• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-01 19:17来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Put the rig pins R-3 and R-4 through the rig pin holes of the two forward quadrants.

 S 024-021

 (2)  
Disconnect the brake pushrods from the bellcranks (Fig. 401).

 S 024-014

 (3)  
Remove the screws that attach the top cover for the rudder pedals to the heel rests (Fig. 402).


FORWARD QUADRANT SEE C
BRAKE
PUSHROD

SEE B
SEE A QUADRANT
PEDAL ARM PUSHROD
(EXAMPLE) (EXAMPLE)
CABIN FWD
FLOOR
BEAM
PIN
SEE D

(R-1 ON THE CAPTAIN'S PEDALS) (R-2 ON THE FIRST OFFICER'S PEDALS)
BELLCRANK
A
(EXAMPLE)
Rudder Pedal Assemblies Installation
Figure 401 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-31
 ALL  ú ú 01 Page 402 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
BUS ROD
FORWARD
QUADRANT

STEERING ARM  FORWARD 
(LEFT QUADRANT ONLY)  RIG PIN 
HOLE 
JACKSHAFT  RIG PIN 
FWD  SUPPORT  (R-3 ON THE CAPTAIN'S QUADRANT) 
CHANNEL  (R-4 ON THE FIRST OFFICER'S QUADRANT) 

FORWARD QUADRANT
FWD
QUADRANT STOP
C
Rudder Pedal Assemblies Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-31
 ALL  ú ú 01 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
1.
 BOLT

2.
 RADIUS FILLER


4.
 RADIUS FILLER

5.
 WASHER


A
737-300/400/500MAINTENANCE MANUAL
STRUCTURE 
RIG PIN 
(R-1 ON THE CAPTAIN'S 
PEDAL ARMS)  PEDAL ARMS 
(R-2 ON THE FIRST OFFICER'S 
PEDAL ARMS) 

SUPPORT SHAFT FOR THE RUDDER PEDAL
SUPPORT SHAFT BRACKET SEE F
BELLCRANK
SEE E FWD
BRAKE PUSHRODS
D
SUPPORT SHAFT BRACKET SUPPORT SHAFT BRACKET
3. SHIM(1 OR 2 AS NECESSARY)
3.
 RADIUS FILLERSTRUCTURE (2 LOCATIONS)

4.
 WASHER


4. RADIUS (2 LOCATIONS)
FILLER
5.
 WASHER

6.
 NUT


E
Rudder Pedal Assemblies Installation
Figure 401 (Sheet 3)

QUADRANT
PUSHRODS

INBD
1.
 BOLT  (2 LOCATIONS)

2.
 RADIUS FILLER (2 LOCATIONS)


5. NUT (2 LOCATIONS)
F
H86863
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-31
 ALL  ú ú 02 Page 404 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 024-015
 (4)  
Remove the top cover for the rudder pedals.

 S 024-016

 (5)  
Disconnect the quadrant pushrods from the pedal arms.

 S 024-017

 (6)  
Remove the four bolts that attach the support shaft bracket to the airplane.

 S 024-022

 (7)  
Hold the rudder pedals, and remove the support shaft for the rudder pedals.

 S 024-023

 (8)
Pull the rudder pedals up, through the floor, to remove them.


 NOTE: The left and right foot pedals and the shaft support bracket
____ will disconnect after you remove them.
 The outer bearing will be free to fall from the pedal bellcrank when you remove the rudder pedals.
 TASK 27-21-31-404-010
 2.  Install the Rudder Pedal Assemblies (Fig. 401)___________________________________
 A. Special Tools and Equipment
 (1)  F70207-93 Rig Pin Kit:
 ~........................................................................ | | F70207 | DIAMETER | LENGTH | | | REF NO. | -( ) | (INCHES) | (INCHES) | FUNCTION | .......................................................................... | R-1 | -14 | 0.309-0.311 | 12.7 |0.25 | RUDDER PEDAL ARMS | | | | | | | | R-2 | -14 | 0.309-0.311 | 12.7 |0.25 | RUDDER PEDAL ARMS | | | | | | | | R-3 | -11 | 0.309-0.311 | 6.7 |0.25 | RUDDER FORWARD QUADRANT | | | | | | | | R-4 | -11 | 0.309-0.311 | 6.7 |0.25 | RUDDER FORWARD QUADRANT | 2.........….........….............…............….........................1
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 2(47)