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时间:2011-04-10 09:54来源:蓝天飞行翻译 作者:航空
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A
747-400 MAINTENANCE MANUAL
 AILERON FORCE LIMITER - REMOVAL/INSTALLATION
____________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of the aileron force limiter. The procedure has these parts:
 (1)
The removal of the aileron force limiter

 (2)
The installation of the aileron force limiter

 (3)
The adjustment of the aileron trim system.


 TASK 27-11-26-004-001
 2.  Aileron Force Limiter Removal_____________________________
 A.  Special Tools and Equipment
 (1)
G12001-50 Rig Pin Kit

 (2)
MIT65B04001-41 Control Wheel Straightedge

 (3)
4MIT65B80307-1 Protractor (Preferred)

 (4)
F52485-500 Protractor (Optional)

 (5)
3MIT65B80307-1 Control Wheel Adapter

 B.  
References

 (1)
24-22-00/201, Manual Control

 (2)
29-11-00/201, Main Hydraulic Supply System

 (3)
32-00-30/201, Landing Gear Door Locks

 (4)
IPC 27-11-08, Fig. 1

 (5)
IPC 27-11-10, Fig. 1

 (6)
IPC 27-11-55, Fig. 1

 C.  
Access

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


 D.  
Prepare for Removal

 (1)
Make sure the ground locks on the landing gear are installed.


 S 494-002
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 27-11-26
 ALL  ú ú 03 Page 401 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

RIG INBOARDPIN A/S-8
AILERON QUADRANT
AILERON WING CABLE PULLEY AND BRACKET (WHEEL WELL) SEE ARIG PIN A/S-2
LEFT WHEEL WELL RIGHT CLCP (RIGHT AUTOPILOT) 1
RIGGING BEAM
LEFT CLCP (LEFT AUTOPILOT) 2
RIGHT WHEEL WELL RIGGING BEAM
RIG PIN A/S-7
13. CABLE AB
LEFT AILERON
PROGRAMMER

RIGHT AILERON
RIG
SEE B PROGRAMMER
PIN A/S-6
12. TURNBUCKLE
A
14. CLCP CONTROL ROD
1. FORCE LIMITER ROD
11. CABLE AA
2.
 BOLT

3.
 COLLAR


10. QUADRANT
SEE C
9. INPUT 4. INSTALLATION SEE D
CRANK SUPPORT ROD
5.
 BOLT

6.
 WASHER

7.
 NUT

8.
 BUSHING


1
INSTALLED IN THE LEFT WHEEL WELL
2
INSTALLED IN THE RIGHT WHEEL WELL
B
Aileron Force Limiter Installation Figure 401 (Sheet 1)
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 27-11-26
 ALL  ú ú 01 Page 402 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


24.
 BOLT

25.
 WASHER  23. FORCE


21. ROD END

MAXIMUM DIMENSIONS
FORCE LIMITER ROD
VERNIER ADJUSTMENT

 

19.
 MOUNTING BOLT

20.
 WASHER (2 LOCATIONS)

 

Aileron Force Limiter Installation
Figure 401 (Sheet 2)

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 27-11-26
 ALL  ú ú 01 Page 403 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

TABLE 1 
(`F) TEMPERATURE 1  TENSION IN POUNDS CABLE RIGGING ADJUSTMENT LOADS 4 
BODY/WING CABLE 2  CONTROL WHEEL BUS CABLE 3
5  6 
110 (43`C)  123  153  93 
90 (32`C)  114  141  84 
80 (27`C)  110  135  80 
70 (21`C)  105  130  75 
 
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