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时间:2011-03-31 15:23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

3.  Splice Electrical Harness
A.  Cut electrical harness at approximately 12 inches from the sensor in the vicinity of wire harness clamp.
B.  Splice new sensor to remaining wire harness. Insulate splice with sleeving.
C.  Complete installation of replacement proximity sensor.
500 
Aug 15/71  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  78-36-12 Page 801 


THRUST REVERSER HYDRAULIC SYSTEM PRESSURE SWITCH - REMOVAL/INSTALLATION
1.  Equipment and Materials
A.  Thrust Reverser Isolation Valve Ground Lock Cap and Pin Assembly - F80109-3 or F80109-9 or equivalent
2.  Prepare for Removal
A.  Deactivate thrust reverser hydraulic system by installing ground locks at both thrust reverser isolation valves.
WARNING:  SERIOUS INJURY CAN RESULT TO PERSONNEL IF GROUND LOCKS ARE NOT PROPERLY INSTALLED. ATTEMPT TO DEPLOY THRUST REVERSERS AFTER INSTALLING GROUND LOCKS. REVERSERS MUST NOT MOVE HYDRAULICALLY.
B. Remove access panel from forward wing-to-body fairing to gain access to pressure switch.
3.  Remove Hydraulic System Pressure Switch
A.  Disconnect electrical connector from pressure switch. (See figure 401.)
B.  Remove clamp attaching pressure switch to support bracket.
C.  Remove pressure switch from T-fitting.
NOTE: Rotate switch with a wrench at the switch fitting to keep from breaking tack weld.
4.  Install Hydraulic System Pressure Switch
A.  Install pressure switch in T-fitting. (See figure 401.)
NOTE: Rotate switch with a wrench at the switch fitting to keep from breaking tack weld.
B.  Attach pressure switch to bracket with clamp.
C.  Connect electrical connector to pressure switch.
D.  Reactivate thrust reverser hydraulic system by removing ground locks from isolation valves.
E.  Perform isolation valve indicating system test to check for proper operation of pressure switch and to check hydraulic lines for leaks. Refer to 78-36-01, Thrust Reverser Indicating Systems -Adjustment/Test.
F.  Replace access panel on wing-to-body fairing.
525 
May 01/03  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  78-36-41 Page 401 


H27673
Thrust Reverser Pressure Switch Installation  500 
78-36-41 Page 402  Figure 401 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Aug 15/72 


 


 
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