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时间:2011-04-02 05:43来源:蓝天飞行翻译 作者:航空
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 S 864-017
 (6)  Make sure that system A hydraulic power is not on.
 S 094-018
 (7)  Remove the spoiler ground locks.
 S 864-019
 (8)  Supply the system A hydraulic power (AMM 27-62-00/201).
 S 864-020
 (9)  Move the speed brake lever to the DOWN position to lower the ground spoilers.

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 27-62-12
 ALL  ú ú 03 Page 404 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 224-021
 (10)
 Make sure the clearance between the spoiler panel and the wing structure is 0.40 |0.05 inch.

 S 214-022

 (11)
 Make sure the inboard and outboard seals between the ground spoiler and the wing structure touch tightly.

 S 214-023

 (12)
 Examine the compression of the short vertical bulb seal between the ground spoiler and the top wing surface:

 (a)  
Make sure the seal is compressed 0.15 |0.05 inch.

 (b)  
Make sure the seal is a minimum of 50 percent covered by the ground spoiler.


 S 824-024
 (13)
 Do the ground spoiler adjustment (AMM 27-62-12/501).

 S 724-025

 (14)
 Do the ground spoiler functional test (AMM 27-62-12/501).

 F.
Put the Airplane Back to its Usual Condition


 S 374-026
 (1)  
If it is necessary, apply the nonskid overwing escape route marks (AMM 51-21-97/701).

 (2)  
Remove the system A hydraulic power (AMM 27-62-00/201).

 (3)  
Move the FLT CONTROLS SPOILER A and B switches to the ON position.

 (4)  
Remove the electrical power (AMM 24-22-00/201).


 S 864-027
 S 864-028
 S 864-029
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 27-62-12
 ALL  ú ú 02 Page 405 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 NO. 4 AND 5 GROUND SPOILER - ADJUSTMENT/TEST
____________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There are tasks for the adjustment and the functional test of the No. 4 and 5 ground spoilers.
 TASK 27-62-12-825-001
 2.  No. 4 and 5 Ground Spoiler Adjustment (Fig. 501)_____________________________________
 A.  Consumable Materials
 (1)  
A00247 Sealant BMS 5-95

 (2)  
B00365 Solvent - Methyl-Ethyl-Ketone TT-M-261

 (3)  
C00308 Compound - Corrosion Preventive MIL-C-11796, Class 3

 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.  
Prepare for the Adjustment


 S 865-002
 (1)  
Supply the electrical power (Ref 24-22-00/201).

 S 865-003

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

 S 865-004

 (3)  
Move the speed brake lever to the UP position to lift the spoilers.

 S 865-005

 (4)  
Move the flap control lever to the UP position to fully retract the trailing edge flaps.

 S 865-006

 (5)  
Move the speed brake lever to the DOWN position to lower the spoilers.

 S 865-007

 (6)  
Move the FLT CONTROL SPOILER A and B switches to the OFF position.

 E.  
Adjust the Ground Spoiler


 S 225-008
 (1)
Examine the clearance between the ground spoiler and the flap:

 (a)  
Make sure the clearance is in the tolerance for each actuator shown in Fig. 501.


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