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

INSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_449

INSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_451

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 n. Install new spring (26) into hole in disc slot using tweezers (18). GO TO NEXT PAGE 2 - 3 4

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