Airport Engineering Conical surface of the approach area rises outwards 1 in 20 1 in 15 1 in 25 1 in 10 1 in 20 1 in 15 1 in 25 1 in 10 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 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 22.5 m × 22.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle 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 Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The distance between main gears is 10 m, and the distance of nose gear from centre of main gears is 30 m. If the angle of turning is 60°, the distance of centre of rotation from the nearer main gear, is 11.30 m 9.30 m 12.30 m 10.30 m 11.30 m 9.30 m 12.30 m 10.30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the transitional surface for A, B and C type of runway shall be 0.045138888888889 0.046527777777778 0.05 0.048611111111111 0.045138888888889 0.046527777777778 0.05 0.048611111111111 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered 13 Both (C) and (D) 31 135° 13 Both (C) and (D) 31 135° ANSWER DOWNLOAD EXAMIANS APP
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