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INSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_448
INSTALL COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_450
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
m.
Reinsert blade (23) rearward
part way into
disc slot. Use rawhide mallet and installation
tool and rod contained in kit (T31) (24).
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