TM 1-1520-238-23
2-282
Change 3
2.81.
MAIN LANDING GEAR CROSS TUBE REMOVAL/INSTALLATION – continued
b. Remove tube (2) from fuselage (3).
2.81.4. Cleaning
a. Clean removed and attaching parts and sur-
faces (para 1.47).
2.81.5. Inspection
a. Check mounting points and bearings for
cracks and wear.
(1) Repairable limits after clean up are no greater
than 0.75 INCH diameter and no greater than
0.215 INCH deep.
b. Check cross tube for corrosion (para 1.49).
2.81.6. Installation
a. Install tube (2) in fuselage (3).
b. Install two spacers (1) on tube (2).
c. Inspect (QA).
d. Install main landing gear trailing arm assem-
bly (para 3.16).
e. Install main landing gear shock struts (para
3.18).
f. Remove tripod jacks (para 1.66).
END OF TASK
2
M04-2679-3
3
2
M04-2679-4
1
3
