Airport Engineering Which of the following is an example of failure in flexible pavements? Mud pumping Shrinkage cracks Alligator cracking Warping cracks Mud pumping Shrinkage cracks Alligator cracking Warping cracks ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, the minimum basic runway length for A and E type of airport will be 2100 m and 750 m 1500 m and 600 m 1500 m and 750 m 2100 m and 600 m 2100 m and 750 m 1500 m and 600 m 1500 m and 750 m 2100 m and 600 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of clear zone for none instrument runway of a small aircraft is 300 m 750 m 600 m 150 m 300 m 750 m 600 m 150 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of runway under standard conditions is 2000 m. The elevation of airport site is 300 m. Its reference temperature is 33.05°C. If the runway is to be constructed with an effective gradient of 0.25 percent, the corrected runway length will be 2800 m 2600 m 2500 m 2700 m 2800 m 2600 m 2500 m 2700 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
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