sheet 01

Installation of the New Sensing Elements between FR50 and FR53.6 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 185

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

FR52

FR53

FR53.1

FR53.2

FR53.4

FR53.5

307HF

306HF

101HF

FUSELAGE TRACE

FR51

FR52

FR53

FR53.1

FR53.2

FR53.3

FR53.4

FR53.5

FR53.6

106

106

107 23HF 108

104 308HF

M

C OR

G

H

11

15

27

15

27

27

15

30

25

OR

TYPICAL

B X Y

FR53.3

BELLY FAIRING TRACE

106 102HF

15

G_SB_363038_5_BGAA_02_00

Figure A-FBGAA - Sheet 02

Installation of the New Sensing Elements between FR50 and FR53.6 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 186

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

J K

FR53.2 FR53.3 FR53.4

A

A A

A

D

A

A

F

FR51 FR52 FR53 FR53.1

C

C

C

C

C

C

14

20

14

20 14

20 70

10 10 13 13 10

K

72

10 13

14

16

21

10 13 10 10 13

14

20

75 14

16

21

14

16

21

10 13 10 13

E

82

F

14

20

14

16

21

14

20

10 13 10 13

14

20

14

16

21

74

J

14

16

21

14

20

10 13

10 13

83

73

14

20

L

13

A

A

A

A

A

A

FR53.2

FWD

C X Y

42

43

30

40

41

101HF 106

306HF 106

G

14

20

14

20

D

L

H

13

14

29

14

20

E

G_SB_363038_5_BGAA_03_00

Figure A-FBGAA - Sheet 03

Installation of the New Sensing Elements between FR50 and FR53.6 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 187

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

10 13

14

20

77

14

29

14

29

13 84 10

14

20

14

20

14

22

28

10

10 13

13

14

20

76

STGR36

STGR37

STGR38

STGR39

STGR40

STGR41

STGR42

STGR43

STGR44

STGR45

STGR46

STGR47

STGR48

STGR49

STGR50

FR53.5 FR53.6

C

C

C

C

C

C

T

FWD

N

43

42

45

44

30

X Y

R

S

T

C

C

C C

C

C

B

B

N

P

Q

R

C

C

T

107

106

307HF

102HF

104

108

308HF

23HF

VIEW LOOKING FORWARD

M

79

14

29

13

10

14

29

U

T

U

18

10

14 13

24

16

13

10

14

21

13

10

14

20

A A B B C C

P

Q

45

44

25

X

S

Y

G_SB_363038_5_BGAA_04_00

Figure A-FBGAA - Sheet 04

Installation of the New Sensing Elements between FR50 and FR53.6 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 188

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

B

A

FR56

FR53.5

FR45

FR39

AFTER

112

111

109

110

312HF

25HF

24HF

311HF

A

Z190

G_SB_363038_5_BHAA_01_00

Figure A-FBHAA - Sheet 01

Installation of the New Sensing Elements between FR53.6 and FR55 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 189

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

OR

27

15

27 15

27

15

30

11

P

J

C

24HF 109

312HF

TYPICAL

N

FUSELAGE TRACE

112

FR53.6

FR53.7

FR53.8

FR53.9

FR54

FR55

B

111 25HF

110 311HF

15

G_SB_363038_5_BHAA_02_00

Figure A-FBHAA - Sheet 02

Installation of the New Sensing Elements between FR53.6 and FR55 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 190

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

N F

89

30

91

90 88

FWD

H

27 J

J

10

14

20

13

14

20

93

10

14

20

13

F

14

29

79

13

10

14

29

G

FWD

D

D

H

13 H

14

20

86

D

VIEW LOOKING FORWARD

G

E

C

C

G

G

D

D

B B

B B

D D

B B

D

D E

112 312HF

111 25HF

24HF 108

110 311HF

C

FWD

FWD

92

27

85

J J

H H

55°

27

D

D

D

F

G_SB_363038_5_BHAA_03_00

E

E

D

D

B

B

D

D

H

A A

Figure A-FBHAA - Sheet 03

Installation of the New Sensing Elements between FR53.6 and FR55 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 191

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

FR53.9 FR55

K L

D FR54

D

D

D

14

16

94

14

20

14

20

10 10

13

14

16

94

13

95

13

10

14

16

94

10

14

16

94

14

16

94

13

13

10

J

K L

13

10

14

87

17

13

10

14

26

17

13

10

14

26

10

14

20 13

13

14

21

10

16

14

87

13

86

18 13

10

14

20

13

10

14

20 13

E E G G

D D

C C

B B

A A

18

70

G_SB_363038_5_BHAA_04_00

Figure A-FBHAA - Sheet 04

Installation of the New Sensing Elements between FR53.6 and FR55 on LH side

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 192

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

B

Z150

FR53.3

FR54

A

FR53.5

FR53.6

AFTER

B

C

D

G_SB_363038_5_BJAA_01_02

Figure A-FBJAA - Sheet 01

Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of

Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 193

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

169

169

(155)

1S 2SG

REPLACED SENSING

FWD

14

169

(155)

169

(175)

(175)

(175)

(174)

175

310HF

138HF

137HF

309HF 174

(14)

(18)

(168)

C

REPLACED SENSING

G_SB_363038_5_BJAA_02_02

27

3593VS

3503VS

27

Figure A-FBJAA - Sheet 02

Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of

Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 194

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

EXAMPLE OF INSTALLATION OF WIRE−LOCK PN MS20995C32 (ITEM )

D

27

G_SB_363038_5_BJAA_03_01

Figure A-FBJAA - Sheet 03

Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of

Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 195

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

Z190

B

FR44

A

98

99

C

A A

VIEW LOOKING FORWARD

B C

184.5 mm

(7.26 in)

G_SB_363038_5_BKAA_01_00

Figure A-FBKAA - Sheet 01

Installation of Two New Brackets at FR44

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 196

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

99

98

F

W

D

A A

ASNA2050DCJ3215 3.25 mm

(0.128 in)

3.35 mm

(0.132 in)

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

RIVET

01 APPLY MAT. No. 09−005A TO THE INTERFACE

02 SEALANT BEAD WITH MAT No. 09−016B.

03 WET INSTALL THE FASTENERS WITH MAT. No. 09−005A.

NOTE:

OF THE NEW BRACKET AND THE STRUCTURE.

03

01

02

01

02

109 mm

(4.29 in)

97

G_SB_363038_5_BKAA_02_00

Figure A-FBKAA - Sheet 02

Installation of Two New Brackets at FR44

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 197

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A Z192

B

FR39

FR40

A

(125)

(126)

(127) B

G_SB_363038_5_BPAA_01_00

Figure A-FBPAA - Sheet 01

Removal/Installation of the Ducts Between FR39 and FR40 for Access

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 198

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

Z190

3520VP EXISTING HARNESS 2SG

A

301HF

FR37

FR39.1

FR39.2

FR56

FR57

FR58

B C

G_SB_363038_5_BMAA_01_00

Figure A-FBMAA - Sheet 01

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 199

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

2HR 2M

1M 2S

2MK/2M1K

2SK/2S1K

2MK/2M1K

2S 2M

2SK/2S1K

1HR

1M

1M−2M

1M 2M

1SK/1S2K

1MK/1M2K

1M

1S

1S

1SK/1S2K

1M 1S

1MK/1M2K

FR38 FR39 FR39.1 FR39.2 FR40

STGR36

STGR38

STGR40

STGR42

STGR44

STGR46

STGR48

STGR50

STGR52

STGR54

STGR54

STGR52

STGR50

STGR48

STGR46

STGR44

STGR42

STGR40

STGR38

STGR36

A/C CL

BEFORE

FWD B

D 3501VS

H

J

M

N

K

1M

Q

W

Y

A A

A C

F

G_SB_363038_5_BMAA_02_00

U

Figure A-FBMAA - Sheet 02

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 200

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

2HR 2M

1M 2S

2MK/2M1K

2SK/2S1K

2MK/2M1K

2S 2M

2SK/2S1K

1HR

1M

1M

2SG

1M−2M

1M 2M

1SK/1S2K

1MK/1M2K

1M

1S

1S

2SG

1SK/1S2K

1M 1S

1MK/1M2K

NEW HARNESS

NEW HARNESS

NEW HARNESS

FR38 FR39 FR39.1 FR39.2 FR40

STGR36

STGR38

STGR40

STGR42

STGR44

STGR46

STGR48

STGR50

STGR52

STGR54

STGR54

STGR52

STGR50

STGR48

STGR46

STGR44

STGR42

STGR40

STGR38

STGR36

A/C CL

AFTER

FWD C

3501VS

3591VS

A B

A D

Z

X

V

P

A N

A M

A L

E

R

L

G

G_SB_363038_5_BMAA_03_00

Figure A-FBMAA - Sheet 03

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 201

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

2SG

1S

Y2390

Z−2250

VIEW LOOKING FORWARD

2SG

1S

FUSELAGE CONTOUR

BELLY−FAIRING AREA

BEFORE

FWD

FR39.1

STGR38

STGR39

STGR40

B

B

B

B

B

B

B B

B

B

B

B

G_SB_363038_5_BMAA_04_00

A E

A F

D

A A

A E

3501VS

3591VS

C

C

Figure A-FBMAA - Sheet 04

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 202

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

2SG

1S

Y2390

Z−2250

VIEW LOOKING FORWARD

2SG

1S

FUSELAGE CONTOUR

BELLY−FAIRING AREA

AFTER

FWD

3591VS

3501VS

E

FR39.1

STGR38

STGR39

STGR40

G_SB_363038_5_BMAA_05_00

A G

A H

A G

D D

E

E

E

E

E

E

E E

E

E

E

E

F

F

Figure A-FBMAA - Sheet 05

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 203

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

2SG

2SG

1S

BEFORE AFTER

(150)

(152)

131

(154)

(151)

131 (151)

(154)

FWD

(152)

(150)

(150)

G_SB_363038_5_BMAA_06_00

2SG

1S

(151) (153)

(154)

(152)

(150)

(150)

FWD

2SG

1S (150)

(152)

131

(154)

(151)

VIEW LOOKING FORWARD

VIEW LOOKING FORWARD

2SG

1S

(150)

(152)

(153)

(154)

(151)

2SG

1S

(155)

(152)

(153)

(154)

(151)

VIEW LOOKING FORWARD

VIEW LOOKING FORWARD

A A D D

1S

B B E E

C C F F

Figure A-FBMAA - Sheet 06

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 204

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

BEFORE

FWD

G_SB_363038_5_BMAA_07_00

2SG

A F

G

G

H

H

Figure A-FBMAA - Sheet 07

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 205

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

AFTER

FWD

2SG

G_SB_363038_5_BMAA_08_00

A H

K

K

J

J

Figure A-FBMAA - Sheet 08

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 206

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

1S

2SG

1S

2SG

1S

2SG

1M

BEFORE AFTER

(135) (134)

(152)

(150)

131

(154) (151)

BEFORE

AFTER

(150)

(152)

131

(154)

151

150

151

(155)

150

(152)

131

(154)

F G

FWD

FWD

FWD FWD

FWD

1S

2SG

1S

2SG

(150)

(152)

(153)

(154)

(151)

(155)

(151)

(155)

(152)

(153)

(154)

FWD G G H H

J J K K

1S

2SG

1M

(135) (134)

(152)

(150)

(153)

(154) (151)

G_SB_363038_5_BMAA_09_01

Figure A-FBMAA - Sheet 09

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 207

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

STGR45

1M

STGR45

1M

FR39.1

FR39.1

BEFORE

H AFTER

A L

FWD

FWD

G_SB_363038_5_BMAA_10_00

L L

M M

N N

P P

Figure A-FBMAA - Sheet 10

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 208

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

1S 1M

1M

2SG

BEFORE

AFTER

(151)

(134)

(152)

(150)

131

(154)

(135)

(138)

FWD

1S

1M

2SG

(134)

(152)

(150)

(151) (135)

131

(154)

G_SB_363038_5_BMAA_11_00

FWD

1S 1M

1M

2SG

(151)

(134)

(152)

(150)

(153)

(154)

(135)

(138)

FWD

1S

1M

2SG

(134)

(152)

(150)

(151) (135)

(153)

(154)

FWD

L L M M

N N P P

Figure A-FBMAA - Sheet 11

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 209

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

STGR49

STGR48

STGR47

FR39.1 FR39.2

STGR49

STGR48

STGR47

FR39.1 FR39.2

BEFORE

AFTER

J

A M

FWD

FWD

R R

Q Q

G_SB_363038_5_BMAA_12_00

Figure A-FBMAA - Sheet 12

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 210

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

1M

2SG

AFTER

FWD

FUSELAGE CONTOUR

(138)

(150)

(151)

(152)

131

(154)

FWD

BEFORE

G_SB_363038_5_BMAA_13_00

1M

2SG

BEFORE

FWD

FUSELAGE CONTOUR

(138)

(150)

(151)

(152)

(153)

(154)

2SG

1S 1M

1M

(135)

(139)

151

(134)

(152)

(150)

131

2SG

1S 1M

1M

(135)

(139)

(157)

(134)

(152)

(150)

(153)

AFTER

(154) (154)

FWD

Q Q R R

K L

(16)

Figure A-FBMAA - Sheet 13

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 211

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

1M

1M

2SG

STGR54 STGR54

BEFORE AFTER

FWD FWD

M

(140)

(141)

(150)

(138)

131

(154)

BEFORE AFTER

FWD FWD

A N

G_SB_363038_5_BMAA_14_00

S S T T

S S T T

1M

1M

2SG

(140)

(141)

(150)

(138)

(153)

(154)

Figure A-FBMAA - Sheet 14

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 212

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

2SG

1M

1M

2SG

BEFORE AFTER

(138)

(152)

(150)

(151)

131

(154)

(138) (150)

153

158

BEFORE AFTER

FWD FWD

FWD FWD

P

Q R

G_SB_363038_5_BMAA_15_00

2SG

1M

(138)

(152)

(150)

(151)

(153)

(154)

1M

2SG

(138) (150)

(153)

(167)

N

Figure A-FBMAA - Sheet 15

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 213

6

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@A330

SERVICE BULLETIN

**CONF ALL

AFTER

NOTE:

ONLY ONE CONFIGURATION SHOWN.

EQUIPMENT MAY DIFFER DEPENDING ON AIRCRAFT CONFIGURATION.

2S

2M

V

2S

2SG

BEFORE

STGR46

U U V V

V V

FWD

FWD

U

G_SB_363038_5_BMAA_16_02

W W 2SG

2SG

Figure A-FBMAA - Sheet 16

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 214

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

BEFORE

1S

141 179

171

172

FUSELAGE CONTOUR

2S 179

171

172

141

180

180

181

181

2M

FUSELAGE CONTOUR

2SG (134)

(135)

(151)

(18)

(153)

(154)

AFTER

G_SB_363038_5_BMAA_17_00

2S 1S

FUSELAGE CONTOUR

(153)

(183)

(141)

(184)

U U V V

W W

FWD FWD

2S

Figure A-FBMAA - Sheet 17

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 215

6

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@A330

SERVICE BULLETIN

**CONF ALL

2SK/2S1K

2M

FUSELAGE CONTOUR

2SG

2S

2SG

FUSELAGE CONTOUR

2MK/2M1K

BEFORE AFTER

(155) (155)

(152)

22

(163)

(150) 131

(154)

157

16

152

(135)

176

153

(154)

177

178

2SK/2S1K

2SG

FUSELAGE CONTOUR

2MK/2M1K

(155) (155)

(152)

(165)

(163)

(153) (150)

(154)

2M

FUSELAGE CONTOUR

2S

(151)

(18)

(135)

(134)

(153)

(154)

FWD FWD

FWD FWD

W X

Y Z

G_SB_363038_5_BMAA_18_01

Figure A-FBMAA - Sheet 18

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 216

6

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@A330

SERVICE BULLETIN

**CONF ALL

2M

FUSELAGE CONTOUR

(151)

(135)

153

(154)

FUSELAGE CONTOUR FUSELAGE CONTOUR

BEFORE AFTER

2SG

2S

176

(18)

2SG

2S

176

2M

153 (135)

(167)

A A A B

A C A D

FWD FWD

FWD FWD

177

177

178

178

G_SB_363038_5_BMAA_19_00

2S

2M

(135)

(134)

(153)

(167)

2S

2M

FUSELAGE CONTOUR

(151)

(135)

(153)

(154)

(134) (18)

Figure A-FBMAA - Sheet 19

Modification of the Existing Harness 2SG

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 217

6

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@A330

SERVICE BULLETIN

**CONF ALL

Figure A-FWCAA - Sheet 01

Installation of the Wiring of the New Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 218

6

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@A330

SERVICE BULLETIN

**CONF ALL

Figure A-FWBAA - Sheet 01

Modification of the Wiring between the Cargo Compartment and the Avionics Compartment

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 219

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 01

Modification of the Wiring in the Main Rack 800VU

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 220

6

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@A330

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 851VU 2901VT 65M 3612−0078 1M CF24 852VU 1HA2−AB 12A D

 2 851VU 2901VT 54T EN3155−016M2222 3612−0078 1M CF24 3000 120 852VU 1HA2−AB 12A E0170FA2200 (a) A

 3 851VU 2901VT 54X EN3155−016M2222 3612−0112 1M CF24 3000 120 852VU 1HA2−AA 11D E0170FA2200 (a) A

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE F9000095228595

 A = ADDED WIRE

 D = DELETED WIRE

Figure A-FHAAA - Sheet 01

Hook-Up Chart of the Modification of the Wiring in the Main Rack 800VU

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 221

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

Z310

FR80

FR83

FR86

FR88

FR91

FR93 FR95

A

(200)

(201)

(202)

(203)

(204)

A

G_SB_363038_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Removal of the Sleeves from the APU Bleed-Air-Duct

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 222

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 001

A

Z310

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

34HF

361HF

140HF

139HF

33HF

358HF

359HF

360HF

A

B

C

D

E

G

FR89

G_SB_363038_6_BBAA_01_01

Figure A-GBBAA - Sheet 01

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 223

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 001

G_SB_363038_6_BBAA_02_00

FWD

B

C

FR84

F

F

F

FR80

FR83

FR84

Figure A-GBBAA - Sheet 02

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 224

6

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@A330

SERVICE BULLETIN

**CONF 001

FR86 FWD

D

E

F

F

G_SB_363038_6_BBAA_03_00

FR85

Figure A-GBBAA - Sheet 03

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 225

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 001

TYPICAL

(10)

(205)

(13)

F

G_SB_363038_6_BBAA_04_00

G

(205)

Figure A-GBBAA - Sheet 04

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 226

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 002

A

Z310

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

34HF

361HF

140HF

139HF

33HF

358HF

359HF

360HF

A

B

C

D

E

G

FR89

G_SB_363038_6_BBAB_01_01

Figure A-GBBAB - Sheet 01

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 227

6

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@A330

SERVICE BULLETIN

**CONF 002

FWD

B

C

FR84

F

F

G_SB_363038_6_BBAB_02_00

F

F

FR80

FR83

FR84

Figure A-GBBAB - Sheet 02

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 228

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 002

G_SB_363038_6_BBAB_03_00

FR86 FWD

D

E

F

F FR85

Figure A-GBBAB - Sheet 03

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 229

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 002

TYPICAL

(10)

(205)

(13)

F

G

(205)

G_SB_363038_6_BBAB_04_00

Figure A-GBBAB - Sheet 04

Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 230

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

G_SB_363038_6_BCAA_01_00

A

Z310

Z170

FR73

FR77

32HF

31HF

30HF

FR83

355HF

356HF

357HF

A

B

FR73

Figure A-GBCAA - Sheet 01

Removal of the Clamps and the Attaching Parts from the Overheat-Detection Dual Loops at Frame 80

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 231

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

FWD

G_SB_363038_6_BCAA_02_00

FR80

B

C

(205)

(10)

(13)

(13)

C

Figure A-GBCAA - Sheet 02

Removal of the Clamps and the Attaching Parts from the Overheat-Detection Dual Loops at Frame 80

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 232

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

A

Z310

Z170

FR73

FR77

32HF

31HF

30HF

FR83

355HF

356HF

357HF

A

NOTE:

THE SENSING ELEMENTS MUST BE INSTALLED IN FRONT OF THE VENTILATION HOLES.

THE LENGTH COMPENSATION OF THE SENSING ELEMENTS MUST BE DONE AT

THE COUPLINGS OR RETAINER RINGS

B

FR73

G_SB_363038_6_BDAA_01_00

Figure A-GBDAA - Sheet 01

Rerouting of the Sensing Elements 32HF and 357HF and Installation of Clamps

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 233

6

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@A330

SERVICE BULLETIN

**CONF ALL

FWD

FR80

B

C

G_SB_363038_6_BDAA_02_00

C

01 TORQUE VALUE 0.25m.daN (22lbf.in)

NOTE:

16 13

13 207 86

86

01

Figure A-GBDAA - Sheet 02

Rerouting of the Sensing Elements 32HF and 357HF and Installation of Clamps

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 234

6

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@A330

SERVICE BULLETIN

**CONF ALL

G_SB_363038_6_BEAA_01_00

Z310

A

FR80

FR83

FR84

FR90

FR91

FR93

5866VB /2S

A

5208VP

5151VS

5215VC

5410VS

5866VB /2S

B

Figure A-GBEAA - Sheet 01

Replacement of the Clamp between Frame 90 and Frame 91

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 235

6

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@A330

SERVICE BULLETIN

**CONF ALL

5866VB /2S

G_SB_363038_6_BEAA_02_00

VIEW LOOKING UP

FWD

FR90 FR91

STGR6LH

STGR10LH

STGR6RH

STGR10RH

AD

B

E

C D

E

E

Figure A-GBEAA - Sheet 02

Replacement of the Clamp between Frame 90 and Frame 91

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 236

6

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@A330

SERVICE BULLETIN

**CONF ALL

TYPICAL PLACARD

INSTALLATION

211

SB 36−3038

G_SB_363038_6_BEAA_03_00

5215VC

5410VC

5866VB /2S

TO

TO

C

(214)

BEFORE

TO

TO

210

AFTER

D

169

E

5215VC

5866VB /2S

5410VC

Figure A-GBEAA - Sheet 03

Replacement of the Clamp between Frame 90 and Frame 91

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 237

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 001

A

Z310

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

34HF

361HF

140HF

139HF

33HF

358HF

359HF

360HF

A

B

E

D

G

J

FR89

G_SB_363038_6_BFAA_01_01

Figure A-GBFAA - Sheet 01

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 238

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 001

FWD

B

G_SB_363038_6_BFAA_02_00

C

13

(10)

13

208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in)

NOTE:

C

FR80

FR83

FR84

Figure A-GBFAA - Sheet 02

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 239

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 001

G_SB_363038_6_BFAA_03_00

FR84

D

MIN 50.8 mm

(2.00 in)

MAX 80.0 mm

(3.15 in)

12.7 mm

(0.49 in)

16.5 mm

(0.65 in)

A A

TYPICAL

A

A

A

A

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU

DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS

02

02

NOTE:

F

F

Figure A-GBFAA - Sheet 03

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 240

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 001

FR86

E

MIN 50.8 mm

(2.00 in)

MAX 80.0 mm

(3.15 in)

12.7 mm

(0.49 in)

16.5 mm

(0.65 in)

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU

DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS

02

G_SB_363038_6_BFAA_04_00

B

B

B B

TYPICAL

02

16

01 TORQUE VALUE 0.25m.daN (22lbf.in)

NOTE:

F

TYPICAL

F

B

B

13

(10)

13

207 01

Figure A-GBFAA - Sheet 04

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 241

6

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@A330

SERVICE BULLETIN

**CONF 001

FWD

FR85

208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in)

NOTE:

G_SB_363038_6_BFAA_05_00

G

H

13 86

86

207

13 16

01

H

J

Figure A-GBFAA - Sheet 05

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 242

6

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@A330

SERVICE BULLETIN

**CONF 002

A

Z310

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

34HF

361HF

140HF

139HF

33HF

358HF

359HF

360HF

A

B

E

D

G

J

FR89

G_SB_363038_6_BFAB_01_01

Figure A-GBFAB - Sheet 01

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 243

6

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@A330

SERVICE BULLETIN

**CONF 002

13

(10)

13

208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in)

NOTE:

C

G_SB_363038_6_BFAB_02_00

FWD

B

C

C

TYPICAL

FR80

FR84 FR83

Figure A-GBFAB - Sheet 02

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 244

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 002

FR84

D

MIN 50.8 mm

(2.00 in)

MAX 80.0 mm

(3.15 in)

12.7 mm

(0.49 in)

16.5 mm

(0.65 in)

A A

TYPICAL

A

A

A

A

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU

DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS

02

02

NOTE:

F

F

G_SB_363038_6_BFAB_03_00

Figure A-GBFAB - Sheet 03

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 245

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 002

FR86

E

MIN 50.8 mm

(2.00 in)

MAX 80.0 mm

(3.15 in)

12.7 mm

(0.49 in)

16.5 mm

(0.65 in)

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU

DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS

02

B

B

B B

TYPICAL

02

01 TORQUE VALUE 0.25m.daN (22lbf.in)

NOTE:

F

B

B

G_SB_363038_6_BFAB_04_00

16

F

TYPICAL

13

(10)

13

207 01

Figure A-GBFAB - Sheet 04

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 246

6

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@A330

SERVICE BULLETIN

**CONF 002

FWD

FR85

208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in)

NOTE:

G

H

13 86

86

207

13 16

01

H

J

G_SB_363038_6_BFAB_05_00

Figure A-GBFAB - Sheet 05

Installation of the Clamp and the Attaching Parts in the Rear Fuselage

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 247

6

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@A330

SERVICE BULLETIN

**CONF ALL

Z310

FR80

FR83

FR86

FR88

FR91

FR93 FR95

01

NOTE:

HOOK AND LOOP TAPE USED FOR CLOSING INSULATION SLEEVE

02 POSITION OF BLOWOUT APERTURE UNDER THE SENSING ELEMENT

01

02

01

02

01

02

A

200

201

202

203

204

A

01

02

01

02

13

B

TYPICAL

B

B

B

G_SB_363038_6_BGAA_01_02

Figure A-GBGAA - Sheet 01

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 248

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SERVICE BULLETIN

**CONF ALL

TOLERANCES FOR WAVINESS AND BEND IN WIRES

C

B

A E

C

E A

E

A

C

D

E

E

E

C

NOTE:

FOR DIMENSIONS, REFER TO SHEET 2

G_SB_363038_6_BHAA_01_01

C

C E

Figure A-GBHAA - Sheet 01

Tolerances for Waviness and Bends in Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 249

6

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@A330

SERVICE BULLETIN

**CONF ALL

mm

DIMENSIONS

(in)

C

D

E

B

A

9.52

MAX 6.4

MIN 12.7 MIN 0.50

MIN 25.4 MIN 1.00

MIN R 25.4 MIN R 1.00

MAX 0.25

0.38

E

01

NOTE:

USE OTHER HOLE OF BRACKET IF NECESSARY

02

01

02

ROTATE CLIP FOR SMOOTH ROUTING OF SENSING ELEMENT IF NECESSARY

F

E

F MAX 203.0 MAX 7.99

G_SB_363038_6_BHAA_02_01

E

E

01

02

Figure A-GBHAA - Sheet 02

Tolerances for Waviness and Bends in Sensing Elements

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 250

6

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@A330

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF ALL

For details concerning the elapsed time assumptions, refer to the Gantt chart shown in the next page:

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 1

6

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@A330

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 001

SB ELAPSED TIME

(HOURS)

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

STEPS

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

ARE NOT REFLECTED IN THIS GANTT CHART.

01

02

NOTES:

PER

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

20.75 4 5.75

4.00 4.00 1

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

MODIFY THE WIRING IN THE MAIN RACK 800VU

4.00 4.00 1

4.00 4.00 1

4.00 4.00 1

1.00 1.00 1

1.00 1.00 1

2.00 2.00 1

1.00 1.00 1

1.00 1.00 1

2.00 2.00 1

14.00 14.00 1

14.00 14.00 1

21.00 21.00 1

14.00 14.00 1

1.00 1.00 1

3.00 3.00 1

10.00 2 5.00

1.00 1.00 1

2.00 2.00 1

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR39 AND FR44

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR35.5 

AND FR35.6 FOR ACCESS

INSTALL A NEW SUPPORT FOR THE ROUTING OF THE 

SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6

IF REMOVED, INSTALL THE DUCTS BETWEEN FR53.5 

AND FR53.6

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR43 AND

FR45 FOR ACCESS

INSTALL THE NEW BRACKETS FOR THE ROUTING OF THE 

SENSING ELEMENTS AT FR44

IF REMOVED, INSTALL THE DUCTS BETWEEN FR43

AND FR45

BETWEEN FR39 AND FR44

MODIFY THE INTERCONNECTING ELECTRICAL WIRE

FIN 309HF AND 310HF, BETWEEN THE SENSING ELEMENTS

MODIFY THE EXISTING HARNESS 2SG

MODIFY THE WIRING BETWEEN THE AVIONICS 

COMPARTMENT AND THE CARGO COMPARTMENT

GET ACCESS 

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038

166.00

88.25

0 5 15 25 35 45 55 65 80 85 90 10 20 30 40 50 60 70 75

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR44 AND FR53.2

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR53.2 AND FR53.6

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR53.6 AND FR55

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR44 AND FR50

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR50 AND FR53.6

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR53.6 AND FR55

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR39 AND

FR40 FOR ACCESS

G_SB_363038_6_GAAA_01_00

Figure A-GGAAA - Sheet 01

Gantt Chart

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 001

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038

SB ELAPSED TIME

(HOURS)

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

166.00

88.25

STEPS

0 75

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

ARE NOT REFLECTED IN THIS GANTT CHART.

01

02

NOTES:

PER

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

2.00 2.00 1

1.25 0.75 2

1.00 0.50 2

0.25 0.25 1

1

1.50 1.50 1

1.00 0.50 2

1.50 0.75 2

4.00 4.00 1

28.50 4 7.50

5 15 25 35 45 55 65 80 85 90 10 20 30 40 50 60 70

REMOVE THE SLEEVES FROM THE AUXILIARY POWER UNIT 

(APU) BLEED−AIR−DUCT

REPLACE THE CLAMP OF THE ELECTRICAL HARNESS 

5866VB/2S IN THE REAR FUSELAGE

INSTALL THE CLAMP AND THE NEW ATTACHING PARTS ON

THE OVERHEAT SENSING ELEMENTS

INSTALL THE SLEEVES ON THE APU BLEED−AIR−DUCT

TEST

CLOSE−UP

REMOVE THE CLAMP AND THE ATTACHING PARTS FROM

THE OVERHEAT SENSING ELEMENTS

REMOVE THE CLAMP FROM THE OVERHEAT−DETECTION

DUAL LOOPS AT FRAME 80

REROUTE THE SENSING ELEMENTS 32HF AND 357HF

IF REMOVED, INSTALL THE DUCTS BETWEEN FR39 

AND FR40

0.25 0.25

G_SB_363038_6_GAAA_02_00

Figure A-GGAAA - Sheet 02

Gantt Chart

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 3

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 002

SB ELAPSED TIME

(HOURS)

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

STEPS

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

ARE NOT REFLECTED IN THIS GANTT CHART.

01

02

NOTES:

PER

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

20.75 4 5.75

4.00 4.00 1

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

MODIFY THE WIRING IN THE MAIN RACK 800VU

4.00 4.00 1

4.00 4.00 1

4.00 4.00 1

1.00 1.00 1

1.00 1.00 1

2.00 2.00 1

1.00 1.00 1

1.00 1.00 1

2.00 2.00 1

14.00 14.00 1

14.00 14.00 1

21.00 21.00 1

14.00 14.00 1

1.00 1.00 1

3.00 3.00 1

10.00 2 5.00

1.00 1.00 1

2.00 2.00 1

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR39 AND FR44

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR35.5 

AND FR35.6 FOR ACCESS

INSTALL A NEW SUPPORT FOR THE ROUTING OF THE 

SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6

IF REMOVED, INSTALL THE DUCTS BETWEEN FR53.5 

AND FR53.6

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR43 AND

FR45 FOR ACCESS

INSTALL THE NEW BRACKETS FOR THE ROUTING OF THE 

SENSING ELEMENTS AT FR44

IF REMOVED, INSTALL THE DUCTS BETWEEN FR43

AND FR45

BETWEEN FR39 AND FR44

MODIFY THE INTERCONNECTING ELECTRICAL WIRE

FIN 309HF AND 310HF, BETWEEN THE SENSING ELEMENTS

MODIFY THE EXISTING HARNESS 2SG

MODIFY THE WIRING BETWEEN THE AVIONICS 

COMPARTMENT AND THE CARGO COMPARTMENT

GET ACCESS 

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038

166.50

88.25

0 5 15 25 35 45 55 65 80 85 90 10 20 30 40 50 60 70 75

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR44 AND FR53.2

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR53.2 AND FR53.6

REMOVE THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR53.6 AND FR55

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR44 AND FR50

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR50 AND FR53.6

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS 

BETWEEN FR53.6 AND FR55

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR39 AND

FR40 FOR ACCESS

G_SB_363038_6_GAAB_01_00

Figure A-GGAAB - Sheet 01

Gantt Chart

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 4

6

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@A330

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 002

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038

STEPS MH ET/S

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

ARE NOT REFLECTED IN THIS GANTT CHART.

01

02

NOTES:

PER

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

2.00 2.00 1

1.25 0.75 2

1.25 0.75 2

0.25 0.25 1

1

1.50 1.50 1

1.25 0.75 2

1.50 0.75 2

4.00 4.00 1

28.50 4 7.50

REMOVE THE SLEEVES FROM THE AUXILIARY POWER UNIT 

(APU) BLEED−AIR−DUCT

REPLACE THE CLAMP OF THE ELECTRICAL HARNESS 

5866VB/2S IN THE REAR FUSELAGE

INSTALL THE CLAMPS AND THE NEW ATTACHING PARTS

ON THE OVERHEAT SENSING ELEMENTS

INSTALL THE SLEEVES ON THE APU BLEED−AIR−DUCT

TEST

CLOSE−UP

REMOVE THE CLAMPS AND THE ATTACHING PARTS FROM

THE OVERHEAT SENSING ELEMENTS

REMOVE THE CLAMP FROM THE OVERHEAT−DETECTION

DUAL LOOPS AT FRAME 80

REROUTE THE SENSING ELEMENTS 32HF AND 357HF

IF REMOVED, INSTALL THE DUCTS BETWEEN FR39 

AND FR40

0.25 0.25

G_SB_363038_6_GAAB_02_00

SB ELAPSED TIME

(HOURS)

TOTAL MANHOURS

SB ELAPSED TIME

166.00

88.25

0 5 15 25 35 45 55 65 80 85 90 10 20 30 40 50 60 70 75

Figure A-GGAAB - Sheet 02

Gantt Chart

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 5

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SERVICE BULLETIN

REPORTING SHEET

TITLE: PNEUMATIC - LEAK DETECTION - ADAPT DUAL LOOP AFTER FIRST

RETROFIT

MODIFICATION No.: 58530D46962

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: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 1

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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: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038

REVISION No.: 00 - Jan 16/12 Page: 1

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