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时间:2011-04-10 10:01来源:蓝天飞行翻译 作者:航空
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 preventative to the support pins on the outside diameter of
 the shank, underside of the head and fillet radius.
 5)  Position the flap manually so that the support pins may be
 inserted.
 6)  Install the support pins.
 7)  Safety the pins with washers and nuts and tighten the nuts
 to 1100 - 1300 pound-inches (124 - 147 newton-meters), then
 back-off to the nearest castellation and install the cotter
 pin.

Install the stop fittings (6), on the lower flange of each flap track (Detail B, Fig. 401). 1) Make sure that the shims (14) are the same thickness as was
 written down when the flaps were removed. 2) Apply primer to all bare surfaces on the shims. 3) Install the stop fitting and shims on the flap track. 4) Install the two bolts (12) and washers (13). 5) Tighten the bolts to 160-190 pound-inches (18-21 N-m).
 Install the lockwire.
 6)  Make sure that the clearance between the stop fitting and the track is in the dimension shown on Section A-A, Fig. 401.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (d)  Install the aft roller supports (7) and shims (8) to the flap
 track (Fig. 401, View A-A):
 1) Make sure the shims (8) are the same thickness as was
 written down when the flaps were removed.
 2) Install the aft roller supports (7) and shims (8) with the
 bolts (9), washers (10) and nuts (11).
 (e)  Release the seals on the inboard end of the flap.
 (f)  Attach the flap to the transmission ball screw nuts with the
 ball returns down.
 1) Set each ball screw nut to the dimension that was measured
 when the flap was removed (Detail D, Fig. 401).
 2) Move the flaps to align the gimbal with the ball screw nut.
 NOTE: Do not change the ball screw nut position or you____
 will change the rigging position.
 3) Apply a layer of corrosion preventive compound to the
 bolts (18) and bolt holes.
 4) Install a sufficient number of washers (19) on the bolts.
 NOTE: The bolts must come out of the nuts 0.05 to 0.08____
 inch (0.1 to 0.2 cm) after you install the locknuts
 (15).
 5) At each ball screw nut, install two gimbal caps (17).
 a) Engage the gimbal cap keys in the slots.
 b) Make sure the bushing flange is against the ball screw
 nut.
 6) Install four bolts with the heads down. Attach the bolts
 with locknuts and washers (16).
 a) On the outboard track, tighten the nuts to 120-150
 pound-inches (14-17 N-m).
 b) On the inboard track, tighten the nuts to 200-240
 pound-inches (23-27 N-m).
 (g)  Remove the ball and screw support tool.
 (h)  Remove the load positioner, spreader bar, strongback and
 turnbuckle from the flap.
 (i)  Replace the screws where the clips were attached.
 (j)  Move the carriage and toggles aft.
 1) On each main carriage, remove the bolts (2), washers (4),
 and nuts (5) from the links.
 2) Lower the cam track to the main carriage to permit room for
 the carriage and toggles to go aft.
 3) Move the carriage and toggles aft and engage the toggle
 rollers with the flap track detents.
 4) Assemble the links, bolts and nuts for the forward end of
 the foreflap cam tracks.
 5) Install cotter pins on the nuts.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 03 Page 420 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 414-074
 (6)  
Install the fixed and movable links of the flap track fairing on the aft end of the flap track (AMM 27-51-44/401).

 S 414-039

 (7)  
Install the inboard foreflap (AMM 27-51-02/401).

 S 214-040
 
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本文链接地址:747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 4(73)