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.Management Sciences
A. 20 m
B. 30 m
C. 45 m
D. 51 m
Related 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...
- Maximum gross take-off weight of an aircraft is__________________?
- A. equal to the maximum structural landing weight B. less than the maximum structural landing weight C. more than the maximum structural landing weight D. equal to the empty operating weight plus the payload...
- The cruising speed of the aircraft is 500 kmph. If there is a head wind of 50 kmph, then the air speed and ground speed of the aircraft respectively will be_________________?
- A. 450 kmph and 500 kmph B. 500 kmph and 450 kmph C. 450 kmph and 450 kmph D. 500 kmph and 500 kmph...
- As per ICAO, the minimum basic runway length for A and E type of airport will be________________?
- A. 1500 m and 600 m B. 2100 m and 750 m C. 1500 m and 750 m D. 2100 m and 600 m...
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