INSPECT COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2

INSPECT COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_414

INSPECT COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_416

TM-55-2840-254-23-2 Engine Aircraft Gas Turbine Model T63-A-720 P/N6887191 Manual
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TM 55-2840-254-23 2-33 INSPECT COMPRESSOR ROTOR BLADES (Continued) 2-33 b. Inspect leading edge (123). There shall be no cracks. There shall be no bends or distortion. There shall be no nicks or dents (124) deeper than 0.100 inch or longer than 0.300 inch. These nicks and dents (124) must be separated by at least the length of the longest nick or dent. GO TO NEXT PAGE 2-308

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