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时间:2010-08-23 15:50来源:蓝天飞行翻译 作者:admin
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trim.
(c) Connect the flexible shaft [21] to the forward control mechanism [43].
1) Make sure that the splines engage before you tighten the union.
SUBTASK 27-41-41-420-007
(11) Install the drip shield [44] to the forward control mechanism [43]:
(a) Put the drip shield [44] under the forward control mechanism [43].
(b) Install the bolts [45], washers [46], and nuts [47].
(c) Install the clamp pad [49] and clamp [48] to the drip shield [44].
SUBTASK 27-41-41-410-001
(12) Close this access panel:
Number Name/Location
112A Forward Access Door
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SUBTASK 27-41-41-410-002
(13) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
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Stabilizer Trim Jackscrew Setting
Figure 402 (Sheet 1 of 2)/27-41-41-990-802
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Stabilizer Trim Jackscrew Setting
Figure 402 (Sheet 2 of 2)/27-41-41-990-802
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STABILIZER FORWARD CONTROL MECHANISM - INSPECTION/CHECK
1. General
A. This procedure contains this task:
(1) Stabilizer forward control mechanism inspection.
TASK 27-41-41-210-801
2. Stabilizer Control Mechanism Detail Visual Inspection
(Figure 601)
A. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
B. Access Panels
Number Name/Location
112A Forward Access Door
C. Procedure
SUBTASK 27-41-41-010-002
(1) Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-41-41-210-001
(2) Do a detail visual inspection of the stabilizer forward control mechanism:
(a) Examine all attachment points for security and damage.
(b) Examine upper and lower turnbuckles for damage or binding.
SUBTASK 27-41-41-410-003
(3) Close this access panel:
Number Name/Location
112A Forward Access Door
------------------------- END OF TASK ---------------------------
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Stabilizer Forward Control Mechanism
Figure 601/27-41-41-990-803
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COLUMN CUTOUT SWITCH - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of a column cutout switch
(2) An installation of a column cutout switch.
B. This procedure is applicable for the captain’s and first officer’s column cutout switches.
(1) Electrical connectors D12156 and D817 are located on the captain’s column cutout switch,
M1983.
(2) Electrical connectors D10553, D2257 and D3124 are located on the first officer’s column cutout
switch, M1201.
TASK 27-41-51-000-801
2. Column Cutout Switch Removal
(Figure 401)
A. References
Reference Title
31-31-52-000-801 Control Column Position Sensor Removal (P/B 401)
B. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
C. Access Panels
Number Name/Location
112A Forward Access Door
D. Prepare for the Removal
SUBTASK 27-41-51-860-001
(1) Open these circuit breakers and install safety tags:
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 27-41-51-010-001
(2) Open this access panel:
Number Name/Location
112A Forward Access Door
 
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