Airport Engineering Beaufort scale is used to determine Direction of winds Height of air-crafts Strength of winds None of these Direction of winds Height of air-crafts Strength of winds None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For the proposed runway stated in if the aerodrome reference temperature is 17.2°, the net designed length of the runway is 2916 m 3016 m 2816 m 2716 m 2916 m 3016 m 2816 m 2716 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, the minimum basic runway length for A and E type of airport will be 2100 m and 600 m 1500 m and 750 m 2100 m and 750 m 1500 m and 600 m 2100 m and 600 m 1500 m and 750 m 2100 m and 750 m 1500 m and 600 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The runway orientation is made so that landing and takeoff are Along the wind direction Against the wind direction None of these Perpendicular to wind direction Along the wind direction Against the wind direction None of these Perpendicular to wind direction ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The cruising speed of the aircraft is 500 kmph. If there is a head wind of 50 kmph, then the air speed and ground speed of the aircraft respectively will be 450 kmph and 450 kmph 450 kmph and 500 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 450 kmph 450 kmph and 500 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 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 60 m × 120 m 22.5 m × 30 m 22.5 m × 22.5 m 30 m × 30 m 60 m × 120 m 22.5 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
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