• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-06 23:21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

 22-13-00
 ALL  ú ú 05 Page 14 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 LATERAL AUTOPILOT SERVO - REMOVAL/INSTALLATION
______________________________________________
 1.  General_______
 A.  This procedure contains two tasks. The first is the removal of the Lateral Autopilot Servo (LAS) from the forward bulkhead of the left wing gear well. The second is for the installation of the LAS. The installation task includes the necessary test steps to make sure the LAS operates correctly.
 B.  Three mounting bolts attach the LAS (B7085) to the structure. The crank arm of the LAS attaches to a control arm. There are two hydraulic lines and one electrical plug that are also attached to the LAS.
 TASK 22-13-01-004-023
 2.  Lateral Autopilot Servo Removal (Fig. 401 and 402)_______________________________
 A.  Special Tools and Equipment
 (1)  
G12001-XX rigging pin #2 (A/S-2). The pin should be 0.309 to 0.311 inch diameter (0.303 to 0.308 is optional), with a minimum length of

 5.5 inches.

 (2)  
G12001-XX rigging pin #3 (A/S-3). The pin should be 0.309 to 0.311 inch diameter (0.303 to 0.308 is optional), with a minimum length of

 2.0 inches.

 (3)
MIT65B04001-41, Control Wheel Straight Edge Miscellaneous Tool


 B.  Standard Tools and Equipment
 (1)  Bucket
 C.  References
 (1)  
24-22-00/201, Manual Control

 (2)  
29-11-00/201, Main Hydraulic Supply System

 (3)  
32-00-30/201, Landing Gear Door Locks

 (4)  
IPC 22-13-01, Fig. 1

 (5)  
IPC 27-11-08, Fig. 1


 D.  Access
 (1)  Location Zone
 135 Wing Landing Gear Well, LH

 E.  Prepare for the Removal
 S 864-024
 (1)  Supply the electrical power (Ref 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-13-01
 ALL  ú ú 01 Page 401 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
SEE B
SEE A
B
RIGGING PIN A/S-2
RIGGING PIN A/S-3
A

Lateral Autopilot Servo Installation and Safety Tools
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-13-01
 ALL  ú ú 01 Page 402 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL 
3. BOLT  4. WASHER 
5.NUT 
2. 1. BOLT BUSHING 
CONTROL ROD 
3. BOLT  6. SERVO AUTOPILOT LATERAL 
4. 5. NUT WASHER 
Figure 402 LAS Mounting Details 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-13-01
 ALL  ú ú 01 Page 403 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 494-056
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO INSTALL
_______ THE DOOR LOCKS ON THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2)  Do this task: "Body Landing Gear Door Lock Installation" (Ref 32-00-30/201).
 S 864-057
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (3)  Remove the hydraulic pressure from hydraulic systems 1, 2, 3, and 4 (Ref 29-11-00/201)
 NOTE: Make sure the hydraulic pressure is down to zero before you
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 空调 AUTO FLIGHT(110)