1. A light aircraft has a mass of 2.0x10^3 kg, a wingspan area of 10.0m^2, an upper wing distance of 1.75m, and a lower wing distance of 1.00m. What minimum takeoff speed must the airplane travel to become airborne? 2. V1= square root of ((2Fw)/(pA(((d2/d1)^2)-1)) 3. How am I supposed to find p and Fw? Which length is d1 and which is d2?