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

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

lNSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_437

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 q. Install new Iockpin (19) into hole in disc slot (4) using tweezers (18) and scribe (20). GO TO NEXT PAGE 2-329

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