Final answer:
Under Part 91, Subpart G of the Federal Aviation Regulations, the accelerate-stop distance for a turbine-engine-powered transport category airplane depends on the airplane's maximum certificated takeoff weight and landing weight.
Step-by-step explanation:
Under Part 91, Subpart G of the Federal Aviation Regulations, no person may operate a turbine-engine-powered transport category airplane unless the accelerate-stop distance is not greater than a specified value. The specified value depends on the airplane's maximum certificated takeoff weight and landing weight. For example, for an airplane with a maximum certificated takeoff weight of 75,000 pounds or less, the accelerate-stop distance must be not greater than 115% of the airplane's effective length. The effective length is the distance from the point on the centerline of the nose wheel or tail wheel to the most remote point on the fuselage, measured parallel to the longitudinal axis of the airplane.