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者

MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO
EQUIPMENT.
(3) Pressurize hydraulic systems A and B, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-11-00-480-016
(4) Install the adapter, SPL-1674 to the captain’s control wheel.
NOTE: If the adapter is not available, put a tangent force to the captain’s control wheel at a 6.5
inch (165 millimeters) radius.
SUBTASK 27-11-00-480-017
(5) Install the mount, SPL-1670 and the control column assembly protractor, SPL-1680 to the first
officer’s control wheel.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 555
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
E. Do a Test of the Control Wheel Force
SUBTASK 27-11-00-730-002
(1) Do a check of the control wheel force:
(a) Set the indicator on the control column assembly protractor, SPL-1680 to zero degrees.
(b) Turn the control wheel clockwise until the aileron starts to move.
1) Make sure the force to turn the control wheel is not more than 29.0 pound-inches (3.2
newton-meters) or 4.5 pounds (20.0 newtons).
(c) Continue to turn the control wheel clockwise to 5 degrees.
1) Make sure the force to turn the control wheel is not more than 35.5 pound-inches (4.0
newton-meters) or 5.5 pounds (24.4 newtons).
(d) Continue to turn the control wheel clockwise to 20 degrees.
1) Make sure the force to turn the control wheel is not more than 56.0 pound-inches (6.3
newton-meters) or 8.5 pounds (37.8 newtons).
(e) Continue to turn the control wheel clockwise to 40 degrees.
1) Make sure the force to turn the control wheel is not more than 89.5 pound-inches (10.1
newton-meters) or 14.0 pounds (62.2 newtons).
(f) Continue to turn the control wheel clockwise to 75 degrees.
1) Make sure the force to turn the control wheel is not more than 123.5 pound-inches (13.9
newton-meters) or 19.0 pounds (84.5 newtons).
(g) Release the control wheel.
1) Make sure the control wheel goes back to the neutral position.
(h) Turn the control wheel counterclockwise until the aileron starts to move.
1) Make sure the force to turn the control wheel is not more than 29.0 pound-inches (3.2
newton-meters) or 4.5 pounds (20.0 newtons).
(i) Continue to turn the control wheel counterclockwise to 5 degrees.
1) Make sure the force to turn the control wheel is not more than 35.5 pound-inches (4.0
newton-meters) or 5.5 pounds (24.4 newtons).
(j) Continue to turn the control wheel counterclockwise to 20 degrees.
1) Make sure the force to turn the control wheel is not more than 56.0 pound-inches (6.3
newton-meters) or 8.5 pounds (37.8 newtons).
(k) Continue to turn the control wheel counterclockwise to 40 degrees.
1) Make sure the force to turn the control wheel is not more than 89.5 pound-inches (10.1
newton-meters) or 14.0 pounds (62.2 newtons).
(l) Continue to turn the control wheel counterclockwise to 75 degrees.
1) Make sure the force to turn the control wheel is not more than 123.5 pound-inches (13.9
newton-meters) or 19.0 pounds (84.5 newtons).
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-11-00-080-013
(1) Remove the adapter, SPL-1674 from the captain’s aileron control wheel.
SUBTASK 27-11-00-080-014
(2) Remove the mount, SPL-1670 and the control column assembly protractor, SPL-1680 from the
first officer’s control wheel.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 556
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-11-00-080-015
(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.
SUBTASK 27-11-00-860-092
(4) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
------------------------- END OF TASK ---------------------------
TASK 27-11-00-730-801
13. Aileron Trim Response Test
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
24-22-00-860-812 Remove Electrical Power (P/B 201)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊1(121)