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 2) Make sure the spoilers move to the retracted position.
 3) Make sure the ARMED and the DO NOT ARM lights are off.
 (y) On the antiskid control unit, move the WHEEL SELECT knob to the
 OFF position.
 S 864-017
 (5)  Remove the systems A and B hydraulic power (AMM 27-62-00/201).
 ú
 ú  S 864-011
 ú  (6)  Remove the electrical power (AMM 24-22-00/201).
 S 864-012
 (7)  Remove the DO-NOT-CLOSE tags and close these circuit breakers:
 (a) P6-2 Panel
 1) AUTOSLAT NO. 1 DC
 2) AUTOSLAT NO. 2 DC
 3) AIRPLANES WITH AUTOSLAT COMPUTER;
 AUTOSLAT NO. 1 AC
 AUTOSLAT NO. 2 AC
 S 864-022
 (8)  Do a test of throttle switches S3 and S5:
 (a) If you replaced engine throttle switch S3, do the Landing
 Warning System Test (AMM 31-26-00/501).

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A
737-300/400/500MAINTENANCE MANUAL
 (b)  If you replaced the engine throttle switch S5, do the Thrust Reverser Normal Operation Test (AMM 78-31-00/501).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 NO. 4 AND 5 GROUND SPOILER - REMOVAL/INSTALLATION
_________________________________________________
 1.  General
_______
 A.  There are two tasks in this procedure. There is a task for the removal and a task for the installation of a No. 4 or 5 ground spoiler.
 B.  The graphite/composite ground spoilers and the aluminum/fiberglass ground spoilers are interchangeable.
 TASK 27-62-12-004-001
 2.  No. 4 and 5 Ground Spoiler Removal (Fig. 401)
__________________________________
 A.  Special Tools and Equipment
 (1)  
F80040-2 Spoiler Ground Lock

 B.  
References

 (1)  
AMM 24-22-00/201, Spoiler Position Sensor

 (2)  
AMM 27-62-00/201, Speed Brake Control System

 C.  
Access

 (1)  
Location Zone 309, 409 Wing Trailing Edge Inboard Flap and Spoilers

 D.  
Procedure

 S 864-002
 (1)  
Supply the electrical power (AMM 24-22-00/201).

 S 864-003

 (2)  
Supply the system B hydraulic power (AMM 27-62-00/201).

 S 864-004

 (3)  
Move the flap control lever to the 40-unit position to extend the trailing edge flaps.

 S 864-005

 (4)  
Move the FLT CONTROLS SPOILER A and B switches to the OFF position.

 S 864-006

 (5)  
Remove the system B hydraulic power (Ref 27-62-00/201).

 (6)  
Supply the system A hydraulic power (Ref 27-62-00/201).

 S 864-008

 (7)  
Move the speed brake lever to the UP position to lift the ground spoilers.

 (8)  
Install the spoiler ground locks.

 (9)  
Remove the system A hydraulic power (Ref 27-62-00/201).

 S 864-007
 S 494-009
 S 864-010
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

SEE A
SEE A
OUTER HINGE BOLT (2 LOCATIONS)
GROUND SPOILER
PANEL
PUSHROD BOLT
(2 LOCATIONS)
GROUND SPOILER HINGE FITTING
CENTER HINGE BOLT 
(2 LOCATIONS) 
BONDING JUMPER 
　
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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 飛行操縱 FLIGHT CONTROLS 5(104)