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Figure 7-8. Fahrenheit to Celsius Temperature Conversion
Figure 7-10. Take-Off Weight - Flaps 40%, To Achieve Positive One-Engine Inoperative Climb at Lift-Off
TM-55-1510-219-10 Army Aviation Maintenance Engineering Manual Weight and Balance
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TM 55-1510-219-10
Figure 7-9. Take-Off Weight - Flaps 0%, To Achieve Positive One-Engine Inoperative Climb at Lift-Off
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