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时间:2011-04-01 19:17来源:蓝天飞行翻译 作者:航空
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 S 824-032 (19) Adjust the torque tube (Ref 27-21-71/501).
 S 414-029 (20) Install the access panels 9516L and 9517L (Ref 12-31-51/201).

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 27-21-71
 ALL  ú ú 02.1 Page 407 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 RUDDER CONTROL TORQUE TUBE - ADJUSTMENT/TEST
____________________________________________
 1.  General_______
 A.  This procedure contains the adjustment and test tasks for the rudder control torque tube.
 TASK 27-21-71-825-001
 2.  Rudder Control Torque Tube Adjustment_____________________________________
 A.  References
 (1)
27-21-24/501, Standby Rudder Actuator

 (2)
27-21-91/501, Rudder Power Control Unit

 B.  
Access

 (1)  
Location Zones
 101/102 Control Cabin (Left/Right)
 706 Vertical Stabilizer
 708 Rudder


 (2)  
Access Panels
 9516L TE Access Panel - Rudder
 9517L TE Access Panel - Rudder


 C.  
Procedure


 S 825-036
 (1)
Adjust the rudder power control unit (Ref 27-21-91/501).

 S 825-037

 (2)
Adjust the standby rudder actuator (Ref 27-21-24/501).


 TASK 27-21-71-725-019
 3.  Rudder Control Torque Tube Test_______________________________
 A.  References
 (1)
12-31-51/201, Fin and Rudder Access Doors and Panels

 (2)
27-21-00/201, Rudder and Rudder Trim Control System

 B.  
Access

 (1)  
Location Zones
 101/102 Control Cabin (Left/Right)
 706 Vertical Stabilizer
 708 Rudder

 

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 27-21-71
 ALL  ú ú 01 Page 501 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
RUDDER

Rudder Travel and Index Plate
Figure 501

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 27-21-71
 ALL  ú ú 01 Page 502 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL 
RUDDER 
TORQUE TUBE ASEE  BSEE ACTUATOR STANDBY RUDDER 
FWD  PIN R-5 RIG  RUDDER POWER CONTROL UNIT  SEE C ROD CONTROL VERNIER 
TORQUE TUBE 
MECHANISM CENTERING FEEL AND 
TORQUE TUBE A 
VERTICAL FIN 
ACTUATOR RUDDER STANDBY 
RUDDER 
INPUT ROD 
STANDBY RUDDER ACTUATOR INPUT CRANK MARKS INDEX B  FWD 
Rudder Aft Control Mechanism Adjustment Figure 502 (Sheet 1) 

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 27-21-71
 ALL  ú ú 01 Page 503 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
STANDBY INPUT ROD  STRUCTURE 
UPPER CRANK 
TORQUE TUBE  CENTER CRANK  CHECKNUT  VERNIER CONTROL ROD 
AFT QUADRANT CONTROL ROD  CLEVIS  CHECKNUT  SLEEVE STRUCTURE 
FWD  LOWER CRANK (BELLCRANK) 
C VERNIER CONTROL ROD CONNECTION 
Rudder Control Torque Tube Figure 502 (Sheet 2) 

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