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时间:2011-04-19 08:02来源:蓝天飞行翻译 作者:航空
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 S 034-010

 (3)  
Remove the cable clamps and rig pins from the control cable and drums.

 S 434-011

 (4)  
Tighten the cable as told in the temperature - tension chart in the system chapter.


 NOTE:____Use a tensiometer to do a check on the cable tension. Apply the tensiometer to the cable a minimum of 6 inches from the turnbuckle terminal or other fittings. To make sure you get the correct cable tension, permit a minimum of 1 hour at constant ambient temperature (|5°F) for the airframe temperature to become stable.
 S 434-012
 (5)  
Install the turnbuckle locking clips on all the adjusted turnbuckles (Ref 20-10-05).

 S 714-013

 (6)  
Operate the controls (refer to the applicable system chapter) through full travel.

 (a)  
Make sure the controls move freely.

 (b)  
Make sure too much force is not necessary.

 


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 20-10-07
 ALL  ú ú 01 Page 403 ú Mar 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 CONTROL CABLE QUICK STOPS - REMOVAL/INSTALLATION
________________________________________________
 1.  General_______
 A.  This procedure contains one task. The task is the replacement of the control cable quick stops (referred to as cable stops in this procedure).
 B.  Cable stops give protection to the control stand cable drums if an engine separation occurs.
 TASK 20-10-08-964-001
 2.  Replace the Cable Stop (Fig. 401).______________________
 A.  References
 (1)  20-10-23/401, Lockwires
 B.  Remove the Cable Stop
 S 034-002
 (1)  
Remove the lockwire that connects the cable stop to the swaged cable terminal stud.

 S 024-003

 (2)  
Move the cable stop longitudinally away from the terminal stud until the cable stop disengages.

 S 024-004

 (3)  
Move the cable stop laterally and let the cable go through the slot in the cable stop.


 C.  Install the Cable Stop
 S 424-005
 (1)  
With the large center hole of the cable stop to the swaged cable terminal stud, move the slot of the cable stop over the cable.

 S 424-006

 (2)  
Push the cable stop on the end of the swaged cable terminal stud until the cable stop fully engages.

 (3)  
Twist the swaged cable terminal stud to get the dimension shown.

 S 434-008

 (4)  
Install the lockwire from the cable stop to the swaged cable terminal stud (Ref 20-10-23).


 S 824-007
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 20-10-08
 ALL  ú ú 01 Page 401 ú Mar 20/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

CABLE STOP LOCKWIRE  SWAGED CABLE

Control Cable Stops Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 20-10-08
 ALL  ú ú 01 Page 402 ú Dec 15/82
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 FLARELESS TUBING ASSEMBLY - REMOVAL/INSTALLATION
________________________________________________
 1.  General_______
 A.  This procedure contains six tasks:
 (1)  
The first task is to remove the flareless tubing assembly.

 (2)  
The second task is to install the flareless tubing assembly.

 (3)  
The third task is electrical resistance specifications in the fuel tank.

 (4)  
The fourth task is the installation of flareless fittings in pressurized areas, fuel tanks or cargo areas.

 (5)  
 
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本文链接地址:757 AMM 飞机维护手册 STANDARD PRACTICES - AIRFRAME(12)