曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

wheel at 6.5 inches (165 millimeters) radius.
E. Aileron Spring Cartridge and Transfer Mechanism Functional Test
SUBTASK 27-11-00-720-004
(1) Do the functional test of the aileron spring cartridge and transfer mechanism:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 562
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Operate the two aileron trim switches to put the aileron control wheels to the neutral (zero
unit) position.
(b) Shake the control wheel to center the aileron system.
(c) Hold the first officer’s control wheel at the neutral position.
(d) Turn the captain’s control wheel clockwise to 75 degrees from the neutral position.
1) Make sure the aileron spring cartridge [17] extends while you turn the control wheel.
2) Make sure the maximum breakout force is 436 pound-inches (49.2 newton-meters) or
67 pounds (298.0 newtons).
NOTE: The ‘‘breakout’’ force occurs when the captain’s control wheel starts to move
with the first officer’s control wheel hold in the neutral position.
3) Make sure the maximum force at 75 degrees is 676 pound-inches (76.3 newton-meters)
or 104 pounds (462.6 newtons).
(e) Turn the captain’s control wheel counterclockwise to 75 degrees from the neutral position.
1) Make sure the aileron spring cartridge [17] compresses while you turn the control
wheel.
2) Make sure the maximum breakout force is 436 pound-inches (49.2 newton-meters) or
67 pounds (298.0 newtons).
3) Make sure the maximum force at 75 degrees is 676 pound-inches (76.3 newton-meters)
or 104 pounds (462.6 newtons).
(f) Turn and hold the first officer’s control wheel clockwise at 80 degrees from the neutral
position.
(g) Turn the captain’s control wheel counterclockwise until the transfer mechanism stops
touch.
1) Make sure the captain’s control wheel turns a minimum of 138 degrees from the
starting position.
2) Make sure the transfer mechanism can move freely when you turn the control wheel.
(h) Turn and hold the first officer’s control wheel counterclockwise at 80 degrees from the
neutral position.
(i) Turn the captain’s control wheel clockwise until the transfer mechanism stops touch.
1) Make sure the captain’s control wheel turns a minimum of 138 degrees from the
starting position.
2) Make sure the transfer mechanism can move freely when you turn the control wheel.
(j) Turn and hold the captain’s control wheel clockwise at 80 degrees from the neutral
position.
(k) Turn the first officer’s control wheel counterclockwise 130 degrees from the starting
position (80 degrees clockwise).
1) Make sure the aileron spring cartridge [17] extends and can move freely while you turn
the control wheel.
2) Make sure the maximum force to turn the captain’s control wheel is 1000 pound-inches
(112.9 newton-meters) or 154 pounds (684.0 newtons).
(l) Turn and hold the captain’s control wheel counterclockwise at 80 degrees from the neutral
position.
(m) Turn the first officer’s control wheel clockwise 130 degrees from the starting position (80
degrees counterclockwise).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 563
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Make sure the aileron spring cartridge [17] compresses and can move freely while you
turn the control wheel.
2) Make sure the maximum force to turn the captain’s control wheel is 1000 pound-inches
(112.9 newton-meters) or 154 pounds (684.0 newtons).
(n) Return both control wheels to neutral.
(o) Insert a 0.0625 inch (1.6 mm) pin a minimum distance of .50 inch (12.7 mm) into the
inspection hole in the aileron input crank (Fig. 501) to verify that the crank has not moved on
the shaft and the shear rivets in the crank are not sheared.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-11-00-860-055
(1) Remove power from hydraulic systems A and B, do this task: Hydraulic System A or B Power
Removal, TASK 29-11-00-860-805.
SUBTASK 27-11-00-080-016
(2) Remove the adapter, SPL-1674, the mount, SPL-1670, and the control column assembly
protractor, SPL-1680 from the captain’s control wheel.
SUBTASK 27-11-00-860-095
(3) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
------------------------- END OF TASK ---------------------------
TASK 27-11-00-700-807
16. Control Wheel Travel Stop Test
A. References
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機(jī)維護(hù)手冊1(125)