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时间:2011-04-01 19:23来源:蓝天飞行翻译 作者:航空
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____
 (b)  Remove the two gimbal bushings from the sides of the gimbals on the two ballscrews: 1) Remove the three bolts that attach the gimbal bushings from
 the attach fitting. 2) Remove the gimbal bushings and shims from the attach fitting. 3) Write down the number and the location of the shims.
 S 034-011
 (4)  Remove the carriage stop from the lower surface of the flap track (Fig. 401).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 024-035
 CAUTION: MAKE SURE THE CABLES ON THE SLING DO NOT TOUCH THE TRAILING
_______ EDGE OF THE SPOILERS. THE CABLES CAN CAUSE DAMAGE TO THE SPOILERS. DISCONNECT THE SPOILERS AND MOVE THEM FORWARD IF IT IS NECESSARY.
 (5)  Move the flap aft off the flap tracks.
 NOTE: The total weight of the outboard midflap and aftflap is 343
____ pounds. Use the sling to hold the flaps.
 S 034-013
 (6)  
If you will install a different midflap:

 (a)  
Remove the bolts that connect the aftflap pushrods to the aftflap (Fig. 401).

 (b)  
Remove the bolts that connect the fairing support pushrods to the fairing support arms (Fig. 402).

 (c)  
Remove the bolts that connect the fairing support pushrods to the flap carriages.

 (d)  
Remove the carriage bearing support from the midflap: 1) Remove the access panels from the top surface of the midflap to get access to the carriage bearing support. 2) Remove the bolts that attach the carriage bearing support to the midflap. 3) Remove the carriage bearing support and shims from the


 midflap. 4) Measure and make a record of the thickness of the shims.
 TASK 27-51-34-404-014
 3. Outboard Trailing Edge Flap Installation
________________________________________
 A. Special Tools and Equipment
 (1)  
Trailing Edge Flaps Sling Assembly - F80213-78

 (2)  
Flap Drive Screw Support Assembly - F-80057-1

 (3)  
Flight Spoiler Ground Lock set - C27001-24

 B.
Consumable Materials

 (1)  
A00247 Sealant - BMS 5-95 Class B

 (2)  
C00308 Corrosion Preventive Compound - MIL-C-11796

 (3)  
D00014 Grease - MIL-G-21164

 C.
References

 (1)  
AMM 27-51-00/201, Trailing Edge Flap Systems


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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SHIM

Outboard Trailing Edge Flap Positioning
Figure 402

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
GIMBAL BUSHING
BALLSCREW NUT
CLAMP-UP BOLT  DOWNSTOP

Flap Transmission Assembly Adjustment
Figure 403

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  
AMM 27-51-34/601, Outboard Trailing Edge Flap

 (3)  
AMM 27-51-37/401, Outboard Foreflap

 (4)  
AMM 27-51-52/401, Outboard Flap Track Fairings

 D.  
Access

 (1)  
 
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