Figure 7-10. Maximum Take-off Weight Permitted by Enroute Climb Requirement

Figure 7-9. Minimum Take-off Power at 2000RPM

Figure 7-11. Take-off Weight - Flaps 0%, to Achieve Positive One-Engine Climb

TM-55-1510-220-10 Army RC-12D Aircraft Manual
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TM 55-1510-220-10 MAXIMUM TAKEOFF WEIGHT PERMITTED BY ENROUTE CLIMB REQUIREMENT Figure 7-10. Maximum Take-off Weight Permitted by Enroute Climb Requirement 7-19

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