32-13-09
ALL ú ú 01 Page 201 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 842-036
(3)
Do this task: "The Installation of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).
S 842-044
(4)
Lift the airplane on jacks until the wheels are off the ground (AMM 07-11-01/201).
S 842-006
(5)
Decrease the pressure on the hydraulic system No. 1
(AMM 29-11-00/201).
S 492-007
WARNING: YOU MUST HOLD THE BUNGEE WITH SPRING BEFORE YOU REMOVE THE
_______ PINS. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(6)
Install the bungee restraining tool.
E.
Remove the Jury Strut Spindle (Fig. 201)
S 032-008
(1)
Remove the conduit from the upper jury strut and the support structure.
S 032-009
(2)
Remove the cotter pin and loosen the spindle nut (8).
S 032-010
(3)
Remove the ground lock.
S 032-011
(4)
Remove the spindle bolt (1), the upper conduit bracket (2), the washers, the end caps (4) and the pin (3).
(5)
Pull the jury strut back from the spindle (6).
S 032-045
(6)
Tighten the bungee clamp until you get sufficient clearance to remove the spindle.
S 032-012
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-13-09
ALL ú ú 01 Page 202 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
SEE A
A
A
1. SPINDLE
BOLT
FWD
STRUCTURE
8. SPINDLE CONDUIT
NUT BRACKET
7. SPLINED
WASHER
6. SPINDLE
CONDUIT2.
JURY BRACKET
STRUT
FWD
3. PIN
4. END CAP
(2 LOCATIONS)
5. NUT
A
Body Gear Jury Strut Spindle Installation
Figure 201 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-13-09
ALL ú ú 01 Page 203 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
10. BUSHING/SPINDLE
A-A
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER WEAR MITTED PER-DIM. 3 ANCE MAX CLEAR-DIAM
MIN MAX
9 BUSHING ID 1.8760 1.8770 1.8815 0.0077 X 2
SPINDLE OD 1.8720 1.8740 1.8690 X 1
10 BUSHING ID 2.1260 2.1270 2.1320 0.0080 X 2
SPINDLE OD 2.1220 2.1240 2.1190 X 1
11 SHOULDER/WASHER 5.5100 5.5270 5.5400 0.0700 X 1
BUSHINGS 5.4800 5.5100 5.4600 X 2
PART IS REPAIRABLE. REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION.
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 起落架 LANDING GEAR 3(17)