TM 55-2840-254-23
2-35 INSTALL COMPRESSOR ROTOR BLADES (Continued)
2-35
s. Inspect for blade (23) protrusion
from disc.
Protrusion at rear face (28) shall not exceed
0010 inch. Protrusion at forward face (29)
shall not exceed following limits:
(1)
(2)
(3)
INSPECT
Second stage 0.015 inch.
Third stage 0.014 inch.
Fourth through seventh stage 0.018 inch.
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