Figure 7-12. Takeoff Weight - Flaps 40%, To Achieve Positive One-Engine Climb at Lift-Off Flaps 40%

Figure 7-11. Takeoff Weight - Flaps 0%, To Achieve Positive One-Engine Climb at Lift-Off

Figure 7-13. Wind Components

TM-55-1510-221-10 Army Model RC-12D Aircraft Manual
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TM 55-1510-221-10 TAKEOFF WEIGHT - FLAPS 40% TO ACHIEVE POSITIVE ONE-ENGINE-INOPERATIVE CLIMB AT LIFT-OFF Figure 7-12. Takeoff Weight - Flaps 40%, To Achieve Positive One-Engine Climb at Lift-Off Flaps 40% 7-17

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