lNSTALL COMPRESSOR ROTOR BLADES.

INSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_429

lNSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_431

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 lNSTALL COMPRESSOR ROTOR BLADES (Continued) 2-35 i. Measure tip clearance of serviceable blade(1) using thickness gage (13). GO TO NEXT PAGE 2-323

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