INSTALL EXIT VANE ASSEMBLY - TM-55-2840-254-23-3

INSTALL EXIT VANE ASSEMBLY - TM-55-2840-254-23-3_753

INSTALL EXIT VANE ASSEMBLY - TM-55-2840-254-23-3_755

TM-55-2840-254-23-3 TURBPROP Aircraft Engine Model T74-CP-700 Manual
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TM 55-2840-254-23 4-82 INSTALL EXIT VANE ASSEMBLY (Continued) 4-82 NOTE If necessary, use a soft faced mallet to align bolt holes. 1. Position exit vane assembly (1) in fourth turbine nozzle (2). Align bolt holes (3). GO TO NEXT PAGE 4-505

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