TM 55-2840-254-23
2-33 INSPECT COMPRESSOR ROTOR BLADES (Continued)
2-33
Inspect airfoil surfaces (129). There shall be
no cracks. There shall be no bends or distor-
tion. There shall be no nicks or dents (130)
deeper than 0.030 inch or longer than 0.350
inch. These nicks and dents (130) must be
separated by 1/2-inch minimum.
FOLLOW-ON MAINTENANCE:
None
END OF TASK
2-311
