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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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 S 014-005

 (4)  
Open the access door for the neutral shift and override mechanism, 313AL (Ref 06-42-00).

 S 864-006

 (5)  
Move the horizontal stabilizer until Dimension B on the stabilizer ballscrew actuator is 15.89 | 0.01 inches


 (403.6 +/- 0.25 mm) (Fig. 401).
 S 864-007
 (6)  
Remove the pressure from the right and center hydraulic systems (Ref 29-11-00).

 S 864-008

 (7)  
Put the L, R, and C FLT CONTROL SHUTOFF switches on the right side panel, P61, to the OFF position.

 S 864-009

 (8)  
Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the CUTOUT position.

 S 864-010

 (9)  
Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags:

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


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 27-31-21
 ALL  ú ú 02 Page 405 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 (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

 E.
Remove the Neutral Shift and Override Mechanism (Fig. 402)


 S 494-011
 (1)  
Install rig pin E/ST7 in the aft quadrants.

 S 494-012

 (2)  
Install rig pin E/ST10 in the neutral shift housing.

 S 034-013

 (3)  
Disconnect the two control rods that connect the neutral shift mechanism to the feel and centering unit.


 NOTE: Do not change the adjustment of the control rods.
____
 S 034-014
 (4)  
Remove the three fasteners that connect the neutral shift link to the neutral shift mechanism at the stabilizer input lever.

 S 034-015

 (5)  
Remove the two grounding springs that connect the neutral shift mechanism to the torque box bracket on the elevator aft mechanism.


 NOTE: Each spring has a force of 150 pounds (667 newtons).
____
 S 034-016
 (6)  
Remove the four fasteners that attach the neutral shift mechanism to the torque box of the elevator aft mechanism.

 (7)  
Remove the neutral shift and override mechanism.


 S 024-017
 TASK 27-31-21-424-018
 3.  Install the Neutral Shift and Override Mechanism________________________________________________
 A. References
 (1)  
06-42-00/201, Empennage Access Doors and Panels

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

 (3)  
27-31-00/501, Elevator Control System


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 27-31-21
 ALL  ú ú 02 Page 406 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 B. Access
 (1)  
Location Zones
 211/212 Control Cabin
 311/312 Area Aft of Pressure Bulkhead to BS 1787.45
 313/314 Stabilizer Center Section Compartment


 (2)  
Access Panels
 311AL Forward Stabilizer Compartment
 313AL Elevator Neutral Shift and Override Mechanism


 C.
Install the Neutral Shift and Override Mechanism (Fig. 402)


 S 434-019
 (1)  
Install the four fasteners to attach the neutral shift mechanism to the torque box for the elevator aft mechanism.

 S 434-020

 (2)  
Install the two grounding springs between the neutral shift mechanism and the torque box for the elevator aft mechanism.

 S 434-021

 (3)  
Install the three fasteners to connect the neutral shift link to the neutral shift mechanism at the stabilizer input lever.
 
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