TM 1-1520-240-MTF
2-13
EXTERIOR (CONT.)
Top of Fuselage
1-4.
1. No. 2 engine — Check 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 and condition. If
FOD screens are installed, check security
and condition.
O b. EAPS for general condition. Check vortex
tubes for erosion and damage. Check seals
for condition. Check rail and slide
mechanisms.
CAUTION
If engine is to be operated with the engine
transmission fairing removed, be sure barrel
nuts are secured or removed
c. Oil level and cap secured.
d. 712 Check N1 topping stop installed if
required.
e. Tailpipe and diffuser for cracks, hot spots,
and security.
f. Power turbine section — Check upper
portion of engine for condition, security, and
leaks.
