• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-20 07:56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

MAINTENANCE MANUAL

SEE  A 
TORQUE 
TUBES  APCS OUTPUT 
(REF)  RODS (REF) 
(3 LOCATIONS) 
TORQUE BOX 
(REF) 
AFT  LEFT APCS 
QUADRANT (REF)  SEE  B 

SEE B CENTER APCS 
RIG PIN E/ST 7  FEEL AND CENTERING UNIT (REF)  A FWD SEE B RIGHT APCS OUTBD 
Figure 401 (Sheet 1) Autopilot Pitch Control Servo 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-12-01
 ALL  ú ú 01 Page 402 ú Jun 15/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

HYDRAULIC RETURN (REF)
ELECTRICAL CONNECTOR (REF)
HYDRAULIC
PRESSURE
(REF)

8.
 FILTER

9.
 PACKING

10.
 UNION


7. ROD ASSEMBLY
11.
 PACKING

12.
 UNION


1.
 BOLT

2.
 WASHER


TORQUE BOX (REF)
3. SERVO ASSEMBLY
4. BOLT  OUTPUT CRANK 
JAMNUT  (REF) 
(REF) 
5. WASHER 
6. NUT 

AUTOPILOT PITCH CONTROL SERVO (TYPICAL)
B
Autopilot Pitch Control Servo
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-12-01
 ALL  ú ú 01 Page 403 ú Jun 15/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 (e)  
For the center servo: 1) 11E20, FLT CONT CMPTR PWR CENTER 2) 11E21, FLT CONT CMPTR SERVO CENTER

 (f)  
For the right servo: 1) 11E35, FLT CONT CMPTR PWR RIGHT 2) 11E36, FLT CONT CMPTR SERVO RIGHT


 S 014-006
 WARNING:_______STAY OFF THE CONTROLS BAY ACCESS DOOR, 313AL. THE WEIGHT OF PERSONS ON THIS DOOR COULD CAUSE ITS SPRING-LOADED LATCHES TO RELEASE. PERSONS COULD FALL THROUGH THE OPENING AND BE INJURED.
 WARNING:  STAY OFF THE SERVICE ACCESS DOOR, 311AL, IF IT IS OPENED (NOT REQUIRED FOR THIS PROCEDURE). THE WEIGHT OF PERSONS ON THIS DOOR COULD CAUSE ITS SPRING-LOADED LATCHES TO RELEASE. PERSONS COULD FALL THROUGH THE OPENING AND BE INJURED.
 (6)  Open access panel 313AL (Ref 06-42-00).
 D. Remove Autopilot Pitch Control Servo
 S 034-007
 (1)  
Disconnect the electrical connector from servo.

 S 034-008

 (2)  
Remove the bolt (4), the nut (6) and the washer (5) from the rod assembly (7).

 S 034-066

 (3)  
Disconnect the rod assembly from the servo output crank.

 S 034-009

 (4)  
Disconnect the hydraulic lines.

 S 434-010

 (5)
Seal the hydraulic lines and servo hydraulic ports with caps.

 S 024-011

 (6)  
Hold the servo and remove the bolts (1), the washers (2) and the servo (3).


 NOTE: The servo assembly weighs 17 pounds.
____
 TASK 22-12-01-424-067
 3.  Install the Autopilot Pitch Control Servo_________________________________________
 A. Equipment
 (1)  Rig Pin E/ST 7 - P/N B20003-21 from set
 B20003-XX (Ref 20-10-24)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-12-01
 ALL  ú ú 01 Page 404 ú Dec 20/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 B. Parts
 ~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Bolt | 27-31-53| 01 | 113 | | | 2 | Washer | | | 114 | | | 3 | Servo Assembly | | | 112 | | | 4 | Bolt | | | 95 | | | 5 | Washer | | | 97 | | | 6 | Nut | | | 99 | | | 7 | Rod Assembly | | | 101 | 2......…........…...................................…..........…......…........1
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:757 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 1(140)