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时间:2010-08-24 13:01来源:蓝天飞行翻译 作者:admin
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(c) Connect the electrical connectors.
SUBTASK 27-41-51-420-004
(4) Connect the rod assemblies [8] to the column cutout switch arms [3]:
(a) Install the rig pin E-1 from the rig pin kit, SPL-1585 through the left forward control quadrant.
(b) Install the rig pin ST-4 from the rig pin kit, SPL-1585 in the column cutout switch.
(c) Remove the lockwires from the rod assembly [8].
(d) Turn the jamnuts [7] until you can easily install the bolt that connect the rod assembly [8] to
the column cutout switch arm [3].
(e) Install the bolt [4], washer [5], and nut [6] to connect the rod assembly [8] to the column
cutout switch arm [3].
(f) Tighten the jamnuts [7].
(g) Install the lockwire, G01048.
(h) Remove the rig pin E-1 from the left forward control quadrant.
(i) Remove the rig pin ST-4 from the control column switch.
SUBTASK 27-41-51-860-002
(5) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
D 10 C00840 FLIGHT CONTROL STAB TRIM ACTUATOR
SUBTASK 27-41-51-710-001
(6) Do this task: Column Cutout Switches Test, TASK 27-41-00-700-810.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-41-51-410-001
(1) Close this access panel:
Number Name/Location
112A Forward Access Door
------------------------- END OF TASK ---------------------------
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
HORIZONTAL STABILIZER TRIM CONTROL WHEEL - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) Stabilizer Trim Control Wheel Removal.
(2) Stabilizer Trim Control Wheel Installation.
TASK 27-41-61-010-801
2. Stabilizer Trim Control Wheel Removal
(Figure 401)
A. Location Zones
Zone Area
212 Flight Compartment - Right
B. Stabilizer Trim Control Wheel Removal
SUBTASK 27-41-61-010-001
(1) Remove the stabilizer trim wheel [1] from the control stand [7]:
(a) Remove the bolt [2] that attaches the stabilizer trim wheel [1] to the shaft.
(b) Remove the stabilizer trim wheel [1] from the shaft.
SUBTASK 27-41-61-010-002
(2) As necessary, remove the upper side cover [3] and lower side cover [5] from the right side of the
control stand [7]:
(a) Remove the screws [6] and the pocket assembly [8] from the lower side cover [5].
(b) Remove the screws [4] that attach the upper side cover [3] and the lower side cover [5] to
the control stand [7].
(c) Remove the upper side cover [3] and the lower side cover [5] from the control stand [7].
------------------------- END OF TASK ---------------------------
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Stabilizer Trim Control Wheel Installation
Figure 401/27-41-61-990-801
737-600/700/800/900
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EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-41-61-410-801
3. Stabilizer Trim Control Wheel Installation
(Figure 401)
A. Location Zones
Zone Area
212 Flight Compartment - Right
B. Stabilizer Trim Control Wheel Installation
SUBTASK 27-41-61-410-002
(1) As necessary, install the upper side cover [3] and lower side cover [5] on the control stand [7]:
(a) Install the upper side cover [3] and the lower side cover [5] on the control stand [7].
(b) Install the screws [4] that attach the upper side cover [3] and the lower side cover [5] to the
control stand [7].
(c) Install the screws [6] in the pocket assembly [8] and the lower side cover [5].
SUBTASK 27-41-61-410-003
(2) Install the stabilizer trim wheel [1] on the control stand [7]:
(a) Install the stabilizer trim wheel [1] on the shaft with the handle 90 +/- 15 degrees apart
from the handle on the other stabilizer trim wheel.
(b) Install the bolt [2] that attaches the stabilizer trim wheel [1] to the shaft.
------------------------- END OF TASK ---------------------------
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
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STABILIZER TRIM MOTOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
 
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