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Figure 7-15. Takeoff Gross Weight Limit Flaps 40% (To Achieve 100 FPM One Engine Inoperative Rate-of-Climb At Liftoff)
Figure 7-17. Minimum Take-Off Power at 2000 RPM (Ice Vanes Extended), (65 Knots)
TM-1-1510-218-10 Army C12C Aircraft Army C12D Aircraft Army C12T Aircraft Manual
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TM 1-1510-218-10
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Figure 7-16. Minimum Take-Off Power at 2000 RPM (Ice Vanes Retracted), (65 Knots)