S 434-067
(20)
Install the turnbuckle clip locks.
S 434-068
(21)
Install the cable shields and clamps.
S 824-069
(22)
Adjust the left aileron control cables AA and AB:
(a)
With a clamp, attach a straightedge across the top ends of the two aileron control wheels to keep them in the neutral position.
NOTE: One end of the first officer's control wheel cannot be
____ farther than 0.20 inch from the straightedge.
(b)
Make sure the rigging pin A/S-15 is installed.
(c)
Make sure the trim roller in in the cam detent.
(d)
Tighten the left cables AA and AB to the specified tension (Fig. 402).
(e)
Remove the rigging pin A/S-15.
(f)
Operate the captain's aileron control wheel through a minimum of two full cycles.
(g)
Install the rigging pins A/S-1, A/S-1A and A/S-15 to do a check on the rigging.
(h)
Make sure the cable tension is in the specified values (Fig. 402).
(i)
Remove all the rigging pins.
(j)
Install the turnbuckle clip locks.
S 714-070
(23)
Do this task to do a test on the control wheel drum: "Aileron Control Wheel Drum Adjustment Test" (AMM 27-11-51/501).
S 824-071
(24)
Do this task: "Roll Force Transducer Adjustment" (AMM 22-11-11/501).
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A
737-300/400/500MAINTENANCE MANUAL
S 714-072
(25)
Do this task: "Roll Force Transducer Test" (AMM 22-11-11/501).
S 714-074
(26)
AIRPLANES WITH THE AILERON FORCE LIMITER; Do this task: "Aileron Force Limiter Test" (AMM 22-11-13/501).
S 414-075
(27)
Close the access door of the lower nose compartment.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AILERON CONTROL WHEEL DRUM - ADJUSTMENT/TEST
____________________________________________
1. General
_______
A. This procedure contains the data necessary to do a test on the aileron control wheel drum.
TASK 27-11-51-735-014
2. Aileron Control Wheel Drum Test
_______________________________
A. Special Tools and Equipment
(1)
F72790- Control Wheel Protractor Mount
(2)
4MIT65B80307-1- Control Surface Protractor
(3)
F72867-1 - Adapter-Torque and Force Test Control Wheel
B.
Access
(1)
Location Zones
101/102 Control Cabin - Left/Right
202 Lower Nose Compartment
(2)
Access Panel
1103 Forward Access Door
C.
Prepare for Test
S 015-001
(1)
Open the forward access door.
S 485-002
(2)
Install the control wheel protractor and protractor mount on the first officer's aileron control wheel (Fig. 501).
S 485-003
(3)
Install the adapter on the captain's aileron control wheel (Fig. 501).
S 865-004
(4)
Make sure the aileron trim system is at the center.
D.
Procedure
S 735-015
(1)
Do a test of the aileron control drum:
(a)
Use a torque wrench on the adapter to measure the force necessary to turn the captain's aileron control wheel clockwise and counterclockwise.
NOTE: If the adapter is not available, put a tangent force
____ to the captain's control wheel at a 6.5 inch radius.
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本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(136)
