Airport Engineering Beaufort scale is used to determine Direction of winds None of these Strength of winds Height of air-crafts Direction of winds None of these Strength of winds Height of air-crafts 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 × 22.5 m 60 m × 120 m 22.5 m × 30 m 30 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 22.5 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The fuse large includes Tail of aircraft All listed here Passengers chamber Pilot's cabin Tail of aircraft All listed here Passengers chamber Pilot's cabin ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The coordinates of the ends of a runway are (5000, 5000) and (8000, 7000). The co-ordinates of another runway are (4600, 5100) and (7000, 5300). The co-ordinates of the A.R.P. are (61500, 5600) (8000, 7000) (5800, 5200) (6500, 6000) (61500, 5600) (8000, 7000) (5800, 5200) (6500, 6000) 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 500 kmph and 450 kmph 450 kmph and 500 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 500 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Assertion A : The ratio of arriving and departing aircrafts influences the airport capacity: Reason R : Landing operation is generally given priority over the taking off operation. Select your answer based on the coding system given below: A is true but R is false Both A and R is true and R is the correct explanation of A Both A and R is true and R is not the correct explanation of A A is false but R is true A is true but R is false Both A and R is true and R is the correct explanation of A Both A and R is true and R is not the correct explanation of A A is false but R is true ANSWER DOWNLOAD EXAMIANS APP
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