曝光臺 注意防騙
網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者
STABILIZER TRIM LIMIT SWITCHES - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of a stabilizer trim limit switch
(2) An installation of a stabilizer trim limit switch.
B. The stabilizer trim limit switch is referred to as the "limit switch" in this procedure.
C. There are three limit switches (S144, S145, and S844) and two stabilizer takeoff warning switches
(S132 and S546) on the brackets along the stabilizer jackscrew.
D. This procedure is applicable to all three limit switches.
TASK 27-41-94-000-801
2. Stabilizer Trim Limit Switch Removal
(Figure 401)
A. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
B. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
C. Prepare for the Removal
SUBTASK 27-41-94-860-001
(1) Open this circuit breaker and install safety tag:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
SUBTASK 27-41-94-010-001
(2) To get access to the limit switch, do this step:
Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-41-94-860-002
(3) Move the stabilizer until the cam is not in contact with the limit switch.
D. Limit Switch Removal
SUBTASK 27-41-94-020-001
(1) Remove the limit switch [1]:
(a) Disconnect the limit switch [1] wire from the wire connection.
(b) Remove the locknut [4] and washer [3] which attach the limit switch arm [5] to the limit
switch [1].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-94
Page 401
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(c) Remove the lockwasher [6] and retainer nut [7] which attach the limit switch [1] to the
bracket assembly [2].
(d) Remove the limit switch [1] from the bracket assembly [2].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-94
Page 402
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Trim Limit Switches Installation
Figure 401 (Sheet 1 of 3)/27-41-94-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-94
Page 403
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Trim Limit Switches Installation
Figure 401 (Sheet 2 of 3)/27-41-94-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-94
Page 404
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Trim Limit Switches Installation
Figure 401 (Sheet 3 of 3)/27-41-94-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-94
Page 405
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-41-94-400-801
3. Stabilizer Trim Limit Switch Installation
(Figure 401)
A. References
Reference Title
27-41-94-700-801 Stabilizer Trim Limit Switches Test (P/B 501)
27-41-94-820-801 Stabilizer Trim Limit Switches Adjustment (P/B 501)
B. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
C. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
D. Limit Switch Installation
SUBTASK 27-41-94-420-001
(1) Install the limit switch [1]:
(a) Install the limit switch [1] through the bracket assembly [2].
(b) Install the retainer nut [7] and lockwasher [6] to attach the limit switch [1] to the bracket
assembly [2].
(c) Torque retainer nut [7] to 15 in-lb (2 Nm) to 25 in-lb (3 Nm).
(d) Install lockwire on retainer nut [7].
(e) Turn the limit switch arm [5] to the approximate position for installation but make sure that
it does not touch the cam.
(f) Put the limit switch arm [5] on the limit switch [1] to engage the serrations.
(g) Install the washer [3] and locknut [4].
1) Tighten the locknut [4] by hand.
NOTE: You will tighten the locknut [4] after you adjust the limit switch [1].
(h) Connect the limit switch [1] wire at the wire connection.
中國航空網 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4(22)
