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Figure 7A-16. Takeoff Weight to Achieve Positive One-Engine-Inoperative Climb at Lift-Off, Flaps APPROACH
Figure 7A-18. Minimum Takeoff Power With 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
7A-21
Figure 7A-17. Minimum Takeoff Power at 2000 RPM With Ice Vanes Retracted (65 Knots)