Airport Engineering The length of runway is increased per 300 m rise above M.S.L. 0.03 0.07 0.04 0.05 0.03 0.07 0.04 0.05 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
Airport Engineering According to I.C.A.O. the recommended length of air ports is decided on Standard sea level temperature (15°C) All listed here Sea level elevation Effective gradient percentage Standard sea level temperature (15°C) All listed here Sea level elevation Effective gradient percentage ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to I.C.A.O. the slope of transitional surface at right angles to the centre line of runway, is kept 1 in 7 1 in 6 1 in 5 1 in 4 1 in 7 1 in 6 1 in 5 1 in 4 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The air is blowing at a speed of 75 knots in the direction of the aircraft flying at a ground speed of 775 knots. The air speed of the aircraft, is 675 knots 775 knots 850 knots 75 knots 675 knots 775 knots 850 knots 75 knots ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 60 m × 120 m 22.5 m × 22.5 m 22.5 m × 30 m 30 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 22.5 m × 30 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
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