737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(127)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 trigger assembly. 7) Carefully pull the assembly from the control wheel.
 NOTE: The interphone switch is part of the assembly.
____
 8) Remove the two screws which hold the memory device (not on
 all airplanes). 9) Pull the memory device from the control wheel. 10) Disconnect the wires from the memory device.
 S 974-016
 (7)  
Write down and make a mark of the configuration of the identified color wires.

 S 034-008

 (8)  
Disconnect the wires from the terminals of the autopilot disengage, microphone, and interphone switches (Fig. 402).

 (9)
Carefully disengage the wire bundle from the control wheel.

 S 034-009
 TASK 27-11-41-404-010
 3. Aileron Control Wheel Installation
__________________________________
 A. Standard Tools and Equipment
 (1)  Insulation Tester - Biddle Model 656, Megger (500 volts)
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-41
 ALL  ú ú 02 Page 405 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
MICROPHONE SWITCH

SWITCH
INTERPHONE SWITCH
BLACK/RED BLACK/BROWN BLACK-RED

BASIC WIRING CONFIGURATION FOR CONTROL WHEEL

Control Wheel Wiring Diagram
Figure 402

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-41
 ALL  ú ú 01 Page 406 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 B. Special Tools and Equipment
 (1)
SE27-0001 - Control Wheel Straightedge

 (2)
F70207-93 or -97 Rigging Pins Kit:

 ~.............................................................................. | | | DIAMETER | LENGTH | | | REF NO. | F70207-( ) | (INCHES) | (INCHES) | FUNCTION | ................................................................................ | A/S-1 | -13 | 0.309-0.311 | 2.35 |0.06 | AILERON TRANSFER | | | | | | MECHANISM | | A/S-1A | -19 | 0.309-0.311 | 8.25 +/- 0.25 | AILERON TRANSFER | | | | | | MECHANISM | | A/S-15 | -85 | 0.309-0.311 | 2.5 |0.25 | AILERON TRIM MECHANISM| 2.........…............…...............…...............….......................1
 C. Consumable Materials
 (1)
A00607 Dow Corning Compound No. 5

 D.
Access

 (1)  
Location Zone
 101 Control Cabin, LH
 102 Control Cabin, RH

 

Aileron Control Wheel Alignment (Neutral Position)
Figure 403

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-41
 ALL  ú ú 01 Page 407 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  
Access Panel
 1103 Forward Access Door

 E.
Procedure

 S 424-011
 (1)  
Install the aileron control wheel:

 (a)  
Use a wire leader to put the electrical wires in the aileron control wheel.

 (b)  
Pull the wires away from the switch holes.

 (c)  
Install the teflon sleeves on the wires.

 (d)  
Find and connect the correct color wires to the autopilot disengage, microphone, interphone switches, and memory device (Fig. 402). 1) Tape and put away the wires that you did not use.

 (e)  
Install the microphone switch and the trigger assembly in the aileron control wheel with two screws (Fig. 401).

 (f)  
Install the autopilot disengage switch in the aileron control wheel with the retainer and screw.

 (g)  
Install the memory device in the control wheel with two screws.

 (h)  
Apply the Dow Corning Compound No. 5 to the part you can get access to on the wire bundle.

 (i)  
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(127)