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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.  Special Tools and Equipment
 (1)  
G12001-50 Rig Pin Kit

 (2)  
MIT65B04001-41 Control Wheel Straightedge

 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 27-11-04 Fig. 1

 (5)  
SSM 27-11-01

 (6)  
WDM 27-11-11

 C.  
Access

 (1)  
Location Zone
 221 Control Cabin Floor, LH
 222 Control Cabin Floor, RH


 (2)  
Access Panel 211 Passenger Cabin, LH (Second and third center ceiling panels from the forward end)


 212  Passenger Cabin, RH (Second and third center ceiling panels from the forward end)
 D.  Prepare for Removal
 S 494-001
 (1) Make sure the ground locks are installed on the landing gear.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-04
 ALL  ú ú 01 Page 401 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

SEE A
AILERON 
CONTROL 
DRUM 
CABLE AB 
SEE  B 
AILERON CONTROL 
LOAD LIMITER 
TURNBUCKLE 
CABLE AA  CABLE ACBA 
POSITION 
NEGATOR TRANSMITTER  CABLE ACBB 
SPRING 
CABLE AA 
FWD 
CABLE 
AB 

RIG PIN A/S-1 

Aileron Control Drum Installation
Figure 401 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-04
 ALL  ú ú 01 Page 402 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

CABLE AB
CABLE AA
POSITION TRANSMITTER NEGATOR SPRING
LOWER BEAM BOLT (6 LOCATIONS) LOWER BEAM
B
CAPTAIN'S 
CONTROL 
COLUMN 
UPPER BEAM 
CABLE ACBA 
CABLE ACBB 
DRUM ATTACH 
BOLT (4 LOCATIONS 
LOWER, 4 LOCATIONS 
HIGHER)

Aileron Control Drum Installation
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-04
 ALL  ú ú 01 Page 403 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

1
TABLE 1
CABLE RIGGING ADJUSTMENT LOADS TENSION IN POUNDS 2
4
TEMPERATURE (`F)
BODY/WING
2
CABLE
1
5
123
110 (43`C)
114
90 (32`C)
110
80 (27`C)
105
70 (21`C)
101
60 (16`C)
97
50 (10`C)
93
40 (4`C)
89
30 (-1`C)
80
10 (-12`C)
72
-10 (-23`C)
64
-30 (-34`C)
58
-40 (-40`C)
6
153 141 135 130 125 120 115 110 99 89 79 71
AILERON TRIM AND FEEL MECHANISM RIG PIN A/S-2
CABLE AA
CABLE AB
SEE A TO GET THE CORRECT CABLE TENSION, MAKE SURE THE AIRFRAME TEMPERATURE IS STABLE (USE A TOLERANCE OF |5`F) FOR A MINIMUM OF 1 HOUR.
CONTROL WHEEL 
BUS CABLE 
3  3 
93 
84  4 
80 
75 
71  5 
67  6 
63 
59 
50 
42 
34 
28 

THE SYSTEM MUST BE ADJUSTED WHEN THE CABLE LOADS ARE MORE THAN |15 LBS FROM THE TABLE VALUES. WHEN RIGGING THE SYSTEM, CABLE LOADS SHOULD BE |5 LBS FROM THE TABLE VALUES.
THE SYSTEM MUST BE ADJUSTED WHEN THE CABLE LOADS ARE MORE THAN |20 LBS FROM THE TABLE VALUES. WHEN RIGGING THE SYSTEM, CABLE LOADS SHOULD BE |15 LBS FROM THE TABLE VALUES.
 
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