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时间:2011-10-11 13:04来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 29-11-00
 ALL  ú ú 03 Page 657 ú Jun 20/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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C.
D.
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MAINTENANCE MANUAL

 (b)  Hydraulic Service Cart(s) - Commercially
 Available, which can supply 6 GPM to each
 system (18 GPM total) at 3000 psi
 NOTE:____ The service cart is not necessary
 if you use the ACMP to pressurize
 the hydraulic system.
 (3)  Elevator pogo compressor, B27032-9
 (4)  Yaw Damper Module simulator, B29005-2 (2
 necessary) part of kit B29005-1
 (5)  Mechanic's Stethoscope, GA 111 D, Snap-On-Tools
 Corporation, Kenosha, Wisconsin

References
 (1)
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)
AMM 06-42-00/201, Empennage Access Doors and Panels

 (3)
AMM 06-43-00/201, Engine and Nacelle Strut Access Doors and Panels

 (4)
AMM 12-12-01/301, Hydraulic Systems

 (5)
AMM 22-21-00/501, Yaw Damper System

 (6)
AMM 24-22-00/201, Electrical Power - Control

 (7)
AMM 29-11-00/201, Main (Left, Right and Center) Hydraulic System

 (8)
AMM 32-00-15/201, Landing Gear Door Locks

 (9)
AMM 32-00-20/201, Landing Gear DownlocksAccess

 (1)
Location Zones


 119/120 197 211/212 330/340 434/444  Main Equipment CenterWing to Body - Aft Lower Half (Left)Control CabinHorizontal Stabilizer and ElevatorNacelle Strut - Aft Fairing
 (2)  Access Panels 119BL 197KL 335DB  Main Equipment CenterCentral Hydraulic Service CenterLeft Elevator PCAs
 345DB  Right Elevator PCAs

 434AL/444AL Hydraulic BayPrepare for the Internal Leakage Check of the Elevator and Rudder PCAs S 866-227
 (1)  Supply electrical power (AMM 24-22-00/201).
 (2)  S 616-228Do a check of the fluid level in the hydraulic reservoirs (AMM 12-12-01/301).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-00
 ALL  ú ú 06 Page 658 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 S 866-382

 CAUTION:_______ DO NOT OPERATE THE HYDRAULIC PUMPS WITHOUT A MINIMUM QUANTITY
 OF FUEL IN THE TANKS OR AFTER THE OVERHEAT LIGHT COMES ON.  IF
 THE HEAT EXCHANGERS OF THE HYDRAULIC SYSTEM ARE NOT FULLY INTO

 THE FUEL, THE HYDRAULIC FLUID CAN BECOME TOO HOT.
 
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