# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS IN S19. MODIFICATION No.: 202216C10899 202216C10898 202216C10846 This page transmits Revision No.01 of Service Bulletin No.A330-36-3040 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 issued to correct the description of Service Bulletin Configurations 003 and 004. CHANGES The main changes of this revision are: - Effectivity . Note added to inform about the Airbus Mod. No. applied in production line for the same intent as the Service Bulletin. - Effectivity by Operator . Operator update for some MSNs. - Configuration definition . The statement "Modification No. 49813D44055 is embodied" is replaced by "Modification No. 40019D16555 is embodied" for Configurations 003 and 004. SUMMARY EFFECTIVITY OPERATOR LIST UPDATED R

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 1 0

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# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONF 003 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R CONF 004 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R
FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS No previous revision REVISION SEQUENCE ORIGINAL: Sep 18/12 REVISION No. : 01 - Nov 26/12

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 2 0

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# @A330 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORY MANDATORY MANDATORY ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS IN S19. **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 202216C10899 202216C10898 202216C10846 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES A global review of the compliance of the JAR 25.0863 and SFAR88 has highlighted potential deviations in specific cases. In particular, deviations have been found in Section 19, consequently, it has been required to introduce several flexible thermal insulation muffs in the ducting of the APU Pneumatics Distribution (Bleed) System. The goal is avoiding hot surfaces during APU Bleed operation. Thermal Insulation Muffs will be installed on joint connections ducts and retainer rings of APU Bleed System in rear fuselage zone thru frame 95. The Muffs have a venting hole to point-leaking hot air directly towards the adjacent sensing elements of the Overheat Detection System (OHDS). This Service Bulletin is issued to give the instructions to install Insulation Muffs and to modify the OHDS sensing element installation. The accomplishment of this Service Bulletin will minimize the possible ignition sources. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 1 0

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# @A330 SERVICE BULLETIN SUMMARY EVALUATION TABLE STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1) : Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 363040D01R01 1 3,060.00 Sleeves Kit 363040D04R00 1 1,880.00 Sensing element, sleeves, spacer, cable ties, clamps and attaching parts TOTAL 4,940.00 **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 363040D02R00 1 3,440.00 Sleeves Kit 363040D05R01 1 33.00 Sleeves and screw TOTAL 3,473.00 **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 363040D03R00 1 3,700.00 Sleeves Kit 363040D05R01 1 33.00 Sleeves and screw TOTAL 3,733.00 **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 363040D02R00 1 3,440.00 Sleeves Kit 363040D05R01 1 33.00 Sleeves and screw TOTAL 3,473.00

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 2 0

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# @A330 SERVICE BULLETIN SUMMARY **CONF 005 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 363040D03R00 1 3,700.00 Sleeves Kit 363040D05R01 1 33.00 Sleeves and screw TOTAL 3,733.00 EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

38W AAR ACA ACI AEA AFR ALK AZA BEL BER BMA BTV CAL CPA CRL CSC CSN DAH DAL DGA DLH EDW EIN ETD EVA FWI GFA GIA GRL HDA HFY HVN I2L IAC IWD IYE JAV JST KAL KLM MAS MON MSR OHY PAL QAF QFA QTR RSY RYN SAI SAS SWR TAM TAP TCX THA THY TSC UAE USA VKG VLK VOZ XAX XLF This modification is applicable by Service Bulletin only. NOTE: The intent of this modification is achieved on MSN 0690 and subsequent through modification Mod. No. 52260D44330. NOTE: If Service Bulletin A330-36-3038 or Service Bulletin A330-36-3037 has been embodied previously on aircraft, then Service Bulletin A330-36-3040 should be disregarded. Service Bulletin No. A330-36-3038: - Pneumatic - Leak Detection - Adapt Dual Loop After First Retrofit Service Bulletin No. A330-36-3037: - Pneumatic - Leak Detection - Introduce Adapted Dual Loop Overheat Leak On APU Bleed Air Duct CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 3 0

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# @A330 SERVICE BULLETIN SUMMARY NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 363040-831-943-001: Modification TOTAL MANHOURS 14.50 ELAPSED TIME (HOURS) 14.00 **CONF 002 Task 363040-831-943-001: Modification TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF 003 Task 363040-831-943-001: Modification TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF 004 Task 363040-831-943-001: Modification TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF 005 Task 363040-831-943-001: Modification TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 APPENDICES **CONF ALL Appendix 01: Elapsed Time Assumptions

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 4 0

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# @A330 SERVICE BULLETIN SUMMARY
**CONF 001

Z310 

### A

FR80 FR83 FR85 FR86 FR88 FR91 FR93 FR95 FR98 FR100



## A INSULATION SLEEVES AND SENSING ELEMENT 140HF

G_SB_363040_6_SAAA_01_03 Figure A-GSAAA - Sheet 01
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 5 0

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# @A330 SERVICE BULLETIN SUMMARY
**CONF 002 thru 005

Z310 

### A

FR80 FR83 FR85 FR86 FR88 FR91 FR93 FR95 FR98 FR100



## A INSULATION SLEEVES AND SENSING ELEMENT 140HF

G_SB_363040_6_SAAB_01_03 Figure A-GSAAB - Sheet 01
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 6 0

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# @A330 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS IN S19. MODIFICATION No.: 202216C10899 202216C10898 202216C10846 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY This modification is applicable by Service Bulletin only. NOTE: The intent of this modification is achieved on MSN 0690 and subsequent through modification Mod. No. 52260D44330. NOTE: If Service Bulletin A330-36-3038 or Service Bulletin A330-36-3037 has been embodied previously on aircraft, then Service Bulletin A330-36-3040 should be disregarded. Service Bulletin No. A330-36-3038: - Pneumatic - Leak Detection - Adapt Dual Loop After First Retrofit Service Bulletin No. A330-36-3037: - Pneumatic - Leak Detection - Introduce Adapted Dual Loop Overheat Leak On APU Bleed Air Duct (1) Models 330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 1 0

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# @A330 SERVICE BULLETIN
330-322 330-323 330-341 330-342 330-343 (2) Effectivity by MSN 0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0069-0073 0077 0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116 0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 38W 0401 AAR 0640 0676 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0505 0526 0551 0597 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 ALK 0303 0306 0311 0313 0404 0456 0627 AZA 0272 0339 BEL 0030 0037 0045 0082 0095 0229 0249 BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 BMA 0398 BTV 0205 0330 CAL 0602 0607 0641 0671 0675 CPA 0012 0017 0102 0113 0118 0121 0155 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 CRL 0285 0320 CSC 0462 CSN 0649 0652 0656 0664 DAH 0644 0647 0650 0653 0667 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 2 0

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# @A330 SERVICE BULLETIN
OPERATOR MSN DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620 0621 0631 0633 0663 0674 DGA 0240 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 EDW 0291 EIN 0269 0397 ETD 0658 0688 EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 FWI 0253 GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 GIA 0138 0140 0144 0148 0153 0165 GRL 0230 HDA 0071 0083 0099 0106 0109 0234 0244 0405 0479 0512 0581 0654 0662 HFY 0096 0211 0262 HVN 0275 0294 0299 0366 I2L 0358 0364 IAC 0353 0362 IWD 0461 0670 IYE 0625 0632 JAV 0255 JST 0506 0508 0513 0522 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0425 0428 0484 0490 0550 KLM 0682 0686 MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300 MON 0261 0265 MSR 0600 0610 0666 0683 OHY 0072 0087 0098 0143 PAL 0183 0184 0188 0189 0191 0198 0200 0203 QAF 0487 0605 QFA 0553 0558 0564 0574 0593 0595 0603 QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659 0680 0684 RSY 0171 RYN 0343 SAI 0055 0070 SAS 0496 0497 0515 0568 SWR 0324 TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 TAP 0181 0195 0223 0305 0308 0312 0317 TCX 0254 0266 0301 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 THY 0463 0504 TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 3 0

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# @A330 SERVICE BULLETIN
OPERATOR MSN UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382 0384 0392 0396 0409 0437 0451 0452 0455 0491 0494 0509 0518 0525 0536 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 VKG 0309 0349 0356 0357 VLK 0086 VOZ 0365 0372 XAX 0054 XLF 0501 0635 (4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064 0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083 0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109 0110 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177 0183 0184 0188 0189 0191 001

0181 0195 0205 0211 0222 0223 0226 0229 0230 0232 0238 0240 0247 0248 0249 0250 0251 0253 0254 0255 0258 0259 0261 0262 0265 0266 0269 0271 0272 0275 0276 0281 0283 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314 0316 0317 0320 0322 0324 0326 0328 0330 0334 0339 0340 0343 0345 0348 0353 0358 0361 0362 0364 0365 0366 0369 0372 0382 0384 0392 0396 0397 0398 0401 0403 0404 0409 0422 0427 0432 0437 0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473 0476 0477 0480 0481 0486 0487 0489 0491 0493 0494 0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511 0513 0516 0518 0519 0521 0522 0525 0526 0527 0529 0530 0532 0535 0536 0551 0567 0584 0597 0627 0635 0657 004

0198 0200 0203 0206 0209 0219 0224 0231 0234 0241 0244 0256 0267 0277 0279 0284 0315 0323 0333 0337 0338 0342 0344 0346 0349 0350 0351 0356 0357 0368 0370 0375 0380 0386 0388 0389 0393 0400 0405 0407 0408 0412 0418 0419 0420 0421 0423 0425 0428 0439 0479 0484 0490 0496 0497 0512 0515 0539 0548 0550 0565 0568 0581 002

0524 0533 0542 0549 0552 0553 0558 0564 0570 0574 0576 0578 0579 0588 0591 0593 0595 0602 0603 0607 0623 0629 0636 0637 0640 0641 0642 0645 0648 0654 0659 0662 0663 0669 0670 0671 0673 0674 0675 0676 0679 0680 0687 005

0555 0571 0573 0587 0600 0605 0609 0610 0612 0614 0616 0618 0620 0621 0625 0631 0632 0633 0634 0638 0644 0647 0649 0650 0652 0653 0655 0656 0658 0661 0664 0665 0666 0667 0678 0682 0683 0684 0686 0688 003

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 4 0

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# @A330 SERVICE BULLETIN (5) Configuration definition **CONF 001 Config. 001 is valid for A330-300 aircraft given in the effectivity of this Service Bulletin on which: - Modification No. 44579D40539 is not embodied - Modification No. 48980D42587 is not embodied - Modification No. 40019D16555 is embodied **CONF 002 Config. 002 is valid for A330-300 aircraft given in the effectivity of this Service Bulletin on which: - Modification No. 44579D40539 is embodied - Modification No. 48980D42587 is not embodied - Modification No. 40019D16555 is embodied **CONF 003 Config. 003 is valid for A330-200 aircraft given in the effectivity of this Service Bulletin on which: - Modification No. 44579D40539 is embodied - Modification No. 48980D42587 is embodied - Modification No. 40019D16555 is embodied **CONF 004 Config. 004 is valid for A330-200 aircraft given in the effectivity of this Service Bulletin on which: - Modification No. 44579D40539 is embodied - Modification No. 48980D42587 is not embodied - Modification No. 40019D16555 is embodied **CONF 005 Config. 005 is valid for A330-300 aircraft given in the effectivity of this Service Bulletin on which: - Modification No. 44579D40539 is embodied - Modification No. 48980D42587 is embodied - Modification No. 40019D16555 is embodied (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Kit 363040D01R01 1 Kit 363040D04R00 1 Consumable CMLD01 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Kit 363040D02R00 1 Kit 363040D05R01 1 Consumable CMLD01 1 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 5 0

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# @A330 SERVICE BULLETIN
**CONF 003 MATERIAL QTY PER A/C SEE NOTES Kit 363040D03R00 1 Kit 363040D05R01 1 Consumable CMLD01 1 **CONF 004 MATERIAL QTY PER A/C SEE NOTES Kit 363040D02R00 1 Kit 363040D05R01 1 Consumable CMLD01 1 **CONF 005 MATERIAL QTY PER A/C SEE NOTES Kit 363040D03R00 1 Kit 363040D05R01 1 Consumable CMLD01 1 **CONF ALL B. CONCURRENT REQUIREMENTS None C. REASON (1) History A global review of the compliance of the JAR 25.0863 and SFAR88 has highlighted potential deviations in specific cases. In particular, deviations have been found in Section 19, consequently, it has been required to introduce several flexible thermal insulation muffs in the ducting of the APU Pneumatics Distribution (Bleed) System. The goal is avoiding hot surfaces during APU Bleed operation. (2) Objective/Action Thermal Insulation Muffs will be installed on joint connections ducts and retainer rings of APU Bleed System in rear fuselage zone thru frame 95. The Muffs have a venting hole to point-leaking hot air directly towards the adjacent sensing elements of the Overheat Detection System (OHDS). This Service Bulletin is issued to give the instructions to install Insulation Muffs and to modify the OHDS sensing element installation. (3) Advantages The accomplishment of this Service Bulletin will minimize the possible ignition sources.
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 6 0

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# @A330 SERVICE BULLETIN (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 363040-831-943-001: Modification (1) Remove the sensing element 140HF (2) Install the insulation sleeves (3) Install the new sensing element 140HF **CONF 002 Task 363040-831-943-001: Modification (1) Loosen the sensing element 140HF (2) Install the insulation sleeves (3) Reroute the sensing element 140HF **CONF 003 Task 363040-831-943-001: Modification (1) Loosen the sensing element 140HF (2) Install the insulation sleeves (3) Reroute the sensing element 140HF **CONF 004 Task 363040-831-943-001: Modification (1) Loosen the sensing element 140HF (2) Install the insulation sleeves (3) Reroute the sensing element 140HF **CONF 005 Task 363040-831-943-001: Modification (1) Loosen the sensing element 140HF DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 7 0

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# @A330 SERVICE BULLETIN (2) Install the insulation sleeves (3) Reroute the sensing element 140HF **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. The accomplishment timescale, which has not yet been defined, will be given in the AD. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. **CONF 001 Task 363040-831-943-001: Modification Get Access 0.75 On Aircraft Remove the sensing element 140HF 4.50 Install the insulation sleeves 1.50 Install the new sensing element 140HF 6.25 Tests 1.00 Close-Up 0.50 TOTAL MANHOURS 14.50 ELAPSED TIME (HOURS) 14.00
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 8 0

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# @A330 SERVICE BULLETIN
**CONF 002 Task 363040-831-943-001: Modification Get Access 0.75 On Aircraft Loosen the sensing element 140HF 2.00 Install the insulation sleeves 2.25 Reroute the sensing element 140HF 1.75 Tests 1.00 Close-Up 0.50 TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF 003 Task 363040-831-943-001: Modification Get Access 0.75 On Aircraft Loosen the sensing element 140HF 2.00 Install the insulation sleeves 2.25 Reroute the sensing element 140HF 1.75 Tests 1.00 Close-Up 0.50 TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF 004 Task 363040-831-943-001: Modification Get Access 0.75 On Aircraft Loosen the sensing element 140HF 2.00 Install the insulation sleeves 2.25 Reroute the sensing element 140HF 1.75 Tests 1.00 Close-Up 0.50 TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF 005 Task 363040-831-943-001: Modification Get Access 0.75 On Aircraft Loosen the sensing element 140HF 2.00 Install the insulation sleeves 2.25 Reroute the sensing element 140HF 1.75 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 9 0

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# @A330 SERVICE BULLETIN
Task 363040-831-943-001: Modification Tests 1.00 Close-Up 0.50 TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF ALL H. WEIGHT AND BALANCE **CONF 001 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +1.736 KG (+3.8271 LB) Effect on Balance +110.142 KGM (+796.657 LB.FT ) **CONF 002 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +1.559 KG (+3.4369 LB) Effect on Balance +99.068 KGM (+716.558 LB.FT ) **CONF 003 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +1.503 KG (+3.3135 LB) Effect on Balance +87.336 KGM (+631.701 LB.FT ) **CONF 004 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +1.559 KG (+3.4369 LB) Effect on Balance +90.579 KGM (+655.157 LB.FT ) **CONF 005 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07. DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 10 0

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# @A330 SERVICE BULLETIN Manufacturers Empty Weight +1.503 KG (+3.3135 LB) Effect on Balance +95.529 KGM (+690.961 LB.FT ) **CONF ALL I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 36-22-00 36-22-17 52-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-05-01 Standards Manual (SM) Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 36-22-00 36-22-17 52-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00 Standards Manual (SM) Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 003 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 36-22-00 36-22-17 52-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00 Standards Manual (SM) Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 004 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 36-22-00 36-22-17 52-41-00 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 11 0

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# @A330 SERVICE BULLETIN Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00 Standards Manual (SM) Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 005 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 36-22-00 36-22-17 52-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00 Standards Manual (SM) Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF ALL K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 36-12-41 36-22-17 Illustrated Parts Catalog (IPC) 36-12-04 36-22-04 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 12 0

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# @A330 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 363040D01R01 Kit 363040D02R00 Kit 363040D03R00 Kit 363040D04R00 Kit 363040D05R01 Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 Hamburg Germany For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 2590 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability

Kit 363040D01R01 Cost 3,060.00 USD Availability 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 363040D02R00 Cost 3,440.00 USD Availability 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 363040D03R00 Cost 3,700.00 USD Availability 150 calendar days from receipt of order DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 13 0

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# @A330 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 363040D04R00 Cost 1,880.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 363040D05R01 Cost 33.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS Kit 363040D01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 F3617062400000 1 SLEEVE 2 F3617062400200 1 SLEEVE 3 F3617062400400 1 SLEEVE 4 F3617062400600 1 SLEEVE 5 F3617062400800 1 SLEEVE 6 F3617062401000 1 SLEEVE 7 F3617062401800 1 SLEEVE 8 F3617062405200 1 SLEEVE 9 F3617062404200 1 SLEEVE DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 14 0

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 17 NSA5539S 1 SLEEVE NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363040D02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 F3617062400000 1 SLEEVE 2 F3617062400200 1 SLEEVE 9 F3617062404200 1 SLEEVE 12 F3617062405000 1 SLEEVE 13 F3617062401600 1 SLEEVE 14 F3617062403800 1 SLEEVE 15 F3617062404800 1 SLEEVE 16 F3617062404400 1 SLEEVE 17 NSA5539S 3 SLEEVE NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363040D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 9 F3617062404200 1 SLEEVE 10 F3617062404600 1 SLEEVE 11 F3617062402200 1 SLEEVE 12 F3617062405000 1 SLEEVE 13 F3617062401600 1 SLEEVE 14 F3617062403800 1 SLEEVE 15 F3617062404800 1 SLEEVE 16 F3617062404400 1 SLEEVE 17 NSA5539S 4 SLEEVE NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 15 0

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# @A330 SERVICE BULLETIN
Kit 363040D04R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 17 NSA5539S 22 SLEEVE 18 35660-2-310 1 ELEMENT 19 NSA935401-04 1 TIE 27 NSA5110-3-1 2 NUT 29 NAS1801-3-5 2 SCREW 31 NAS1149D0332K 3 WASHER 32 NSA5538-00 4 CLAMP 33 NSA5527-03-13 1 SPACER 34 NAS1801-3-28 1 SCREW 35 NAS1801-3-13 1 SCREW 36 NSA5527-03-08D 1 SPACER NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363040D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 17 NSA5539S 5 SLEEVE 35 NAS1801-3-13 1 SCREW NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required Lockwire Stainless Steel or Nickel Alloy 19-018 As required (2) Components None

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 16 0

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# @A330 SERVICE BULLETIN (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 17 0

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# @A330 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 18 0

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# @A330 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 363040-831-943-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone 210 310 Modified FIN 313AL 312AR 34HF 139HF 140HF Access Door 312AR 313AL Manpower TOTAL MANHOURS 14.50 ELAPSED TIME (HOURS) 14.00 **CONF 002 Zone 210 310 Modified FIN 313AL 312AR 140HF Access Door 312AR 313AL Manpower TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 19 0

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# @A330 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 140HF Access Door 312AR 313AL Manpower TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF 005 Zone 210 310 Modified FIN 313AL 312AR 140HF Access Door 312AR 313AL Manpower TOTAL MANHOURS 8.25 ELAPSED TIME (HOURS) 7.75 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 363040-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 20 0

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# @A330 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001). (c) For the Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001). (d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block 001). (e) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM 20-25-51). (f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA). (g) Tag all the parts you must remove and retain to make the subsequent installation easier. (h) Put blanking plugs on the disconnected line ends. (2) Subtask 363040-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 363040-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Consumable Material List (CML) DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 21 0

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# @A330 SERVICE BULLETIN
References Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001). (c) For the Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001). (d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block 001). (e) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM 20-25-51). (f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA). (g) Tag all the parts you must remove and retain to make the subsequent installation easier. (h) Put blanking plugs on the disconnected line ends. (2) Subtask 363040-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 003 (1) Subtask 363040-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 22 0

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# @A330 SERVICE BULLETIN
References Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001). (c) For the Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001). (d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block 001). (e) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM 20-25-51). (f) For tolerances for waviness and bends in sensing element wire (Refer to Fig. AGBEAA). (g) Tag all the parts you must remove and retain to make the subsequent installation easier. (h) Put blanking plugs on the disconnected line ends. (2) Subtask 363040-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 004 (1) Subtask 363040-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 23 0

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# @A330 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 363040-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 005 (1) Subtask 363040-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001). (c) For the Frames (FR) identification (Refer to AMM 06-31-53, Page Block 001). DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 24 0

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# @A330 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 363040-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 363040-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 52-41-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position below the access doors 312AR and 313AL. (c) Open and safety the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (d) Open and safety the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (e) Set the light switch 4LJ in the ON position. DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 25 0

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# @A330 SERVICE BULLETIN
**CONF 002 (1) Subtask 363040-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 52-41-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position below the access doors 312AR and 313AL. (c) Open and safety the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (d) Open and safety the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (e) Set the light switch 4LJ in the ON position. **CONF 003 (1) Subtask 363040-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 52-41-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position below the access doors 312AR and 313AL. (c) Open and safety the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001).
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 26 0

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# @A330 SERVICE BULLETIN (d) Open and safety the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (e) Set the light switch 4LJ in the ON position. **CONF 004 (1) Subtask 363040-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 52-41-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position below the access doors 312AR and 313AL. (c) Open and safety the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (d) Open and safety the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (e) Set the light switch 4LJ in the ON position. **CONF 005 (1) Subtask 363040-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 52-41-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position below the access doors 312AR and 313AL. DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 27 0

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# @A330 SERVICE BULLETIN (c) Open and safety the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (d) Open and safety the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (e) Set the light switch 4LJ in the ON position. **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 363040-831-201-001 - Remove the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Work location from Frame 88 to Frame 93 Manpower Resources Manhours 4.50 Minimum number of person 1 Subtask elapsed time 4.50 Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-802 Fig. A-GBBAA Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) As a standard procedure clean the work areas if necessary, with: Solvent General Purpose 11-026 As required
and Lint-Free Cotton Cloth 19-003 As required DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 28 0

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# @A330 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.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 29 0

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# @A330 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 363040-831-202-001 - Install the insulation sleeves Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Work location from Frame 83 to Frame 94 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills NON SPECIFIC
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 30 0

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363040D01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 F3617062400000 1 SLEEVE 2 F3617062400200 1 SLEEVE 3 F3617062400400 1 SLEEVE 4 F3617062400600 1 SLEEVE 5 F3617062400800 1 SLEEVE 6 F3617062401000 1 SLEEVE 7 F3617062401800 1 SLEEVE 8 F3617062405200 1 SLEEVE 9 F3617062404200 1 SLEEVE References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-400-801 Fig. A-GBCAA Installation of the Sleeves on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 (a) Install the insulation sleeves on the APU bleed-air duct. Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 03

. 1 Loosen the remaining sensing elements 139HF and 33HF between Frame 83 thru Frame 88, in preparation for the installation of the insulation sleeves, refer to AMM Task 36-22-17-000-801. 2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU bleed-air-duct: Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 03

. 1 Sleeve Assy F3617062400000 Item 1 1 Sleeve Assy F3617062400200 Item 2 1 Sleeve Assy F3617062400400 Item 3 1 Sleeve Assy F3617062400600 Item 4 1 Sleeve Assy F3617062400800 Item 5 1 Sleeve Assy F3617062401000 Item 6 1 Sleeve Assy F3617062401800 Item 7
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 31 0

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# @A330 SERVICE BULLETIN 1 Sleeve Assy F3617062405200 Item 8 1 Sleeve Assy F3617062404200 Item 9 NOTE: Make sure that the sensing element goes across the blowout apertures. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. 3 Reinstall the remaining sensing elements between Frame 83 thru Frame 88, refer to AMM Task 36-22-17-400-801. (3) Subtask 363040-831-203-001 - Install the new sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 88 to Frame 95 Manpower Resources Manhours 6.25 Minimum number of person 1 Subtask elapsed time 6.25 Skills ELECTRICAL Material necessary to do the job Kit 363040D01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 17 NSA5539S 1 SLEEVE Kit 363040D04R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 17 NSA5539S 22 SLEEVE 18 35660-2-310 1 ELEMENT 19 NSA935401-04 1 TIE 27 NSA5110-3-1 2 NUT 29 NAS1801-3-5 2 SCREW 31 NAS1149D0332K 3 WASHER 32 NSA5538-00 4 CLAMP 33 NSA5527-03-13 1 SPACER 34 NAS1801-3-28 1 SCREW 35 NAS1801-3-13 1 SCREW 36 NSA5527-03-08D 1 SPACER

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 32 0

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# @A330 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.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 33 0

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# @A330 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.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 34 0

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# @A330 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.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 35 0

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# @A330 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.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 36 0

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# @A330 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 363040-831-201-002 - Loosen the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 93 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-802 Fig. A-GBBAB Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct Sheet 01 Sheet 02 (a) As a standard procedure clean the work areas if necessary, with: Solvent General Purpose 11-026 As required
and

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 37 0

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# @A330 SERVICE BULLETIN
Lint-Free Cotton Cloth 19-003 As required (b) Loosen the sensing element 140HF from the APU bleed-air-duct. Refer to Fig. A-GBBAB Sheet 01 and Fig. A-GBBAB Sheet 02

. Refer to AMM Task 36-22-17-000-802. 1 Between Frame 91 thru Frame 93, open the clamps: Refer to Fig. A-GBBAB Sheet 02, View E. 4 Clamp-single NAS5538-00 Item (26) Retain and remove: 4 Sleeve-Protective NSA5539S Item (17) Discard 2 At Frame 93, remove: Refer to Fig. A-GBBAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item (17) Discard 1 Spacer NSA5527-03-01 Item (24) Retain 1 Clamp-single NAS5538-00 Item (26) Retain with 1 Screw NAS1096-3-13 Item (30) Discard 3 Between Frame 93 and Frame 94, open the upper part of the double clamp and remove: Refer to Fig. A-GBBAB Sheet 02, View C. 1 Sleeve-Protective NSA5539S Item (17) Discard 4 Between Frame 91 thru Frame 94, remove the sensing element from the opened clamps: Refer to AMM Task 36-22-17-000-802. Refer to Fig. A-GBBAB Sheet 02, View B. 1 Sensing Element 140HF Item (36) Retain

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 38 0

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# @A330 SERVICE BULLETIN (2) Subtask 363040-831-202-002 - Install the insulation sleeves Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 83 to Frame 94 Manpower Resources Manhours 2.25 Minimum number of person 1 Subtask elapsed time 2.25 Skills NON SPECIFIC Material necessary to do the job Kit 363040D02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 F3617062400000 1 SLEEVE 2 F3617062400200 1 SLEEVE 9 F3617062404200 1 SLEEVE 12 F3617062405000 1 SLEEVE 13 F3617062401600 1 SLEEVE 14 F3617062403800 1 SLEEVE 15 F3617062404800 1 SLEEVE 16 F3617062404400 1 SLEEVE 17 NSA5539S 3 SLEEVE References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-400-801 Fig. A-GBCAB Installation of the Sleeves on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 (a) Install the insulation sleeves on the APU bleed-air duct. Refer to Fig. A-GBCAB Sheet 01 thru Fig. A-GBCAB Sheet 03

. 1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame 94, in preparation for the installation of the insulation sleeves, refer to AMM Task 36-22-17-000-801. 2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU bleed-air-duct: Refer to Fig. A-GBCAB Sheet 01 thru Fig. A-GBCAB Sheet 03

. 1 Sleeve Assy F3617062400000 Item 1
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 39 0

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# @A330 SERVICE BULLETIN 1 Sleeve Assy F3617062400200 Item 2 1 Sleeve Assy F3617062404200 Item 9 1 Sleeve Assy F3617062405000 Item 12 1 Sleeve Assy F3617062401600 Item 13 1 Sleeve Assy F3617062404800 Item 15 1 Sleeve Assy F3617062404400 Item 16 NOTE: Make sure that the sensing element goes across the blowout apertures. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. 3 Install the insulation sleeve between Frame 86 and Frame 87. Refer to Fig. A-GBCAB Sheet 03, View F. a For the installation of the insulation sleeve, Item 14, open the detection clips and lift the sensing element from the brackets. b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the brackets and install: 1 Sleeve Assy F3617062403800 Item 14
c Reinstall the sensing element. 4 Install new protective sleeves on the sensing elements between Frame 84 and Frame 85, at Frame 88, and at Frame 91: Refer to Fig. A-GBCAB Sheet 02, View D, and Fig. A-GBCAB Sheet 03, Views G and H. 3 Sleeve-Protective NSA5539S Item 17 5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the sensing element 140HF (Refer to AMM Task 36-22-17-400-801). (3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 94

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 40 0

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 1.75 Minimum number of person 1 Subtask elapsed time 1.75 Skills ELECTRICAL Material necessary to do the job Kit 363040D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 17 NSA5539S 5 SLEEVE 35 NAS1801-3-13 1 SCREW References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802 Fig. A-GBDAB Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02
NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. (a) Reroute the sensing element 140HF on the APU bleed-air duct and install the clamps. Refer to Fig. A-GBDAB Sheet 01 thru Fig. A-GBDAB Sheet 03

. Refer to AMM Task 36-22-17-400-802. 1 Between Frame 90 and Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View E. 4 Sleeve-Protective NSA5539S Item 17 and close: 4 Clamp-single NAS5538-00 Item (26) Retained at removal 2 At Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item 17

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 41 0

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# @A330 SERVICE BULLETIN 1 Spacer NSA5527-03-01 Item (24) Retained at removal 1 Clamp-single NAS5538-00 Item (26) Retained at removal with 1 Screw NAS1801-3-13 Item 35 3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in). 4 Between Frame 93 and Frame 94, close the upper part of the double clamp without the sensing element 140HF. Refer to Fig. A-GBDAB Sheet 02, View C. NOTE: Only the lower part of the clamp stays in use. 5 Between Frame 90 thru 94, reroute the sensing element 140HF. a STEP 1 thru STEP 2: Refer to Fig. A-GBDAB Sheet 03

. <1> From Frame 94 to Frame 93, route the sensing element 140HF straight from the clamp at STEP 1 to the next clamp at STEP 2. 1 Sensing Element 140HF Item (36) Retained at removal NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. b STEP 3 thru STEP 6 Refer to Fig. A-GBDAB Sheet 03

. <1> Install the sensing element 140HF by following the installation position sequence STEP 3 thru STEP 6. NOTE: Make sure that the sensing element wire is routed with an acceptable distance to the insulation sleeve at STEP 6. NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 42 0

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# @A330 SERVICE BULLETIN Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. **CONF 003 (1) Subtask 363040-831-201-002 - Loosen the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 93 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-802 Fig. A-GBBAB Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct Sheet 01 Sheet 02 (a) As a standard procedure clean the work areas if necessary, with: Solvent General Purpose 11-026 As required
and Lint-Free Cotton Cloth 19-003 As required (b) Loosen the sensing element 140HF from the APU bleed-air-duct. Refer to Fig. A-GBBAB Sheet 01 and Fig. A-GBBAB Sheet 02

. DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 43 0

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# @A330 SERVICE BULLETIN
Refer to AMM Task 36-22-17-000-802. 1 Between Frame 91 thru Frame 93, open the clamps: Refer to Fig. A-GBBAB Sheet 02, View E. 4 Clamp-single NAS5538-00 Item (26) Retain and remove: 4 Sleeve-Protective NSA5539S Item (17) Discard 2 At Frame 93, remove: Refer to Fig. A-GBBAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item (17) Discard 1 Spacer NSA5527-03-01 Item (24) Retain 1 Clamp-single NAS5538-00 Item (26) Retain with 1 Screw NAS1096-3-13 Item (30) Discard 3 Between Frame 93 and Frame 94, open the upper part of the double clamp and remove: Refer to Fig. A-GBBAB Sheet 02, View C. 1 Sleeve-Protective NSA5539S Item (17) Discard 4 Between Frame 91 thru Frame 94, remove the sensing element from the opened clamps: Refer to AMM Task 36-22-17-000-802. Refer to Fig. A-GBBAB Sheet 02, View B. 1 Sensing Element 140HF Item (36) Retain (2) Subtask 363040-831-202-003 - Install the insulation sleeves Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 83 to Frame 94

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 44 0

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 2.25 Minimum number of person 1 Subtask elapsed time 2.25 Skills NON SPECIFIC Material necessary to do the job Kit 363040D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 9 F3617062404200 1 SLEEVE 10 F3617062404600 1 SLEEVE 11 F3617062402200 1 SLEEVE 12 F3617062405000 1 SLEEVE 13 F3617062401600 1 SLEEVE 14 F3617062403800 1 SLEEVE 15 F3617062404800 1 SLEEVE 16 F3617062404400 1 SLEEVE 17 NSA5539S 4 SLEEVE References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-400-801 Fig. A-GBCAC Installation of the Sleeves on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 (a) Install the insulation sleeves on the APU bleed-air duct. Refer to Fig. A-GBCAC Sheet 01 thru Fig. A-GBCAC Sheet 03

. 1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame 94, in preparation for the installation of the insulation sleeves, refer to AMM Task 36-22-17-000-801. 2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU bleed-air-duct: Refer to Fig. A-GBCAC Sheet 01 thru Fig. A-GBCAC Sheet 03

. 1 Sleeve Assy F3617062404200 Item 9 1 Sleeve Assy F3617062404600 Item 10 1 Sleeve Assy F3617062402200 Item 11 1 Sleeve Assy F3617062405000 Item 12
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 45 0

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# @A330 SERVICE BULLETIN 1 Sleeve Assy F3617062401600 Item 13 1 Sleeve Assy F3617062404800 Item 15 1 Sleeve Assy F3617062404400 Item 16 NOTE: Make sure that the sensing element goes across the blowout apertures. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. 3 Install the insulation sleeve between Frame 86 and Frame 87. Refer to Fig. A-GBCAC Sheet 03, View F. a For the installation of the insulation sleeve, Item 14, open the detection clips and lift the sensing element from the brackets. b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the brackets and install: 1 Sleeve Assy F3617062403800 Item 14
c Reinstall the sensing element. 4 Install new protective sleeves on the sensing elements at Frame 83, between Frame 84 and Frame 85, at Frame 88, and at Frame 91: Refer to Fig. A-GBCAC Sheet 02, Views B and D, and Fig. A-GBCAC Sheet 03, Views G and H. 4 Sleeve-Protective NSA5539S Item 17 5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the sensing element 140HF (Refer to AMM Task 36-22-17-400-801). (3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 94 Manpower Resources Manhours 1.75 Minimum number of person 1 Subtask elapsed time 1.75 Skills ELECTRICAL

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 46 0

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363040D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 17 NSA5539S 5 SLEEVE 35 NAS1801-3-13 1 SCREW References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802 Fig. A-GBDAB Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02
NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. (a) Reroute the sensing element 140HF on the APU bleed-air duct and install the clamps. Refer to Fig. A-GBDAB Sheet 01 thru Fig. A-GBDAB Sheet 03

. Refer to AMM Task 36-22-17-400-802. 1 Between Frame 90 and Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View E. 4 Sleeve-Protective NSA5539S Item 17 and close: 4 Clamp-single NAS5538-00 Item (26) Retained at removal 2 At Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item 17 1 Spacer NSA5527-03-01 Item (24) Retained at removal 1 Clamp-single NAS5538-00 Item (26) Retained at removal with
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 47 0

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# @A330 SERVICE BULLETIN
1 Screw NAS1801-3-13 Item 35 3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in). 4 Between Frame 93 and Frame 94, close the upper part of the double clamp without the sensing element 140HF. Refer to Fig. A-GBDAB Sheet 02, View C. NOTE: Only the lower part of the clamp stays in use. 5 Between Frame 90 thru 94, reroute the sensing element 140HF. a STEP 1 thru STEP 2: Refer to Fig. A-GBDAB Sheet 03

. <1> From Frame 94 to Frame 93, route the sensing element 140HF straight from the clamp at STEP 1 to the next clamp at STEP 2. 1 Sensing Element 140HF Item (36) Retained at removal NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. b STEP 3 thru STEP 6 Refer to Fig. A-GBDAB Sheet 03

. <1> Install the sensing element 140HF by following the installation position sequence STEP 3 thru STEP 6. NOTE: Make sure that the sensing element wire is routed with an acceptable distance to the insulation sleeve at STEP 6. NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 48 0

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# @A330 SERVICE BULLETIN
**CONF 004 (1) Subtask 363040-831-201-002 - Loosen the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 93 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-802 Fig. A-GBBAB Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct Sheet 01 Sheet 02 (a) As a standard procedure clean the work areas if necessary, with: Solvent General Purpose 11-026 As required
and Lint-Free Cotton Cloth 19-003 As required (b) Loosen the sensing element 140HF from the APU bleed-air-duct. Refer to Fig. A-GBBAB Sheet 01 and Fig. A-GBBAB Sheet 02

. Refer to AMM Task 36-22-17-000-802. 1 Between Frame 91 thru Frame 93, open the clamps: Refer to Fig. A-GBBAB Sheet 02, View E. 4 Clamp-single NAS5538-00 Item (26) Retain DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 49 0

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# @A330 SERVICE BULLETIN
and remove: 4 Sleeve-Protective NSA5539S Item (17) Discard 2 At Frame 93, remove: Refer to Fig. A-GBBAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item (17) Discard 1 Spacer NSA5527-03-01 Item (24) Retain 1 Clamp-single NAS5538-00 Item (26) Retain with 1 Screw NAS1096-3-13 Item (30) Discard 3 Between Frame 93 and Frame 94, open the upper part of the double clamp and remove: Refer to Fig. A-GBBAB Sheet 02, View C. 1 Sleeve-Protective NSA5539S Item (17) Discard 4 Between Frame 91 thru Frame 94, remove the sensing element from the opened clamps: Refer to AMM Task 36-22-17-000-802. Refer to Fig. A-GBBAB Sheet 02, View B. 1 Sensing Element 140HF Item (36) Retain (2) Subtask 363040-831-202-002 - Install the insulation sleeves Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 83 to Frame 94 Manpower Resources Manhours 2.25 Minimum number of person 1 Subtask elapsed time 2.25 Skills NON SPECIFIC

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 50 0

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363040D02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 F3617062400000 1 SLEEVE 2 F3617062400200 1 SLEEVE 9 F3617062404200 1 SLEEVE 12 F3617062405000 1 SLEEVE 13 F3617062401600 1 SLEEVE 14 F3617062403800 1 SLEEVE 15 F3617062404800 1 SLEEVE 16 F3617062404400 1 SLEEVE 17 NSA5539S 3 SLEEVE References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-400-801 Fig. A-GBCAB Installation of the Sleeves on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 (a) Install the insulation sleeves on the APU bleed-air duct. Refer to Fig. A-GBCAB Sheet 01 thru Fig. A-GBCAB Sheet 03

. 1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame 94, in preparation for the installation of the insulation sleeves, refer to AMM Task 36-22-17-000-801. 2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU bleed-air-duct: Refer to Fig. A-GBCAB Sheet 01 thru Fig. A-GBCAB Sheet 03

. 1 Sleeve Assy F3617062400000 Item 1 1 Sleeve Assy F3617062400200 Item 2 1 Sleeve Assy F3617062404200 Item 9 1 Sleeve Assy F3617062405000 Item 12 1 Sleeve Assy F3617062401600 Item 13 1 Sleeve Assy F3617062404800 Item 15 1 Sleeve Assy F3617062404400 Item 16 NOTE: Make sure that the sensing element goes across the blowout DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 51 0

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# @A330 SERVICE BULLETIN apertures. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. 3 Install the insulation sleeve between Frame 86 and Frame 87. Refer to Fig. A-GBCAB Sheet 03, View F. a For the installation of the insulation sleeve, Item 14, open the detection clips and lift the sensing element from the brackets. b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the brackets and install: 1 Sleeve Assy F3617062403800 Item 14
c Reinstall the sensing element. 4 Install new protective sleeves on the sensing elements between Frame 84 and Frame 85, at Frame 88, and at Frame 91: Refer to Fig. A-GBCAB Sheet 02, View D, and Fig. A-GBCAB Sheet 03, Views G and H. 3 Sleeve-Protective NSA5539S Item 17 5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the sensing element 140HF (Refer to AMM Task 36-22-17-400-801). (3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 94 Manpower Resources Manhours 1.75 Minimum number of person 1 Subtask elapsed time 1.75 Skills ELECTRICAL Material necessary to do the job Kit 363040D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 17 NSA5539S 5 SLEEVE 35 NAS1801-3-13 1 SCREW
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 52 0

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# @A330 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802 Fig. A-GBDAB Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02
NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. (a) Reroute the sensing element 140HF on the APU bleed-air duct and install the clamps. Refer to Fig. A-GBDAB Sheet 01 thru Fig. A-GBDAB Sheet 03

. Refer to AMM Task 36-22-17-400-802. 1 Between Frame 90 and Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View E. 4 Sleeve-Protective NSA5539S Item 17 and close: 4 Clamp-single NAS5538-00 Item (26) Retained at removal 2 At Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item 17 1 Spacer NSA5527-03-01 Item (24) Retained at removal 1 Clamp-single NAS5538-00 Item (26) Retained at removal with 1 Screw NAS1801-3-13 Item 35 3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in). 4 Between Frame 93 and Frame 94, close the upper part of the double clamp without the sensing element 140HF. Refer to Fig. A-GBDAB Sheet 02, View C.
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 53 0

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# @A330 SERVICE BULLETIN
NOTE: Only the lower part of the clamp stays in use. 5 Between Frame 90 thru 94, reroute the sensing element 140HF. a STEP 1 thru STEP 2: Refer to Fig. A-GBDAB Sheet 03

. <1> From Frame 94 to Frame 93, route the sensing element 140HF straight from the clamp at STEP 1 to the next clamp at STEP 2. 1 Sensing Element 140HF Item (36) Retained at removal NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. b STEP 3 thru STEP 6 Refer to Fig. A-GBDAB Sheet 03

. <1> Install the sensing element 140HF by following the installation position sequence STEP 3 thru STEP 6. NOTE: Make sure that the sensing element wire is routed with an acceptable distance to the insulation sleeve at STEP 6. NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. **CONF 005 (1) Subtask 363040-831-201-002 - Loosen the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 93 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 54 0

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-802 Fig. A-GBBAB Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct Sheet 01 Sheet 02 (a) As a standard procedure clean the work areas if necessary, with: Solvent General Purpose 11-026 As required
and Lint-Free Cotton Cloth 19-003 As required (b) Loosen the sensing element 140HF from the APU bleed-air-duct. Refer to Fig. A-GBBAB Sheet 01 and Fig. A-GBBAB Sheet 02

. Refer to AMM Task 36-22-17-000-802. 1 Between Frame 91 thru Frame 93, open the clamps: Refer to Fig. A-GBBAB Sheet 02, View E. 4 Clamp-single NAS5538-00 Item (26) Retain and remove: 4 Sleeve-Protective NSA5539S Item (17) Discard 2 At Frame 93, remove: Refer to Fig. A-GBBAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item (17) Discard DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 55 0

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# @A330 SERVICE BULLETIN 1 Spacer NSA5527-03-01 Item (24) Retain 1 Clamp-single NAS5538-00 Item (26) Retain with 1 Screw NAS1096-3-13 Item (30) Discard 3 Between Frame 93 and Frame 94, open the upper part of the double clamp and remove: Refer to Fig. A-GBBAB Sheet 02, View C. 1 Sleeve-Protective NSA5539S Item (17) Discard 4 Between Frame 91 thru Frame 94, remove the sensing element from the opened clamps: Refer to AMM Task 36-22-17-000-802. Refer to Fig. A-GBBAB Sheet 02, View B. 1 Sensing Element 140HF Item (36) Retain (2) Subtask 363040-831-202-003 - Install the insulation sleeves Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 83 to Frame 94 Manpower Resources Manhours 2.25 Minimum number of person 1 Subtask elapsed time 2.25 Skills NON SPECIFIC Material necessary to do the job Kit 363040D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 9 F3617062404200 1 SLEEVE 10 F3617062404600 1 SLEEVE 11 F3617062402200 1 SLEEVE 12 F3617062405000 1 SLEEVE 13 F3617062401600 1 SLEEVE 14 F3617062403800 1 SLEEVE 15 F3617062404800 1 SLEEVE DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 56 0

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 16 F3617062404400 1 SLEEVE 17 NSA5539S 4 SLEEVE References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-400-801 Fig. A-GBCAC Installation of the Sleeves on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 (a) Install the insulation sleeves on the APU bleed-air duct. Refer to Fig. A-GBCAC Sheet 01 thru Fig. A-GBCAC Sheet 03

. 1 Loosen the sensing elements 139HF and 33HF between Frame 83 thru Frame 94, in preparation for the installation of the insulation sleeves, refer to AMM Task 36-22-17-000-801. 2 Between Frame 83 thru Frame 94, install the insulation sleeves on the APU bleed-air-duct: Refer to Fig. A-GBCAC Sheet 01 thru Fig. A-GBCAC Sheet 03

. 1 Sleeve Assy F3617062404200 Item 9 1 Sleeve Assy F3617062404600 Item 10 1 Sleeve Assy F3617062402200 Item 11 1 Sleeve Assy F3617062405000 Item 12 1 Sleeve Assy F3617062401600 Item 13 1 Sleeve Assy F3617062404800 Item 15 1 Sleeve Assy F3617062404400 Item 16 NOTE: Make sure that the sensing element goes across the blowout apertures. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. 3 Install the insulation sleeve between Frame 86 and Frame 87. Refer to Fig. A-GBCAC Sheet 03, View F. a For the installation of the insulation sleeve, Item 14, open the detection clips and lift the sensing element from the brackets. DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 57 0

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# @A330 SERVICE BULLETIN
b Pull the anti-rotation devices of the insulation sleeve, Item 14, over the brackets and install: 1 Sleeve Assy F3617062403800 Item 14
c Reinstall the sensing element. 4 Install new protective sleeves on the sensing elements at Frame 83, between Frame 84 and Frame 85, at Frame 88, and at Frame 91: Refer to Fig. A-GBCAC Sheet 02, Views B and D, and Fig. A-GBCAC Sheet 03, Views G and H. 4 Sleeve-Protective NSA5539S Item 17 5 Reinstall the sensing elements between Frame 83 thru Frame 94, except the sensing element 140HF (Refer to AMM Task 36-22-17-400-801). (3) Subtask 363040-831-203-002 - Reroute the sensing element 140HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Work location from Frame 90 to Frame 94 Manpower Resources Manhours 1.75 Minimum number of person 1 Subtask elapsed time 1.75 Skills ELECTRICAL Material necessary to do the job Kit 363040D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 17 NSA5539S 5 SLEEVE 35 NAS1801-3-13 1 SCREW References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-802 Fig. A-GBDAB Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct Sheet 01 Sheet 02 Sheet 03 Fig. A-GBEAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02
NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 58 0

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# @A330 SERVICE BULLETIN (a) Reroute the sensing element 140HF on the APU bleed-air duct and install the clamps. Refer to Fig. A-GBDAB Sheet 01 thru Fig. A-GBDAB Sheet 03

. Refer to AMM Task 36-22-17-400-802. 1 Between Frame 90 and Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View E. 4 Sleeve-Protective NSA5539S Item 17 and close: 4 Clamp-single NAS5538-00 Item (26) Retained at removal 2 At Frame 93, install: Refer to Fig. A-GBDAB Sheet 02, View D. 1 Sleeve-Protective NSA5539S Item 17 1 Spacer NSA5527-03-01 Item (24) Retained at removal 1 Clamp-single NAS5538-00 Item (26) Retained at removal with 1 Screw NAS1801-3-13 Item 35 3 Torque tighten the screw, Item 35, to 0.40m.daN (35.403lbf.in). 4 Between Frame 93 and Frame 94, close the upper part of the double clamp without the sensing element 140HF. Refer to Fig. A-GBDAB Sheet 02, View C. NOTE: Only the lower part of the clamp stays in use. 5 Between Frame 90 thru 94, reroute the sensing element 140HF. a STEP 1 thru STEP 2: Refer to Fig. A-GBDAB Sheet 03

. <1> From Frame 94 to Frame 93, route the sensing element 140HF straight from the clamp at STEP 1 to the next clamp at STEP 2. 1 Sensing Element 140HF Item (36) Retained at removal DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 59 0

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# @A330 SERVICE BULLETIN
NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. b STEP 3 thru STEP 6 Refer to Fig. A-GBDAB Sheet 03

. <1> Install the sensing element 140HF by following the installation position sequence STEP 3 thru STEP 6. NOTE: Make sure that the sensing element wire is routed with an acceptable distance to the insulation sleeve at STEP 6. NOTE: For tolerances for waviness and bends in sensing element wire, refer to Fig. A-GBEAA Sheet 01 and Fig. A-GBEAA Sheet 02

. NOTE: The positions of the blowout apertures of the APU bleed-air duct must be under the sensing element. NOTE: Make sure that there is no contact between the sensing element and the insulation sleeves. **CONF ALL D. TEST **CONF 001 (1) Subtask 363040-710-201-001 - Operational Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806 (a) Set the light switch 4LJ in the OFF position. (b) Do the operational test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 60 0

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# @A330 SERVICE BULLETIN
**CONF 002 (1) Subtask 363040-710-201-001 - Operational Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806 (a) Set the light switch 4LJ in the OFF position. (b) Do the operational test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). **CONF 003 (1) Subtask 363040-710-201-001 - Operational Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806 (a) Set the light switch 4LJ in the OFF position. (b) Do the operational test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). **CONF 004 (1) Subtask 363040-710-201-001 - Operational Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806 DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 61 0

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# @A330 SERVICE BULLETIN (a) Set the light switch 4LJ in the OFF position. (b) Do the operational test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). **CONF 005 (1) Subtask 363040-710-201-001 - Operational Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806 (a) Set the light switch 4LJ in the OFF position. (b) Do the operational test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 363040-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (c) Release and close the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (d) Remove the access platform(s). DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 62 0

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# @A330 SERVICE BULLETIN (e) Remove the warning notices from the cockpit. **CONF 002 (1) Subtask 363040-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (c) Release and close the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (d) Remove the access platform(s). (e) Remove the warning notices from the cockpit. **CONF 003 (1) Subtask 363040-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (c) Release and close the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 63 0

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# @A330 SERVICE BULLETIN (d) Remove the access platform(s). (e) Remove the warning notices from the cockpit. **CONF 004 (1) Subtask 363040-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (c) Release and close the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (d) Remove the access platform(s). (e) Remove the warning notices from the cockpit. **CONF 005 (1) Subtask 363040-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001).
DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 64 0

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# @A330 SERVICE BULLETIN (c) Release and close the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (d) Remove the access platform(s). (e) Remove the warning notices from the cockpit.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 65 0

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# @A330 SERVICE BULLETIN

**CONF 001

Z310 

### A

FR80 FR88 FR95 FR98 FR100

140HF



## A (18) 

### B

G_SB_363040_6_BBAA_01_01 Figure A-GBBAA - Sheet 01 Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 66 0

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# @A330 SERVICE BULLETIN

**CONF 001

140HF (18)

**FWD**



## B **C**

**D E**  **F G**  **H**
**H H**  **H**

**H H**  **H H**  **H H**  **H J**  FR95 FR93

FR91

FR90

FR89

G_SB_363040_6_BBAA_02_02 FR88

Figure A-GBBAA - Sheet 02 Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 67 0

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# @A330 SERVICE BULLETIN

**CONF 001

LOCKWIRE (MAT. NO. 19−018) **NOTE:** 01 TYPICAL

(23)

(17) (30) (24) (27)
(23)

(29) (17) 

## C (28) (23)

(17) 

## D

**E** (28) 

## F 01 (18) (25) 01

G_SB_363040_6_BBAA_03_01 34HF

140HF

Figure A-GBBAA - Sheet 03 Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 68 0

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# @A330 SERVICE BULLETIN

**CONF 001

(24) (30) (17)

(26)


## G **H** TYPICAL (17)

(26)

(18) 

## J

LOCKWIRE (MAT. NO. 19−018) **NOTE:** 01 01

G_SB_363040_6_BBAA_04_01 140HF

139HF

Figure A-GBBAA - Sheet 04 Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 69 0

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# @A330 SERVICE BULLETIN

**CONF 002 thru 005

Z310 

### A

FR80 FR88 FR90 FR95 FR98 FR100

140HF



## A (36) 

### B

G_SB_363040_6_BBAB_01_02 Figure A-GBBAB - Sheet 01 Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 70 0

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# @A330 SERVICE BULLETIN

**CONF 002 thru 005

140HF (36)

**FWD**



## B FR95

FR93

FR91 

### C **D**

**E E**  **E**

(17)

OPEN ONLY THIS CLAMP **NOTE:** 01 01



## C

(24) (30)

(26)


## D TYPICAL (17)

(26)



## E (17) 

### E

G_SB_363040_6_BBAB_02_02 FR94

Figure A-GBBAB - Sheet 02 Removal of the Sensing Element 140HF from the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 71 0

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# @A330 SERVICE BULLETIN

**CONF 001

Z310

FR80 FR83 FR86 FR88 FR91 FR93 FR95 FR98 FR100



## A **A**

**B C**  **D E**  **G F**  **H J**  **K**

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

01 02

G_SB_363040_6_BCAA_01_01 Figure A-GBCAA - Sheet 01 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 72 0

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# @A330 SERVICE BULLETIN

**CONF 001



## B

OVERHEAT SENSING ELEMENT MUST BE OUTSIDE THE INSULATION SLEEVE **NOTE:** 03 03



## C

**D** 03



## E 1 2

3 4

03 03 FR83

FR84

FR84

FR85

G_SB_363040_6_BCAA_02_02 Figure A-GBCAA - Sheet 02 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 73 0

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# @A330 SERVICE BULLETIN

**CONF 001

OVERHEAT SENSING ELEMENT MUST BE OUTSIDE THE INSULATION SLEEVE **NOTE:** 03 9 

## G 5 

## F 03

6

7



## H 03 17

8

03 03



## J

**K** 03 FR87 FR88

FR90 FR91

FR94

G_SB_363040_6_BCAA_03_03 Figure A-GBCAA - Sheet 03 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 74 0

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# @A330 SERVICE BULLETIN

**CONF 002, 004

Z310

FR80 FR83 FR86 FR88 FR91 FR93 FR95 FR98 FR100



## A **A**

**B C**  **D E** 
**F G**  **H J** 

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

01 02

01 02
01 02

G_SB_363040_6_BCAB_01_01 Figure A-GBCAB - Sheet 01 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 75 0

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# @A330 SERVICE BULLETIN

**CONF 002, 004

OVERHEAT SENSING ELEMENTS MUST BE OUTSIDE THE INSULATION SLEEVE **NOTE:** 03 12 13



## D 03

03 

## E 17 

## B 03



## C 1 03 2 FR83

FR84

FR84

FR86

G_SB_363040_6_BCAB_02_02 Figure A-GBCAB - Sheet 02 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 76 0

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# @A330 SERVICE BULLETIN

**CONF 002, 004

14 15

16 9 03 

## F

04

05 06

05 06 04

03 

## G 17

17 03



## H 03



## J FR86 FR88

FR91

FR94

OVERHEAT SENSING ELEMENTS MUST BE OUTSIDE THE INSULATION SLEEVE **NOTE:** 03 FOR INSTALLATION OF THE INSULATION SLEEVE OPEN THE DETECTION CLIP AND LIFT THE SENSING ELEMENT FROM THE BRACKET 04 PULL ANTI−ROTATION DEVICE OF THE INSULATION SLEEVE OVER THE BRACKET 05 REINSTALLATION OF SENSING ELEMENT 06 G_SB_363040_6_BCAB_03_03 Figure A-GBCAB - Sheet 03 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 77 0

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# @A330 SERVICE BULLETIN

**CONF 003, 005

Z310 

### A

FR80 FR83 FR86 FR88 FR91 FR93 FR95 FR98 FR100



## A **B C**  **D E** 
**F G**  **H J** 

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

01 02

01 02
01 02

G_SB_363040_6_BCAC_01_01 Figure A-GBCAC - Sheet 01 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 78 0

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# @A330 SERVICE BULLETIN

**CONF 003, 005



## B

OVERHEAT SENSING ELEMENTS MUST BE OUTSIDE THE INSULATION SLEEVE **NOTE:** 03 03 10 11

13 03



## C

03 

## E 17 FR83 FR84

FR86

12



## D 03

17 FR84

G_SB_363040_6_BCAC_02_02 Figure A-GBCAC - Sheet 02 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 79 0

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# @A330 SERVICE BULLETIN

**CONF 003, 005

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

G_SB_363040_6_BCAC_03_03 Figure A-GBCAC - Sheet 03 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 80 0

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# @A330 SERVICE BULLETIN

**CONF 001

Z310 

### A

FR80 FR88 FR95 FR98 FR100

140HF



## A 18 

### B **M**

G_SB_363040_6_BDAA_01_01 Figure A-GBDAA - Sheet 01 Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 81 0

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# @A330 SERVICE BULLETIN

**CONF 001

**FWD** 

## B 140HF 18 FR95 FR93

FR91

FR90

FR89 

### C

**E F**  **K**
**K K**  **K**

**K K**  **K**

**K K**  **K L**  **K G**  **J**

**H**

G_SB_363040_6_BDAA_02_01 FR88

Figure A-GBDAA - Sheet 02 Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 82 0

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# @A330 SERVICE BULLETIN

**CONF 001



## 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**

G_SB_363040_6_BDAA_03_02 ~30°

Figure A-GBDAA - Sheet 03 Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 83 0

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# @A330 SERVICE BULLETIN

**CONF 001

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) G_SB_363040_6_BDAA_04_01 34HF

140HF

140HF

139HF

Figure A-GBDAA - Sheet 04 Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 84 0

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# @A330 SERVICE BULLETIN

**CONF 001

G_SB_363040_6_BDAA_05_02 **FWD** 140HF 18 FR95 FR93

FR91

FR90

FR89 STEP 1

03 WAY OF WORKING STEPS **NOTE:** 

## M STEP 3 STEP 4 STEP 5 STEP 6 STEP 7 STEP 8 STEP 10
STEP 11 STEP 12 STEP 13

STEP 14

STEP 15

STEP 16
STEP 17
STEP 18
STEP 19

STEP 20 STEP 21 STEP 22 

### A **A**

03

03
03
03
03

03 03 03 03 03 03 03 03 03 03 03

03

03 03



## A **A** STEP 2 STEP 903 03 12.7 mm (0.50 in)

04 COVERED WITH 360° LOOPS 04 04

INSULATION SLEEVE INSULATION SLEEVE

INSULATION SLEEVE

FR88

Figure A-GBDAA - Sheet 05 Installation of the Sensing Element 140HF on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 85 0

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# @A330 SERVICE BULLETIN

**CONF 002 thru 005

Z310 

### A

FR80 FR91 FR93 FR95 FR98 FR100

140HF



## A (36) 

### B **F**

G_SB_363040_6_BDAB_01_02 Figure A-GBDAB - Sheet 01 Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 86 0

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# @A330 SERVICE BULLETIN

**CONF 002 thru 005

140HF (36)

**FWD**



## B FR95

FR93

CLOSE THIS CLAMP **NOTE:** 01 01



## C

(24) 35 (26)



## D 17 

### D

**C**

G_SB_363040_6_BDAB_02_01 FR91 

### E **E E** 

TYPICAL 17

(26)



## E **E**

Figure A-GBDAB - Sheet 02 Rerouting of the Sensing Element 140HF on the APU Bleed-Air-Duct DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 87 0

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# @A330 SERVICE BULLETIN

**CONF 002 thru 005

140HF (36) **FWD**

02 WAY OF WORKING STEPS **NOTE:** 

## F

G_SB_363040_6_BDAB_03_01 FR95

FR93



### C FR91 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.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 88 0

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# @A330 SERVICE BULLETIN

**CONF ALL

G_SB_363040_6_BEAA_01_00 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 Figure A-GBEAA - Sheet 01 Tolerances for Waviness and Bends in Sensing Elements DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 89 0

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# @A330 SERVICE BULLETIN

**CONF ALL

mm DIMENSIONS (in)

C D E B A 9.52 MAX 6.4
MIN 12.7 MIN 0.50 MIN 25.4 MIN 1.00 MIN R 25.4 MIN R 1.00 MAX 0.25

0.38

F MAX 203.0 MAX 7.99 RAD MIN 25.4 mm RAD MAX 40.0 mm RAD MIN (1.00 in) RAD MAX (1.57 in) PRINCIPLE VIEW OF LOOP

C 

### A



## A C

G_SB_363040_6_BEAA_02_01 Figure A-GBEAA - Sheet 02 Tolerances for Waviness and Bends in Sensing Elements DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 90 0

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# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions **CONF ALL For the elapsed time assumptions, refer to: **CONF 001 Fig. A-GAAAA **CONF 002 thru 005 Fig. A-GAAAB

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 1 0

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# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 001

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

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 14.50 14.00 STEPS

0.75 0.50

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

G_SB_363040_6_AAAA_01_00 Figure A-GAAAA - Sheet 01 Gantt Chart DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 2 0

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# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 002 thru 005

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

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 8.25 7.75 STEPS

0.75 0.50

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 G_SB_363040_6_AAAB_01_00 INSTALL THE INSULATION LOOSEN THE SENSING

REROUTE THE SENSING
TEST 1.75 1.75

1.00 1.00 1

1
CLOSE−UP 0.50 0.25 2 ELEMENT
SLEEVES

ELEMENT

7 8 9

Figure A-GAAAB - Sheet 01 Gantt Chart DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 3 0

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE INSULATION MUFFS IN S19. MODIFICATION No.: 202216C10899 202216C10898 202216C10846 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 1 0

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# @A330 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Sep 18/12 SERVICE BULLETIN No.: A330-36-3040 REVISION No.: 01 - Nov 26/12 Page: 1 0

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