List of top Flight Mechanics Questions

\(W_A\) and \(W_B\) are the respective maximum take-off weights of an aircraft for two ambient air conditions given below.
Condition A: \(p = 1\) bar, \(T = 50^{\circ}\)C; Condition B: \(p = 0.66\) bar, \(T = -30^{\circ}\)C
If all other parameters relevant for take-off are kept the same in these two conditions, the ratio \(W_B/W_A\) is ________ (rounded off to 3 decimal places).
An aircraft starts gliding in power-off condition at an altitude of 4 km. Given that the maximum lift to drag ratio of the aircraft is 15, the maximum glide range that the aircraft can cover, measured along the ground, is _______ km (rounded off to the nearest integer).
Which of the following statements is/are TRUE about the stability of an aircraft?
The primary load-carrying structural component of an aircraft wing is:
Which control surface is mainly used to control the yaw motion of an aircraft?