Airport Engineering Beaufort scale is used to determine Direction of winds Strength of winds None of these Height of air-crafts Direction of winds Strength of winds None of these Height of air-crafts 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 2500 m 2600 m 2700 m 2800 m 2500 m 2600 m 2700 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The height of the pilot's eye above the runway surface is assumed 5 m 3 m 1 m 4 m 5 m 3 m 1 m 4 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The maximum length and pavement strength of the runway is that of A 1 G 7 B 3 B 2 A 1 G 7 B 3 B 2 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Equal to the empty operating weight plus the payload Equal to the maximum structural landing weight Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the empty operating weight plus the payload Equal to the maximum structural landing weight Less than the maximum structural landing weight More than the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
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