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An A-26C aircraft has 2 piston engines driving propellers. It is climbing at a flight-path angle of 10 degrees. The aircraft weighs 32,000 pounds (142,343 Newtons). For a steady climb, EACH engine must overcome how much weight in addition to the drag of the airplane?

Respuesta :

segunare233

Answer:

320lbs

Explanation:

Weight = T–D / %gradient x 100

Where T = thrust and D = Drag

Due to engine out case, thrust will be from 2 engines piston i.e. 32,000x 2 = 64,000

Weight = (64,000-)/2x 100

Weight = 320lbs

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