曝光臺(tái) 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

(d) Move and hold the STAB TRIM switches on the captain’s control wheel to the NOSE DOWN
position.
1) Make sure that stabilizer leading edge moves up (APL NOSE DOWN).
2) Release the STAB TRIM switches.
(e) Move the stabilizer to approximately 12 units of trim.
(f) Move the STAB TRIM switches on the captain’s control wheel to the NOSE UP position until
the stabilizer stops automatically.
1) Use the bar, SPL-1677 to measure the "B" dimension.
2) Make sure the "B" dimension is 24.80 ±0.10 in. (629.9 ±2.6 mm).
SUBTASK 27-41-94-410-003
(4) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-94
Page 513
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
STABILIZER TRIM CONTROL SWITCH - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of a stabilizer trim control switch
(2) An installation of the stabilizer trim control switch.
B. The stabilizer trim control switch is referred to as the "switch assembly" in this procedure.
C. The switch assembly has an electrical cable which connects to the terminal block in the control
wheel. If a switch becomes defective, the switch and electrical cable are replaced as an assembly.
D. This procedure is applicable for the captain’s and first officer’s switch assembly.
TASK 27-41-97-000-801
2. Stabilizer Trim Control Switch Removal
(Figure 401)
A. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
B. Prepare for the Removal
SUBTASK 27-41-97-860-005
(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
C. Switch Assembly Removal
SUBTASK 27-41-97-020-001
(1) Remove the medallion [2] from the control wheel.
SUBTASK 27-41-97-020-002
(2) Remove the screws [4] from the terminal block cover [3].
(a) Remove the terminal block cover [3].
SUBTASK 27-41-97-020-003
(3) Remove the switch assembly [1]:
(a) Remove the screws [9], washers [8], and washers [10] to disconnect the switch wires from
the terminal block [7].
(b) Remove the terminals from the switch wires to help the removal.
(c) Attach a threading wire to the switch electrical cable.
NOTE: This threading wire that is attached to the electrical cable is to help with the
installation of the switch assembly.
(d) Remove the screws [5] which attach the switch assembly [1] to the control wheel handle.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-97
Page 401
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(e) Slowly pull the switch assembly [1] from the horn of the control wheel until the switch wires
show.
NOTE: Pull until approximately 3 in. (76 mm) of the threaded wire comes out of the
control wheel handle. Do not remove the threaded wire from the control wheel. It
is necessary to use this threaded wire for installation.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-97
Page 402
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Trim Control Switch Installation
Figure 401 (Sheet 1 of 2)/27-41-97-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-97
Page 403
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Trim Control Switch Installation
Figure 401 (Sheet 2 of 2)/27-41-97-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-97
Page 404
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-41-97-400-801
3. Stabilizer Trim Control Switch Installation
(Figure 401)
A. References
Reference Title
27-41-97-700-801 Stabilizer Trim Control Switch Test (P/B 501)
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Switch Assembly Installation
SUBTASK 27-41-97-420-001
(1) Install the switch assembly [1]:
　
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(jī)維護(hù)手冊(cè)4(27)