27-61-07
ALL ú
ú 01 Page 206
ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
B. Access
(1)
Location Zone
135 Wing Landing Gear Wheel Well, LH
136 Wing Landing Gear Wheel Well, RH
C.
Procedure
S 022-011
(1)
Remove the quadrant.
S 222-012
(2)
Examine the splines, bearing, and the bushing on the quadrant for worn areas.
(a)
Remove the parts to be examined.
(b)
Measure the parts.
NOTE: Use a micrometer and/or a vernier caliper.
____
(c)
Compare the dimensions you measured with the permitted dimensions shown in Fig. 201.
(d)
Repair or replace the parts which are out of the tolerance.
(e)
Install the parts.
S 422-013
(3) Install the quadrant.
TASK 27-61-07-402-014
4. Quadrant Installation
_____________________
A. Special Tools and Equipment
(1)
G12001-50 Rig Pin Kit
B.
Standard Tools and Equipment
(1)
Tensiometer - Cable, 0-150 pound range for 1/8-inch cable
C.
References
(1)
27-61-03/201, Spoiler Differential Mechanism
(2)
29-11-00/201, Main Hydraulic Supply System
(3)
32-00-30/201, Landing Gear Door Locks
(4)
IPC 27-61-20, Fig. 1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-61-07
ALL ú ú 01 Page 207 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
D. Access
(1)
Location Zone
135 Wing Landing Gear Wheel Well, LH
136 Wing Landing Gear Wheel Well, RH
E.
Procedure (Fig. 201)
S 422-015
(1)
Install the quadrant.
(a)
Put the quadrant shaft through the bearing in the rig beam.
(b)
Install the spacer, washer and the nut.
(c)
Tighten the nut to a minimum of 250 pound-inches (28.45Nm). Continue to tighten the nut until the cotter pin can be installed.
(d)
Install the cotter pin.
(e)
Attach the cables to the quadrant with the cotter pins.
S 832-016
(2)
Adjust the wing spoiler cables (WS1A and WS1B or WS2A and WS2B) which are controlled by the differential mechanism quadrant which was removed.
(a)
Make sure the trim and feel mechanism is in the center and that the rig pin A/S-2 is installed.
(b)
Install rig pins A/S-14 or A/S-15 and A/S-16 or A/S-17 in the spoiler differential mechanism quadrant.
(c)
Install the rig pins in the spoiler control package quadrants which you removed (Fig. 201). 1) Install rig pins A/S-19 and A/S-22 for the left side
outboard quadrant. 2) Install rig pins A/S-21 and A/S-23 for the left side inboard quadrant. 3) Install rig pin A/S-20 for the right side outboard quadrant. 4) Install rig pin A/S-18 for the right side inboard quadrant.
(d)
With the rig pins installed, tighten the cables at the turnbuckles make sure that the tension is in the limits shown in Fig. 201.
(e)
Make sure you can install the rig pins freely.
(f)
Remove all of the rig pins.
(g)
Install the cable turnbuckle lock clips.
S 412-017
(3)
Do the spoiler differential mechanism installation
(Ref 27-61-03/201).
(4)
Pressurize the hydraulic systems (Ref 29-11-00/201).
S 862-018
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-61-07
ALL ú ú 03 Page 208 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 6(93)
