(b)
Remove the cables from the quadrant.
(c)
Make sure there is a small tension on the cables to keep them on the pulleys.
S 024-019
(2)
Remove the quadrant:
(a)
Remove the coupling and the crank from the quadrant shaft if it is necessary.
(b)
Remove the bolts, spacer, nuts, and washers to remove the stop fitting.
(c)
Remove the bolts, spacer, washers and nuts to remove the guard.
(d)
Remove the nut and washer that attach the quadrant to the shaft.
(e)
Remove the quadrant.
TASK 27-62-13-404-012
3. Speed Brake Sequence Mechanism Quadrant Installation (Fig. 401)____________________________________________________
A. Special Tools and Equipment
(1)
G12001-50 Rig Pin Kit
B.
Standard Tools and Equipment
(1)
Scale - spring, 0- to 50-pound capacity
C.
Consumable Materials
(1)
C00528 Compound - Corrosion Preventive, MIL-C-16173 Grade 2
D.
References
(1)
27-62-06/401, Speed Brake Sequence Mechanism
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-62-13
ALL ú ú 01 Page 402 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
CABLE SBA
A
STOP FITTING
QUADRANTCOUPLING RIG PIN SB-1
CABLE
SBB
SEE A CRANK
A
TEMPERATURE CABLE RIG LOAD - SPEED BRAKE SYSTEM GUARD
`F (C`) TENSION 2
1 POUNDS (+10/-0) kg (+4.5/-0) A
110 (43) 118 54
90 (32) 109 49
70 (21) 100 45
50 (10) 92 42 QUADRANT
30 (-1) 84 38
10 (-12) 75 34
-10 (-23) 67 30
-30 (-34) 59 27 COUPLING
-40 (-40) 53 24 WASHER
NUT
1 TO MAKE SURE THAT YOU GET THE CORRECT CABLE TENSION, LET THE AMBIENT TEMPERATURE OF THE AIRFRAME STAY CONSTANT |5`F (|3`C) FOR A MINIMUM OF 1 HOUR.
SHAFT
2 THE SYSTEM MUST BE ADJUSTED WHEN THE CABLE LOADS ARE MORE THAN |15 LBS (|7 kg)
BEARING FROM THE TABLE VALUES. HOUSING
CRANK
A-A
Speed Brake Sequence Mechanism Quadrant Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-62-13
ALL ú ú 01 Page 403 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(2)
32-00-30/201, Landing Gear Door Locks
(3)
IPC 27-62-15 Fig. 1
E.
Access
(1)
Location Zone
136 Wing Landing Gear Well, RH
F.
Procedure
S 424-013
(1)
Install the quadrant:
(a)
Apply a thin layer of the corrosion preventive compound on the quadrant shaft splines.
(b)
Put the quadrant in its position.
(c)
Put the quadrant shaft in its position on the quadrant and install the nut and washer.
(d)
Tighten the nut to 400-450 pound-inches (45-56Nm).
(e)
Install the guard with the bolts, washers, spacers and nuts.
(f)
Install the stop fitting with the bolts, washers, spacer and nuts.
S 434-020
(2)
Attach the speed brake cables SBA and SBB to the quadrant:
(a)
Attach the cables to the quadrant with the cotter pins.
(b)
Attach the cables to the turnbuckles.
S 834-014
(3)
Adjust the speed brake cables:
(a)
Put the speed brake lever in the FLIGHT detent.
(b)
Adjust the cables to the tension shown in Fig. 401.
(c) 中國航空網 www.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 7(28)
