Airport Engineering Conical surface of the approach area rises outwards 1 in 20 1 in 25 1 in 15 1 in 10 1 in 20 1 in 25 1 in 15 1 in 10 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Effective length of a runway is the distance between Point of intersection of the obstruction clearance line and the extended plane of the runway surface, and the other end of the runway Ends of the runway Ends of the clear way on either side Point of intersection of the glide path and the extended plane of the runway surface and the other end of the runway Point of intersection of the obstruction clearance line and the extended plane of the runway surface, and the other end of the runway Ends of the runway Ends of the clear way on either side Point of intersection of the glide path and the extended plane of the runway surface and the other end of the runway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering From the end of an instrumental runway, the approach surface rises outwards 1 in 50 1 in 20 1 in 30 1 in 40 1 in 50 1 in 20 1 in 30 1 in 40 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 22.5 m × 22.5 m 60 m × 120 m 30 m × 30 m 22.5 m × 30 m 22.5 m × 22.5 m 60 m × 120 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to maximum landing weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to maximum landing weight Equal to empty operating weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Load of the wings ANSWER DOWNLOAD EXAMIANS APP
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