Civil Engineering Mcqs

Zero fuel weight of an aircraft is_________________?
  • (A)  equal to empty operating weight
  • (B)  equal to maximum landing weight
  • (C)  less than empty operating weight
  • (D)  equal to sum of empty operating weight and the maximum pay load
Castor angle is defined as the angle______________?
  • (A)  formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear
  • (B)  between the direction of wind and the longitudinal axis of the runway
  • (C)  between the true speed of the aircraft and the crosswind component
  • (D)  between the horizontal and the fuselage axis