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时间:2011-04-01 19:23来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (f)  Make sure the trailing edge of the aftflap is 0.00 to 0.25 inch below the wing chord plane.
 NOTE: If you cannot get this dimension with the 0.23-inch
____ maximum permitted shim thickness, use a 0.23-inch shim. If you made trim corrections with the outboard TE flaps, the dimension can be more than the 0.00 to 0.25 inch limit. Examine the condition of the outboard flap track shim (AMM 27-51-49/401).
1.60
1.40
1.20
TRAILING EDGE MOVEMENT - INCHES


1.00
0.08
0.60
0.40
0.20 0
CHANGE IN SHIM THICKNESS - INCHES
Outboard Trailing Edge Flap Positioning
Figure 501 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 (g)

(h)

(i)

(j)

(k)

(l)


A
737-300/400/500MAINTENANCE MANUAL
Remove the outboard flap rigging beam.
Make sure the trailing edge of the opposite flap aligns in the
 limit of 0.10 inch.
With the aftflap in the retracted position, measure the
 position of the trailing edge of the aftflap and the outboard
 fixed rib.
Make sure the trailing edge of the aftflap is 0.00 to 0.25 inch
 below the outboard fixed rib.

 NOTE: If you cannot get this dimension with the 0.23-inch

____ maximum permitted shim thickness, use a 0.23-inch shim. If you made trim corrections with the outboard TE flaps, the dimension can be more than the 0.00 to 0.25 inch limit. Examine the condition of the outboard flap track shim (AMM 27-51-49/401).
Make sure the trailing edge of the opposite flap aligns in the
 limit of 0.10 inch.
If the trailing edge of the aftflap is not in the limits,
 adjust the thickness of the shims:
 1) Use the chart on Fig. 501 to find the necessary shim

 thickness. 2) The thickness of the shims on the inboard and the outboard carriages must be equal in the limit of 0.12 inch. 3) Remove the access panels from the top surface of the
 midflap. 4) Install a support to hold the flap. 5) Remove the bolts that attach the carriage bearing support
 to the midflap (Fig. 503).
 NOTE: Do not remove more than one carriage bearing at a
____
 time.

 6) Install the correct shims between the carriage bearing
 support and the midflap. 7) Apply a layer of sealant on the shims. 8) Install the bolts that attach the carriage bearing support
 to the midflap.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL


FILL THE CLEARANCE WITH BMS 5-95 SEALANT
Flap Clearance and Misfair Requirements Figure 502
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CARRIAGE


FILLER

Outboard Trailing Edge Flap Leaf Spring Adjustment
Figure 503

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A
737-300/400/500MAINTENANCE MANUAL
 9) Tighten the 1/4 inch nuts to 50-70 pound-inches. 10) Tighten the 5/16 inch nuts to 100-140 pound-inches.
 
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