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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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 (c)  
11C13, STAB TRIM SHUTOFF RIGHT

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

 (e)  
11H18, FLT CONT SHUTOFF TAIL CTR

 (f)  
11H20, STAB TRIM CONT R

 (g)  
11H28, FLT CONT SHUTOFF TAIL RIGHT


 S 864-025
 (4)  
Put the R and C FLT CONTROL SHUTOFF switches on the right side panel, P61, to the ON position.

 S 864-026

 (5)  
Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the NORM position.

 S 414-027

 (6)  
Close the access doors for the auxiliary power unit, 315AL and 316AR (Ref 06-42-00).


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 27-31-02
 ALL  ú ú 02 Page 407 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 S 414-028
 (7)  Close the access door for the forward stabilizer compartment, 311AL (Ref 06-42-00).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-02
 ALL  ú ú 01 Page 408 ú Jun 20/96
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A

757 MAINTENANCE MANUAL
 ASYMMETRY LIMITER ACTUATOR - REMOVAL/INSTALLATION
_________________________________________________
 1.  General_______
 A.  This procedure contains steps to remove and install the asymmetry limiter actuator for the elevator control system.
 B.  The asymmetry limiter actuator must be in the retracted position when you remove and install it.
 TASK 27-31-03-024-001
 2.  Remove the Asymmetry Limiter Actuator_____________________________________
 A.  Equipment
 (1)  
Rig Pins from Set B20003-XX (Ref 20-10-24):

 (a)  
E/ST6 - P/N B20003-21

 (b)  
E/ST7 - P/N B20003-21

 B.  
References

 (1)  
06-41-00/201, Fuselage Access Doors and Panels

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

 (3)  
20-10-24/201, Rig Pins

 (4)  
24-22-00/201, Electrical Power - Control

 C.  
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


 D.  
Prepare for the Removal

 (1)  
Supply electrical power (Ref 24-22-00).

 (2)
Make sure that the control columns are in their neutral position.

 S 864-004

 (3)  
Put the R, L, and C FLT CONTROL SHUTOFF switches on the right side panel, P61, to the OFF position.

 S 864-005

 (4)  
Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the CUTOUT position.


 S 864-002
 S 214-003
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-03
 ALL  ú ú 02 Page 401 ú Dec 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 
MAINTENANCE MANUAL 
ASYMMETRY 
LIMITER 
ACTUATOR 
ASYMMETRY  BOLT DETAIL 
LIMITER 
ACTUATOR  ELECTRICAL  SEE  B 
SEE  A  CONNECTOR 
BOLT DETAIL 
SEE  C 
FIRST OFFICER'S 
AFT QUADRANT 
TORQUE BOX 
FOR THE AFT 
MECHANISM 

E/ST 7 RIG PIN HOLE 
FWD 
A ASYMMETRY LIMITER ACTUATOR 
BOLT  WASHER NUT  BOLT  WASHER 
 
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