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时间:2011-04-01 08:47来源:蓝天飞行翻译 作者:航空
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 NOTE: The nominal length of the rod assembly is 9.43 inches.
____
 (c)  
Tighten the locknut on the rod end.

 (d)  
Install the bolt, washer, and nut.


 NOTE: The bolt must go smoothly through the rod end and
____
 actuator lever.

 S 865-051
 (8)  
Move the aft quadrant lightly. Make sure that the trailing edge of the right elevator aligns with the index mark |0.06 inch.

 S 435-054

 (9)  
Install the rod assembly between the actuator A lever and torque tube lever:


 (a)  The bolt should go smoothly through the rod end and actuator A lever. If adjustment is necessary, loosen the rod assembly jam nuts and make the adjustment.
 NOTE: The nominal length of the rod assembly is 17.52 inches.
____
 (b)  Make sure that you can see the rod end threads through the inspection hole at both ends of the rod assembly. Adjust the rod assembly if it is necessary.
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737-300/400/500MAINTENANCE MANUAL
 (c)  
Tighten the jam nuts on the rod ends.

 (d)  
Install the bolt, washer, and nut.


 NOTE: The bolt must go smoothly through the rod end and lever.
____
 S 835-072
 (10) Do the Elevator Rigging Test (tests 51.06 through 51.46) in this task: "Rigging Tests" (AMM 22-11-00/501 or AMM 22-11-01/501).
 NOTE: Push the LSK adjacent to <CONTINUE to continue the elevator
____
 rigging test.

 S 745-052
 (11)
 Push the INIT REF key on the CDU keyboard to get out of the BITE.

 S 415-045

 (12)
 Close the tail cone access panel, 3802 (AMM 12-31-41/201).


 TASK 22-11-26-715-041
 4. Autopilot Elevator Actuator Test
________________________________
 A. References
 (1)  
AMM 22-11-00/501 or AMM 22-11-01/501, Digital Flight Control System

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 29-15-00/201, Hydraulic A, B, and Standby System


 B. Access
 (1)  Location Zones
 101 Control Cabin, Left
 102 Control Cabin, Right

 C. Autopilot Elevator Actuator Test - DFCS BITE
 S 745-073
 (1)  
Do the preparation for the DFCS BITE test in this task: "Operational Test - Digital Flight Control System" (AMM 22-11-00/501 or AMM 22-11-01/501).

 S 745-040

 (2)  
Do the actuator test:

 (a)  
Push the INIT REF key on the CDU keyboard.

 (b)  
Push the LSK adjacent to <INDEX.

 (c)  
Push the LSK adjacent to MAINT>.

 


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 ALL  ú ú 02 Page 518 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (d)  
Push the LSK adjacent to <DFCS.

 (e)  
Push the NEXT PAGE key on the CDU keyboard.

 (f)  
Push the LSK adjacent to <GROUND FUNCTIONAL.

 (g)  
Push the LSK adjacent to <CHANNEL A or <CHANNEL B.

 (h)  
Push the LSK adjacent to <TEST SELECTION.

 (i)  
Use the CDU keyboard to put the library test No. 30 into the scratchpad.

 (j)  
Push the LSK adjacent to ENTER>.

 (k)  
Push the LSK adjacent to <EXECUTE to start the test 60.30 (ELEVATOR).

 (l)  
Follow the CDU instructions until the test 60.30 is completed with no failure.

 (m)  
Push the INIT REF key on the CDU keyboard to get out of the BITE.


 D. Autopilot Elevator Actuator - Manual Test
 S 715-037
 (1)  Do the actuator test:
 (a)  
Engage the autopilot A or B (if it is applicable) to the CWS mode.
 
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