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时间:2011-04-21 08:04来源:蓝天飞行翻译 作者:航空
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 A.  General
 (1) This task contains these procedures:
 -
Remove the Input Crank Assembly

 -
Remove the Top Compensating Rod

 -
Remove the Multiplier Crank

 -
Remove the Bottom Compensating Rod.


 Because this task contains four procedures, do only the applicable groups of steps.
 To start one of these procedures, do the "Prepare for the Removal" group of steps. Then, do the group of steps that is necessary to remove the component.
 B.  Equipment
 (1)
Nose Gear Towing Lever Lockpin - A09003-1

 (2)
Rig Pins from Set B20003-XX (Ref 20-10-24):

 (a)
R3 - P/N B20003-16

 (b)
R4 - P/N B20003-19

 C.  
References

 (1)
06-42-00/201, Empennage Access Doors and Panels

 (2)
20-10-24/201, Rig Pins

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

 (4)
27-21-17/401, Yaw Damper Summing Lever

 D.  
Access

 (1)  
Location Zone 342 Vertical Stabilizer - Rear Spar to Trailing Edge

 (2)  
Access Panels
 311AL Tailcone Compartment
 322BZ Bottom Forward Torque Box
 324AL Body to Fin Seal
 324BL Aft Side of Rear Spar and Rudder Hinge
 324CL Rudder Hinge and PCAs

 

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 27-21-19
 ALL  ú ú 03 Page 401 ú Jun 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

CONTROL LINKAGES
SEE A
YAW DAMPER POWER CONTROL
MECHANISM
ACTUATOR (3) SEE B
322BZ
CONTROL RODS
TO THE PCA'S
SUMMING INPUT CRANK
LEVER RIGHT OUTBOARD GROUNDING SPRING PRIMARY CONTROL ROD
LEFT 
OUTBOARD SPRING GROUNDING  MECHANISM YAW DAMPER
SEE  B  POSITION 
TRANSMITTER 

RATIO CHANGER POGOBIAS POGO
ROD (SECONDARY CONTROL ROD) YAW
RUDDER THERMAL RUDDER RATIODAMPER COMPENSATING CHANGER MECHANISMSERVO LINKAGE
(2 LOCATIONS) SEE C AFT QUADRANT
RA
YAW DAMPER MECHANISM FEEL, CENTERING,
RB
B  AND TRIM MECHANISM
FWD
AUTOPILOT ROLLOUT GUIDANCE SERVOS (3)
CONTROL LINKAGES
A
Rudder Thermal Compensating Linkage Installion
Figure 401 (Sheet 1)

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 27-21-19
 ALL  ú ú 04 Page 402 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL


RUDDER THERMAL COMPENSATING LINKAGE


Rudder Thermal Compensating Linkage Installation
Figure 401 (Sheet 2)

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 27-21-19
 ALL  ú ú 04 Page 403 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

MIDDLE POWER
CONTROL ACTUATOR

SEE D
FEEL, CENTERING,
YAW DAMPER AND TRIM MECHANISM
MECHANISM SEE B
SEE A
RATIO CHANGER POGO ROD SEE E
SUMMING LEVER
YAW DAMPER
BIAS POGO

SEE C
CONTROL ROD FROM THE RATIO CHANGER MECHANISM
YAW DAMPER
SERVOS

RIG PIN HOLE R3
FWD INBD
YAW DAMPER MECHANISM FEEL, CENTERING, AND TRIM MECHANISM
A B
Rigging Pin Installation Figure 402 (Sheet 1)
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 27-21-19
 ALL  ú ú 04 Page 404 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A


 
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