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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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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
M13996
A 737-300/400/500MAINTENANCE MANUAL
 S 026-008
 (2)
Remove the standby rudder actuator (AMM 27-21-24/401).

 S 226-009

 (3)  
Measure the parts of the standby rudder actuator for worn areas.

 S 226-010

 (4)  
Compare the dimensions that you measured with the permitted dimensions shown in Figure 601.

 S 436-011

 (5)
Replace or repair the parts that are not in the tolerance.

 S 426-012

 (6)
Install the standby rudder actuator (AMM 27-21-24/401).


 TASK 27-21-24-216-015
 3. Standby Rudder Actuator Visual Inspection (Fig. 602)
_________________________________________
 A. 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


 B.
Procedure


 S 016-016
 (1)  
Open these access panels to get access to the stanby rudder actuator: 9515L, 9528R, and 9529R.

 (2)  
Do a general visual inspection of the standby rudder actuator.


 S 216-017
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 27-21-24
 ALL  ú ú 01 Page 606 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 416-018
 (3) Close these access panels: 9515L, 9528R, and 9529R.
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 27-21-24
 ALL  ú ú 01 Page 607 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 RUDDER PEDAL ASSEMBLIES - REMOVAL/INSTALLATION
______________________________________________
 TASK 27-21-31-004-003
 1.  Remove the Rudder Pedal Assembly________________________________
 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
 B. Standard Tools and Equipment
 (1)  
Ruler - 2 feet long, graduated hundredths of an inch, Commercialy Available

 C.
Consumable Materials

 (1)
C00528 Compound - Corrosion Preventive, MIL-C-11796, Class 3

 D.
References

 (1)  
27-21-00/201, Rudder and Rudder Trim Control Systems

 E.
Access

 (1)  
Location Zones
 101/102 Control Cabin
 202 Lower Nose Compartment
 203 Nose Wheel Well


 F.
Prepare for Removal


 S 014-007
 (1)  
Open the forward access door (1103) to get access to the nose compartment.

 (2)
Remove the forward access panels from the nose wheel well.


 S 014-008
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 27-21-31
 ALL  ú ú 01 Page 401 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500MAINTENANCE MANUAL
 G. Remove the Rudder Pedal Assembly
 S 484-012
 (1)  
 
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