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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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 (6)  
Connect the input rod to the actuator with the bolt, washer and nut.

 S 714-021

 (7)  
Adjust and do a test of the standby rudder actuator
 (Ref 27-21-24/501).


 (8)  
Fill the hydraulic reservoirs if it is necessary (Ref 12-12-00/301).


 S 434-020
 S 614-022
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-24
 ALL  ú ú 01 Page 404 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 STANDBY RUDDER ACTUATOR - ADJUSTMENT/TEST
_________________________________________
 1.  General_______
 A.  This procedure gives you the instructions to adjust and test the standby rudder actuator.
 TASK 27-21-24-825-001
 2.  Standby Rudder Actuator Adjustment__________________________________
 A.  Special Tools and Equipment
 (1) F70207-93 Rig Pin Kit:
 -------------------------------------------------------------------| | | DIAMETER | LENGTH | | | REF NO. | F70207-( )| (INCHES) | (INCHES) | FUNCTION | -------------------------------------------------------------------| R-5 | -11 | 0.309-0.311 | 6.7 -0.25 | RUDDER FEEL AND | | | | | | CENTERING UNIT | -------------------------------------------------------------------
B.  References
 (1)
27-21-00/201, Rudder and Rudder Trim Control System

 (2)
29-15-00/201, Hydraulic Systems A, B, and Standby

 C.  
Access

 (1)  
Location Zones
 706 Vertical Fin
 708 Rudder


 (2)  
Access Panels
 9515L TE Access Panel - Rudder
 9528R Access Door - Rudder
 9529R Access Door - Rudder
 9555R Cover - Rudder Nose
 9556L Cover - Rudder Nose


 D.  
Prepare to Adjust the Standby Rudder Actuator

 (1)
Supply power to the standby hydraulic system (AMM 29-15-00/201).


 S 865-011
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-24
 ALL  ú ú 01 Page 501 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

RUDDER
LOCKNUT
ROD END
A

Standby Rudder Actuator Adjustment
Figure 501

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-24
 ALL  ú ú 01 Page 502 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 875-014
 (2)  
Move the rudder pedals through ten cycles to flush and bleed the standby rudder actuator.

 S 865-012

 (3)
Remove power from the standby hydraulic system (AMM 29-15-00/201).

 S 865-002

 (4)  
Supply the rudder hydraulic power systems A and B
 (Ref 27-21-00/201).


 S 015-003

 (5)  
Open the access panel on the right side of the vertical fin to get access to the standby rudder actuator.

 S 865-004

 (6)  
Set the rudder trim to zero units of trim.

 S 865-005

 (7)  
Shake the rudder pedals to make sure the rudder is in its neutral position.

 S 495-006

 (8)  
Install the rig pin R-5:

 (a)  
Open the access door at the bottom of the vertical fin on the left side.

 (b)  
Put the rig pin R-5 in the output crank of the feel and centering unit.


 NOTE: The rig pin must install easily without movement of the
____
 output crank.

 S 865-008
 WARNING:_______MAKE SURE THE HYDRAULIC POWER IS OFF. IF THE HYDRAULIC POWER IS ON, THE RUDDER CAN MOVE AND CAUSE DAMAGE TO EQUIPMENT AND INJURY TO PERSONS.
 (9)  
 
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