27-62-91
 ALL  ú ú 01 Page 404 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 3)  Use the milliohmmeter to make sure the resistance of the bonding jumper connection is less that 0.10 ohms.
 (5)  S 714-015Move the spoiler panel through its full travel. (a) Make sure the spoiler panel moves freely.
 (6)  S 434-016Install the bolt that attaches the rod end for the spoiler actuator to the spoiler: (a) Apply a layer of the BMS 3-24 grease to the bolt. (b) Install the bolt with its head outboard. (c) Install the washers and the nut on the bolt. (d) Tighten the nut to 660-780 pound-inches. (e) Apply the BMS 3-24 grease to the bolt, washer, and nut.
 (7)  S 864-017Make sure the hydraulic power is not on.
 S 094-028

 CAUTION: INSPECT THE LOCK WIRE AND LOCKING KEY OF THE SPOILER ACTUATOR
_______ AFTER REMOVAL OF THE GROUND LOCK TOOL. IF YOU SEE DAMAGE REPLACE THE LOCKING KEY OR LOCK WIRE. FAILURE TO INSPECT THE LOCK WIRE AND LOCKING KEY CAN CAUSE DAMAGE TO THE AIRPLANE.
 (8)
Remove the spoiler ground locks.

 S 984-019

 (9)
Move the spoiler to the down position.

 S 224-020

 (10)
 Make sure the clearance between the spoiler panel and the wing structure is 0.40 |0.05 inch at the aft end of the spoiler panel.

 NOTE: The clearance is specified as the distance between the metal
____ surfaces.
 S 224-021
 (11) Make sure the clearance between the adjacent spoilers is
 0.70 |0.10 inch.
 S 224-022
 (12)
 Make sure the clearance between the seals on the adjacent spoilers is 0.000 to 0.020 inch.

 S 214-023

 (13)
 Make sure the seals between the spoiler and the wing structure touch tightly.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-62-91
 ALL  ú ú 02 Page 405 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 824-024
 (14)
 Do the No. 0, 1, 8 and 9 ground spoiler adjustment (Ref 27-62-91/501).

 S 724-025

 (15)
 Do the test of the No. 0, 1, 8 and 9 ground spoilers (Ref 27-62-91/501).

 S 864-026

 (16)
 Remove the electrical power (Ref 24-22-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-62-91
 ALL  ú ú 02 Page 406 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 NO. 0, 1, 8 AND 9 GROUND SPOILERS - ADJUSTMENT/TEST
___________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is a task for the
 adjustment and a task for the test of the ground spoilers.

 TASK 27-62-91-825-001
 2.  No. 0, 1, 8, and 9 Ground Spoiler Adjustment____________________________________________
 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 307, 407 Wing Trailing Edge Outboard Flap and Spoilers

 D.  
Prepare for the Adjustment of the Ground Spoilers

 S 865-003
 (1)  
Supply the electrical power (Ref 24-22-00/201).

 S 865-004

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

 S 865-005
 WARNING: MAKE SURE THE SPEED BRAKE ARMED LIGHT IS ON WHEN YOU LIFT THE
_______ SPEED BRAKES WITH THE SPEED BRAKE LEVER. THE SPEED BRAKE ACTUATOR CAN AUTOMATICALLY RETRACT THE SPOILERS. THIS CAN CAUSE INJURY TO PERSONS.
 (3)  
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 飛行操縱 FLIGHT CONTROLS 6(5)