@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 36

TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS

IN S19.

MODIFICATION No.: 202216C10899 202216C10898 202216C10846

This page transmits Revision No.01 of Service Bulletin No.A330-36-3040

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to correct the description of Service Bulletin Configurations 003 and 004.

CHANGES

The main changes of this revision are:

- Effectivity

. Note added to inform about the Airbus Mod. No. applied in production line for the same intent

as the Service Bulletin.

- Effectivity by Operator

. Operator update for some MSNs.

- Configuration definition

. The statement "Modification No. 49813D44055 is embodied" is replaced by "Modification No.

40019D16555 is embodied" for Configurations 003 and 004.

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 003 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 004 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Sep 18/12

REVISION No. : 01 - Nov 26/12

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 2

0

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 36

TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS

IN S19.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 202216C10899 202216C10898 202216C10846

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

A global review of the compliance of the JAR 25.0863 and SFAR88 has highlighted potential deviations

in specific cases. In particular, deviations have been found in Section 19, consequently, it has been

required to introduce several flexible thermal insulation muffs in the ducting of the APU Pneumatics

Distribution (Bleed) System. The goal is avoiding hot surfaces during APU Bleed operation.

Thermal Insulation Muffs will be installed on joint connections ducts and retainer rings of APU Bleed

System in rear fuselage zone thru frame 95. The Muffs have a venting hole to point-leaking hot air

directly towards the adjacent sensing elements of the Overheat Detection System (OHDS).

This Service Bulletin is issued to give the instructions to install Insulation Muffs and to modify the OHDS

sensing element installation.

The accomplishment of this Service Bulletin will minimize the possible ignition sources.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 1

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 363040D01R01 1 3,060.00 Sleeves

Kit 363040D04R00 1 1,880.00 Sensing element, sleeves, spacer, cable

ties, clamps and attaching parts

TOTAL 4,940.00

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 363040D02R00 1 3,440.00 Sleeves

Kit 363040D05R01 1 33.00 Sleeves and screw

TOTAL 3,473.00

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 363040D03R00 1 3,700.00 Sleeves

Kit 363040D05R01 1 33.00 Sleeves and screw

TOTAL 3,733.00

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 363040D02R00 1 3,440.00 Sleeves

Kit 363040D05R01 1 33.00 Sleeves and screw

TOTAL 3,473.00

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 2

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

SUMMARY

**CONF 005

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 363040D03R00 1 3,700.00 Sleeves

Kit 363040D05R01 1 33.00 Sleeves and screw

TOTAL 3,733.00

EFFECTIVITY

**CONF ALL

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

38W AAR ACA ACI AEA AFR ALK AZA BEL BER BMA BTV CAL

CPA CRL CSC CSN DAH DAL DGA DLH EDW EIN ETD EVA FWI

GFA GIA GRL HDA HFY HVN I2L IAC IWD IYE JAV JST KAL

KLM MAS MON MSR OHY PAL QAF QFA QTR RSY RYN SAI SAS

SWR TAM TAP TCX THA THY TSC UAE USA VKG VLK VOZ XAX

XLF

This modification is applicable by Service Bulletin only.

NOTE: The intent of this modification is achieved on MSN 0690 and subsequent through

modification Mod. No. 52260D44330.

NOTE: If Service Bulletin A330-36-3038 or Service Bulletin A330-36-3037 has been embodied

previously on aircraft, then Service Bulletin A330-36-3040 should be disregarded.

Service Bulletin No. A330-36-3038:

- Pneumatic - Leak Detection - Adapt Dual Loop After First Retrofit

Service Bulletin No. A330-36-3037:

- Pneumatic - Leak Detection - Introduce Adapted Dual Loop Overheat Leak On APU

Bleed Air Duct

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 3

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@A330

SERVICE BULLETIN

SUMMARY

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 363040-831-943-001: Modification

TOTAL MANHOURS 14.50

ELAPSED TIME (HOURS) 14.00

**CONF 002

Task 363040-831-943-001: Modification

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 003

Task 363040-831-943-001: Modification

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 004

Task 363040-831-943-001: Modification

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 005

Task 363040-831-943-001: Modification

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

APPENDICES

**CONF ALL

Appendix 01: Elapsed Time Assumptions

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 4

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@A330

SERVICE BULLETIN

SUMMARY

**CONF 001

Z310

A

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

FR98

FR100

A

INSULATION SLEEVES

AND SENSING ELEMENT

140HF

G_SB_363040_6_SAAA_01_03

Figure A-GSAAA - Sheet 01

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 5

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SERVICE BULLETIN

SUMMARY

**CONF 002 thru 005

Z310

A

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

FR98

FR100

A

INSULATION SLEEVES

AND SENSING ELEMENT

140HF

G_SB_363040_6_SAAB_01_03

Figure A-GSAAB - Sheet 01

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 6

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 36

TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS

IN S19.

MODIFICATION No.: 202216C10899 202216C10898 202216C10846

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.

NOTE: The intent of this modification is achieved on MSN 0690 and subsequent

through modification Mod. No. 52260D44330.

NOTE: If Service Bulletin A330-36-3038 or Service Bulletin A330-36-3037 has been

embodied previously on aircraft, then Service Bulletin A330-36-3040 should

be disregarded.

Service Bulletin No. A330-36-3038:

- Pneumatic - Leak Detection - Adapt Dual Loop After First Retrofit

Service Bulletin No. A330-36-3037:

- Pneumatic - Leak Detection - Introduce Adapted Dual Loop Overheat Leak

On APU Bleed Air Duct

(1) Models

330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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@A330

SERVICE BULLETIN

330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0069-0073 0077

0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116

0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211

0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256

0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288

0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320

0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353

0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386

0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423

0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458

0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487

0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522

0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558

0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588

0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618

0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650

0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688

(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

38W 0401

AAR 0640 0676

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0505 0526 0551 0597

AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657

ALK 0303 0306 0311 0313 0404 0456 0627

AZA 0272 0339

BEL 0030 0037 0045 0082 0095 0229 0249

BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665

BMA 0398

BTV 0205 0330

CAL 0602 0607 0641 0671 0675

CPA 0012 0017 0102 0113 0118 0121 0155 0386 0389 0393 0418 0420

0421 0423 0439 0539 0548 0565 0669 0673 0679

CRL 0285 0320

CSC 0462

CSN 0649 0652 0656 0664

DAH 0644 0647 0650 0653 0667

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 2

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@A330

SERVICE BULLETIN

OPERATOR MSN

DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674

DGA 0240

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687

EDW 0291

EIN 0269 0397

ETD 0658 0688

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678

FWI 0253

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HDA 0071 0083 0099 0106 0109 0234 0244 0405 0479 0512 0581 0654

0662

HFY 0096 0211 0262

HVN 0275 0294 0299 0366

I2L 0358 0364

IAC 0353 0362

IWD 0461 0670

IYE 0625 0632

JAV 0255

JST 0506 0508 0513 0522

KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0425 0428 0484 0490 0550

KLM 0682 0686

MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300

MON 0261 0265

MSR 0600 0610 0666 0683

OHY 0072 0087 0098 0143

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

QFA 0553 0558 0564 0574 0593 0595 0603

QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659

0680 0684

RSY 0171

RYN 0343

SAI 0055 0070

SAS 0496 0497 0515 0568

SWR 0324

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486

TAP 0181 0195 0223 0305 0308 0312 0317

TCX 0254 0266 0301

THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346

THY 0463 0504

TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

OPERATOR MSN

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382

0384 0392 0396 0409 0437 0451 0452 0455 0491 0494 0509 0518

0525 0536

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388

VKG 0309 0349 0356 0357

VLK 0086

VOZ 0365 0372

XAX 0054

XLF 0501 0635

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064

0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083

0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109

0110 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127

0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171

0172 0177 0183 0184 0188 0189 0191

001

0181 0195 0205 0211 0222 0223 0226 0229 0230 0232 0238

0240 0247 0248 0249 0250 0251 0253 0254 0255 0258 0259

0261 0262 0265 0266 0269 0271 0272 0275 0276 0281 0283

0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299

0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314

0316 0317 0320 0322 0324 0326 0328 0330 0334 0339 0340

0343 0345 0348 0353 0358 0361 0362 0364 0365 0366 0369

0372 0382 0384 0392 0396 0397 0398 0401 0403 0404 0409

0422 0427 0432 0437 0441 0443 0444 0448 0451 0452 0454

0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473

0476 0477 0480 0481 0486 0487 0489 0491 0493 0494 0498

0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510

0511 0513 0516 0518 0519 0521 0522 0525 0526 0527 0529

0530 0532 0535 0536 0551 0567 0584 0597 0627 0635 0657

004

0198 0200 0203 0206 0209 0219 0224 0231 0234 0241 0244

0256 0267 0277 0279 0284 0315 0323 0333 0337 0338 0342

0344 0346 0349 0350 0351 0356 0357 0368 0370 0375 0380

0386 0388 0389 0393 0400 0405 0407 0408 0412 0418 0419

0420 0421 0423 0425 0428 0439 0479 0484 0490 0496 0497

0512 0515 0539 0548 0550 0565 0568 0581

002

0524 0533 0542 0549 0552 0553 0558 0564 0570 0574 0576

0578 0579 0588 0591 0593 0595 0602 0603 0607 0623 0629

0636 0637 0640 0641 0642 0645 0648 0654 0659 0662 0663

0669 0670 0671 0673 0674 0675 0676 0679 0680 0687

005

0555 0571 0573 0587 0600 0605 0609 0610 0612 0614 0616

0618 0620 0621 0625 0631 0632 0633 0634 0638 0644 0647

0649 0650 0652 0653 0655 0656 0658 0661 0664 0665 0666

0667 0678 0682 0683 0684 0686 0688

003

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 4

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SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for A330-300 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is not embodied

- Modification No. 48980D42587 is not embodied

- Modification No. 40019D16555 is embodied

**CONF 002

Config. 002 is valid for A330-300 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is embodied

- Modification No. 48980D42587 is not embodied

- Modification No. 40019D16555 is embodied

**CONF 003

Config. 003 is valid for A330-200 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is embodied

- Modification No. 48980D42587 is embodied

- Modification No. 40019D16555 is embodied

**CONF 004

Config. 004 is valid for A330-200 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is embodied

- Modification No. 48980D42587 is not embodied

- Modification No. 40019D16555 is embodied

**CONF 005

Config. 005 is valid for A330-300 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is embodied

- Modification No. 48980D42587 is embodied

- Modification No. 40019D16555 is embodied

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 363040D01R01 1

Kit 363040D04R00 1

Consumable CMLD01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 363040D02R00 1

Kit 363040D05R01 1

Consumable CMLD01 1

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 5

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@A330

SERVICE BULLETIN

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 363040D03R00 1

Kit 363040D05R01 1

Consumable CMLD01 1

**CONF 004

MATERIAL QTY PER A/C SEE NOTES

Kit 363040D02R00 1

Kit 363040D05R01 1

Consumable CMLD01 1

**CONF 005

MATERIAL QTY PER A/C SEE NOTES

Kit 363040D03R00 1

Kit 363040D05R01 1

Consumable CMLD01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

A global review of the compliance of the JAR 25.0863 and SFAR88 has highlighted

potential deviations in specific cases. In particular, deviations have been found in

Section 19, consequently, it has been required to introduce several flexible thermal

insulation muffs in the ducting of the APU Pneumatics Distribution (Bleed) System. The

goal is avoiding hot surfaces during APU Bleed operation.

(2) Objective/Action

Thermal Insulation Muffs will be installed on joint connections ducts and retainer rings of

APU Bleed System in rear fuselage zone thru frame 95. The Muffs have a venting hole

to point-leaking hot air directly towards the adjacent sensing elements of the Overheat

Detection System (OHDS).

This Service Bulletin is issued to give the instructions to install Insulation Muffs and to

modify the OHDS sensing element installation.

(3) Advantages

The accomplishment of this Service Bulletin will minimize the possible ignition sources.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 6

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@A330

SERVICE BULLETIN

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 363040-831-943-001: Modification

(1) Remove the sensing element 140HF

(2) Install the insulation sleeves

(3) Install the new sensing element 140HF

**CONF 002

Task 363040-831-943-001: Modification

(1) Loosen the sensing element 140HF

(2) Install the insulation sleeves

(3) Reroute the sensing element 140HF

**CONF 003

Task 363040-831-943-001: Modification

(1) Loosen the sensing element 140HF

(2) Install the insulation sleeves

(3) Reroute the sensing element 140HF

**CONF 004

Task 363040-831-943-001: Modification

(1) Loosen the sensing element 140HF

(2) Install the insulation sleeves

(3) Reroute the sensing element 140HF

**CONF 005

Task 363040-831-943-001: Modification

(1) Loosen the sensing element 140HF

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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@A330

SERVICE BULLETIN

(2) Install the insulation sleeves

(3) Reroute the sensing element 140HF

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. The accomplishment timescale, which has not yet been

defined, will be given in the AD.

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.

**CONF 001

Task 363040-831-943-001: Modification

Get Access 0.75

On Aircraft

Remove the sensing element 140HF 4.50

Install the insulation sleeves 1.50

Install the new sensing element 140HF 6.25

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 14.50

ELAPSED TIME (HOURS) 14.00

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 8

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**CONF 002

Task 363040-831-943-001: Modification

Get Access 0.75

On Aircraft

Loosen the sensing element 140HF 2.00

Install the insulation sleeves 2.25

Reroute the sensing element 140HF 1.75

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 003

Task 363040-831-943-001: Modification

Get Access 0.75

On Aircraft

Loosen the sensing element 140HF 2.00

Install the insulation sleeves 2.25

Reroute the sensing element 140HF 1.75

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 004

Task 363040-831-943-001: Modification

Get Access 0.75

On Aircraft

Loosen the sensing element 140HF 2.00

Install the insulation sleeves 2.25

Reroute the sensing element 140HF 1.75

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 005

Task 363040-831-943-001: Modification

Get Access 0.75

On Aircraft

Loosen the sensing element 140HF 2.00

Install the insulation sleeves 2.25

Reroute the sensing element 140HF 1.75

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 9

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@A330

SERVICE BULLETIN

Task 363040-831-943-001: Modification

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**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 +1.736 KG (+3.8271 LB)

Effect on Balance +110.142 KGM (+796.657 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 +1.559 KG (+3.4369 LB)

Effect on Balance +99.068 KGM (+716.558 LB.FT )

**CONF 003

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 +1.503 KG (+3.3135 LB)

Effect on Balance +87.336 KGM (+631.701 LB.FT )

**CONF 004

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 +1.559 KG (+3.4369 LB)

Effect on Balance +90.579 KGM (+655.157 LB.FT )

**CONF 005

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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Manufacturers Empty Weight +1.503 KG (+3.3135 LB)

Effect on Balance +95.529 KGM (+690.961 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

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

12-34-24 36-22-00 36-22-17

52-41-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-05-01

Standards Manual (SM)

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 06-41-53

12-34-24 36-22-00 36-22-17

52-41-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 003

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

12-34-24 36-22-00 36-22-17

52-41-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 004

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

12-34-24 36-22-00 36-22-17

52-41-00

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Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 005

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

12-34-24 36-22-00 36-22-17

52-41-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 36-12-41 36-22-17

Illustrated Parts Catalog (IPC) 36-12-04 36-22-04

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 363040D01R01

Kit 363040D02R00

Kit 363040D03R00

Kit 363040D04R00

Kit 363040D05R01

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 363040D01R01

Cost 3,060.00 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. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

Kit 363040D02R00

Cost 3,440.00 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. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

Kit 363040D03R00

Cost 3,700.00 USD

Availability 150 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. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

Kit 363040D04R00

Cost 1,880.00 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. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

Kit 363040D05R01

Cost 33.00 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. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

B. INDUSTRY SUPPORT INFORMATION

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

C. LIST OF COMPONENTS

Kit 363040D01R01

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

NOTES

1 F3617062400000 1 SLEEVE

2 F3617062400200 1 SLEEVE

3 F3617062400400 1 SLEEVE

4 F3617062400600 1 SLEEVE

5 F3617062400800 1 SLEEVE

6 F3617062401000 1 SLEEVE

7 F3617062401800 1 SLEEVE

8 F3617062405200 1 SLEEVE

9 F3617062404200 1 SLEEVE

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SERVICE BULLETIN

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

NOTES

17 NSA5539S 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.

Kit 363040D02R00

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

NOTES

1 F3617062400000 1 SLEEVE

2 F3617062400200 1 SLEEVE

9 F3617062404200 1 SLEEVE

12 F3617062405000 1 SLEEVE

13 F3617062401600 1 SLEEVE

14 F3617062403800 1 SLEEVE

15 F3617062404800 1 SLEEVE

16 F3617062404400 1 SLEEVE

17 NSA5539S 3 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.

Kit 363040D03R00

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

NOTES

9 F3617062404200 1 SLEEVE

10 F3617062404600 1 SLEEVE

11 F3617062402200 1 SLEEVE

12 F3617062405000 1 SLEEVE

13 F3617062401600 1 SLEEVE

14 F3617062403800 1 SLEEVE

15 F3617062404800 1 SLEEVE

16 F3617062404400 1 SLEEVE

17 NSA5539S 4 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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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Kit 363040D04R00

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

NOTES

17 NSA5539S 22 SLEEVE

18 35660-2-310 1 ELEMENT

19 NSA935401-04 1 TIE

27 NSA5110-3-1 2 NUT

29 NAS1801-3-5 2 SCREW

31 NAS1149D0332K 3 WASHER

32 NSA5538-00 4 CLAMP

33 NSA5527-03-13 1 SPACER

34 NAS1801-3-28 1 SCREW

35 NAS1801-3-13 1 SCREW

36 NSA5527-03-08D 1 SPACER

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 363040D05R01

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

NOTES

17 NSA5539S 5 SLEEVE

35 NAS1801-3-13 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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

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

Lockwire Stainless Steel or Nickel

Alloy

19-018 As required

(2) Components

None

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 363040-831-943-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Zone

210 310

Modified FIN

313AL 312AR 34HF 139HF 140HF

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 14.50

ELAPSED TIME (HOURS) 14.00

**CONF 002

Zone

210 310

Modified FIN

313AL 312AR 140HF

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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**CONF 003

Zone

210 310

Modified FIN

313AL 312AR 140HF

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 004

Zone

210 310

Modified FIN

313AL 312AR 140HF

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF 005

Zone

210 310

Modified FIN

313AL 312AR 140HF

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 363040-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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SERVICE BULLETIN

References

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

06-31-53, 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-GBEAA

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 Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001).

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

001).

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

20-25-51).

(f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA).

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

easier.

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

(2) Subtask 363040-839-201-001 - 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 002

(1) Subtask 363040-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 21

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SERVICE BULLETIN

References

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

20-33-44

Fig. A-GBEAA

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 Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001).

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

001).

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

20-25-51).

(f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA).

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

easier.

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

(2) Subtask 363040-839-201-001 - 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 003

(1) Subtask 363040-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

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

20-33-44

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

References

Fig. A-GBEAA

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 Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001).

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

001).

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

20-25-51).

(f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA).

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

easier.

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

(2) Subtask 363040-839-201-001 - 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 004

(1) Subtask 363040-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

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

20-33-44

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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@A330

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(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 Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001).

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

001).

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

20-25-51).

(f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA).

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

easier.

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

(2) Subtask 363040-839-201-001 - 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 005

(1) Subtask 363040-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

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

20-33-44

Fig. A-GBEAA

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 Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001).

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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

001).

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

20-25-51).

(f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA).

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

easier.

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

(2) Subtask 363040-839-201-001 - 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 363040-941-201-001 - 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) Task 12-34-24-860-802

52-41-00, 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 below the access doors 312AR and 313AL.

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

Block 001).

(d) Open and safety the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(e) Set the light switch 4LJ in the ON position.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

**CONF 002

(1) Subtask 363040-941-201-001 - 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) Task 12-34-24-860-802

52-41-00, 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 below the access doors 312AR and 313AL.

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

Block 001).

(d) Open and safety the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(e) Set the light switch 4LJ in the ON position.

**CONF 003

(1) Subtask 363040-941-201-001 - 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) Task 12-34-24-860-802

52-41-00, 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 below the access doors 312AR and 313AL.

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

Block 001).

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

(d) Open and safety the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(e) Set the light switch 4LJ in the ON position.

**CONF 004

(1) Subtask 363040-941-201-001 - 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) Task 12-34-24-860-802

52-41-00, 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 below the access doors 312AR and 313AL.

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

Block 001).

(d) Open and safety the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(e) Set the light switch 4LJ in the ON position.

**CONF 005

(1) Subtask 363040-941-201-001 - 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) Task 12-34-24-860-802

52-41-00, 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 below the access doors 312AR and 313AL.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

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

Block 001).

(d) Open and safety the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(e) Set the light switch 4LJ in the ON position.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 363040-831-201-001 - Remove the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 313AL, Door 312AR

Work location from Frame 88 to Frame 93

Manpower Resources

Manhours 4.50

Minimum number of person 1

Subtask elapsed time 4.50

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) Task 36-22-17-000-802

Fig. A-GBBAA

Removal of the Sensing Element 140HF

from the APU Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) As a standard procedure clean the work areas if necessary, with:

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

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SERVICE BULLETIN

(b) Remove the sensing element 140HF from the APU bleed-air-duct.

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

Refer to AMM Task 36-22-17-000-802.

1 Between Frame 88 and Frame 89, cut and discard the lockwires and

disconnect the sensing element 140HF from the sensing element 139HF, refer

to Fig. A-GBBAA Sheet 04, View J and AMM Task 36-22-17-000-802.

2 At Frame 93, cut and discard the lockwires and disconnect the sensing

element 140HF from the connecting cable 34HF, refer to AMM Task

36-22-17-000-802.

Refer to Fig. A-GBBAA Sheet 03, View F.

Remove:

1 Nut NSA5542-00 Item (25) Retain

3 Between Frame 88 thru Frame 93, open the clamps:

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

H.

11 Clamp-single NAS5538-00 Item (26) Retain

and remove:

11 Sleeve-Protective NSA5539S Item (17) Discard

4 At Frame 93, remove:

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

G.

1 Sleeve-Protective NSA5539S Item (17) Discard

1 Spacer NSA5527-03-01 Item (24) Retain

1 Clamp-single NAS5538-00 Item (26) Retain

1 Screw NAS1096-3-13 Item (30) Discard

5 Between Frame 93 and Frame 94, remove:

Refer to Fig. A-GBBAA Sheet 02, View B and Fig. A-GBBAA Sheet 03, View

E.

2 Sleeve-Protective NSA5539S Item (17) Discard

1 Clamp-double NSA5543-00 Item (23) Discard

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1 Spacer NSA5527-03-01 Item (24) Retain

1 Washer NAS1149D0332K Item (28) Discard

1 Screw NAS1096-3-13 Item (30) Discard

6 Between Frame 94 and Frame 95, remove:

Refer to Fig. A-GBBAA Sheet 02, View B and Fig. A-GBBAA Sheet 03, Views

C and D.

4 Sleeve-Protective NSA5539S Item (17) Discard

2 Clamp-double NSA5543-00 Item (23) Retain

and

2 Sleeve-Protective NSA5539S Item (17) Discard

1 Clamp-double NSA5543-00 Item (23) Discard

1 Nut NSA5110-3-1 Item (27) Discard

1 Washer NAS1149D0332K Item (28) Discard

1 Screw NAS1096-3-5 Item (29) Discard

7 Between Frame 88 and Frame 95, remove the sensing element 140HF:

Refer to AMM Task 36-22-17-000-802.

Refer to Fig. A-GBBAA Sheet 01, View A and Fig. A-GBBAA Sheet 02, View

B.

FIN 140HF

1 Sensing Element 35636-2-310 Item (18) Discard

(2) Subtask 363040-831-202-001 - Install the insulation sleeves

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 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

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Material necessary to do the job

Kit 363040D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F3617062400000 1 SLEEVE

2 F3617062400200 1 SLEEVE

3 F3617062400400 1 SLEEVE

4 F3617062400600 1 SLEEVE

5 F3617062400800 1 SLEEVE

6 F3617062401000 1 SLEEVE

7 F3617062401800 1 SLEEVE

8 F3617062405200 1 SLEEVE

9 F3617062404200 1 SLEEVE

References

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

Task 36-22-17-400-801

Fig. A-GBCAA

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

(a) Install the insulation sleeves on the APU bleed-air duct.

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

1 Loosen the remaining sensing elements 139HF and 33HF between Frame 83

thru Frame 88, in preparation for the installation of the insulation sleeves, refer

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

2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU

bleed-air-duct:

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

1 Sleeve Assy F3617062400000 Item 1

1 Sleeve Assy F3617062400200 Item 2

1 Sleeve Assy F3617062400400 Item 3

1 Sleeve Assy F3617062400600 Item 4

1 Sleeve Assy F3617062400800 Item 5

1 Sleeve Assy F3617062401000 Item 6

1 Sleeve Assy F3617062401800 Item 7

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1 Sleeve Assy F3617062405200 Item 8

1 Sleeve Assy F3617062404200 Item 9

NOTE: Make sure that the sensing element goes across the blowout

apertures.

NOTE: Make sure that there is no contact between the sensing

element and the insulation sleeves.

3 Reinstall the remaining sensing elements between Frame 83 thru Frame 88,

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

(3) Subtask 363040-831-203-001 - Install the new sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 88 to Frame 95

Manpower Resources

Manhours 6.25

Minimum number of person 1

Subtask elapsed time 6.25

Skills ELECTRICAL

Material necessary to do the job

Kit 363040D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 1 SLEEVE

Kit 363040D04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 22 SLEEVE

18 35660-2-310 1 ELEMENT

19 NSA935401-04 1 TIE

27 NSA5110-3-1 2 NUT

29 NAS1801-3-5 2 SCREW

31 NAS1149D0332K 3 WASHER

32 NSA5538-00 4 CLAMP

33 NSA5527-03-13 1 SPACER

34 NAS1801-3-28 1 SCREW

35 NAS1801-3-13 1 SCREW

36 NSA5527-03-08D 1 SPACER

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainless Steel or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-05-01

Fig. A-GBDAA

Installation of the Sensing Element

140HF on the APU Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

Fig. A-GBCAA

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

NOTE: For tolerances for waviness and bends in sensing element wire, refer to

Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02.

(a) Install the sensing element 140HF on the APU bleed-air-duct.

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

Refer to AMM Task 36-22-17-400-802.

1 Between Frame 88 thru Frame 95, put the sensing element 140HF in position:

Refer to Fig. A-GBDAA Sheet 02, View B.

FIN 140HF

1 ElementSensing,Overheat35660-2-310 Item 18

2 Between Frame 88 thru Frame 93, install:

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

K.

11 Sleeve-Protective NSA5539S Item 17

and close:

11 Clamp-single NAS5538-00 Item (26) Retained at

removal

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3 Install a new protective sleeve on the sensing element at Frame 91:

Refer to Fig. A-GBCAA Sheet 03, View J.

1 Sleeve-Protective NSA5539S Item 17

4 At Frame 93, install:

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

J.

1 Sleeve-Protective NSA5539S Item 17

1 Spacer NSA5527-03-01 Item (24) Retained at

removal

1 Clamp-single NAS5538-00 Item (26) Retained at

removal

1 Screw NAS1801-3-13 Item 35

5 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in).

6 Between Frame 93 and Frame 94, loosely install:

Refer to Fig. A-GBDAA Sheet 02, View B and Fig. A-GBDAA Sheet 03, View

G.

2 Sleeve-Protective NSA5539S Item 17

1 Spacer NSA5527-03-01 Item (24) Retained at

removal

1 Washer NAS1149D0332K Item 31

2 Clamp NSA5538-00 Item 32

1 Spacer NSA5527-03-13 Item 33

1 Screw NAS1801-3-28 Item 34

7 Hand tighten the screw, Item 34, then after you have installed the

sensing element 140HF, torque tighten the screw, Item 34, to 0.40m.daN

(35.403lbf.in).

8 Between Frame 94 and Frame 95, loosely install:

Refer to Fig. A-GBDAA Sheet 02, View B and Fig. A-GBDAA Sheet 03, Views

C, D and F.

4 Sleeve-Protective NSA5539S Item 17

and close:

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2 Clamp-double NSA5543-00 Item (23) Retained at

removal

and

2 Sleeve-Protective NSA5539S Item 17

2 Nut NSA5110-3-1 Item 27

2 Screw NAS1801-3-5 Item 29

2 Washer NAS1149D0332K Item 31

2 Clamp NSA5538-00 Item 32

NOTE: The clamps, Item 32, must be installed with the given angle,

refer to Fig. A-GBDAA Sheet 03, View C.

9 Torque tighten the screws, Item 29, to 0.40m.daN (35.403lbf.in).

10 Between Frame 88 and Frame 95, install the sensing element 140HF.

a STEP 1:

Refer to Fig. A-GBDAA Sheet 02, Fig. A-GBDAA Sheet 04 and Fig. AGBDAA Sheet 05.

<1> At Frame 93, connect the sensing element 140HF, Item 18, to

the coupling of the sensing element 34HF, refer to AMM Task

36-22-17-400-802 with:

Refer to Fig. A-GBDAA Sheet 04, View H.

1 Nut NSA5542-00 Item (25) Retained at

removal

<2> Torque tighten the nut, Item (25), to 0.25m.daN (22.13lbf.in).

<3> Safety the couplings of the sensing elements and the nut, Item (25),

with lockwire, refer to Process and Material Specification (PMS)

01-05-01:

Lockwire Stainless

Steel or Nickel Alloy

19-018 As required

b STEP 2:

Refer to Fig. A-GBDAA Sheet 05.

<1> Route the sensing element 140HF, Item 18, to the next clamp at the

position of STEP 2.

NOTE: For tolerances for waviness and bends in sensing

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element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: Make sure that the sensing element goes across the

blowout apertures.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

c STEP 3 thru STEP 11:

Refer to Fig. A-GBDAA Sheet 05.

<1> Install the sensing element 140HF, follow the installation position

sequence STEP 3 thru STEP 11.

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: Make sure that the sensing element goes across the

blowout apertures.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

<2> Between Frame 94 and Frame 95, install on the sensing element:

Refer to Fig. A-GBDAA Sheet 03, View E.

2 Sleeve-Protective NSA5539S Item 17

1 Tie-Cable NSA935401-04 Item 19

1 Spacer NSA5527-03-08D Item 36

d STEP 12 thru STEP 22:

Refer to Fig. A-GBDAA Sheet 05.

<1> Install the sensing element 140HF, follow the installation position

sequence STEP 12 thru STEP 22.

Adjust the over-all length of the sensing element 140HF with two

360 degree loops between the brackets at Frame 89 and at Frame

92.

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

<2> Between Frame 88 and Frame 89, connect the sensing element

140HF, Item 18, with the sensing element 139HF, refer to Fig. AGBDAA Sheet 04, View L.

<3> Safety the sensing element couplings with lockwire, refer to Process

and Material Specification (PMS) 01-05-01:

Lockwire Stainless

Steel or Nickel Alloy

19-018 As required

**CONF 002

(1) Subtask 363040-831-201-002 - Loosen the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 93

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

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) Task 36-22-17-000-802

Fig. A-GBBAB

Removal of the Sensing Element 140HF

from the APU Bleed-Air-Duct

Sheet 01

Sheet 02

(a) As a standard procedure clean the work areas if necessary, with:

Solvent General

Purpose

11-026 As required

and

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

Lint-Free Cotton

Cloth

19-003 As required

(b) Loosen the sensing element 140HF from the APU bleed-air-duct.

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

Refer to AMM Task 36-22-17-000-802.

1 Between Frame 91 thru Frame 93, open the clamps:

Refer to Fig. A-GBBAB Sheet 02, View E.

4 Clamp-single NAS5538-00 Item (26) Retain

and remove:

4 Sleeve-Protective NSA5539S Item (17) Discard

2 At Frame 93, remove:

Refer to Fig. A-GBBAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item (17) Discard

1 Spacer NSA5527-03-01 Item (24) Retain

1 Clamp-single NAS5538-00 Item (26) Retain

with

1 Screw NAS1096-3-13 Item (30) Discard

3 Between Frame 93 and Frame 94, open the upper part of the double clamp

and remove:

Refer to Fig. A-GBBAB Sheet 02, View C.

1 Sleeve-Protective NSA5539S Item (17) Discard

4 Between Frame 91 thru Frame 94, remove the sensing element from the

opened clamps:

Refer to AMM Task 36-22-17-000-802.

Refer to Fig. A-GBBAB Sheet 02, View B.

1 Sensing Element

140HF

Item (36) Retain

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

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SERVICE BULLETIN

(2) Subtask 363040-831-202-002 - Install the insulation sleeves

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 83 to Frame 94

Manpower Resources

Manhours 2.25

Minimum number of person 1

Subtask elapsed time 2.25

Skills NON SPECIFIC

Material necessary to do the job

Kit 363040D02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F3617062400000 1 SLEEVE

2 F3617062400200 1 SLEEVE

9 F3617062404200 1 SLEEVE

12 F3617062405000 1 SLEEVE

13 F3617062401600 1 SLEEVE

14 F3617062403800 1 SLEEVE

15 F3617062404800 1 SLEEVE

16 F3617062404400 1 SLEEVE

17 NSA5539S 3 SLEEVE

References

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

Task 36-22-17-400-801

Fig. A-GBCAB

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

(a) Install the insulation sleeves on the APU bleed-air duct.

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

1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame

94, in preparation for the installation of the insulation sleeves, refer to AMM

Task 36-22-17-000-801.

2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU

bleed-air-duct:

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

1 Sleeve Assy F3617062400000 Item 1

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 39

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

1 Sleeve Assy F3617062400200 Item 2

1 Sleeve Assy F3617062404200 Item 9

1 Sleeve Assy F3617062405000 Item 12

1 Sleeve Assy F3617062401600 Item 13

1 Sleeve Assy F3617062404800 Item 15

1 Sleeve Assy F3617062404400 Item 16

NOTE: Make sure that the sensing element goes across the blowout

apertures.

NOTE: Make sure that there is no contact between the sensing

element and the insulation sleeves.

3 Install the insulation sleeve between Frame 86 and Frame 87.

Refer to Fig. A-GBCAB Sheet 03, View F.

a For the installation of the insulation sleeve, Item 14, open the detection

clips and lift the sensing element from the brackets.

b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the

brackets and install:

1 Sleeve Assy F3617062403800 Item 14

c Reinstall the sensing element.

4 Install new protective sleeves on the sensing elements between Frame 84 and

Frame 85, at Frame 88, and at Frame 91:

Refer to Fig. A-GBCAB Sheet 02, View D, and Fig. A-GBCAB Sheet 03,

Views G and H.

3 Sleeve-Protective NSA5539S Item 17

5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the

sensing element 140HF (Refer to AMM Task 36-22-17-400-801).

(3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 94

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 40

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SERVICE BULLETIN

Manpower Resources

Manhours 1.75

Minimum number of person 1

Subtask elapsed time 1.75

Skills ELECTRICAL

Material necessary to do the job

Kit 363040D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 5 SLEEVE

35 NAS1801-3-13 1 SCREW

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802

Fig. A-GBDAB

Rerouting of the Sensing Element

140HF on the APU Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

NOTE: For tolerances for waviness and bends in sensing element wire, refer to

Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02.

(a) Reroute the sensing element 140HF on the APU bleed-air duct and install the

clamps.

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

Refer to AMM Task 36-22-17-400-802.

1 Between Frame 90 and Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View E.

4 Sleeve-Protective NSA5539S Item 17

and close:

4 Clamp-single NAS5538-00 Item (26) Retained at

removal

2 At Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item 17

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 41

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SERVICE BULLETIN

1 Spacer NSA5527-03-01 Item (24) Retained at

removal

1 Clamp-single NAS5538-00 Item (26) Retained at

removal

with

1 Screw NAS1801-3-13 Item 35

3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in).

4 Between Frame 93 and Frame 94, close the upper part of the double clamp

without the sensing element 140HF.

Refer to Fig. A-GBDAB Sheet 02, View C.

NOTE: Only the lower part of the clamp stays in use.

5 Between Frame 90 thru 94, reroute the sensing element 140HF.

a STEP 1 thru STEP 2:

Refer to Fig. A-GBDAB Sheet 03.

<1> From Frame 94 to Frame 93, route the sensing element 140HF

straight from the clamp at STEP 1 to the next clamp at STEP 2.

1 Sensing Element

140HF

Item (36) Retained at

removal

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

b STEP 3 thru STEP 6

Refer to Fig. A-GBDAB Sheet 03.

<1> Install the sensing element 140HF by following the installation

position sequence STEP 3 thru STEP 6.

NOTE: Make sure that the sensing element wire is routed

with an acceptable distance to the insulation sleeve

at STEP 6.

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 42

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@A330

SERVICE BULLETIN

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

**CONF 003

(1) Subtask 363040-831-201-002 - Loosen the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 93

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

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) Task 36-22-17-000-802

Fig. A-GBBAB

Removal of the Sensing Element 140HF

from the APU Bleed-Air-Duct

Sheet 01

Sheet 02

(a) As a standard procedure clean the work areas if necessary, with:

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Loosen the sensing element 140HF from the APU bleed-air-duct.

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 43

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Refer to AMM Task 36-22-17-000-802.

1 Between Frame 91 thru Frame 93, open the clamps:

Refer to Fig. A-GBBAB Sheet 02, View E.

4 Clamp-single NAS5538-00 Item (26) Retain

and remove:

4 Sleeve-Protective NSA5539S Item (17) Discard

2 At Frame 93, remove:

Refer to Fig. A-GBBAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item (17) Discard

1 Spacer NSA5527-03-01 Item (24) Retain

1 Clamp-single NAS5538-00 Item (26) Retain

with

1 Screw NAS1096-3-13 Item (30) Discard

3 Between Frame 93 and Frame 94, open the upper part of the double clamp

and remove:

Refer to Fig. A-GBBAB Sheet 02, View C.

1 Sleeve-Protective NSA5539S Item (17) Discard

4 Between Frame 91 thru Frame 94, remove the sensing element from the

opened clamps:

Refer to AMM Task 36-22-17-000-802.

Refer to Fig. A-GBBAB Sheet 02, View B.

1 Sensing Element

140HF

Item (36) Retain

(2) Subtask 363040-831-202-003 - Install the insulation sleeves

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 83 to Frame 94

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 44

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

Manpower Resources

Manhours 2.25

Minimum number of person 1

Subtask elapsed time 2.25

Skills NON SPECIFIC

Material necessary to do the job

Kit 363040D03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

9 F3617062404200 1 SLEEVE

10 F3617062404600 1 SLEEVE

11 F3617062402200 1 SLEEVE

12 F3617062405000 1 SLEEVE

13 F3617062401600 1 SLEEVE

14 F3617062403800 1 SLEEVE

15 F3617062404800 1 SLEEVE

16 F3617062404400 1 SLEEVE

17 NSA5539S 4 SLEEVE

References

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

Task 36-22-17-400-801

Fig. A-GBCAC

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

(a) Install the insulation sleeves on the APU bleed-air duct.

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

1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame

94, in preparation for the installation of the insulation sleeves, refer to AMM

Task 36-22-17-000-801.

2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU

bleed-air-duct:

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

1 Sleeve Assy F3617062404200 Item 9

1 Sleeve Assy F3617062404600 Item 10

1 Sleeve Assy F3617062402200 Item 11

1 Sleeve Assy F3617062405000 Item 12

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 45

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

1 Sleeve Assy F3617062401600 Item 13

1 Sleeve Assy F3617062404800 Item 15

1 Sleeve Assy F3617062404400 Item 16

NOTE: Make sure that the sensing element goes across the blowout

apertures.

NOTE: Make sure that there is no contact between the sensing

element and the insulation sleeves.

3 Install the insulation sleeve between Frame 86 and Frame 87.

Refer to Fig. A-GBCAC Sheet 03, View F.

a For the installation of the insulation sleeve, Item 14, open the detection

clips and lift the sensing element from the brackets.

b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the

brackets and install:

1 Sleeve Assy F3617062403800 Item 14

c Reinstall the sensing element.

4 Install new protective sleeves on the sensing elements at Frame 83, between

Frame 84 and Frame 85, at Frame 88, and at Frame 91:

Refer to Fig. A-GBCAC Sheet 02, Views B and D, and Fig. A-GBCAC Sheet

03, Views G and H.

4 Sleeve-Protective NSA5539S Item 17

5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the

sensing element 140HF (Refer to AMM Task 36-22-17-400-801).

(3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 94

Manpower Resources

Manhours 1.75

Minimum number of person 1

Subtask elapsed time 1.75

Skills ELECTRICAL

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 46

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

Material necessary to do the job

Kit 363040D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 5 SLEEVE

35 NAS1801-3-13 1 SCREW

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802

Fig. A-GBDAB

Rerouting of the Sensing Element

140HF on the APU Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

NOTE: For tolerances for waviness and bends in sensing element wire, refer to

Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02.

(a) Reroute the sensing element 140HF on the APU bleed-air duct and install the

clamps.

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

Refer to AMM Task 36-22-17-400-802.

1 Between Frame 90 and Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View E.

4 Sleeve-Protective NSA5539S Item 17

and close:

4 Clamp-single NAS5538-00 Item (26) Retained at

removal

2 At Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item 17

1 Spacer NSA5527-03-01 Item (24) Retained at

removal

1 Clamp-single NAS5538-00 Item (26) Retained at

removal

with

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 47

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

1 Screw NAS1801-3-13 Item 35

3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in).

4 Between Frame 93 and Frame 94, close the upper part of the double clamp

without the sensing element 140HF.

Refer to Fig. A-GBDAB Sheet 02, View C.

NOTE: Only the lower part of the clamp stays in use.

5 Between Frame 90 thru 94, reroute the sensing element 140HF.

a STEP 1 thru STEP 2:

Refer to Fig. A-GBDAB Sheet 03.

<1> From Frame 94 to Frame 93, route the sensing element 140HF

straight from the clamp at STEP 1 to the next clamp at STEP 2.

1 Sensing Element

140HF

Item (36) Retained at

removal

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

b STEP 3 thru STEP 6

Refer to Fig. A-GBDAB Sheet 03.

<1> Install the sensing element 140HF by following the installation

position sequence STEP 3 thru STEP 6.

NOTE: Make sure that the sensing element wire is routed

with an acceptable distance to the insulation sleeve

at STEP 6.

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 48

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SERVICE BULLETIN

**CONF 004

(1) Subtask 363040-831-201-002 - Loosen the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 93

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

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) Task 36-22-17-000-802

Fig. A-GBBAB

Removal of the Sensing Element 140HF

from the APU Bleed-Air-Duct

Sheet 01

Sheet 02

(a) As a standard procedure clean the work areas if necessary, with:

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Loosen the sensing element 140HF from the APU bleed-air-duct.

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

Refer to AMM Task 36-22-17-000-802.

1 Between Frame 91 thru Frame 93, open the clamps:

Refer to Fig. A-GBBAB Sheet 02, View E.

4 Clamp-single NAS5538-00 Item (26) Retain

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 49

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

and remove:

4 Sleeve-Protective NSA5539S Item (17) Discard

2 At Frame 93, remove:

Refer to Fig. A-GBBAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item (17) Discard

1 Spacer NSA5527-03-01 Item (24) Retain

1 Clamp-single NAS5538-00 Item (26) Retain

with

1 Screw NAS1096-3-13 Item (30) Discard

3 Between Frame 93 and Frame 94, open the upper part of the double clamp

and remove:

Refer to Fig. A-GBBAB Sheet 02, View C.

1 Sleeve-Protective NSA5539S Item (17) Discard

4 Between Frame 91 thru Frame 94, remove the sensing element from the

opened clamps:

Refer to AMM Task 36-22-17-000-802.

Refer to Fig. A-GBBAB Sheet 02, View B.

1 Sensing Element

140HF

Item (36) Retain

(2) Subtask 363040-831-202-002 - Install the insulation sleeves

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 83 to Frame 94

Manpower Resources

Manhours 2.25

Minimum number of person 1

Subtask elapsed time 2.25

Skills NON SPECIFIC

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 50

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Material necessary to do the job

Kit 363040D02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F3617062400000 1 SLEEVE

2 F3617062400200 1 SLEEVE

9 F3617062404200 1 SLEEVE

12 F3617062405000 1 SLEEVE

13 F3617062401600 1 SLEEVE

14 F3617062403800 1 SLEEVE

15 F3617062404800 1 SLEEVE

16 F3617062404400 1 SLEEVE

17 NSA5539S 3 SLEEVE

References

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

Task 36-22-17-400-801

Fig. A-GBCAB

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

(a) Install the insulation sleeves on the APU bleed-air duct.

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

1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame

94, in preparation for the installation of the insulation sleeves, refer to AMM

Task 36-22-17-000-801.

2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU

bleed-air-duct:

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

1 Sleeve Assy F3617062400000 Item 1

1 Sleeve Assy F3617062400200 Item 2

1 Sleeve Assy F3617062404200 Item 9

1 Sleeve Assy F3617062405000 Item 12

1 Sleeve Assy F3617062401600 Item 13

1 Sleeve Assy F3617062404800 Item 15

1 Sleeve Assy F3617062404400 Item 16

NOTE: Make sure that the sensing element goes across the blowout

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 51

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

apertures.

NOTE: Make sure that there is no contact between the sensing

element and the insulation sleeves.

3 Install the insulation sleeve between Frame 86 and Frame 87.

Refer to Fig. A-GBCAB Sheet 03, View F.

a For the installation of the insulation sleeve, Item 14, open the detection

clips and lift the sensing element from the brackets.

b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the

brackets and install:

1 Sleeve Assy F3617062403800 Item 14

c Reinstall the sensing element.

4 Install new protective sleeves on the sensing elements between Frame 84 and

Frame 85, at Frame 88, and at Frame 91:

Refer to Fig. A-GBCAB Sheet 02, View D, and Fig. A-GBCAB Sheet 03,

Views G and H.

3 Sleeve-Protective NSA5539S Item 17

5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the

sensing element 140HF (Refer to AMM Task 36-22-17-400-801).

(3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 94

Manpower Resources

Manhours 1.75

Minimum number of person 1

Subtask elapsed time 1.75

Skills ELECTRICAL

Material necessary to do the job

Kit 363040D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 5 SLEEVE

35 NAS1801-3-13 1 SCREW

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 52

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802

Fig. A-GBDAB

Rerouting of the Sensing Element

140HF on the APU Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

NOTE: For tolerances for waviness and bends in sensing element wire, refer to

Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02.

(a) Reroute the sensing element 140HF on the APU bleed-air duct and install the

clamps.

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

Refer to AMM Task 36-22-17-400-802.

1 Between Frame 90 and Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View E.

4 Sleeve-Protective NSA5539S Item 17

and close:

4 Clamp-single NAS5538-00 Item (26) Retained at

removal

2 At Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item 17

1 Spacer NSA5527-03-01 Item (24) Retained at

removal

1 Clamp-single NAS5538-00 Item (26) Retained at

removal

with

1 Screw NAS1801-3-13 Item 35

3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in).

4 Between Frame 93 and Frame 94, close the upper part of the double clamp

without the sensing element 140HF.

Refer to Fig. A-GBDAB Sheet 02, View C.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 53

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@A330

SERVICE BULLETIN

NOTE: Only the lower part of the clamp stays in use.

5 Between Frame 90 thru 94, reroute the sensing element 140HF.

a STEP 1 thru STEP 2:

Refer to Fig. A-GBDAB Sheet 03.

<1> From Frame 94 to Frame 93, route the sensing element 140HF

straight from the clamp at STEP 1 to the next clamp at STEP 2.

1 Sensing Element

140HF

Item (36) Retained at

removal

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

b STEP 3 thru STEP 6

Refer to Fig. A-GBDAB Sheet 03.

<1> Install the sensing element 140HF by following the installation

position sequence STEP 3 thru STEP 6.

NOTE: Make sure that the sensing element wire is routed

with an acceptable distance to the insulation sleeve

at STEP 6.

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

**CONF 005

(1) Subtask 363040-831-201-002 - Loosen the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 93

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 54

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

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) Task 36-22-17-000-802

Fig. A-GBBAB

Removal of the Sensing Element 140HF

from the APU Bleed-Air-Duct

Sheet 01

Sheet 02

(a) As a standard procedure clean the work areas if necessary, with:

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Loosen the sensing element 140HF from the APU bleed-air-duct.

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

Refer to AMM Task 36-22-17-000-802.

1 Between Frame 91 thru Frame 93, open the clamps:

Refer to Fig. A-GBBAB Sheet 02, View E.

4 Clamp-single NAS5538-00 Item (26) Retain

and remove:

4 Sleeve-Protective NSA5539S Item (17) Discard

2 At Frame 93, remove:

Refer to Fig. A-GBBAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item (17) Discard

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 55

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SERVICE BULLETIN

1 Spacer NSA5527-03-01 Item (24) Retain

1 Clamp-single NAS5538-00 Item (26) Retain

with

1 Screw NAS1096-3-13 Item (30) Discard

3 Between Frame 93 and Frame 94, open the upper part of the double clamp

and remove:

Refer to Fig. A-GBBAB Sheet 02, View C.

1 Sleeve-Protective NSA5539S Item (17) Discard

4 Between Frame 91 thru Frame 94, remove the sensing element from the

opened clamps:

Refer to AMM Task 36-22-17-000-802.

Refer to Fig. A-GBBAB Sheet 02, View B.

1 Sensing Element

140HF

Item (36) Retain

(2) Subtask 363040-831-202-003 - Install the insulation sleeves

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 83 to Frame 94

Manpower Resources

Manhours 2.25

Minimum number of person 1

Subtask elapsed time 2.25

Skills NON SPECIFIC

Material necessary to do the job

Kit 363040D03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

9 F3617062404200 1 SLEEVE

10 F3617062404600 1 SLEEVE

11 F3617062402200 1 SLEEVE

12 F3617062405000 1 SLEEVE

13 F3617062401600 1 SLEEVE

14 F3617062403800 1 SLEEVE

15 F3617062404800 1 SLEEVE

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 56

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

16 F3617062404400 1 SLEEVE

17 NSA5539S 4 SLEEVE

References

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

Task 36-22-17-400-801

Fig. A-GBCAC

Installation of the Sleeves on the APU

Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

(a) Install the insulation sleeves on the APU bleed-air duct.

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

1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame

94, in preparation for the installation of the insulation sleeves, refer to AMM

Task 36-22-17-000-801.

2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU

bleed-air-duct:

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

1 Sleeve Assy F3617062404200 Item 9

1 Sleeve Assy F3617062404600 Item 10

1 Sleeve Assy F3617062402200 Item 11

1 Sleeve Assy F3617062405000 Item 12

1 Sleeve Assy F3617062401600 Item 13

1 Sleeve Assy F3617062404800 Item 15

1 Sleeve Assy F3617062404400 Item 16

NOTE: Make sure that the sensing element goes across the blowout

apertures.

NOTE: Make sure that there is no contact between the sensing

element and the insulation sleeves.

3 Install the insulation sleeve between Frame 86 and Frame 87.

Refer to Fig. A-GBCAC Sheet 03, View F.

a For the installation of the insulation sleeve, Item 14, open the detection

clips and lift the sensing element from the brackets.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 57

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SERVICE BULLETIN

b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the

brackets and install:

1 Sleeve Assy F3617062403800 Item 14

c Reinstall the sensing element.

4 Install new protective sleeves on the sensing elements at Frame 83, between

Frame 84 and Frame 85, at Frame 88, and at Frame 91:

Refer to Fig. A-GBCAC Sheet 02, Views B and D, and Fig. A-GBCAC Sheet

03, Views G and H.

4 Sleeve-Protective NSA5539S Item 17

5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the

sensing element 140HF (Refer to AMM Task 36-22-17-400-801).

(3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR, Door 313AL

Work location from Frame 90 to Frame 94

Manpower Resources

Manhours 1.75

Minimum number of person 1

Subtask elapsed time 1.75

Skills ELECTRICAL

Material necessary to do the job

Kit 363040D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 5 SLEEVE

35 NAS1801-3-13 1 SCREW

References

Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802

Fig. A-GBDAB

Rerouting of the Sensing Element

140HF on the APU Bleed-Air-Duct

Sheet 01

Sheet 02

Sheet 03

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

NOTE: For tolerances for waviness and bends in sensing element wire, refer to

Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 58

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SERVICE BULLETIN

(a) Reroute the sensing element 140HF on the APU bleed-air duct and install the

clamps.

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

Refer to AMM Task 36-22-17-400-802.

1 Between Frame 90 and Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View E.

4 Sleeve-Protective NSA5539S Item 17

and close:

4 Clamp-single NAS5538-00 Item (26) Retained at

removal

2 At Frame 93, install:

Refer to Fig. A-GBDAB Sheet 02, View D.

1 Sleeve-Protective NSA5539S Item 17

1 Spacer NSA5527-03-01 Item (24) Retained at

removal

1 Clamp-single NAS5538-00 Item (26) Retained at

removal

with

1 Screw NAS1801-3-13 Item 35

3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in).

4 Between Frame 93 and Frame 94, close the upper part of the double clamp

without the sensing element 140HF.

Refer to Fig. A-GBDAB Sheet 02, View C.

NOTE: Only the lower part of the clamp stays in use.

5 Between Frame 90 thru 94, reroute the sensing element 140HF.

a STEP 1 thru STEP 2:

Refer to Fig. A-GBDAB Sheet 03.

<1> From Frame 94 to Frame 93, route the sensing element 140HF

straight from the clamp at STEP 1 to the next clamp at STEP 2.

1 Sensing Element

140HF

Item (36) Retained at

removal

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 59

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SERVICE BULLETIN

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

b STEP 3 thru STEP 6

Refer to Fig. A-GBDAB Sheet 03.

<1> Install the sensing element 140HF by following the installation

position sequence STEP 3 thru STEP 6.

NOTE: Make sure that the sensing element wire is routed

with an acceptable distance to the insulation sleeve

at STEP 6.

NOTE: For tolerances for waviness and bends in sensing

element wire, refer to Fig. A-GBEAA Sheet 01 and

Fig. A-GBEAA Sheet 02.

NOTE: The positions of the blowout apertures of the APU

bleed-air duct must be under the sensing element.

NOTE: Make sure that there is no contact between the

sensing element and the insulation sleeves.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 363040-710-201-001 - 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) Set the light switch 4LJ in the OFF position.

(b) Do the operational test of the overheat detection system (Refer to AMM Task

36-22-00-710-806).

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 60

0

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@A330

SERVICE BULLETIN

**CONF 002

(1) Subtask 363040-710-201-001 - 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) Set the light switch 4LJ in the OFF position.

(b) Do the operational test of the overheat detection system (Refer to AMM Task

36-22-00-710-806).

**CONF 003

(1) Subtask 363040-710-201-001 - 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) Set the light switch 4LJ in the OFF position.

(b) Do the operational test of the overheat detection system (Refer to AMM Task

36-22-00-710-806).

**CONF 004

(1) Subtask 363040-710-201-001 - 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

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 61

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SERVICE BULLETIN

(a) Set the light switch 4LJ in the OFF position.

(b) Do the operational test of the overheat detection system (Refer to AMM Task

36-22-00-710-806).

**CONF 005

(1) Subtask 363040-710-201-001 - 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) Set the light switch 4LJ in the OFF position.

(b) 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 363040-942-201-001 - Close-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) Make sure that the work areas are clean and clear of tools and other items of

equipment.

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

Block 001).

(c) Release and close the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(d) Remove the access platform(s).

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 62

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SERVICE BULLETIN

(e) Remove the warning notices from the cockpit.

**CONF 002

(1) Subtask 363040-942-201-001 - Close-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) Make sure that the work areas are clean and clear of tools and other items of

equipment.

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

Block 001).

(c) Release and close the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(d) Remove the access platform(s).

(e) Remove the warning notices from the cockpit.

**CONF 003

(1) Subtask 363040-942-201-001 - Close-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) Make sure that the work areas are clean and clear of tools and other items of

equipment.

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

Block 001).

(c) Release and close the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 63

0

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@A330

SERVICE BULLETIN

(d) Remove the access platform(s).

(e) Remove the warning notices from the cockpit.

**CONF 004

(1) Subtask 363040-942-201-001 - Close-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) Make sure that the work areas are clean and clear of tools and other items of

equipment.

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

Block 001).

(c) Release and close the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(d) Remove the access platform(s).

(e) Remove the warning notices from the cockpit.

**CONF 005

(1) Subtask 363040-942-201-001 - Close-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) Make sure that the work areas are clean and clear of tools and other items of

equipment.

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

Block 001).

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 64

0

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@A330

SERVICE BULLETIN

(c) Release and close the accessory-compartment access door 313AL (Refer to AMM

52-41-00, Page Block 001).

(d) Remove the access platform(s).

(e) Remove the warning notices from the cockpit.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 65

0

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@A330

SERVICE BULLETIN

**CONF 001

Z310

A

FR80

FR88

FR95

FR98

FR100

140HF

A

(18)

B

G_SB_363040_6_BBAA_01_01

Figure A-GBBAA - Sheet 01

Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 66

0

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@A330

SERVICE BULLETIN

**CONF 001

140HF

(18)

FWD

B

C

D

E

F

G H

H

H

H

H

H

H

H

H

H

H J

FR95

FR93

FR91

FR90

FR89

G_SB_363040_6_BBAA_02_02

FR88

Figure A-GBBAA - Sheet 02

Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 67

0

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@A330

SERVICE BULLETIN

**CONF 001

LOCKWIRE (MAT. NO. 19−018)

NOTE:

01

TYPICAL

(23)

(17) (30)

(24)

(27)

(23)

(29) (17)

C

(28)

(23)

(17)

D

E

(28)

F

01

(18)

(25)

01

G_SB_363040_6_BBAA_03_01

34HF

140HF

Figure A-GBBAA - Sheet 03

Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 68

0

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@A330

SERVICE BULLETIN

**CONF 001

(24)

(30)

(17)

(26)

G

H

TYPICAL

(17)

(26)

(18)

J

LOCKWIRE (MAT. NO. 19−018)

NOTE:

01

01

G_SB_363040_6_BBAA_04_01

140HF

139HF

Figure A-GBBAA - Sheet 04

Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 69

0

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@A330

SERVICE BULLETIN

**CONF 002 thru 005

Z310

A

FR80

FR88

FR90

FR95

FR98

FR100

140HF

A

(36)

B

G_SB_363040_6_BBAB_01_02

Figure A-GBBAB - Sheet 01

Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 70

0

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@A330

SERVICE BULLETIN

**CONF 002 thru 005

140HF

(36)

FWD

B

FR95

FR93

FR91

C

D

E

E

E

(17)

OPEN ONLY THIS CLAMP

NOTE:

01

01

C

(24)

(30)

(26)

D

TYPICAL

(17)

(26)

E

(17)

E

G_SB_363040_6_BBAB_02_02

FR94

Figure A-GBBAB - Sheet 02

Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 71

0

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@A330

SERVICE BULLETIN

**CONF 001

Z310

FR80

FR83

FR86

FR88

FR91

FR93 FR95

FR98

FR100

A

A

B

C

D

E

G

F

H

J

K

POSITION OF BLOWOUT APERTURE MUST BE UNDER THE SENSING ELEMENT

NOTE:

01

02 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 

SENSING ELEMENT AND THE INSULATION SLEEVE

01

02

01

02

01

02

01

02

G_SB_363040_6_BCAA_01_01

Figure A-GBCAA - Sheet 01

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 72

0

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@A330

SERVICE BULLETIN

**CONF 001

B

OVERHEAT SENSING ELEMENT MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

03

C

D

03

E

1 2

3

4

03

03

FR83

FR84

FR84

FR85

G_SB_363040_6_BCAA_02_02

Figure A-GBCAA - Sheet 02

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 73

0

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@A330

SERVICE BULLETIN

**CONF 001

OVERHEAT SENSING ELEMENT MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

9

G

5

F

03

6

7

H

03

17

8

03

03

J

K

03

FR87

FR88

FR90

FR91

FR94

G_SB_363040_6_BCAA_03_03

Figure A-GBCAA - Sheet 03

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 74

0

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@A330

SERVICE BULLETIN

**CONF 002, 004

Z310

FR80

FR83

FR86

FR88

FR91

FR93 FR95

FR98

FR100

A

A

B

C

D

E

F

G

H J

POSITION OF BLOWOUT APERTURE MUST BE UNDER THE SENSING ELEMENT

NOTE:

01

02 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 

SENSING ELEMENT AND THE INSULATION SLEEVE

01

02

01

02

01

02

01

02

G_SB_363040_6_BCAB_01_01

Figure A-GBCAB - Sheet 01

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 75

0

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@A330

SERVICE BULLETIN

**CONF 002, 004

OVERHEAT SENSING ELEMENTS MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

12

13

D

03

03

E

17

B

03

C

1

03

2

FR83

FR84

FR84

FR86

G_SB_363040_6_BCAB_02_02

Figure A-GBCAB - Sheet 02

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 76

0

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@A330

SERVICE BULLETIN

**CONF 002, 004

14

15

16

9

03

F

04

05

06

05

06

04

G 03

17

17

03

H

03

J

FR86

FR88

FR91

FR94

OVERHEAT SENSING ELEMENTS MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

FOR INSTALLATION OF THE INSULATION SLEEVE OPEN THE DETECTION

CLIP AND LIFT THE SENSING ELEMENT FROM THE BRACKET

04

05 PULL ANTI−ROTATION DEVICE OF THE INSULATION SLEEVE OVER THE BRACKET

06 REINSTALLATION OF SENSING ELEMENT G_SB_363040_6_BCAB_03_03

Figure A-GBCAB - Sheet 03

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 77

0

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@A330

SERVICE BULLETIN

**CONF 003, 005

Z310

A

FR80

FR83

FR86

FR88

FR91

FR93 FR95

FR98

FR100

A

B

C

D

E

F

G

H J

POSITION OF BLOWOUT APERTURE MUST BE UNDER THE SENSING ELEMENT

NOTE:

01

02 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 

SENSING ELEMENT AND THE INSULATION SLEEVE

01

02

01

02

01

02

01

02

G_SB_363040_6_BCAC_01_01

Figure A-GBCAC - Sheet 01

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 78

0

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@A330

SERVICE BULLETIN

**CONF 003, 005

B

OVERHEAT SENSING ELEMENTS MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

03

10

11

13

03

C

03

E

17

FR83

FR84

FR86

12

D

03

17

FR84

G_SB_363040_6_BCAC_02_02

Figure A-GBCAC - Sheet 02

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 79

0

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SERVICE BULLETIN

**CONF 003, 005

14

15

03

F

04

05

06

05

06

04

G 03

17

OVERHEAT SENSING ELEMENTS MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

FOR INSTALLATION OF THE INSULATION SLEEVE OPEN THE DETECTION

CLIP AND LIFT THE SENSING ELEMENT FROM THE BRACKET

04

05 PULL ANTI−ROTATION DEVICE OF THE INSULATION SLEEVE OVER THE BRACKET

06 REINSTALLATION OF SENSING ELEMENT

FR86

FR88

16 FR93

9

17

03

H

03

J

FR91

G_SB_363040_6_BCAC_03_03

Figure A-GBCAC - Sheet 03

Installation of the Sleeves on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 80

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SERVICE BULLETIN

**CONF 001

Z310

A

FR80

FR88

FR95

FR98

FR100

140HF

A

18

B M

G_SB_363040_6_BDAA_01_01

Figure A-GBDAA - Sheet 01

Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 81

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SERVICE BULLETIN

**CONF 001

FWD

B

140HF

18

FR95

FR93

FR91

FR90

FR89

C

E

F

K

K

K

K

K

K

K

K

K

K

L

K

G

J

H

G_SB_363040_6_BDAA_02_01

FR88

Figure A-GBDAA - Sheet 02

Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 82

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SERVICE BULLETIN

**CONF 001

C

~30°

D

D

27

31

31

29

29

32

32

17

17

E

36

19

17

17

TYPICAL

(23)

17 F 33 17

17 34 32

32

01

01 TORQUE VALUE 0.40m.daN (35.403lbf.in)

NOTE:

G

31

(24)

FWD

G_SB_363040_6_BDAA_03_02

~30°

Figure A-GBDAA - Sheet 03

Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 83

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SERVICE BULLETIN

**CONF 001

02 SAFETY WITH LOCKWIRE (MAT. NO. 19−018)

18

(25)

02

H

(24)

35

17

(26)

TYPICAL

17

(26) 18

01

NOTE:

01

J

K

L

02

02

TORQUE VALUE 0.40m.daN (35.403lbf.in)

G_SB_363040_6_BDAA_04_01

34HF

140HF

140HF

139HF

Figure A-GBDAA - Sheet 04

Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 84

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SERVICE BULLETIN

**CONF 001

G_SB_363040_6_BDAA_05_02

FWD

140HF

18

FR95

FR93

FR91

FR90

FR89

STEP 1

03 WAY OF WORKING STEPS

NOTE:

M

STEP 3

STEP 4

STEP 5

STEP 6

STEP 7

STEP 8

STEP 10

STEP 11

STEP 12

STEP 13

STEP 14

STEP 15

STEP 16

STEP 17

STEP 18

STEP 19

STEP 20

STEP 21

STEP 22

A

A

03

03

03

03

03

03

03

03

03

03

03

03

03

03

03

03

03

03

03

A A

STEP 2

STEP 9

03

03

12.7 mm

(0.50 in)

04 COVERED WITH 360° LOOPS

04

04

INSULATION

SLEEVE

INSULATION

SLEEVE

INSULATION

SLEEVE

FR88

Figure A-GBDAA - Sheet 05

Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 85

0

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SERVICE BULLETIN

**CONF 002 thru 005

Z310

A

FR80

FR91

FR93

FR95

FR98

FR100

140HF

A

(36)

B F

G_SB_363040_6_BDAB_01_02

Figure A-GBDAB - Sheet 01

Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 86

0

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SERVICE BULLETIN

**CONF 002 thru 005

140HF

(36)

FWD

B

FR95

FR93

CLOSE THIS CLAMP

NOTE:

01

01

C

(24)

35

(26)

D

17

D

C

G_SB_363040_6_BDAB_02_01

FR91

E

E

E

TYPICAL

17

(26)

E

E

Figure A-GBDAB - Sheet 02

Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 87

0

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SERVICE BULLETIN

**CONF 002 thru 005

140HF

(36)

FWD

02 WAY OF WORKING STEPS

NOTE:

F

G_SB_363040_6_BDAB_03_01

FR95

FR93

C

FR91

02 STEP 1 02 STEP 2

02 STEP 3

02 STEP 4

02 STEP 5

02 STEP 6

INSULATION

SLEEVE

Figure A-GBDAB - Sheet 03

Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 88

0

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SERVICE BULLETIN

**CONF ALL

G_SB_363040_6_BEAA_01_00

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

Figure A-GBEAA - Sheet 01

Tolerances for Waviness and Bends in Sensing Elements

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 89

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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

F MAX 203.0 MAX 7.99

RAD MIN 25.4 mm 

RAD MAX 40.0 mm

RAD MIN (1.00 in)

RAD MAX (1.57 in)

PRINCIPLE VIEW OF LOOP

C

A

A

C

G_SB_363040_6_BEAA_02_01

Figure A-GBEAA - Sheet 02

Tolerances for Waviness and Bends in Sensing Elements

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 90

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SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF ALL

For the elapsed time assumptions, refer to:

**CONF 001 Fig. A-GAAAA

**CONF 002 thru 005 Fig. A-GAAAB

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 1

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SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 001

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3040

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

14.50

14.00

STEPS

0.75 0.50

0 5

4.50 4.50

1.50 1.50

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

2

1

1

:

:

SB ELAPSED TIME

(HOURS)

123 4 6

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

INSTALL THE INSULATION

REMOVE THE SENSING 

INSTALL THE NEW SENSING

TEST

6.25 6.25

1.00 1.00

1

1

CLOSE−UP 0.50 0.25 2

ELEMENT

SLEEVES

ELEMENT

789 10 11 12 13 14

G_SB_363040_6_AAAA_01_00

Figure A-GAAAA - Sheet 01

Gantt Chart

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 2

0

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SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 002 thru 005

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3040

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

8.25

7.75

STEPS

0.75 0.50

0 5

2.00 2.00

2.25 2.25

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

2

1

1

:

:

SB ELAPSED TIME

(HOURS)

123 4 6

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

G_SB_363040_6_AAAB_01_00

INSTALL THE INSULATION

LOOSEN THE SENSING 

REROUTE THE SENSING

TEST

1.75 1.75

1.00 1.00

1

1

CLOSE−UP 0.50 0.25 2

ELEMENT

SLEEVES

ELEMENT

7 8 9

Figure A-GAAAB - Sheet 01

Gantt Chart

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 3

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SERVICE BULLETIN

REPORTING SHEET

TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS

IN S19.

MODIFICATION No.: 202216C10899 202216C10898 202216C10846

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: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 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: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040

REVISION No.: 01 - Nov 26/12 Page: 1

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