27-51-25
ALL ú ú 01 Page 401 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 014-003
(2)
Remove the foreflap carriage and toggle (Ref 27-51-24/401).
S 014-004
(3)
Remove the flap transmission and ball screw (Ref 27-51-33/401).
S 494-026
(4)
Attach a load positioner to a hoist above the wing.
S 494-027
(5)
Prepare the sling for the removal of flap track 3 (Fig. 402).
(a)
Move the balance weight to the left side of the sling.
(b)
Attach the load positioner to the left side of the lift lug on the sling.
S 494-028
(6)
Prepare the sling for the removal of flap track 6.
(a)
Move the balance weight to the right side of the sling.
(b)
Attach the load positioner to the right side of the lift lug on the sling.
S 494-029
(7)
Lower the sling to the position to attach the flap track.
S 494-030
(8)
Turn the hand knob at the bottom of the sling to adjust the clamp for the width of the flap track.
S 494-031
(9)
Make sure the distance is 104.6 inches (265.7 cm) between the edge of the clamp and the centerline of the forward hinge of the flap track.
(10)
Turn the hand knob to tighten the clamp on the flap track.
S 864-033
NOTE: Do not use a tool to tighten the hand knob.
____
E. Remove the Inboard Flap Outboard Track
S 034-005
(1)
Remove the support strap:
(a)
Remove the bolts, washers and the nuts.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-25
ALL ú ú 01 Page 402 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
SEE A
SEE B SEE D
FITTING SUPPORT STRAP SUPPORT SEE C
(4 LOCATIONS) BOLT A
BOLT FUSE B TRACK FLAP
B FWD B A TRACK FLAP
A
C
Figure 401 (Sheet 1) Inboard Flap Outboard Track Installation
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-25
ALL ú ú 01 Page 403 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
BEARING WASHER
A AND B IS 0.01 TO 0.09 INCH
THE BUSHING MUST NOT EXTEND ABOVE THE SKIN
MEASURE WITH THE FLAP TRACK FULLY SUPPORTED BY MOUNTING BOLTS. DESIGN LIMITS 0.002 TO
0.045 INCH BETWEEN TRACK AND BEARING WASHER. THE MAXIMUM WEAR IS A 0.060 INCH GAP. MEASURE FROM THE FORWARD SIDE OF THE FLAP TRACK, DUE TO THE TAPERED TOP SURFACE.
Inboard Flap Outboard Track Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-25
ALL ú ú 01 Page 404 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
Inboard Flap Outboard Track Installation
Figure 401 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-25
ALL ú ú 01 Page 405 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
TO HOIST
A
THE BALANCE WEIGHT AND LOAD POSITIONER ARE ON THE RIGHT SIDE FOR THE REMOVAL OF FLAP TRACK 6.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 5(14)