List of top Flight Mechanics Questions asked in GATE AE

For a conventional fixed-wing aircraft in a 360\(^\circ\) inverted vertical loop maneuver, what is the load factor ($n$) at the topmost point of the loop? Assume the flight to be steady at the topmost point.
For a conventional fixed-wing aircraft, which of the following statements are true?
For the jet aircraft data provided, the speed for maximum endurance in steady level flight is \(\underline{\hspace{1cm}}\) m/s (round off to two decimal places).