Airport Engineering The height of the pilot's eye above the runway surface is assumed 3 m 1 m 4 m 5 m 3 m 1 m 4 m 5 m 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 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 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 500 kmph and 450 kmph 500 kmph and 500 kmph 450 kmph and 500 kmph 450 kmph and 450 kmph 500 kmph and 450 kmph 500 kmph and 500 kmph 450 kmph and 500 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.5 0.4 0.75 0.6 0.5 0.4 0.75 0.6 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 Both (C) and (D) 13 31 135° Both (C) and (D) 13 31 135° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In Instrumental landing system, the middle markers are located About 1 km. ahead of the runway threshold At the runway threshold Along the extended centre line of runway end About 7 km. ahead of the runway threshold About 1 km. ahead of the runway threshold At the runway threshold Along the extended centre line of runway end About 7 km. ahead of the runway threshold ANSWER DOWNLOAD EXAMIANS APP
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