TM 1-1520-240-MTF
2-26
EXTERIOR (CONT.)
Left Cabin (Cont.)
18. Left aft landing gear — Check as follows:
a. Left aft Landing gear support structure —
Check for cracks or distortion.
b. Tires — Check for inflation and condition.
c. Static ground wire — Check wire secure and
contacting the ground.
d. Shock strut — Check proper extension,
cleanliness, and static lock unlocked.
e. Electrical connections — Check condition
and security.
f. Landing gear proximity switch — Check
condition, linkage adjustment, and security.
19. No. 1 engine — Check lower side as follows:
NOTE
If TEAC/PAC is to be performed, all preflight
inspection requirements/checks required prior to
TEAC/PAC must be accomplished. In this case,
EAPS must be moved forward of the engine to
gain access for inspection. If TEAC/PAC is not
required, EAPS will remain locked into position in
front of the engine.
a. Inlet for foreign objects, hinge, latch
secured, and condition.
O b. EAPS for general condition. Check vortex
tubes for erosion and damage. Check seals
for condition. Check rail and slide
mechanisms. Inspect blower fan blades for
damage and erosion. Check condition of
electrical connectors, and harness.
