Figure 7-15.  Takeoff Weight to Achieve Positive One-Engine-Inoperative Climb at Lift-Off, Flaps UP
Figure 7-17.  Minimum Takeoff Power at 2000 RPM With Ice Vanes Retracted (65 Knots)

TM-1-1510-225-10 Army C-12R Aircraft Army C-12T3 Aircraft Army C-12F3 Aircraft Manual
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