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HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 36 L.E.P. 1- 9 REVISED TO REFLECT THIS REVISION INDICATING ?NEW,REVISED, AND/OR DELETED PAGES T. OF C. ?REVISED TO REFLECT THIS REVISION 1-15 36-00-00 EFFECTIVITY UPDATED 1-2, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 5, 9- 10, 14, ?17-18, ?21-24
36-10-00 EFFECTIVITY UPDATED 1, 3, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 5, 7, 10-11, ?13
36-11-00 EFFECTIVITY UPDATED 7, 19-MOD.31526P7136 INCORPORATED A014 ?PNEUMATIC ENGINE BLEED AIR SUPPLY SYSTEM-INTRODUCE MODIFIED TEMPERATURE LIMITATION THERMOSTAT (TLT) P/N 341F01 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 36-11-00 EFFECTIVITY UPDATED 402, 404, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 406, 411, 413, 416, 418, 421, 425, 427, 430, 432, 436, 438 36-11-00 EFFECTIVITY UPDATED 516- 528, CORRECTION/ADDITION/AMPLIFICATION 001-049, 051-099, 101-149,151-199, 201-299, 401-499, 106-149, 151-199, 211-299,301-399, 401-499, 401-499, 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499, 004-049, 055-099, 101-149,151-199, 201-299, 301-399,401-499, ALL ?36-HIGHLIGHTS Page 1 of REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
545, 550, 560, 562, 565, 576? REVISED TITLETITLE OF TASK(S) DATA UPDATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)? 36-11-41 402? EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)? 36-11-41 602, 606? LAYOUT IMPROVED OR EFFECTIVITY UPDATED 36-11-42 405? LAYOUT IMPROVED OR EFFECTIVITY UPDATED 36-11-43 402- 403, 405- 406, 408, 410-411, 414-423? EFFECTIVITY UPDATEDCORRECTION/ADDITION/AMPLIFICATION ADDED STEP TO APPLY LUBRICANT CIRCUIT BREAKER(S) DATA UPDATED? EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)? 36-11-43 701- 703? EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT)? 36-11-44 405- 406? LAYOUT IMPROVED OR EFFECTIVITY UPDATED 36-11-48 402, 408, 411- 413, 421- 425, 428- 430, 433, 436-437, 439-440? EFFECTIVITY UPDATEDTITLE OF TASK(S) DATA UPDATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)? 36-11-49 428, 450, 453- 455, 457, 459, 461- 462, EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT)? CES?
ALL 001-049, 051-099, 101-149, ?151-199, 201-299, 303-399, ?401-499,
001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
001-049, 056-099, 101-149, 151-199, 201-299, 301-399, 401-499, 001-049, 056-099, 101-149, 151-199, 201-299, 301-399, ?401-499, 001-049, 056-099, 101-149, ?151-199, 201-299, 301-399, ?401-499,
001-049, 056-099, 101-149, ?151-199, 201-299, 301-399, ?401-499,
ALL 106-149, 211-299, 301-399, 401-499,
106-149, 151-199, 219-299,301-399, 401-499, ?36-HIGHLIGHTS Page 2 of REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
468, 470, ?474- 477, ?479, 481-483, 485, ?488, 490, ?492, 498,
A401-A403 36-11-49 01 MOD.20011P0003 INCORPORATED 601- 631 ?ELECTRICS- GENERATION- DISTRIBUTION-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20130P0118 INCORPORATED POWER PLANT - DEFINE NACELLE FOR CFM 56-5 ENGINE MOD.20192P0593 INCORPORATED PNEUMATIC-ENGINE AND APU BLEED AIR SUPPLY SYSTEM MOD.33035P7986 INCORPORATED POWER PLANT - GENERAL - ECS - REMOVE FWD LINK ON 9TH STAGE HP DUCT (CFM56-5B) SIL36-0054 INCORPORATED INSPECTION OF HP BLEED DUCT ON CFM56-5B ENGINES. NEW TOPIC/NEW CONFIGURATION 36-11-49 02 TOPIC CANCELLED 601- 606 36-11-51 EFFECTIVITY UPDATED ?501- 512 ?MOD.31502P7140 INCORPORATED PNEUMATIC-ENGINE BLEED AIR SUPPLY SYSTEM-INTRODUCE HP BLEED VALVE (HPV) P/N 6773F01 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 36-11-52 EFFECTIVITY UPDATED 523- 525, MOD.31530P7137 INCORPORATED 527- 532 PNEUMATIC-ENGINE BLEED AIR SUPPLY ?SYSTEM-INTRODUCE PRESSURE REGULATING VALVE (PRV) P/N 6774F01 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) CES
ALL ALLALL106-149, 219-299, 301-399, 401-499, ALL ALL
401-499, 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499, 401-499, 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499, ?36-HIGHLIGHTS Page 3 of REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
36-11-53 EFFECTIVITY UPDATED 502, 504, MOD.31501P7139 INCORPORATED 506, 508-PNEUMATIC-ENGINE BLEED AIR SUPPLY 511 SYSTEM-INTRODUCE OVERPRESSURE VALVE (OPV) P/N 6740F01 CORRECTION/ADDITION/AMPLIFICATION REVISED OVERPRESSURE VALVE CLOSING PRESSURE EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) www.aero.cn 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM PNEUMATIC 氣源 1
