2-4 COMPRESSOR ROTOR BLADES (FIRST-STAGE) INSPECTION (AVIM) (Continued)
2-4-1 INSPECTION (Cont)
5. Erosion limits for wide chord blades are as follows:
Maximum material loss from leading edge to highest
point of erosion, must not exceed 0.250 inch.
FOLLOW ON MAINTENANCE:
Installation Air Inlet Screen
END OF TASK