@A340

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.A340-36-4035

ADDITIONAL WORK

**CONF ALL

Additional work is required by this revision for aircraft included in Configurations 002, 003 and 005 that

were modified by the original issue of this Service Bulletin.

The additional work consists in replacing two insulation sleeves installed on the APU Air Bleed Duct

between Frame 83 and 84.

REASON

Revision No. 01 issued to:

- Correct the Part Numbers for two insulation sleeves between Frame 83 and 84 in configurations

002, 003 and 005.

- Add an additional work task for configurations 002, 003 and 005 to replace two insulation sleeves

between Frame 83 and 84.

- Change the insulation sleeves Kit allocation for Configurations 002, 003 and 005 to allocate the

correct kit to every configuration.

CHANGES

The main changes of this Revision are:

SUMMARY:

- Material Price Information

. The price information and quantity per A/C for the new Kits 364035D06 and 364035D07 are

added.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 1

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- Effectivity

. Operator list is updated.

- References / Repercussions

. Reference to SBIT 13-0021 is added.

- Manpower

. Manhour breakdown for the additional work is included for the affected configurations.

. Elapsed time figure is corrected for configuration 004 from 7.75 to 14.00 hours.

1. PLANNING INFORMATION:

- Effectivity

. Effectivity updated.

. Operator-MSN allocation updated.

. Material effectivity section is updated with the allocation and quantities per A/C for the new Kits

3640354D06 and 364035D07.

- Description

. Additional Work task description is added for the affected configurations.

- Compliance

. Accomplishment timescale sentence is updated as consequence of the linked Airworthiness

Directive is already published by the time of issuance of this SB Revision 01.

- Manpower

. Manhour breakdown for the additional work has been included for the affected configurations.

. Elapsed time figure is corrected for configuration 004 from 7.75 to 14.00 hours.

2. MATERIAL INFORMATION:

- Price and Availability

. The data for the new kits 364035D06R00 and 364035D07R00 is included.

. Prices are updated for the rest of the Kits.

- Industry Support Information

. Support Information for the Kits of the Additional Work is included.

- List of Components

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 2

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

. The definition of the new Kits 364035D06 and 3640354D07 is added. These kits are needed to

replace the 2 insulation sleeves installed by accomplishment of this SB in its initial issue with 2

other ones which PN match the configuration definition stated in the modification linked to the

present Service Bulletin.

3. ACCOMPLISHMENT INSTRUCTIONS:

- Elapsed time figure is corrected for configuration 004 from 7.75 to 14.00 hours.

- For configurations 002 and 005, in the installation of insulation sleeves, kit allocation is modified to

require Kit 364035D02 instead of Kit 364035D03.

- For configurations 002 and 005, in the installation of insulation sleeves, figure allocation is modified

to refer to Figure GBCAB instead of to GBCAC.

- For configuration 003, in the installation of insulation sleeves, kit allocation is modified to require Kit

364035D03 instead of Kit 364035D02.

- For configuration 003, in the installation of insulation sleeves, figure allocation is modified to refer to

Figure GBCAC instead of to GBCAB.

- New Additional Work task included to give the instructions and material needed to replace the 2

insulation sleeves between Frame 83 and 84 for Configuration 002, 003 and 005.

SUMMARY

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

CONF 002 CONFIGURATION DEFINITION UPDATED R

CONF 004 CONFIGURATION DEFINITION UPDATED R

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 3

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET QUANTITY UPDATED

MATERIAL SET UPDATED

R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL PRICE UPDATED

MATERIAL AVAILABILITY UPDATED

MATERIAL SET UPDATED

R

LIST OF COMPONENTS LIST OF COMPONENTS UPDATED R

Kit 364035D06R00 PART MATERIAL SET ADDED N

Kit 364035D07R00 PART MATERIAL SET ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 364035- 831-942-001-Modification

Task associated data - 004 ELAPSED TIME UPDATED R

Subtask 364035-831-202-002 SUBTASK SOLUTION ADDED N

Subtask 364035-831-202-003 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 364035-831-202-003 SUBTASK SOLUTION ADDED N

Subtask 364035-831-202-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 364035-831-202-002 SUBTASK SOLUTION ADDED N

Subtask 364035-831-202-003 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 4

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

TASK 364035- 831-943-001-Modification -

ADDITIONAL WORK - Required to

replace the insulation sleeves between

Frame 83 and Frame 84 (For aircraft

included in either Configuration 002, 003

or 005 that were modified by the

accomplishment of this Service Bulletin in

its initial revision).

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Task associated data - 003 TASK ASSOCIATED DATA ADDED N

Task associated data - 004 TASK ASSOCIATED DATA ADDED N

Task associated data - 005 TASK ASSOCIATED DATA ADDED N

Subtask 364035-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-941-203-001 SUBTASK SOLUTION ADDED N

Subtask 364035-941-203-001 SUBTASK SOLUTION ADDED N

Subtask 364035-941-203-001 SUBTASK SOLUTION ADDED N

Subtask 364035-831-205-002 SUBTASK SOLUTION ADDED N

Subtask 364035-831-205-001 SUBTASK SOLUTION ADDED N

Subtask 364035-831-205-002 SUBTASK SOLUTION ADDED N

Subtask 364035-710-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-710-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-710-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-942-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-942-202-001 SUBTASK SOLUTION ADDED N

Subtask 364035-942-202-001 SUBTASK SOLUTION ADDED N

Fig. A-GBCAB FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-GBCAC FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-GBFAA FIGURE SOLUTION ADDED N

Fig. A-GBFAA Sheet 01 SHEET ADDED N

Fig. A-GBFAA Sheet 02 SHEET ADDED N

Fig. A-GBGAA FIGURE SOLUTION ADDED N

Fig. A-GBGAA Sheet 01 SHEET ADDED N

Fig. A-GBGAA Sheet 02 SHEET ADDED N

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 5

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Sep 18/12

REVISION No. : 01 - Sep 24/13

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 6

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 LROPS AFFECTED NO

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 1

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035D01R01 1 3,310.00 Sleeves

Kit 364035D04R00 1 2,030.00 Sensing element, sleeves. spacer, cable

ties, clamps and attaching parts

TOTAL 5,340.00

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 364035D02R00 1 3,720.00 Sleeves

Kit 364035D05R00 1 35.60 Sleeves and screw

Kit 364035D06R00 1 635.00 Sleeves Frame 83-84

TOTAL 4,390.60

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 364035D03R00 1 4,000.00 Sleeves

Kit 364035D05R00 1 35.60 Sleeves and screw

Kit 364035D07R00 1 908.00 Sleeves Frame 83-84 and Sens. Element

Sleeve

TOTAL 4,943.60

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 364035D01R01 1 3,310.00 Sleeves

Kit 364035D04R00 1 2,030.00 Sensing element, sleeves. spacer, cable

ties, clamps and attaching parts

TOTAL 5,340.00

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 2

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

**CONF 005

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 364035D02R00 1 3,720.00 Sleeves

Kit 364035D05R00 1 35.60 Sleeves and screw

Kit 364035D06R00 1 635.00 Sleeves Frame 83-84

TOTAL 4,390.60

EFFECTIVITY

**CONF ALL

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

15R 47W 56W 58X 83V ABD ABQ ACA AFR AIB ALK ARG CAL

CCA CPA DGA DLH FIN GAF GFA HFY I2L IBE IRC IRM KAC

LAN M3R MAU MDG MSR NMB PAL QAF RJA S3R SAA SAS SFB

SLM SWR TAP THT THY UAE VCV VIR XAX

NOTE: If Service Bulletin A340-36-4033 has been embodied previously on aircraft, then Service

Bulletin A340-36-4035 should be disregarded.

- Service Bulletin No. A340-36-4033:

Pneumatic - Leak-Detection - Introduce adapted Dual Loop Overheat Leak Detection 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 SBIT 13-0021

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 3

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 364035-831-942-001: Modification

TOTAL MANHOURS 14.50

ELAPSED TIME (HOURS) 14.00

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

TOTAL MANHOURS 0.00

**CONF 002

Task 364035-831-942-001: Modification

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

**CONF 003

Task 364035-831-942-001: Modification

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

**CONF 004

Task 364035-831-942-001: Modification

TOTAL MANHOURS 14.50

ELAPSED TIME (HOURS) 14.00

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 4

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

TOTAL MANHOURS 0.00

**CONF 005

Task 364035-831-942-001: Modification

TOTAL MANHOURS 8.25

ELAPSED TIME (HOURS) 7.75

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

APPENDICES

**CONF ALL

Appendix 01: Elapsed Time Assumptions

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 5

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

**CONF 001, 004

Z310

A

F_SB_364035_6_SAAA_01_01

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

FR98

FR100

A

INSULATION SLEEVES

AND SENSING ELEMENT

140HF

Figure A-GSAAA - Sheet 01

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 6

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

**CONF 002 thru 003, 005

Z310

A

F_SB_364035_6_SAAB_01_01

FR80

FR83

FR85

FR86

FR88

FR91

FR93

FR95

FR98

FR100

A

INSULATION SLEEVES

AND SENSING ELEMENT

140HF

Figure A-GSAAB - Sheet 01

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 7

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 8

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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: If Service Bulletin A340-36-4033 has been embodied previously on aircraft,

then Service Bulletin A340-36-4035 should be disregarded.

- Service Bulletin No. A340-36-4033:

Pneumatic - Leak Detection - Introduce Adapted Dual Loop Overheat Leak

Detection On APU Bleed Air Duct

(1) Models

340-211 340-212 340-213 340-311 340-312 340-313

(2) Effectivity by MSN

0002 0004-0006 0009 0011 0013-0014 0018-0020 0022-0029 0031-0035 0038 0041

0043-0044 0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081

0084-0085 0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128

0131 0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 1

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 0233

0236-0237 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274

0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329

0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0381

0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424 0429-0430 0433-0435

0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0544-0546

0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646 0651 0668

(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

15R 0151

47W 0009

56W 0011 0013 0018 0019

58X 0004

83V 0280 0292

ABD 0210

ABQ 0216 0257

ACA 0170

AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377

0399

AIB 0131 0141 0161 0182 0302 0318 0332

ALK 0032 0033 0034 0367 0374 0381

ARG 0048 0063 0074 0080 0085 0093 0094 0123 0126 0128 0373

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228

DGA 0075 0081

DLH 0024 0027 0028 0035 0052 0053 0135 0158 0213 0233 0252 0297

0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447

FIN 0058 0168 0174

GAF 0274 0355

GFA 0212 0215 0282 0554

HFY 0117 0133 0190 0202

I2L 0005

IBE 0088 0125 0134 0145 0146 0193 0217 0221 0329 0387 0414 0459

0474 0483

IRC 0002

IRM 0020 0056

KAC 0089 0090 0101 0104

LAN 0167 0359 0363 0429 0442

M3R 0061

MAU 0076 0152 0194 0268

MDG 0319

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 2

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

OPERATOR MSN

MSR 0156 0159 0178

NMB 0047 0051

PAL 0173 0176 0187 0196

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0197 0378 0544 0582 0590 0643 0646 0651

SAS 0413 0424 0430 0435 0450 0467 0470

SFB 0046

SLM 0049

SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561

0562 0585 0598

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446 0668

THY 0023 0025 0057 0115 0180 0270 0331

UAE 0139 0149 0163 0166 0185 0236

VCV 0031

VIR 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0005 0013 0020 0023 0024 0025 0027 0028 0029 0032

0033 0034 0035 0041 0044 0047 0048 0049 0051 0052 0053

0056 0057 0058 0076 0078 0079 0084 0088 0089 0090 0091

0093 0094 0101 0104 0114 0115 0117 0123 0125 0126 0128

0131 0133 0134 0135 0136 0137 0139 0141 0142 0145 0146

0147 0149 0150 0152 0154 0157 0158 0160 0161 0163 0164

0166 0167 0168 0169 0170 0173 0174 0175 0176 0179 0180

0182 0185 0186 0187 0190 0192 0193 0194

001

0004 0006 0009 0011 0014 0018 0019 0022 0026 0031 0038

0043 0046 0061 0063 0074 0075 0080 0081 0085 0151 0156

0159 0178

004

0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214

0215 0216 0217 0218 0220 0221 0225 0227 0228 0233 0236

0237 0242 0243 0245 0246 0252 0257 0260 0263 0264 0268

0270 0273 0274 0278 0280 0282 0292 0297 0302 0304 0307

0310 0318 0319 0321 0325 0327 0329 0331 0332 0335 0347

0352 0354 0355 0359 0363 0367 0373 0374 0377 0378 0379

0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0414

0415 0424 0429 0430 0433 0434 0435 0438 0442 0446 0447

0450 0459 0467 0470 0474 0483 0528 0538 0541 0545 0546

0554 0556 0559 0561 0562

002

0204 005

0544 0582 0585 0590 0598 0643 0646 0651 0668 003

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 3

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for A340-300 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. 40018D16554 is embodied

**CONF 002

Config. 002 is valid for A340-300 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is embodied

- Modification No. 48980D42587 is not embodied

- Modification No. 40018D16554 is embodied

**CONF 003

Config. 003 is valid for A340-300 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is embodied

- Modification No. 48980D42587 is embodied

- Modification No. 40018D16554 is embodied

**CONF 004

Config. 004 is valid for A340-200 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. 40018D16554 is embodied

**CONF 005

Config. 005 is valid for A340-200 aircraft given in the effectivity of this Service Bulletin

on which:

- Modification No. 44579D40539 is embodied

- Modification No. 48980D42587 is not embodied

- Modification No. 40018D16554 is embodied

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 364035D01R01 1

Kit 364035D04R00 1

Consumable CMLD01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 364035D02R00 1

Kit 364035D05R00 1

Consumable CMLD01 1

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 4

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES

Kit 364035D06R00 1 (1)

NOTE (1): Kit D06 is only required for the Additional Work.

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 364035D03R00 1

Kit 364035D05R00 1

Consumable CMLD01 1

Kit 364035D07R00 1 (1)

NOTE (1): Kit D07 is only required for the Additional Work.

**CONF 004

MATERIAL QTY PER A/C SEE NOTES

Kit 364035D01R01 1

Kit 364035D04R00 1

Consumable CMLD01 1

**CONF 005

MATERIAL QTY PER A/C SEE NOTES

Kit 364035D02R00 1

Kit 364035D05R00 1

Consumable CMLD01 1

Kit 364035D06R00 1 (1)

NOTE (1): Kit D06 is only required for the Additional Work.

**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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 5

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(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.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 364035-831-942-001: Modification

(1) Remove the sensing element 140HF

(2) Install the insulation sleeves

(3) Install the new sensing element 140HF

**CONF 002

Task 364035-831-942-001: Modification

(1) Loosen the sensing element

(2) Install the insulation sleeves

(3) Reroute the sensing element 140HF

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either

Configuration 002, 003 or 005 that were modified by the accomplishment of this Service

Bulletin in its initial revision).

(1) Replace the insulation sleeves between Frame 83 and 84

**CONF 003

Task 364035-831-942-001: Modification

(1) Loosen the sensing element

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 6

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(2) Install the insulation sleeves

(3) Reroute the sensing element 140HF

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either

Configuration 002, 003 or 005 that were modified by the accomplishment of this Service

Bulletin in its initial revision).

(1) Replace the insulation sleeves between Frame 83 and 84

**CONF 004

Task 364035-831-942-001: Modification

(1) Remove the sensing element 140HF

(2) Install the insulation sleeves

(3) Install the new sensing element 140HF

**CONF 005

Task 364035-831-942-001: Modification

(1) Loosen the sensing element

(2) Install the insulation sleeves

(3) Reroute the sensing element 140HF

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either

Configuration 002, 003 or 005 that were modified by the accomplishment of this Service

Bulletin in its initial revision).

(1) Replace the insulation sleeves between Frame 83 and 84

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Within 26 months after the effective date of the European Aviation Safety Agency

(EASA) Airworthiness Directive (AD) 2013-0033 (05 March 2013) mandating Revision

No. 00 of this Service Bulletin.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 7

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 supersede EASA AD 2013-0033 and confirm this classification. The AD must be used

as the reference document for the mandated accomplishment timescale.

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 364035-831-942-001: 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

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

On Aircraft

TOTAL MANHOURS 0.00

**CONF 002

Task 364035-831-942-001: Modification

Get Access 0.75

On Aircraft

Loosen the sensing element 2.00

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 8

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Task 364035-831-942-001: Modification

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

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

Get Access 0.75

On Aircraft

Replace the insulation sleeves between Frame 83 and

84

1.00

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

**CONF 003

Task 364035-831-942-001: Modification

Get Access 0.75

On Aircraft

Loosen the sensing element 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

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

Get Access 0.75

On Aircraft

Replace the insulation sleeves between Frame 83 and

84

1.00

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 9

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 004

Task 364035-831-942-001: 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

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

On Aircraft

TOTAL MANHOURS 0.00

**CONF 005

Task 364035-831-942-001: Modification

Get Access 0.75

On Aircraft

Loosen the sensing element 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

Task 364035-831-943-001: Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either Configuration

002, 003 or 005 that were modified by the accomplishment of this Service Bulletin in its initial

revision).

Get Access 0.75

On Aircraft

Replace the insulation sleeves between Frame 83 and

84

1.00

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 10

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**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 +1.721 KG (+3.7941 LB)

Effect on Balance +109.190 KGM (+789.771 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 +98.798 KGM (+714.605 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 +95.258 KGM (+689.001 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 +1.721 KG (+3.7941 LB)

Effect on Balance +101.845 KGM (+736.644 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.

Manufacturers Empty Weight +1.559 KG (+3.4369 LB)

Effect on Balance +92.942 KGM (+672.249 LB.FT )

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 11

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**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

Consumable Material List (CML)

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 12

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 13

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 14

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 364035D01R01

Kit 364035D02R00

Kit 364035D03R00

Kit 364035D04R00

Kit 364035D05R00

Kit 364035D06R00

Kit 364035D07R00

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 364035D01R01

Cost 3,310.00 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 364035D02R00

Cost 3,720.00 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 364035D03R00

Cost 4,000.00 USD

Availability 150 calendar days from receipt of order

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 15

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 364035D04R00

Cost 2,030.00 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 364035D05R00

Cost 35.60 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 364035D06R00

Cost 635.00 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 364035D07R00

Cost 908.00 USD

Availability 150 calendar days from receipt of order

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 16

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 364035D01R01

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

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 364035D02R00

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 17

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Kit 364035D03R00

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.

Kit 364035D04R00

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 364035D05R00

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 18

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Kit 364035D06R00

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

NOTES

1 F3617062400000 1 SLEEVE (10) F3617062404600

2 F3617062400200 1 SLEEVE (11) F3617062402200

Kit 364035D07R00

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

NOTES

10 F3617062404600 1 SLEEVE (1) F3617062400000

11 F3617062402200 1 SLEEVE (2) F3617062400200

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.

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

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 19

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 20

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 364035-831-942-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 21

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**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 34HF 139HF 140HF

Access

Door 312AR 313AL

Manpower

TOTAL MANHOURS 14.50

ELAPSED TIME (HOURS) 14.00

**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 364035-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 22

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-839-201-001 - 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 364035-910-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 23

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-839-201-001 - 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 364035-910-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 24

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-839-201-001 - 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 364035-910-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 25

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(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 364035-839-201-001 - 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 364035-910-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 26

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(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 364035-839-201-001 - 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 364035-941-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 27

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

(1) Subtask 364035-941-201-001 - 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 364035-941-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 28

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-941-201-001 - 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 364035-941-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 29

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-831-201-001 - 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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 30

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 31

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 364035-831-202-001 - 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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 32

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Material necessary to do the job

Kit 364035D01R01

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:

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

1 Sleeve Assy F3617062405200 Item 8

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 33

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 sensing element between Frame 83 thru Frame 88, refer to AMM

Task 36-22-17-400-801.

(3) Subtask 364035-831-203-001 - 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 364035D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 1 SLEEVE

Kit 364035D04R00

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 34

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 35

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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:

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 36

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 37

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 38

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 364035-831-201-002 - Loosen the sensing element

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 39

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 40

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(2) Subtask 364035-831-202-002 - 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 364035D02R00

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 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 41

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-831-203-002 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 42

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035D05R00

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 43

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 44

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-831-201-002 - Loosen the sensing element

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 45

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-831-202-003 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 46

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035D03R00

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 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 47

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-831-203-002 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 48

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Material necessary to do the job

Kit 364035D05R00

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 49

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 50

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 004

(1) Subtask 364035-831-201-001 - 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

(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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 51

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 52

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 364035-831-202-001 - 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

Material necessary to do the job

Kit 364035D01R01

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 53

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

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:

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

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 sensing element between Frame 83 thru Frame 88, refer to AMM

Task 36-22-17-400-801.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 54

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(3) Subtask 364035-831-203-001 - 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 364035D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

17 NSA5539S 1 SLEEVE

Kit 364035D04R00

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

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 55

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

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,Overheat

35660-2-310 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

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 56

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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:

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 57

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 58

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

<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.

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 59

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 005

(1) Subtask 364035-831-201-002 - Loosen the sensing element

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 60

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-831-202-002 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 61

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Material necessary to do the job

Kit 364035D02R00

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 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 62

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 364035-831-203-002 - 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 364035D05R00

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 63

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 64

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 65

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 364035-710-201-001 - Operational

Work Zones and Access Panels

Zone Access/Work location

210

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

**CONF 002

(1) Subtask 364035-710-201-001 - Operational

Work Zones and Access Panels

Zone Access/Work location

210

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

**CONF 003

(1) Subtask 364035-710-201-001 - Operational

Work Zones and Access Panels

Zone Access/Work location

210

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 66

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

**CONF 004

(1) Subtask 364035-710-201-001 - Operational

Work Zones and Access Panels

Zone Access/Work location

210

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

**CONF 005

(1) Subtask 364035-710-201-001 - Operational

Work Zones and Access Panels

Zone Access/Work location

210

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 67

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 364035-942-201-001 - 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 002

(1) Subtask 364035-942-201-001 - 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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 68

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.

**CONF 003

(1) Subtask 364035-942-201-001 - 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 004

(1) Subtask 364035-942-201-001 - 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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 69

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(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 364035-942-201-001 - 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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 70

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Task 364035-831-943-001 - Modification - ADDITIONAL WORK - Required to replace the

insulation sleeves between Frame 83 and Frame 84 (For aircraft included in either

Configuration 002, 003 or 005 that were modified by the accomplishment of this Service

Bulletin in its initial revision).

**CONF ALL

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

Manpower

TOTAL MANHOURS 0.00

**CONF 002

Zone

310

Access

Door 312AR

Manpower

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

**CONF 003

Zone

310

Access

Door 312AR

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 71

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Manpower

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

**CONF 004

Manpower

TOTAL MANHOURS 0.00

**CONF 005

Zone

310

Access

Door 312AR

Manpower

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

(1) Subtask 364035-910-202-001 - 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)

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

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

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

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

001).

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 72

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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

(2) Subtask 364035-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 364035-910-202-001 - 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)

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

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

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

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

001).

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

(2) Subtask 364035-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 004

None

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 73

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 005

(1) Subtask 364035-910-202-001 - 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)

Fig. A-GBEAA

Tolerances for Waviness and Bends in

Sensing Elements

Sheet 01

Sheet 02

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

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

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

001).

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

(2) Subtask 364035-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

None

**CONF 002

(1) Subtask 364035-941-203-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 74

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 an access platform in position below the access doors 312AR.

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

Block 001).

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

**CONF 003

(1) Subtask 364035-941-203-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

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 an access platform in position below the access doors 312AR.

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

Block 001).

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

**CONF 004

None

**CONF 005

(1) Subtask 364035-941-203-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 75

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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 an access platform in position below the access doors 312AR.

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

Block 001).

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

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 364035-831-205-002 - Replace the insulation sleeves between Frame 83

and 84

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 83 to Frame 84

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 364035D06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F3617062400000 1 SLEEVE

2 F3617062400200 1 SLEEVE

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 76

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

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

Task 36-22-17-400-801

Fig. A-GBFAA

ADDITIONAL WORK - Replacement of

the Insulation Sleeves

Sheet 01

Sheet 02

(a) Remove the insulation sleeves from the APU bleed air duct.

Refer to Fig. A-GBFAA Sheet 02, View B and D.

1 Loosen the sensing element between Frame 83 thru Frame 84, in

preparation for the removal of the insulation sleeves, refer to AMM Task

36-22-17-000-801.

2 Between Frame 83 thru Frame 84, remove the insulation sleeves on the APU

bleed-air-duct:

Refer to Fig. A-GBFAA Sheet 02, View B and D.

1 Sleeve Assy F3617062404600 Item (10) Discard

1 Sleeve Assy F3617062402200 Item (11) Discard

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

Refer to Fig. A-GBFAA Sheet 02, View C and E.

1 Between Frame 83 thru Frame 84, install the insulation sleeves on the APU

bleed-air-duct:

Refer to Fig. A-GBFAA Sheet 02, View C and E.

1 Sleeve Assy F3617062400000 Item 1

1 Sleeve Assy F3617062400200 Item 2

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 Reinstall the sensing element between Frame 83 thru Frame 84, refer to AMM

Task 36-22-17-400-801.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 77

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003

(1) Subtask 364035-831-205-001 - Replace the insulation sleeves between Frame 83

and 84

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 83 to Frame 84

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 364035D07R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 F3617062404600 1 SLEEVE

11 F3617062402200 1 SLEEVE

17 NSA5539S 1 SLEEVE

References

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

Task 36-22-17-400-801

Fig. A-GBGAA

ADDITIONAL WORK - Replacement of

the Insulation Sleeves

Sheet 01

Sheet 02

(a) Remove the insulation sleeves from the APU bleed air duct.

Refer to Fig. A-GBGAA Sheet 02, View B and D.

1 Loosen the sensing element between Frame 83 thru Frame 84, in

preparation for the removal of the insulation sleeves, refer to AMM Task

36-22-17-000-801.

2 Between Frame 83 thru Frame 84, remove the insulation sleeves on the APU

bleed-air-duct:

Refer to Fig. A-GBGAA Sheet 02, View B and D.

1 Sleeve Assy F3617062400000 Item (1) Discard

1 Sleeve Assy F3617062400200 Item (2) Discard

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 78

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

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

Refer to Fig. A-GBGAA Sheet 02, View C and E.

1 Between Frame 83 thru Frame 84, install the insulation sleeves on the APU

bleed-air-duct:

Refer to Fig. A-GBGAA Sheet 02, View C and E.

1 Sleeve Assy F3617062404600 Item 10

1 Sleeve Assy F3617062402200 Item 11

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 Install new protective sleeve on the sensing element on Frame 83:

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

1 Sleeve-Protective NSA5539S Item 17

3 Reinstall the sensing element between Frame 83 thru Frame 84, refer to AMM

Task 36-22-17-400-801.

**CONF 004

None

**CONF 005

(1) Subtask 364035-831-205-002 - Replace the insulation sleeves between Frame 83

and 84

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Work location from Frame 83 to Frame 84

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 79

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Material necessary to do the job

Kit 364035D06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F3617062400000 1 SLEEVE

2 F3617062400200 1 SLEEVE

References

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

Task 36-22-17-400-801

Fig. A-GBFAA

ADDITIONAL WORK - Replacement of

the Insulation Sleeves

Sheet 01

Sheet 02

(a) Remove the insulation sleeves from the APU bleed air duct.

Refer to Fig. A-GBFAA Sheet 02, View B and D.

1 Loosen the sensing element between Frame 83 thru Frame 84, in

preparation for the removal of the insulation sleeves, refer to AMM Task

36-22-17-000-801.

2 Between Frame 83 thru Frame 84, remove the insulation sleeves on the APU

bleed-air-duct:

Refer to Fig. A-GBFAA Sheet 02, View B and D.

1 Sleeve Assy F3617062404600 Item (10) Discard

1 Sleeve Assy F3617062402200 Item (11) Discard

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

Refer to Fig. A-GBFAA Sheet 02, View C and E.

1 Between Frame 83 thru Frame 84, install the insulation sleeves on the APU

bleed-air-duct:

Refer to Fig. A-GBFAA Sheet 02, View C and E.

1 Sleeve Assy F3617062400000 Item 1

1 Sleeve Assy F3617062400200 Item 2

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.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 80

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

2 Reinstall the sensing element between Frame 83 thru Frame 84, refer to AMM

Task 36-22-17-400-801.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 364035-710-202-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

**CONF 003

(1) Subtask 364035-710-202-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

**CONF 004

None

**CONF 005

(1) Subtask 364035-710-202-001 - Operational

Manpower Resources

Skills ELECTRICAL

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 81

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 36-22-00-710-801

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

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

36-22-00-710-801).

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 364035-942-202-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

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) Remove the access platform.

**CONF 003

(1) Subtask 364035-942-202-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

References

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 82

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(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) Remove the access platform.

**CONF 004

None

**CONF 005

(1) Subtask 364035-942-202-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

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) Remove the access platform.

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 83

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

FR80

FR88

FR95

FR98

FR100

140HF

A

(18)

B

Z310

A

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 84

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

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

F_SB_364035_6_BBAA_02_01

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 85

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

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

34HF

140HF

F_SB_364035_6_BBAA_03_00

Figure A-GBBAA - Sheet 03

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 86

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

(24)

(30)

(17)

(26)

G

H

TYPICAL

(17)

(26)

(18)

J

LOCKWIRE (MAT. NO. 19−018)

NOTE:

01

01

140HF

139HF

F_SB_364035_6_BBAA_04_00

Figure A-GBBAA - Sheet 04

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 87

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002 thru 003, 005

Z310

A

FR80

FR88

FR90

FR95

FR98

FR100

140HF

A

(36)

B

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 88

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002 thru 003, 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

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 89

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

Z310

A

F_SB_364035_6_BCAA_01_01

FR80

FR83

FR86

FR88

FR91

FR93 FR95

FR98

FR100

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

Figure A-GBCAA - Sheet 01

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 90

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

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

F_SB_364035_6_BCAA_02_01

Figure A-GBCAA - Sheet 02

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 91

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

OVERHEAT SENSING ELEMENT MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

G

5

F

03

6

7

H

03

17

8

03

03

J

FR87

FR88

FR90

FR91

9

K

03

FR94

F_SB_364035_6_BCAA_03_02

Figure A-GBCAA - Sheet 03

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 92

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002, 005

Z310

A

F_SB_364035_6_BCAB_01_01

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

Figure A-GBCAB - Sheet 01

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 93

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002, 005

OVERHEAT SENSING ELEMENTS MUST BE

OUTSIDE THE INSULATION SLEEVE

NOTE:

03

13

03

E

B

03

C

1

03

2

FR83

FR84

FR86

12

D

03

17

FR84

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 94

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002, 005

14

15

03

F

04

05

06

05

06

04

G 03

17

FR86

FR88

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

16

9

17

03

H

03

J

FR91

FR94

F_SB_364035_6_BCAB_03_02

Figure A-GBCAB - Sheet 03

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 95

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003

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

Z310

A

F_SB_364035_6_BCAC_01_01

FR80

FR83

FR86

FR88

FR91

FR93 FR95

FR98

FR100

A

B

C

D

E

F

G

H J

01

02

01

02

01

02

01

02

Figure A-GBCAC - Sheet 01

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 96

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003

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

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 97

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003

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

F_SB_364035_6_BCAC_03_02

Figure A-GBCAC - Sheet 03

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 98

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

FR80

FR88

FR95

FR98

FR100

140HF

A

18

B M

Z310

A

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 99

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

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

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 100

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

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

F_SB_364035_6_BDAA_03_01

~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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 101

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

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)

34HF

140HF

140HF

139HF

F_SB_364035_6_BDAA_04_00

Figure A-GBDAA - Sheet 04

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

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 102

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001, 004

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

F_SB_364035_6_BDAA_05_02

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 103

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002 thru 003, 005

Z310

A

FR80

FR91

FR93

FR95

FR98

FR100

140HF

A

(36)

B F

F_SB_364035_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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 104

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002 thru 003, 005

CLOSE THIS CLAMP

NOTE:

01

F_SB_364035_6_BDAB_02_01

140HF

(36)

FWD

B

FR95

FR93

01

C

(24)

35

(26)

D

17

D

C

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 105

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002 thru 003, 005

02 WAY OF WORKING STEPS

NOTE:

F_SB_364035_6_BDAB_03_01

140HF

(36)

FWD

F

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 106

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

TOLERANCES FOR WAVINESS AND BEND IN WIRES

C

B

A E

C

E A

E

A

C

D

E

E

E

C

NOTE:

FOR DIMENSIONS, REFER TO SHEET 2 F_SB_364035_6_BEAA_01_00

Figure A-GBEAA - Sheet 01

Tolerances for Waviness and Bends in Sensing Elements

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 107

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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

F_SB_364035_6_BEAA_02_00

Figure A-GBEAA - Sheet 02

Tolerances for Waviness and Bends in Sensing Elements

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 108

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002, 005

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

Z310

A

FR80

FR83

FR86

FR88

FR91

FR93 FR95

FR98

FR100

A

01

02

B C

D E

F_SB_364035_6_BFAA_01_00

Figure A-GBFAA - Sheet 01

ADDITIONAL WORK - Replacement of the Insulation Sleeves

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 109

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002, 005

OVERHEAT SENSING ELEMENTS MUST BE OUTSIDE

THE INSULATION SLEEVE

NOTE:

03

B

03

(10)

03

(11)

FR83

FR84

03

BEFORE AFTER

C

D E

BEFORE AFTER

2

1 FR83

FR84

03

(17)

F_SB_364035_6_BFAA_02_02

Figure A-GBFAA - Sheet 02

ADDITIONAL WORK - Replacement of the Insulation Sleeves

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 110

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003

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

Z310

A

FR80

FR83

FR86

FR88

FR91

FR93 FR95

FR98

FR100

A

01

02

B C

D E

F_SB_364035_6_BGAA_01_00

Figure A-GBGAA - Sheet 01

ADDITIONAL WORK - Replacement of the Insulation Sleeves

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 111

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003

B

03

(1)

(2)

FR83

OVERHEAT SENSING ELEMENTS MUST BE OUTSIDE

THE INSULATION SLEEVE

NOTE:

03

AFTER

C

D E

FOR REPLACEMENT OF THE INSULATION SLEEVE OPEN

THE DETECTION CLIP AND LIFT THE SENSING ELEMENT

04

11

10

FR83

FR84

BEFORE

BEFORE

03

03

AFTER

04 17

FR84

03

F_SB_364035_6_BGAA_02_02

Figure A-GBGAA - Sheet 02

ADDITIONAL WORK - Replacement of the Insulation Sleeves

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 112

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF ALL

For the elapsed time assumptions, refer to:

**CONF 001, 004 Fig. A-GAAAA

**CONF 002 thru 003, 005 Fig. A-GAAAB

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 1

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 001, 004

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4035

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

F_SB_364035_6_AAAA_01_00

Figure A-GAAAA - Sheet 01

Gantt Chart

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 2

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 01: Elapsed Time Assumptions

**CONF 002 thru 003, 005

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4035

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

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

F_SB_364035_6_AAAB_01_00

Figure A-GAAAB - Sheet 01

Gantt Chart

DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 3

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 1

0

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.: A340-36-4035

REVISION No.: 01 - Sep 24/13 Page: 1

0

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