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Figure 7-13. Airspeed Calibration Normal System Ground Roll
Figure 7-15. Takeoff Gross Weight Limit Flaps 40% (To Achieve 100 FPM One Engine Inoperative Rate-of-Climb At Liftoff)
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 7-14. Takeoff Gross Weight Limit – Flaps 0% (To Achieve 100 FPM
One Engine Inoperative Rate-of-Climb At Liftoff)
