22-13-01
 ALL  ú ú 01 Page 412 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 S 214-061
 (12) Examine the Autopilot Rollout Control Servos for leaks.
 (a)  Repair leaks that you find.
 E. Put the Airplane Back to Its Usual Condition
 S 034-073
 (1)  Remove the DO-NOT-OPERATE tags.
 S 084-072
 WARNING: STAY AWAY FROM THE NOSE GEAR WHEELS WHEN YOU REMOVE LOCKPIN.
_______ THE NOSE WHEELS CAN MOVE TO THE CENTER POSITION QUICKLY. THIS CAN CAUSE INJURY TO PERSONS OR CAUSE DAMAGE TO EQUIPMENT.
 (2)  
Put the nose gear wheels in the center position.

 S 084-101

 (3)  
Remove the nose gear steering valve lockpin.

 S 864-071

 (4)  
Set the MCDP to off.

 S 864-070

 (5)  
Remove the hydraulic power if it is not necessary
 (AMM 29-11-00/201).

 (6)
Remove the electrical power if is not necessary (AMM 24-22-00/201).

 S 864-069
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-13-01
 ALL  ú ú 01 Page 413 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 ARGS ELECTROHYDRAULIC SERVOVALVE AND SOLENOID VALVES - MAINTENANCE PRACTICES
____________________________________________________________________________
 1.  General
_______
 A.  The three Autopilot Rollout Guidance Servos (ARGS) are in the base of the vertical stabilizer, immediately forward of the rudder hinge line. Each servo unit has one electrohydraulic servovalve (EHSV) and two solenoid valves. The servos can be accessed through panel 324AL on the lower left side of the vertical stabilizer (Ref 6-42-00).
 TASK 22-13-02-002-001
 2.  Remove the ARGS Electrohydraulic Servovalve or Solenoid Valves (Fig. 201)
______________________________________________________________
 A.  References
 (1)  
06-42-00/201, Empennage and Section 48 (Major Zone 300) Access Doors and Panels

 (2)  
24-22-00/201, Electrical Power - Control

 (3)  
29-11-00/201, Pressurize/Depressurize Main Hydraulic System

 B.  Access
 (1)  
Location Zone 324 Vertical Stabilizer, Rear Spar to Trailing Edge

 (2)  
Access Panel
 324AL Body to Fin Seal

 C.  Prepare for Removal
 S 862-002
 (1)  
Supply electrical power (Ref 24-22-00).

 S 862-003

 (2)  
Remove the pressure from the L, C, and R hydraulic system (Ref 29-11-00).

 S 862-004

 (3)  
Set the L, C, and R FLT CONTROL SHUTOFF switches on the P61 panel to OFF.

 S 862-005

 (4)  
Set the L and R STAB TRIM switches on the control stand panel P10 to CUTOUT.

 (5)  
Set the two F/D switches on the MCP to OFF.

 S 862-006
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-13-02
 ALL  ú ú 01 Page 201 ú Sep 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 S 862-007
 (6)  Open these circuit breakers on the overhead circuit breaker panel, P11, and attach DO-NOT-CLOSE tags:
 (a)  
11C12, STAB TRIM SHUTOFF LEFT

 (b)  
11C13, STAB TRIM SHUTOFF RIGHT

 (c)  
11H17, FLT CONT SHUTOFF LEFT

 (d)  
11H18, FLT CONT SHUTOFF CENTER

 (e)  
11H28, FLT CONT SHUTOFF RIGHT

 (f)  
For the left servo: 1) 11E17, FLT CONT COMPUTER POWER LEFT 2) 11E18, FLT CONT COMPUTER SERVO LEFT
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(183)