• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-01 08:47来源:蓝天飞行翻译 作者:航空
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

 (b)  
Make sure that the CWS ROLL and CWS PICTH indications come on.

 (c)  
Make sure that the control column does not move when you engage the autopilot.

 (d)  
Push the control column.

 (e)  
Make sure that the elevator moves down.

 (f)  
Pull the control column.

 (g)  
Make sure that the elevator moves up.

 (h)  
Move the control column to the center.

 (i)  
Disengage the autopilot.


 E. Put the Airplanes Back to Its Initial Condition
 S 865-036
 (1)
Remove hydraulic power if it is not necessary (AMM 29-15-00/201).

 (2)
Remove electrical power if it is not necessary (AMM 24-22-00/201).


 S 865-035
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-11-26
 ALL  ú ú 02 Page 519 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AUTOPILOT ELEVATOR ACTUATOR LINKAGE - INSPECTON/CHECK
____________________________________________________
 1.  General_______
 A.  The data in this procedure contains illustrations and a wear limit table. To get access to the components, or to replace the components during the inspection, refer to AMM 22-11-26/401.
 TASK 22-11-26-206-001
 2.  A/P Elevator Actuator Linkage Wear Limits (Fig. 601)_________________________________________
 A.  General
 (1)  The data in this procedure contains illustrations and a wear limit table. To get access to the components, or to replace the components during the inspection, refer to AMM 22-11-26/401.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-11-26
 ALL  ú ú 02 Page 601 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

737-300/400/500MAINTENANCE MANUAL 
SEE  A 
AUTOPILOT 
B ACTUATOR 
OUTPUT 
QUADRANT 
SHAFT  A/P ACTUATOR B 
LEVER ASSEMBLY 
AUTOPILOT 
A ACTUATOR 
ROD 
ASSEMBLY 
SEE  B 
INPUT QUADRANT  LEVER ASSEMBLY 
FWD  SHAFT 
A/P ACTUATOR A 

ROD ASSEMBLY 
LOWER TORQUE 
TUBE LEVER 
B
A/P Elevator Actuator Linkage Wear Limits 
Figure 601 (Sheet 1) 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-11-26
 ALL  ú ú 01 Page 602 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
A
2. LEVER/BOLT
1. BEARING/BOLT
A
3. BEARING/BOLT
4. LEVER/BOLT
A AA
6. LEVER/BOLT A
5. BEARING/BOLT  LEVER
BEARINGBOLT
A-A
A
8. LEVER/BOLT
A
7. BEARING/BOLT
A/P Elevator Actuator Linkage Wear limits Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-11-26
 ALL  ú ú 01 Page 603 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
NO. INDEX  PART NAME  DIM.  DESIGN (MANUFACTURING) LIMITS  SERVICE (WEAR) LIMITS  REPAIR (REWORK) LIMITS 
DIAMETER  CLEARANCE DIAMETRICAL  DIAMETER  MAX ANCE CLEAR-DIA BUSHING OR PLATING PERMITTED  INTERFERENCE BUSHING 
MIN  MAX  MIN MAX  MIN  MAX  YES  NO  MTL  MIN  MAX 
1  BEARING  ID  0.2497  0.2500  0.0002  0.0015 
 0.2530  3 0.0035  X 
 
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 自动飞行 AUTOFLIGHT 2(12)