737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(85)

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

 (Fig. 501).
 1) If the tension is not as specified, adjust the cables ACBA
 and ACBB.
 NOTE: Before the adjustment, the two ends of the____
 captain's and the first officer's control wheels
 must touch the straightedge. After the adjustment,
 the two ends of the captain's control wheel must
 touch the straightedge. One of the two ends of the
 first officer's control wheel must touch the
 straightedge. The other end of the first officer's
 control wheel cannot be farther than 0.20 inch from
 the straightedge. Do not use force or clamps to
 install the straightedge on the control wheels
 during this check.
 (h)  Make sure that you can easily install and remove the rig pin
 A/S-1A.
 (i)  Make sure that the aileron trim pointers (located on the top of
 both control wheels) align with the zero indication on the
 aileron trim scales (located at the top of each control column)
 to within +/- 0.02 inch. Replace pointer if necessary.
 (j)  Remove the straightedge from the control wheels.
 (k)  Remove all the rig pins.
 (l)  Operate the aileron control system through a minimum of two
 cycles.
 (m)  Make sure that the trim roller is correctly installed in the
 cam detent.
 (n)  Make sure that you can easily install and remove the rig pins
 A/S-1, A/S-1A, A/S-3 and A/S-15.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-00
 ALL  ú ú 01 Page 510 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

CABLE AB 
CABLE AA 
SPOILER CONTROL QUADRANT 
PRESSURE DECK 

ROD END 
RIG PIN A/S-3 
AILERON BUS DRUMS  DRAIN HOLE SPRING CARTRIDGE  FWD 
RIG PIN A/S-4 
Spring Cartridge Adjustment Figure 504 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-00
 ALL  ú ú 01 Page 511 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AILERON TRIM ACTUATOR
SEE  A  RIG PIN 
A/S-15 
B 
FWD  INBD
TOP POWER 
CONTROL UNIT 
PRESSURE 
DECK 
SPRING 
CARTRIDGE 
RIG PIN A/S-4 

A 
ACTUATOR TRIM AILERON MECHANISM SPRING CENTERING  A  SEE  DRUMS AILERON BUS D
BOTTOM POWER CONTROL UNIT 
SEE  B  VALVE ROD SEE C  FWD  INBD
A 
Figure 505 (Sheet 1) Aileron Power Control Unit Adjustment 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-00
 ALL  ú ú 01 Page 512 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

____DIMENSIONS "X" AND "Y" MUST BE
NOTE: EQUAL TO A LIMIT OF |0.01 INCH
Aileron Power Control Unit Adjustment Figure 505 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-00
 ALL  ú ú 01 Page 513 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 825-070
 WARNING:_______ DO NOT PRESSURIZE THE HYDRAULIC SYSTEM DURING THE ADJUSTMENT
 OF THE AILERON SPRING CARTRIDGE.  IF YOU PRESSURIZE THE
 HYDRAULIC SYSTEM, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN

 OCCUR.
 (4)  
　
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(85)