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时间:2011-04-13 08:10来源:蓝天飞行翻译 作者:航空
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 4)  If it is still difficult to find or isolate the source of leakage, do the Engine Bleed, Wing Leading Edge and Body Crossover Duct Audible Check procedure (AMM 36-11-00/601).
References
 (1)
AMM 31-25-00/001, Clock

 (2)
AMM 36-00-00/201, Pneumatic System

 (3)
AMM 36-11-00/501, Engine Bleed Air Supply System

 (4)
AMM 36-11-04/201, Pressure Regulating and Shutoff Valve

 (5)
AMM 36-12-01/401, Engine Bleed Air Precooler

 (6)
AMM 45-10-00/201, Central Maintenance Computer System

 (7)
AMM 49-11-00/201, Auxiliary Power Unit

 (8)
AMM 49-61-07/401, APU Controller

 (9)
AMM 71-11-04/201, Fan Cowl Panels

 (10)
 AMM 71-11-06/201, Core Cowl Panels

 (11)
 AMM 78-31-00/201, Thrust Reverser SystemAccess

 (1)  
Location Zone 412 Engine 1 - Main Gearbox Aft Face 5 o'clock 422 Engine 2 - Main Gearbox Aft Face 5 o'clock 432 Engine 3 - Main Gearbox Aft Face 5 o'clock 442 Engine 4 - Main Gearbox Aft Face 5 o'clock

 (2)  
Access Panel 415 and 416 Thrust Reverser Halves - Engine 1 417 and 418 Core Cowl Panels - Engine 1 425 and 426 Thrust Reverser Halves - Engine 2 427 and 428 Core Cowl Panels - Engine 2 435 and 436 Thrust Reverser Halves - Engine 3 437 and 438 Core Cowl Panels - Engine 3 445 and 446 Thrust Reverser Halves - Engine 4 447 and 448 Core Cowl Panels - Engine 4


Prepare to Do the Leakage Check of the Engine Bleed Air Supply System
 S 866-016
 (1) Supply the electrical power (AMM 24-22-00/201).
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 36-11-00
 ALL  ú ú 02 Page 602 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 866-017
 (2)  
Make sure these circuit breakers are open and attach a DO-NOT-CLOSE tag:

 (a)  
On the main power distribution panel, P6: 1) 6F01, ENG 1 IGN 1 2) 6F02, NG 2 IGN 1 3) 6F03, ENG 3 IGN 1 4) 6F04, ENG 4 IGN 1 5) 6G19, STBY IGN ENG 1 6) 6G20, STBY IGN ENG 2 7) 6G21, STBY IGN ENG 3 8) 6G22, STBY IGN ENG 4 9) 6J18, ENG START AIR CONT 10) 6K18, APU ALTN CONT 11) 6K19, ENG 1 IGN 2 12) 6K20, ENG 2 IGN 2 13) 6K21, ENG 3 IGN 2 14) 6K22, ENG 4 IGN 2 15) 6L10, ENG 1 FUEL CONT VLV 16) 6L11, ENG 2 FUEL CONT VLV 17) 6L12, ENG 3 FUEL CONT VLV 18) 6L13, ENG 4 FUEL CONT VLV


 S 866-018
 (3)  
Make sure these circuit breakers are closed:

 (a)  
On the main power distribution panel, P6: 1) 6C08, WING ANTI-ICE VLV 2) 6C09, WING ANTI-ICE CONT 3) 6F28, ZONE TEMP CONT AC 4) 6F29, ZONE TEMP CONT DC 5) 6F30, MASTER TRIM AIR CONT 6) 6F33, LWR CARGO A/C CONTROL 7) 6F34, CARGO A/C CONT PCA 8) 6H20, L ISO VLV AIR SUPPLY PWR 9) 6H22, APU ISO VLV AIR SUPPLY PWR 10) 6H24, R ISO VLV AIR SUPPLY PWR 11) 6H32, ENG 1 AIR SUPPLY CONT 12) 6H33, ENG 2 AIR SUPPLY CONT 13) 6H34, ENG 3 AIR SUPPLY CONT 14) 6H35, ENG 4 AIR SUPPLY CONT 15) 6H36, APU VLV AIR SUPPLY CONT 16) 6G33, LWR CARGO ZONE TEMP SENSORS

 (b)  
On the overhead circuit breaker panel, P7: 1) 7H09, CARGO HEAT AFT

 (c)  
On the DC power distribution panel, P180: 1) 180F01, FLOW CONT VLV PACK 2 2) 180F27, ALTN TEMP CONT 3) 180J01, FLOW CONT VLV PACK 1 4) 180J16, FLOW CONT VLV PACK 3


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 36-11-00
 ALL  ú ú 11 Page 603 ú Feb 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (d)  On the main power distribution panel, P414:
 1) 414F02, LWR CARGO AIR COND VLVS

 (e)  On the main power distribution panel, P415:
 1) 415L29, AFT CARGO HT PWR

 S 866-019
 (4)  Put these switches in the on the P5 overhead panel to the OPEN position:
 (a)  L ISLN VALVE
 (b)  R ISLN VALVE
 S 866-020
 (5)  Put these switches in the on the P5 overhead panel to the ON position:
 (a)  APU VALVE
 S 866-021
 (6)  Put these switches in the on the P5 overhead panel to the OFF position:
 (a)  PACKS 1
 (b)  PACKS 2
 
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本文链接地址:747-400 AMM 飞机维护手册 气动系统 PNEUMATIC SYSTEM(46)