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时间:2011-03-25 17:53来源:蓝天飞行翻译 作者:admin
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 (t)
 Install the clamp (22), the washer (23) and the screw (24) to the bracket (21).

 (u)
 Connect the electrical connectors (26) to the NLG proximity sensor 24GAA (25).


 1EFF : ALL 1 32-21-43Page 426 1 1 May 01/05R 1 1 1CES 1


 Subtask 32-21-43-865-064
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG, 3GG, 4GG, 1GA, 2GA, 52GA, 3LR, 1LC1, 1GV.
 Subtask 32-21-43-869-058
 C. After you close the LGCIU circuit breakers, put the aircraft back to the correct (ground) condition (Ref. TASK 32-00-00-860-002).
 Subtask 32-21-43-410-052
 D. Close Access
 (1) Remove the access platform(s).
 (2) Close the NLG doors (Ref. TASK 32-22-00-410-001). R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 32-21-43-710-060
 E. Test:
 (1)
 Do the operational test of the taxi and take off light (Ref. TASK 33-46-00-710-001).

 (2)
 Do the operational test of the runway turnoff lights (Ref. TASK 33-43-00-710-001).

 (3)
 Do the operational test of the nose wheel steering (Ref. TASK 32-51-00-710-001).

 (4)
 Do the BITE test of the landing gear (Ref. TASK 32-69-00-740-001).


 1EFF : ALL 1 32-21-43Page 427 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 32-21-43Page 428 1 1 May 01/05 1 1 1CES 1 TASK 32-21-43-000-003


R  **ON A/C 051-099, 
R  Subtask 32-21-43-710-060-A 
R  E. Test: 
R R  (1) Do the operational test of the taxi and take off light (Ref. TASK 33-46-00-710-001). 
R R  (2) Do the operational test of the runway turnoff lights (Ref. TASK 33-43-00-710-001). 
R R  (3) Do the operational test of the nose wheel steering (Ref. TASK 32-51-00-710-001). 
R  (4) Do the BITE test of the landing gear (Ref. TASK 32-69-00-740-001). 
R R  (5) Do the operational test of the tire pressure indicating system (Ref. TASK 32-49-00-710-001). 
R  **ON A/C ALL
 5. Close-up________
 Subtask 32-21-43-942-052
 A. Removal of Equipment
 (1) Remove the warning notice(s).
 (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 

 Removal of the NLG Electrical Harness 2M
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adjustable access platform
 No specific blanking caps
 No specific circuit breaker(s) safety clip(s)
 No specific warning notice(s)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-00-00-481-002 Installation of the Safety Devices on the Landing
 Gear Doors R 32-00-00-860-001 Flight Configuration Precautions with Electrical R Power
 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening
 32-21-43-991-003 Fig. 403

 1EFF : ALL 1 32-21-43Page 429 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------


32-21-43-991-005 Fig. 404
 3. Job Set-up
__________ Subtask 32-21-43-860-056
 A. Aircraft Maintenance Configuration
 (1) Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
 Subtask 32-21-43-941-056
 B. Safety Precautions
 (1)
 Make sure that the safety device are installed on the landing gears (Ref. TASK 32-00-00-481-001).
 
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