TM55-2840-251-23
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
(Task 2-1-5)
END OF TASK
2-25/(2-26 blank)
