What is the potential energy ft-lb of the aircraft after


Given: Gross Weight                          =    300,000 pounds

            Average Drag                         =    15,000 pounds

            Average Friction Force          =    3,000 pounds

            Average Thrust                       =    90,000 pounds

            Lift Off Speed                         =    140 Knots True Airspeed

What is the Potential Energy (ft-lb) of the aircraft after climbing out to 10,000 ft with the new weight at 290,000 lb?

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