(2)
An adjustment of the ball screws at the downstop
(3)
An adjustment of the sequence carriage hook
(4)
An adjustment of the midflap support track
(5)
An adjustment of the ball screws at the upstop
(6)
An adjustment of the midflap droop and symmetry.
(7)
An adjustment of the other clearances
(8)
An adjustment of the aftflaps
B.
If you do the outboard flap adjustment/test procedure after a flap installation, the movable flap track fairing will be installed as part of this procedure. Each flap can be adjusted independently.
C.
The two flap carriages are attached to the midflap with a self-aligning support and a link. Shims at the link control the relation of the midflap and the wing in the vertical direction. This is called the droop. The symmetry is the difference between the left and right outboard midflap droop measurements. The shims you install should be the same thickness as the shims you removed. If the shim thicknesses change, the new flap position will change the trim of the airplane. Therefore, you should write down the shim thickness when you remove a midflap from the airplane. If the shim thickness is not correct, the droop and symmetry will not be correct. This task has steps to measure and adjust the droop and symmetry.
TASK 27-51-04-825-065
2. Adjust The Outboard Flap________________________
A. Special Tools and Equipment
(1)
G27032, Outbd Spoiler Actuator Lock
(2)
MIT65B04008, Flap Manual Drive Tool
B.
Consumable Materials
(1)
A00247, Sealant - Chromate, BMS 5-95, class B
(2)
C00259, Enamel - Primer, Green, BMS 10-11
C.
References
(1)
AMM 06-09-08/201, Dimensions and Areas
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 27-51-31/401, Outboard Flap Track Fairings
(4)
AMM 27-61-00/501, Spoiler Control System
(5)
AMM 29-11-00/201, Main Hydraulic Supply System
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-04
ALL ú ú 01 Page 501 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
D. Access
(1)
Location Zone 567 Outboard Flap Track Fairing, Outboard Flap, LH (Track No. 1) 565 Outboard Flap Track Fairing, Outboard Flap, LH (Track No. 2) 665 Outboard Flap Track Fairing, Outboard Flap, RH (Track No. 7) 667 Outboard Flap Track Fairing, Outboard Flap, RH
(Track No. 8) 581 Rear Spar to Trailing Edge, LH 681 Rear Spar to Trailing Edge, RH
(2)
Access Panel 567BB Outboard Flap Track Fairing, Outbd Flaps 567CB Movable Flap Track Fairing, Outbd Flaps 567DB Movable Flap Track Fairing, Outbd Flaps 567EB Movable Flap Track Fairing, Outbd Flaps 565BB Inboard Flap Track Fairing, Outbd Flaps 565CB Movable Flap Track Fairing, Outbd Flaps 565DB Movable Flap Track Fairing, Outbd Flaps 565EB Movable Flap Track Fairing, Outbd Flaps 665BB Inboard Flap Track Fairing, Outbd Flaps 665CB Movable Flap Track Fairing, Outbd Flaps 665DB Movable Flap Track Fairing, Outbd Flaps 665EB Movable Flap Track Fairing, Outbd Flaps 667BB Outboard Flap Track Fairing, Outbd Flaps 667CB Movable Flap Track Fairing, Outbd Flaps 667DB Movable Flap Track Fairing, Outbd Flaps 667EB Movable Flap Track Fairing, Outbd Flaps
E.
Preconditions
S 865-069
(1)
These conditions are necessary for this task:
(a)
Electrical power is available (AMM 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-04
ALL ú ú 01 Page 502 ú Oct 10/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(b)
The spoilers are serviceable (AMM 27-61-00/501).
(c)
The hydraulic systems are serviceable (AMM 29-11-00/201).
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本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 飛行操縱 FLIGHT CONTROLS 4(103)
