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Calculate the acceleration of the following aircraft: Ta during takeoff = 3,500 lbs, Total drag = 500 lbs, W = 15,000 lbs, VLOF (Liftoff) =

Calculate the acceleration of the following aircraft: Ta during takeoff = 3,500 lbs, Total drag = 500 lbs, W = 15,000 lbs, VLOF (Liftoff) = 130 kts. Group of answer choices 8.6 ft/s2 7.5 ft/s2 8.5 ft/s2 6.4 ft/s2

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