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Figure 7-11. Take-off Weight - Flaps 0%, to Achieve Positive One-Engine Climb
Figure 7-13. Wind Components
TM-55-1510-220-10 Army RC-12D Aircraft Manual
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TM 55-1510-220-10
TAKEOFF WEIGHT - FLAPS 40%
Figure 7-12. Takeoff Weight - Flaps 40%, to Achieve Positive One-Engine Climb
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