(2)
Insert attachment bolt with head end aft. Add washer and nut.
(3)
Tighten nut to driving torque plus 400 pound-inches lube torque.
N. Position shock strut inner door and connect control rod assembly.
O. Install bracket clamp for electrical harness onto lower drag strut.
P. Install hydraulic line support on lower drag strut.
Q. Lower airplane and remove jacks (Ref Chap. 7, Airplane Jacking).
Sep 01/02 32-11-42 Page 401 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
Main Gear T-Bolt Installation 500
32-11-42Page 402 Figure 401 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. May 20/82
MAIN GEAR TORSION LINKS - REMOVAL/INSTALLATION
1. General
A. The main gear torsion links are removed after damage, or when bushings are worn beyond service limits. Removal of upper torsion link also disconnects bottom end of lower drag strut. On the right gear, the upper torsion link is connected to a spoiler lockout mechanism. The main tires should be removed and the shock strut partially extended to provide clearance for the upper torsion link pin when replacing the upper torsion link. The main gear brakes also should be removed to provide clearance for the lower torsion link pin when replacing the lower torsion link.
2. Equipment and Materials
A. Ground Lock Assemblies - (Ref 32-00-01)
B. Grease - MIL-G-21164 or MIL-G-23827 optional to BMS 3-33
3. Remove Main Gear Torsion Links
A. Check that all ground lock assemblies are installed (Ref 32-00-01).
B. If replacing upper torsion link, remove main gear wheels (Ref 32-45-11 R/I) and partially extend shock strut by raising airplane (Ref Chapter 7, Jacking Airplane).
C. If replacing lower torsion link or upper and lower torsion links, remove main gear wheels (Ref 32-45-11 R/I) and main gear brakes (Ref 32-41-41 R/I).
D. Remove pins connecting hydraulic line support brackets (24, Fig. 401) to lower torsion link.
E. Disconnect hydraulic line guides (16) from main gear damper (17). Secure lines clear of torsion links.
F. Disconnect link (21) connecting electrical harness to lower torsion link (23). Observe
spacer (19) and bushing (20).
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