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时间:2011-04-02 16:42来源:蓝天飞行翻译 作者:航空
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 (9)  S 034-021Loosen the two sensor clamp screws.
 S 824-022

 (10) Hold the cable drum and turn the sensor until the mark on the shaft aligns with the mark on the sensor.
 NOTE: No special position of the aligned marks is necessary.
____
 S 434-023
 (11)
 Tighten the clamp screws to 30-35 pound-inches.

 S 434-024

 (12)
 Install the electrical connector on the sensor.

 S 094-025

 (13)
 Remove the rigging pins.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú

 31-24-32
 ú ú 09 Page 403 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 864-026
 (14) Close these circuit breakers:
 (a)  
P6 Panel
 1) FLIGHT CONTROL circuit breakers


 (b)  
P18 Panel
 1) FLIGHT RECORDER AC
 2) FLIGHT RECORDER DC
 3) FLIGHT RECORDER POSITION SENSORS

 

 S 704-027
 (15) Do this task:  Control Wheel Position Sensor - Adjustment/Test (AMM 31-24-32/501).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú

 31-24-32
 ú ú 11 Page 404 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
SENSOR SEE B 
ELECTRICAL CONNECTOR SENSOR  RIGHT ANGLE BRACKET ATTACH BOLT (3 LOCATIONS)  FWD  INBD 
SENSOR CLAMP SCREW (2 LOCATIONS)  CABLE A  A 
RADIUS FILLER 
2.09 |0.02 INCHES 
SENSOR SUPPORT BRACKET BOLT (4 LOCATIONS)  PULLEY  CABLE B 
INBD  SHIM 
FWD  SPRING  PULLEY DRUM 
B  CABLE C  AILERON CONTROL WHEEL DRUM SHAFT 
Figure 401 (Sheet 1) Control Wheel Position Sensor Installation 

F00615
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT SERVICE LETTER ú

 31-24-32
 737-SL-27-089-A  ú ú 09 Page 405 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE C
SENSOR SEE D 
ELECTRICAL CONNECTOR SENSOR  RIGHT ANGLE BRACKET ATTACH BOLT (3 LOCATIONS)  FWD  INBD 
SENSOR CLAMP SCREW (2 LOCATIONS)  CABLE A  C 
RADIUS FILLER 
2.03 |0.02 INCHES 
SENSOR SUPPORT BRACKET BOLT (4 LOCATIONS)  PULLEY  CABLE B 
INBD  SHIM 
FWD  SPRING  PULLEY DRUM 
D  CABLE C  AILERON CONTROL WHEEL DRUM SHAFT 
Control Wheel Position Sensor Installation Figure 401 (Sheet 2) 

F00689
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SERVICE LETTER ú

 31-24-32
 737-SL-27-089-A  ú ú 10 Page 406 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CABLE  DRAWING  NO.  LENGTH  FITTINGS 
REF  NUMBER  REQ  (INCHES)  CABLE SIZE  1  2 
A  69-40951-41  1  4.80 3/64 7 X 7  RA2487-047  RA2487-047 AND
 69-40947-1 
B  69-40951-43  1  5.32  3/64 7 X 7  RA2487-047  RA2487-047 AND
 69-40947-1 
C  69-40951-45  1 11.99  3/64 7 X 7  RA2487-047  RA2487-047 

MATERIAL - CABLE  STAINLESS STEEL CABLE, AIRCRAFT QUALITY, HACKENSACK CABLE CORP., HACKENSACK, NJ, OR EQUIV
TERMINALS AMERICAN CHAIN AND CABLE CO., BRIDGEPORT, CT


 
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