TM 55-2840-254-23
2-33
INSPECT COMPRESSOR ROTOR BLADES (Continued)2-33
k.
Inspect area between 2.375 inches above blade root
(12) and blade tip (4). There shall be no nicks or
dents (17) in edges (7 and 14) deeper than 0.100
inch.
l.
Inspect leading edge of first stage compressor blades
for erosion. Erosion shall be within limits shown.
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Change 6 2-285