A Piper Saratoga has a gross weight of 3,600 pounds, a wing span of 34 feet and an average chord of 5 feet. The maximum lift coefficient for its wing is 1.65. If the plane is cruising at sea level fully loaded, what is the stall speed. If the flaps are lowered 30 degrees, the lift coefficient increases to 2.5. If the saratoga is in a 20 degree bank with the flaps lowered 30 degrees, what is the stall speed at sea level. Solve in British system.

Answer rating: 100% (QA)

To calculate the stall speed of the Piper Saratoga we can use the formula Stall Speed 2 Weight Densi... View the full answer