TM 55-1520-240-PM
PHASE NO. _____
Area Name and No.
Aircraft Serial No.
Date
NO. 2 ENGINE AREA #5
Inspect
Phase
No’s
Inspection Requirements
Status
Faults and/or Remarks
Action Taken
Initial
NO. 2 ENGINE AREA #5
ALL/C
5.1 Engine inlet (screen removed) and
bypass panels for cleanliness, broken
or damaged wire mesh and proper
installation. Fiberglass for cracks or
delamination. Fasteners for security
and loose or missing hardware. Lower
screen inspection panel for security at
hinge and latch mechanism. Access 15
ALL/C
5.2 Engine transmission for leaks,
evidence of chafing, cracks, and
security of components and hardware.
Access 14, 15, 73
CAUTION
Do not remove all bolts from
the adapters at the same time
during inspection. Adapters are
balanced assemblies and requires
replacement if all bolts are removed.
"FOD REMINDER"
Check work area for tools and parts after completion of maintenance and inspection.
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