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

REMOVE COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_363

REMOVE COMPRESSOR ROTOR BLADES - TM-55-2840-254-23-2_365

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 2-31 REMOVE COMPRESSOR ROTOR BLADES (Continued) 2-31 d. Position drift assembly (T19) (7) at rear of blade (l). In following step, be sure that blade root is aligned with slot. Failure to comply will cause damage to No. 1 bearing housing. e. Tap blade (1) firmly forward into slot (3). Use ballpeen hammer. GO TO NEXT PAGE 2-258

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