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INSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_445
INSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_447
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
2-35 INSTALL
COMPRESSOR
ROTOR BLADES (Continued)
2-35
h.
Measure tip clearance
of serviceable blade (23)
using thickness gage (13).
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