# @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



# MANDATORYMANDATORYMANDATORY 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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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. 

# MANDATORYMANDATORYMANDATORY 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

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# @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

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# @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

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# @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

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# @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

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# @A340 SERVICE BULLETIN SUMMARY
**CONF 001, 004

Z310 

### A

F_SB_364035_6_SAAA_01_01 FR80 FR83 FR85FR86 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

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# @A340 SERVICE BULLETIN SUMMARY
**CONF 002 thru 003, 005

Z310 

### A

F_SB_364035_6_SAAB_01_01 FR80 FR83 FR85FR86 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

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# @A340 SERVICE BULLETIN SUMMARY

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DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035 REVISION No.: 01 - Sep 24/13 Page: 8 0

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# @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



# MANDATORYMANDATORYMANDATORY 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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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 EASAAD 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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @A340 SERVICE BULLETIN

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# @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

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# @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

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# @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

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# @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

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# @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

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# @A340 SERVICE BULLETIN

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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 140HF1 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
DATE: Sep 18/12 SERVICE BULLETIN No.: A340-36-4035 REVISION No.: 01 - Sep 24/13 Page: 35 0

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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 140HF1 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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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 **CONFALL 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

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# @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

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# @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. **CONFALL 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

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# @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

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# @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. **CONFALL 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

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# @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

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# @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

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# @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

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# @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

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# @A340 SERVICE BULLETIN
2 Reinstall the sensing element between Frame 83 thru Frame 84, refer to AMM Task 36-22-17-400-801. **CONFALL 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

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# @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). **CONFALL 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

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# @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

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# @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

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# @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

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# @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 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 02 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

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# @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

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# @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 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 02 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

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# @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

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# @A340 SERVICE BULLETIN

**CONF 002, 005

14 15

03 

## F

04

05 06

05 06 04

03 

## G 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 PULL ANTI−ROTATION DEVICE OF THE INSULATION SLEEVE OVER THE BRACKET 05 REINSTALLATION OF SENSING ELEMENT 06 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

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# @A340 SERVICE BULLETIN

**CONF 003

POSITION OF BLOWOUT APERTURE MUST BE UNDER THE SENSING ELEMENT **NOTE:** 01 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 02 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

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# @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

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# @A340 SERVICE BULLETIN

**CONF 003

14 15

03 

## F

04

05 06

05 06 04

03 

## G 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 PULL ANTI−ROTATION DEVICE OF THE INSULATION SLEEVE OVER THE BRACKET 05 REINSTALLATION OF SENSING ELEMENT 06 FR86 FR88

FR93 16 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

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# @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

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# @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

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# @A340 SERVICE BULLETIN

**CONF 001, 004



## C ~30°



### D


## D 27

31 31

29 29 3232 17

17



## E 36 19 17

17

TYPICAL (23)

17 

## F 33 17

34 17 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

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# @A340 SERVICE BULLETIN

**CONF 001, 004

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

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# @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 7STEP 8 STEP 10
STEP 11STEP 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 903 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

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# @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

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# @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

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# @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 STEP 1 02 STEP 2 02

STEP 3 02
STEP 4 02 STEP 5 02

STEP 6 02 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

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# @A340 SERVICE BULLETIN

**CONF ALL

TOLERANCES FOR WAVINESS AND BEND IN WIRES

C

B A E
C

A E

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

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# @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

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# @A340 SERVICE BULLETIN

**CONF 002, 005

POSITION OF BLOWOUT APERTURE MUST BE UNDER THE SENSING ELEMENT **NOTE:** 01 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 02 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

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# @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

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# @A340 SERVICE BULLETIN

**CONF 003

POSITION OF BLOWOUT APERTURE MUST BE UNDER THE SENSING ELEMENT **NOTE:** 01 MAKE SURE THAT THERE IS NO CONTACT BETWEEN THE 02 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

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# @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 17 04

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

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# @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

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# @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

5 0 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

11 789 10 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

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# @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

5 0 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

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# @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.