TM 1-1520-240-MTF
2-12
EXTERIOR (CONT.)
Aft Cabin (Cont.)
c. Shock
strut
for
proper
extension,
cleanliness, and static lock unlocked.
d. Power steering actuator, wheel brakes, and
hoses for leakage, chafing, and security.
e. Electrical connections for condition and
security.
f. Landing gear proximity switch — Condition,
linkage adjustment, and security.
5. Hydraulic system test panel — Check all caps
secure.
6. No. 2 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, hinges, 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, harness.
c. Check fuel, oil, hydraulic, electrical, wash kit
and drain lines for connection and leaks.
d. Check engine for chafing lines and condition
and security of components.
