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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 01 Page 602 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 (5)  S 016-002Open the access panels, 434AL and 444AL, for the hydraulic bay in the aft strut (AMM 06-43-00/201).
 (6)  S 016-009Open the access panel, 197KL, for the central hydraulic service center (AMM 06-41-00/201).
 (7)  S 866-010Extend the ram air turbine (RAT) (AMM 29-21-00/201).
 (8)  S 216-011Examine the hydraulic tubing in the areas that follow for a color change which shows the hydraulic fluid was too hot: (a) Engine (b) Engine strut hydraulic area (c) Left and right wheel wells (d) Aft-left wing/body fairing.
 (9)  S 866-012Pressurize the hydraulic systems and reservoirs (AMM 29-11-00/201).
 S 216-013

 (10)
 Examine all hydraulic line connections, hydraulic fittings, and hydraulic components for signs of external leakage.

 S 866-014

 (11)
 Remove the pressure from the hydraulic systems and reservoirs (AMM 29-11-00/201).

 S 366-015

 (12)
 Replace or repair the hydraulic components which leak or are damaged.

 S 216-021

 (13)
 Do these steps to examine the reservoir pressurization module filter.


 (a) Examine the filter element for a dirty condition.
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 29-11-00
 ALL  ú ú 01 Page 603 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 (b)  If necessary, clean the filter element (Ref 29-11-16/401).
 S 216-379
 (14) Do these steps to examine the RAT checkout module pressure and case drain filters.
 (a)  
Remove the filter elements and check for a dirty condition.

 (b)  
If you find many metal particles, replace the filter element (AMM 29-21-11/401).


 S 866-022
 (15)
 Retract the RAT (AMM 29-21-00/201).

 S 416-023

 (16)
 Close the access panel, 197KL, for the central hydraulic service center (AMM 06-41-00/201).

 S 416-024

 (17)
 Close the access panels, 434AL and 444AL, for the hydraulic bay in the aft strut (AMM 06-43-00/201).

 S 866-026

 (18)
 Do the activation procedure for the thrust reverser (AMM 78-31-00/201).


 S 416-027
 CAUTION:  OBEY THE PRECAUTIONS FOR THE KEVLAR WRAPPING WHEN YOU CLOSE THE
 
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