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时间:2011-04-10 09:50来源:蓝天飞行翻译 作者:航空
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A
747-400
MAINTENANCE MANUAL


HOUSING/BEARING
A-A
INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  PART WORN REPLACE  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  MITTED PER-WEAR DIM.  DIAM CLEAR-ANCE MAX 
MIN  MAX 
LOWER BEARING  ID  1.9373  1.9379  1.941  X 
HOUSING 
1  0.0055 
BEARING  OD  1.9370  1.9375  X 
2  FORK  WTH  0.3194  0.3208  0.3249  0.0060  X 

CONTROL COLUMN  THK  0.3188  0.3193  0.3160  X 
PLATE 

Aileron Control Load Limiter Wear Limits
Figure 601 (Sheet 2)

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 27-11-05
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747-400 MAINTENANCE MANUAL
 AILERON TRIM ACTUATOR AND TRIM AND FEEL MECHANISM - MAINTENANCE PRACTICES
_________________________________________________________________________
 1.  General_______
 A.  There are six tasks in this procedure. These are the tasks:
 (1)  
The removal of the aileron trim system

 (2)  
The installation of the aileron trim system

 (3)  
The removal of the aileron trim and feel mechanism

 (4)  
The installation of the aileron trim and feel mechanism

 (5)  
The test of the aileron trim and feel mechanism

 (6)  
The inspection/check of the aileron trim actuator and the trim and feel mechanism.

 B.  
The aileron trim and feel mechanism gives an alternative feel at the aileron control wheels. It also supplies center and trim of the lateral control system. The mechanism receives its input from the left body control cables. It then supplies an output which operates the central lateral control packages.


 TASK 27-11-06-002-001
 2.  Aileron Trim Actuator Removal_____________________________
 A.  Special Tools and Equipment
 (1)  
G12001-50 Rig Pin Kit

 (2)  
MIT65B04001-41 Control Wheel Straightedge

 (3)  
4MIT65B80307-1 Protractor (Recommended)

 (4)  
F52485-500 Protractor (Optional)

 (5)  
3MIT65B80307-1 Control Wheel Adapter

 B.  
References

 (1)  
06-09-08/201, Wing Access Doors and Panels

 (2)  
24-22-00/201, Manual Control

 (3)  
29-11-00/201, Main Hydraulic Supply System

 (4)  
32-00-30/201, Landing Gear Door Locks

 (5)  
IPC 27-11-06 Fig. 2

 (6)  
SSM 27-11-01

 (7)  
WDM 27-11-11

 C.  
Access

 (1)  
Location Zone
 135 Wing Landing Gear Well, LH
 136 Wing Landing Gear Well, RH

 

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MAINTENANCE MANUAL

SEE A
RIGPIN A/S-2
SEE B
A
Aileron Trim Actuator and Trim and Feel Mechanism Installation
Figure 201 (Sheet 1)

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 27-11-06
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A
747-400
MAINTENANCE MANUAL

31. CABLE AA  ROLLER  FEEL SPRINGS CENTERING AND 
1. AILERON TRIM AND  NUT  1 
 
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