TM55-2840-251-23
Section IV COMPRESSOR ROTOR BLADES
2-4 COMPRESSOR ROTOR BLADES (FIRST-STAGE) INSPECTION (AVIM)
This task covers:
Inspection (2-4-1)
INITIAL SETUP
Applicable Configurations:
All
Tools:
Aircraft Inspector's Tool Kit
NSN 5180-00-323-5114
Materials:
None
Personnel Required:
66G Aircraft Inspector
Equipment Condition:
Air Inlet Screen Removed
(Task 2-1-1)
2-4-1 INSPECTION
1. The maximum acceptable damage and erosion limits,
without
repair,
are
detailed
in
the
following
subparagraphs. If damage or erosion exceeds acceptable
limits, complete engine must be returned to Depot
Maintenance.
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