Assume standard atmospheric conditions The International Civil Aviation Organization (ICAO); (an ICAO atmosphere).

1).    What is the maximum lift possible that can be produced by this aircraft at 300 knots, at Mean Sea Level? Does the maximum lift possible exceed the maximum load factor?
2).    Calculate the stall speed at Mean Sea Level for this aircraft at the 50,000 pound weight. Provide your answer in knots and in feet per second.
3).    Calculate the stall speed at 20,000 feet for this aircraft at the 50,000 pound weight. Provide your answer in knots and in feet per second.
4).    If the aircraft weight is 50,000 pounds, what coefficient of lift is required to maintain straight and level un-accelerated flight at 400 knots, at an altitude of 20,000 feet for this aircraft?

Weight                                                               50,000 lbs.
Wing Airfoil                                                       NACA 64-006
Wing Area                                                         500 sq. feet.
Wing Aspect Ratio                                           3.2
Wing LE Sweep Angle                                      45 degrees
Wing Span                                                         40 Feet
Wing MAC length                                             20 feet
Maximum Positive Lift Coefficient               1.50
Maximum Positive Load Factor                   +10 G's