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时间:2011-04-21 08:06来源:蓝天飞行翻译 作者:航空
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B BOLT DETAIL C BOLT DETAIL  NUT 
Figure 401 Asymmetry Limiter Actuator Installation 

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A
757
MAINTENANCE MANUAL


BASE OF THE CONTROL COLUMN
SEE

Control Column Rig Pin Location
Figure 402

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A

757 MAINTENANCE MANUAL
 S 864-006
 (5)  
Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags:

 (a)  
11B19, STAB TRIM ALT (IF INSTALLED)

 (b)  
11C12, STAB TRIM SHUTOFF LEFT

 (c)  
11C13, STAB TRIM SHUTOFF RIGHT

 (d)  
11H11 or 11C05, STAB TRIM CONT L

 (e)  
11H17, FLT CONT SHUTOFF TAIL LEFT

 (f)  
11H18, FLT CONT SHUTOFF TAIL CTR

 (g)  
11H20, STAB TRIM CONT R

 (h)  
11H28, FLT CONT SHUTOFF TAIL RIGHT


 S 014-007
 (6)  Open the access door for the forward equipment bay, 113AL
 (Ref 06-41-00).

 S 014-008
 WARNING: STAY OFF THE SERVICE ACCESS DOOR, 311AL AND THE ELEVATOR
_______ CONTROL ACCESS DOOR, 313AL. YOUR WEIGHT CAN RELEASE THE SPRING-LOADED LATCHES ON THE DOOR. IF YOU FALL THROUGH THE DOOR, INJURIES CAN OCCUR.
 (7)  
Open the access door for the forward stabilizer compartment, 311AL (Ref 06-42-00).

 S 014-009

 (8)  
Open the access door for the elevator aft quadrants, 313AL (Ref 06-42-00).

 S 494-010

 (9)  
Install rig pins E/ST7 (Fig. 401).

 S 494-011

 (10)
 Install rig pin E/ST6 (Fig. 402).

 E.
Remove the Asymmetry Limiter Actuator (Fig. 401)


 S 214-012
 (1)  
Make sure the asymmetry limiter actuator is in the fully retracted position.

 (2)  
Disconnect the electrical connector.


 S 034-013
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A
757 MAINTENANCE MANUAL
 S 034-014
 (3)  
Remove the bolts, washers, and nuts that attach the asymmetry limiter actuator to the first officer's aft quadrant.

 S 024-015

 (4)  
Remove the asymmetry limiter actuator.


 TASK 27-31-03-424-016
 3.  Install the Asymmetry Limiter Actuator______________________________________
 A. References
 (1)  
06-41-00/201, Fuselage Access Doors and Panels

 (2)  
06-42-00/201, Empennage Access Doors and Panels

 (3)  
24-22-00/201, Electrical Power - Control

 B.
Access

 (1)  
Location Zones 113/114 Area Forward of NLG Wheel Well 211/212 Control Cabin 311/312 Area Aft of Pressure Bulkhead to BS 1787.45 313/314 Stabilizer Center Section Compartment

 (2)  
Access Panels
 113AL Forward Equipment Bay
 311AL Forward Stabilizer Compartment
 313AL Elevator Aft Quadrants


 C.
Install the Asymmetry Limiter Actuator (Fig. 401)


 S 214-017
 (1)  
Make sure the new asymmetry limiter actuator is in the fully retracted position.

 S 424-018

 (2)  
Hold the asymmetry limiter actuator in its correct position on the first officer's aft quadrant.

 S 424-019

 (3)  
Install the bolts, washers, and nuts to attach the asymmetry limiter actuator to the first officer's aft quadrant.
 
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