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时间:2011-04-01 19:15来源:蓝天飞行翻译 作者:航空
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CAPTAIN'S FIRST OFFICER'S CONTROL WHEEL CONTROL WHEEL
CONTROL WHEEL DRUM
CABLE ABSB
CABLE ABSA

Aileron System Rig Pin Locations
Figure 501 (Sheet 1)

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 ALL  ú ú 01 Page 502 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TABLE I
1 TEMPERATURE `F  CABLE TENSION (POUNDS) 
2 CABLES AA AND AB 3  CABLES ABSA AND ABSB 2 3  CABLES ACBA AND ACBB 4 5 
110 90 70 50 30 +10 -10 -30 -40  133 124 115 107 99 90 82 74 68  202 184 165 148 131 113 96 77 66  93 84 75 70 61 53 49 46 44 

 

TO GET THE CORRECT CABLE TENSION, PERMIT A MINIMUM OF ONE HOUR AT A CONSTANT AMBIENT TEMPERATURE OF |5`F FOR THE AIRFRAME TEMPERATURE TO BECOME STABLE.
THE CABLE LOADS MUST NOT BE MORE THAN +10/-0 POUNDS OF THE NOTED TABLE I VALUES WHEN YOU ADJUST THE SYSTEM.
FOR THE NECESSARY REGULAR CHECKS WITHOUT THE SYSTEM DISCREPANCY REPORTS, THE CABLE TENSIONS CAN CHANGE +15/-30 POUNDS FROM THE TABLE I VALUES. FOR CABLE TENSION CHECKS THAT ARE THE RESULT OF THE SYSTEM DISCREPANCY REPORTS, THE TENSIONS CAN CHANGE |15 POUNDS FROM THE TABLE I VALUES. WHEN YOU ADJUST THE CABLES, TABLE I VALUES MUST BE MET WITH

.
THE CABLE LOADS MUST NOT BE MORE THAN |15 POUNDS OF THE TABLE I VALUES WHEN YOU ADJUST THE SYSTEM.
FOR THE NECESSARY REGULAR CHECKS WITHOUT THE SYSTEM DISCREPANCY REPORTS, THE CABLE TENSIONS CAN CHANGE +15/-30 POUNDS FROM THE TABLE I VALUES. FOR CABLE TENSION CHECKS THAT ARE THE RESULT OF THE SYSTEM DISCREPANCY REPORTS, THE TENSIONS CAN CHANGE |15 POUNDS FROM THE TABLE I VALUES. WHEN YOU ADJUST THE CABLES, TABLE I VALUES MUST BE MET WITH

Aileron System Rigging Pin Locations
Figure 501 (Sheet 2)

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 ú  01  Page 503
 ú  Jul 15/91 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

QUADRANT CONTROL AILERON  DECK PRESSURE  AILERON POWER CONTROL UNITS 
CABLE AB  CABLE ABSA 
CABLE AA  CABLE ABSB  CARTRIDGE SPRING AILERON 
CABLE ABSB SHAFT QUADRANT CONTROL  DRUMS BUS AILERON 
ACTUATOR TRIM AILERON  ROD INPUT  CABLE ABSA 
(2 LOCATIONS) CENTERING SPRING  TRIM MECHANISM 
SEE  A 
ACTUATOR TRIM AILERON 
ARM ROLLER ARM ACTUATOR 
POINT ATTACH ACTUATOR  (2 LOCATIONS) SPRING CENTERING TRIM ROLLER 

SUPPORT
AILERON CONTROL

CAMQUADRANT SHAFT
A
Aileron Control System Component Location Figure 502
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 ALL  ú ú 01 Page 504 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AILERON CONTROL CONTROL COLUMN
FIRST OFFICERS BUS DRUM
CAPTAINS AILERON CONTROL WHEEL
SEE A
CABLE ACBA  CABLE AB 
CAPTAINS CONTROL COLUMN  TURNBUCKLE 
CABLE SHIELDS 
SEE  B 
TURNBUCKLE  LOST MOTION DEVICE  AILERON CONTROL DRUM CABLE AA 
CABLE ACBB AILERON CONTROL BUS DRUM  FWD 
CABLE AB 
AILERON CONTROL DRUM 
CABLE AA 

Aileron Control Wheel Adjustment
Figure 503 (Sheet 1)

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 ALL  ú ú 01 Page 505 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

STRAIGHT EDGE
 
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