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时间:2011-03-31 16:16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

 S 712-020

 (6)  
Do the transducer spin test to make sure that the correct brake releases when the transducer movement has stopped (Ref 32-42-00/501).

 S 022-007

 (7)  
Remove the brake system control unit (Ref 32-42-01/401).

 S 752-007

 (8)  
Do a bench test of the brake system control unit.

 S 022-008

 (9)
Remove the related anti-skid control valve (Ref 32-42-02/401).

 S 752-009

 (10)
 Do a bench test of the anti-skid control valve.


 TASK 05-51-25-202-009
 3.  Multiple Flat Spotted or Blown Tire Check_________________________________________
 A. References
 (1)  
05-51-201, Hard Landing or High Drag/Side Load Landing Condition

 (2)  
29-11-29/201, Return Module

 (3)  
32-41-15/601, Landing Gear Brake Unit

 (4)  
32-42-00/501, Brake Control System

 (5)  
32-42-01/401, Brake System Control Unit

 (6)  
32-42-02/401, Antiskid Modular Assembly

 (7)  
32-44-04/401, Parking Brake Module


 B. Procedure
 S 212-018
 (1)  
Do the Phase I and Phase II examinations of the Hard Landing or High Drag/Side Load Landing Condition procedure (Ref 05-51-05/201).

 S 212-010

 (2)  
Examine the brakes for correct operation and condition (Ref 32-41-15/601).

 S 212-011

 (3)  
Do the anti-skid system test to make sure the brake system control unit operates correctly (Ref 32-42-00/501).

 S 712-012

 (4)  
Do the anti-skid system brake release test on the damaged wheels to make sure the brake releasees correctly (Ref 32-42-00/501).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 05-51-25
 ALL  ú ú 01 Page 202 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (5)  S 212-013Examine the hydraulic return filter. Make sure that the hydraulic return filter is not partially or fully blocked (Ref 29-11-29/201).
 (6)  S 212-014Examine the hydraulic lines and electrical wiring. Make sure the hydraulic lines and electrical wirirng are installed correctly.
 (7)  S 712-015Do the transducer spin test to make sure that the correct brake releases when the transducer movement has stopped (Ref 32-42-00/501).
 (8)  S 712-019Do a check of the parking brake valve for correct operation. Make sure that the valve is completely open when the parking brake is released (Ref 32-44-04/401).
 (9)  S 022-016Remove the related anti-skid control valve (Ref 32-42-02/401).
 S 752-017

 (10)
 Do a bench test of the anti-skid control valve. S 022-017

 (11)
 Remove the brake system control unit (Ref 32-42-01/401). S 752-018

 (12)
 Do a bench test of the brake system control unit.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 05-51-25
 ALL  ú ú 01 Page 203 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 HOT OR COLD BRAKES CONDITION - MAINTENANCE PRACTICES
____________________________________________________ (CONDITIONAL INSPECTION)
______________________
 1.  General_______
 A.  One task is supplied in this procedure. The task is hot or cold brakes conditional inspection.
 B.  This task examines a single hot brake, a single cold brake, and all brakes on the left or right side of the airplane hot or cold.
 TASK 05-51-26-202-001
 2.  Hot or Cold Brake Conditional Inspection________________________________________
 A.  References
 (1)  
32-41-00/201, Hydraulic Brake System

 (2)  
32-41-00/501, Hydraulic Brake System

 (3)  
32-41-15/601, Landing Gear Brake Unit

 (4)  
32-42-00/501, Brake Control System

 (5)  
32-42-01/401, Brake System Control Unit
 
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