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
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 22.5 m 30 m × 30 m 22.5 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 30 m × 30 m 22.5 m × 30 m 60 m × 120 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 45° 30° 20° 60° 45° 30° 20° 60° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per UK design criteria, if LCN of aircraft is between 1.25 to 1.5 times the LCN of pavement, then the number of movements allowed are Unrestricted 3000 300 Zero Unrestricted 3000 300 Zero ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Conical surface of the approach area rises outwards 1 in 15 1 in 20 1 in 10 1 in 25 1 in 15 1 in 20 1 in 10 1 in 25 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In Instrumental landing system, the middle markers are located About 7 km. ahead of the runway threshold At the runway threshold Along the extended centre line of runway end About 1 km. ahead of the runway threshold About 7 km. ahead of the runway threshold At the runway threshold Along the extended centre line of runway end About 1 km. ahead of the runway threshold ANSWER DOWNLOAD EXAMIANS APP
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