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时间:2010-08-20 12:27来源:蓝天飞行翻译 作者:admin
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(a) Make sure the top ends of the control wheels touch the straightedge, SPL-1671.
(b) Make sure that one end of the first officer’s control wheel in no more than 0.20 inch (5.1
mm) from the straightedge, SPL-1671.
SUBTASK 27-11-00-860-007
(8) Measure the cable tensions.
(a) Make sure the tension for cables ACBA and ACBB is not out of tolerance (Table 501).
SUBTASK 27-11-00-480-006
(9) Install the turnbuckle clip locks.
H. Aileron Body Cables AA and AB Adjustment
SUBTASK 27-11-00-860-008
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT CONTROL
SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THESE
COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER.
THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Pressurize hydraulic systems A and B, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-11-00-860-009
(2) Operate the aileron trim switches on the control stand panel, P8, until you can freely install and
remove the rig pin A/S-15, from the rig pin kit, SPL-1585 (Figure 501).
SUBTASK 27-11-00-860-010
(3) Remove power from hydraulic systems A and B, do this task: Hydraulic System A or B Power
Removal, TASK 29-11-00-860-805.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 509
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-11-00-210-001
(4) Make sure the centering cam follower roller is firmly in the cam detent Figure 505.
SUBTASK 27-11-00-820-003
(5) If you install new cables AA and AB, do these steps to adjust the cables (Figure 502):
(a) Adjust the cables until you can easily install and remove rig pins A/S-1 and A/S-1A, from
the rig pin kit, SPL-1585, in the aileron transfer mechanism (Figure 501).
(b) Tighten the turnbuckles on the cables to get the tension two times the specified cable
rigging load for cables AA and AB (Table 501).
(c) Operate the captain’s control wheel for 20 times.
1) Do not turn the control wheel more than 100 degrees from the neutral position.
(d) Reduce the tension in the cables to get the specified cable rigging load for cables AA and
AB (Table 501).
(e) Operate the captain’s control wheel two to three times.
(f) Put the captain’s control wheel back to the neutral position.
1) Move the control wheel quickly back and forth about neutral to make sure it is in the
center position.
SUBTASK 27-11-00-820-004
(6) If the cables AA and AB are not new, do these steps to adjust the cables:
(a) Adjust the cables until you can easily install and remove rig pins A/S-1 and A/S-1A, from
the rig pin kit, SPL-1585, in the aileron transfer mechanism (Figure 501).
(b) Tighten the turnbuckles on the cables to get the correct tension for cables AA and AB
(Table 501).
(c) Operate the captain’s control wheel two to three times.
(d) Put the captain’s control wheel back to the neutral position.
1) Move the control wheel quickly back and forth about neutral to make sure it is in the
center position.
SUBTASK 27-11-00-860-011
(7) Make sure you can easily install and remove these rig pins from the rig pin kit, SPL-1585
(Figure 501):
(a) Rig pin A/S-3 in the spoiler shaft
(b) Rig pin A/S-15 in the aileron trim actuator
(c) Rig pins A/S-1 and A/S-1A in the aileron transfer mechanism.
SUBTASK 27-11-00-820-015
(8) If you cannot easily install and remove the rig pin A/S-3, rig pin A/S-15, rig pin A/S-1 or rig pin A/
S-1A, adjust the cables AA and AB:
NOTE: Do not adjust the cables ACBA and ACBB.
(a) Loosen the turnbuckle on one cable and tighten the turnbuckle on the other cable the same
amount until you can easily install and remove the rig pin.
SUBTASK 27-11-00-860-063
(9) Measure the cable tensions.
(a) Make sure the tension for cables AA and AB is not out of tolerance (Table 501).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 510
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-11-00-860-012
(10) Attach the straightedge, SPL-1671 on the captain’s and first officer’s control wheels.
(a) Make sure the top ends of the control wheels touch the straightedge, SPL-1671.
(b) Make sure that one end of the first officer’s control wheel is no more than 0.20 inch (5.1 mm)
from the straightedge, SPL-1671.
SUBTASK 27-11-00-420-001
(11) Install the turnbuckle clip locks.
I. Aileron Wing Cables ABSA and ABSB Adjustment
SUBTASK 27-11-00-820-016
 
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本文链接地址:737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(105)