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 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 Between the direction of wind and the longitudinal axis of the runway 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 2700 m 2500 m 2800 m 2600 m 2700 m 2500 m 2800 m 2600 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For the proposed air port, the survey project provides Grading plan Topographic plan Master plan All listed here Grading plan Topographic plan Master plan All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 180 m 120 m 60 m 240 m 180 m 120 m 60 m 240 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The maximum value of the angle of turning of the nose gear large jet aircrafts, is limited to 20° 60° 30° 45° 20° 60° 30° 45° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to maximum landing weight Less than empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to empty operating weight Equal to maximum landing weight Less than empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to empty operating weight ANSWER DOWNLOAD EXAMIANS APP
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