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

lNSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_433

lNSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_435

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 o. Reinsert blade (1) rearward partway into disc slot (4). GO TO NEXT PAGE 2-327

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