S 864-005
 (4)  
Put the flap control lever to the FLAP DOWN position to extend the trailing edge flaps.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 22-11-27
 ALL  ú ú 02 Page 401 ú Mar 12/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 737-300/400/500MAINTENANCE MANUAL 
SPOILER NO.2  SPOILER NO.7  
SEE  A  SEE  A  
MOUNTING  
BRACKET  
BOLT AND  
LOCK NUT  
MOUNTING  
BRACKET  CRANK CLAMP  
BOLT AND  
LOCK NUT  
SEE  B  
SPOILER  CRANK  
ROD LENGTH  
3.54 INCHES  
NOMINAL 
MICRO ADJUSTMENT  
ROD ASSEMBLY  
SENSOR  
CRANK CLAMP  
BOLT AND  
LOCK NUT 
SPOILER NO. 2 SHOWN, SPOILER NO. 7 OPPOSITE  SENSOR CASE  
A  CRANK SLOT  
ZERO INDEX MARK  
CRANK 
B 
Spoiler Position Sensor Installation Figure 401 
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 22-11-27
 ALL  ú ú 01 Page 402 ú Mar 15/97 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 
737-300/400/500MAINTENANCE MANUAL
 S 864-006
 (5)  
Put the speedbrake control lever to the UP position to extend the spoilers.
S 864-007
 (6) 
Remove system A and B hydraulic power (Ref 27-61-00/201).
S 494-008
 (7)  
Install the spoiler ground lock on spoiler actuator No. 2 or 7.
S 864-009
 (8)  
Open the autopilot circuit breakers on the P6 and P18 circuit breaker panels.
 E. Sensor Removal
 S 034-010
 (1)  
Disconnect the electrical connector to the sensor.
S 034-031
 (2)  
Remove the bolt and lock nut from the crank clamp attached to the micro adjustment rod assembly.
S 034-011
 (3)  
Loosen the mounting bracket bolts and lock nuts to remove the mounting bracket attached to the airplane structure.
S 034-028
 (4)  
Remove the crank clamp bolt and lock nut to remove the crank clamp.
S 034-032
 (5)  
Remove the mounting bracket bolt and lock nut attached to the sensor.
 (6)  
Remove the sensor.
 S 034-012
 TASK 22-11-27-424-013
 3.  Spoiler Position Sensor Installation____________________________________
 A. Standard Tools and Equipment
 (1) Flight Spoiler Ground Lock F80017-33 (Preferred) or F80017-23 (Alternate) (Use with Chamfered Flight Spoiler Clevis).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 22-11-27
 ALL  ú ú 02 Page 403 ú Mar 12/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
 B. 
C. 
D. 
A 
737-300/400/500MAINTENANCE MANUAL
 (2)  
Flight Spoiler Ground Lock C27047-16 (Use with Rounded Flight
Spoiler Clevis).References
 (1)  
12-31-01/201, General Zone Diagram
 (2)  
24-22-00/201, Electrical Power Control
 (3) 
27-61-00/201, Spoiler Control SystemAccess
 (1)  
Location Zone 102 Control Cabin 307 Left Wing Spoiler 407 Right Wing Spoiler
Sensor Installation
 S 864-014
 (1)  
Make sure system A and B hydraulic power is removed.
S 494-015
 (2)  
Make sure the spoiler ground lock is installed on spoiler actuator No. 2 or 7.
S 434-033
 (3)  
Put the sensor into the mounting bracket.
S 434-034
 (4)  
Loosely tighten the mounting bracket bolt and lock nut.
S 824-016
 (5)  
Align the zero index mark on the sensor case with the zero index mark on the sensor shaft.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 2(14)