Main Gear Shock Strut Doors 535
32-13-0Page 2 Figure 1 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Jun 20/86
MAIN GEAR SHOCK STRUT DOORS - REMOVAL/INSTALLATION
1. General
A. The shock strut doors consist of a center door and an inner door joined by hinges.
B. The shock strut doors may be removed and installed as an assembly or the inner door may be removed and installed separately. To remove the center door it is necessary to remove the inner door as well.
2. Equipment and Materials
A. Ground Lock Assemblies (Ref 32-00-01)
B. Hydraulic test bench capable of delivering 20 gpm at 3000 psi
C. Grease - BMS 3-24
D. Paint - BMS 10-60, Type 1, BAC701, Color: Black
3. Shock Strut Door Assembly - Removal/Installation
A. Remove Shock Strut Door Assembly
(1)
Check that ground lock assemblies (Ref 32-00-01) are installed in all gear.
(2)
Disconnect inner door control rod assembly (7, Fig. 401) by removing attachment bolts.
(3)
Disconnect upper (3) and lower (5) drag strut door supports by removing attachment bolts.
(4)
Support strut door assembly and remove mounting screws from upper (10) and lower (8) shock strut door supports. Note position and number of shims.
(5)
Remove door assembly from airplane.
B. Install Shock Strut Door Assembly
(1)
Position door in place on landing gear strut (Fig. 401).
(2)
Install shims and mounting screws in upper (10) and lower (8) shock strut door supports.
(3)
Connect upper (3) and lower (5) drag strut door supports.
(4)
Disconnect outboard wing door control rod.
(5)
Jack airplane until all tires are clear of ground (Ref Chapter 7, Jacking Airplane).
(6)
Check that electrical power is available.
515
Oct 20/92 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 32-13-11 Page 401
Main Gear Shock Strut Door Installation 507
32-13-11 Page 402 Figure 401 (Sheet 1) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Jun 20/85
500 Main Gear Shock Door Installation Oct 20/92 Figure 401 (Sheet 2A) 32-13-11 Page 402A/402B BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
500 Main Gear Shock Strut Door Installation
Feb 15/68 Figure 401 (Sheet 2) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 32-13-11 Page 403
(7)
Connect external hydraulic test bench. Do not pressurize hydraulic system A.
(8)
Remove ground lock assemblies (Ref 32-00-01) on landing gear being repaired.
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