(a)  
Move the speed brake control lever to the UP position to lift the spoiler.

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

 (c)  
With the flaps retracted, make sure the two bulb seals on the fixed upper panel are compressed 0.15 |0.05 inch by the foreflap.

 (d)  
Measure the position of the wing bulb seal in relation to the top surface of the wing.

 (e)  
Make sure the forward bulb seal aligns with the top surface of the wing bulb seal.

 (f)  
Adjust the forward bulb seal if it does not align:
 1) Loosen the bolts that attach the seal.
 2) Move the seal to the correct position.
 3) Tighten the bolts that attach the seal.

 S 225-011
 (4)  
Examine the position of the aft bulb seal if it is installed:

 (a)  
Supply the systems A and B hydraulic power (Ref 27-62-00/201).

 (b)  
Move the flap control lever to the 1-unit position to extend the flaps.

 (c)  
Move the speed brake lever to the DOWN position to lower the spoilers.

 (d)  
Make sure a minimum of 80 percent of the length of the aft bulb seal touches the foreflap.

 (e)  
Make sure the maximum clearance between the aft bulb seal and the foreflap is 0.02 inch.

 (f)  
Install shims if it is necessary to adjust the aft bulb seal.

 (5)  
Do the No. 4 and 5 ground spoilers functional test.

 (6)  
Move the flap control lever to the UP position to retract the flaps.

 S 725-012
 S 865-013
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-62-12
 ALL  ú ú 02 Page 504 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-014
 (7)
Remove the systems A and B hydraulic power (Ref 27-62-00/201).

 S 865-015

 (8)  
Move the FLT CONTROL SPOILER A and B switches to the ON position.

 S 865-016

 (9)  
Remove the electrical power (Ref 24-22-00/201).

 TASK 27-62-12-725-017
 3.  No. 4 and 5 Ground Spoiler Functional Test__________________________________________
 A. Special Tools and Equipment
 (1)  
F52485-500 Control Surface Protractor

 (2)  
F71292-17 Control Surface Protractor Stand Assembly

 B.
References

 (1)  
24-22-00/201, Manual Control

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

 C.
Access

 (1)  
Location Zone 101, 102 Control Cabin 309, 409 Wing Trailing Edge Inboard Flap and Spoilers

 D.
Procedure

 S 865-018
 (1)  
Supply the electrical power (Ref 24-22-00/201).

 S 865-019

 (2)
Supply the systems A and B hydraulic power (Ref 27-62-00/201).

 S 485-020

 (3)  
Install the protractor stand and the control surface protractor on the spoilers.

 NOTE: You can use a hand held protractor on the spoiler.
____
 S 825-022
 (4)  
Set the protractor to zero.

 S 865-023

 (5)  
Move the flap control lever to the UP position to fully retract the trailing edge flaps.

 S 865-024

 (6)  
Move the speed brake lever to the DOWN position to lower the spoilers.

 (7)  
Make sure the ground spoilers are fully retracted.

 S 725-025
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-62-12
 ALL  ú ú 02 Page 505 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 865-026
 (8)  
Move the speed brake lever to the UP position to lift the spoilers.

 S 725-027

 (9)
Make sure the No. 4 and 5 ground spoilers are up 60 |2 degrees.

 S 725-028

 (10)
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護(hù)手冊 飛行操縱 FLIGHT CONTROLS 5(108)