(2)
The installation of the bolt for the walking beam.
(3)
The inspection of the bolt for the walking beam.
B.
The bolt holds the walking beams and the outboard end of the actuator to the support. The support is attached to the airplane structure. The bolt has threads at each end to help the removal and the installation. You must remove the bolt as an assembly with the walking beam support (hanger).
C.
The inspection measures the fit of the bolt.
TASK 32-11-16-002-001
2. Bolt For The Walking Bolt Removal (Fig. 201)
_________________________________
A. References
(1)
AMM 06-09-08/201, Wing Access Doors and Panels
(2)
AMM 09-11-00/201, Towing
(3)
AMM 29-11-00/201, Main Hydraulic Supply System
(4)
AMM 32-00-30/201, Landing Gear Door Locks
(5)
AMM 32-11-15/401, Wing Gear Walking Beam
(6)
AMM 32-11-18/401, Walking Beam Support
(7)
AMM 32-32-01/401, Wing Gear Actuator
(8)
AIPC 32-11-15 Fig. 2
B.
Access
(1)
Location Zone 571 Rear Spar to Landing Gear Support Beam, LH 671 Rear Spar to Landing Gear Support Beam, RH
C.
Prepare for the Removal
S 862-025
WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Install the ground locks in all landing gear (AMM 09-11-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-16
ALL ú ú 01 Page 201 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
SEE A
HANGER BEAM WALKING
NUT
GREASE
FITTING
LUBRICATION INSERT
BOLT
1
4. WIDTH OVER FLANGE
BOLT DIRECTION OPTIONAL
1
747-400 MAINTENANCE MANUAL
WALKING BEAM SUPPORT
A LOCKBOLT
BOLT
A
WALKING BEAM
RETRACT
ACTUATOR FWD
A
ACTUATOR
HEAD WITH
SPHERICAL
3. BEARING/BEARING BOLT 2. BUSHING/BOLT
ANTIROTATION
BOLT
1. BUSHING/BOLT
THIN NYLON
WASHER
THICK NYLON
WASHER
WIDE
NARROW
SPACER THREADED SPACER 5. WIDTHSPACER
SPACER OVER
NUT FLANGE
A-A
Hanger Bolt Installation
Figure 201 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-16
ALL ú ú 01 Page 202 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER DIM. ALLOWED WEAR 5 ANCE MAX CLEAR-DIAM
MIN MAX
1 BUSHING ID 3.000 3.0015 3.0050 0.0080 X
BOLT OD 2.9970 2.9980 2.9935 X 1
2 BUSHING ID 3.0000 3.0015 3.0050 0.0080 X
BOLT OD 2.9970 2.9980 2.9935 X 1
3 BEARING ID 2.9993 3.0000 3.0035 0.0065 X
BOLT OD 2.9970 2.9980 2.9935 X 1
4 2 3.0020 3.0335 3.0440 0.0470 X
3 2.9970 3.0010 *[4] X
5 2 3.0030 3.0175 3.028 0.0310
3 2.9970 3.0010 *[4]
WORN PART IS REPAIRABLE. REFER TO OVERHAUL MANUAL FOR REPAIR INSTRUCTIONS.
DISTANCE FROM BOLT SHOULDER TO SPACER (NUT NOT TIGHTENED TO INSTALLATION LIMITS).
WIDTH OVER FLANGES OF BUSHINGS IN WALKING BEAM AND HANGER (SUPPORT).
1/4 THICKNESS OF EACH INDIVIDUAL BUSHING FLANGE.
中國航空網(wǎng) 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 起落架 LANDING GEAR 2(24)
