27-61-51
 ALL  ú ú 02 Page 402 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 C. Procedure
 S 864-002
 (1)  
Supply the electrical power (Ref 24-22-00/201).

 S 864-003

 (2)  
Supply the systems A and B hydraulic power (Ref 27-61-00/201).

 S 864-004

 (3)  
Move the flap control lever to the DOWN position to extend the trailing edge flaps.

 S 864-005

 (4)  
Remove the systems A and B hydraulic power (Ref 27-61-00/201).

 S 864-006

 (5)  
Remove the electrical power (Ref 24-22-00/201).

 S 024-007

 (6)  
Remove the actuator for the flight spoilers:

 (a)  
Remove the bolt, washers and nut to remove the piston rod end from the spoiler panel.

 (b)  
Disconnect the hydraulic lines from the actuator: 1) Put a container below the actuator to catch the hydraulic

 fluid. 2) Disconnect the two hydraulic lines from the actuator. 3) Install the caps on the hydraulic lines.

 (c)  
Remove the four bolts that attach the actuator to the structure.

 (d)  
Remove the actuator from the airplane.

 (e)  
Remove the bolt that attaches the actuator link to the input arm.

 S 034-008
 (7)  
If it is necessary, remove the hydraulic unions from the actuator.

 (a)  
Install the caps in the ports on the actuator.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-61-51
 ALL  ú ú 02 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 27-61-51-404-009
 3.  Flight Spoiler Actuator Installation____________________________________
 A. Special Tools and Equipment
 (1)  
4MIT65B80307-1 Control Surface Protractor

 (2)  
F71292-17 Control Surface Protractor Stand (Optional)

 (3)  
F72790 Aileron Control Wheel Protractor Mount

 (4)  
SE27-0001 Control Wheel Straightedge

 B.
Consumable Materials

 (1)  
A00247 Sealant BMS 5-95

 (2)  
A00249 Sealant BMS 5-26 Type II

 (3)  
B00365 Solvent - Methyl-Ethyl-Ketone TT-M-261

 (4)  
C00308 Compound - Corrosion Preventive MIL-C-11796, Class 3

 (5)  
D00015 Corrosion Preventive Grease BMS 3-24

 (6)  
D00196 Hydraulic Fluid BMS 3-11

 (7)  
D00567 Skydrol Assembly Lube MCS 352

 C.
References

 (1)  
AMM 12-12-00/301, Hydraulic Reservoir

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 27-61-00/201, Spoiler Control System

 (4)  
AMM 27-61-51/601, Flight Spoiler Actuator

 D.
Access

 (1)  
Location Zone 101, 102 Control Cabin 307, 407 Wing Trailing Edge Outboard Flaps and Spoilers

 (2)  
Access Panels
 8208, 8708 Outboard TE Flap Access Panel

 E.
Procedure

 S 224-010
 (1)  
Examine the flight spoiler actuator rod end for worn areas (Ref 27-61-51/601).

 S 434-011

 (2)  
If it is necessary, install the hydraulic unions on the actuator (Fig. 401):

 (a)  
Apply a layer of the hydraulic fluid or the skydrol assembly lube on the O-rings.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-61-51
 ALL  ú ú 01 Page 404 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
　
中國航空網(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 飛行操縱 FLIGHT CONTROLS 5(64)