S 824-013
(4)
Align the splines of the camshaft arm (13) and the camshaft (12) and start the camshaft arm on the splines.
(5)
Move the sleeve (14) above the camshaft (10).
S 824-015
(6)
Align the splines of the cam (15) and the camshaft (10) and start the cam on the splines.
S 424-014
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-34-21
ALL ú ú 01 Page 403 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 434-016
(7) Install the spacer (16) on the camshaft (10).
S 424-017
(8) Install the camshaft forward bearing (17) in the structure.
S 424-018
(9) Insert the camshaft (10) through the forward bearing (17) and
install shim (18A).
(a) Make sure all parts are tightly stack-up.
(b) Keep a gap between the end of the bearing (17) and shim (18A)
to 0.005 - 0.015 inches (See Figure 401, view A-A) before you
install washer (18).
NOTE:____ Use micrometer to measure the gap.
(c) Install the washer (18) and the nut (19).
S 434-019
(10) Install the spacer (2) in the quadrant assembly (4).
NOTE: When you install the spacer (2), temporarily put in a 3/8
____ inch diameter rod (approximately 3-1/4 inches long) through the quadrant assembly to keep the spacer aligned.
S 424-029
(11)
Put the quadrant assembly (4) in the quadrant support (1).
(a)
Push the temporary rod you installed on step (10) and put the bolt (3) through the quadrant support and the quadrant assembly.
S 434-020
(12)
Install the washer (8) and the nut (9) on the bolt (3).
S 434-021
(13)
Install the cable MLGEA on the quadrant assembly (4).
S 424-022
(14)
Connect the uplock release rod (6) to the quadrant assembly (4)
S 424-023
(15)
Connect the uplock release rod (6) to the camshaft arm (13).
NOTE: Do not tighten nut until you do the adjustment on the
____ manual extension system.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-34-21
ALL ú ú 02 Page 404 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 434-024
(16)
Connect the return spring (5) to the quadrant assembly (4).
S 434-025
(17)
Connect the cable MLGEA at approximately body station 420.
S 824-026
(18)
Adjust the manual extension system (Ref 32-34-00/501).
S 714-027
(19)
Do a test on the manual extension system (Ref 32-34-00/501).
S 414-028
(20)
Install the ceiling panels of the cargo compartment.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-34-21
ALL ú ú 01 Page 405 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
MAIN LANDING GEAR MANUAL EXTENSION SYSTEM CABLES - REMOVAL/INSTALLATION
_______________________________________________________________________
1. General
_______
A. This procedure contains two tasks:
(1)
The removal of the cables of the manual extension system from the left or the right main landing gear.
(2)
The installation of the cables of the manual extension system of the main landing gear.
TASK 32-34-31-004-001
2. Main Landing Gear Manual Extension Systems Cables Removal (Fig. 401)
_________________________________________________________
A. Procedure to Remove the Cables of the Manual Extension System
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 2(137)
