Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 180 m 120 m 240 m 60 m 180 m 120 m 240 m 60 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Aircraft rear loading door is far away from terminal building All listed here Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here Hot blast is directed towards the terminal building Overall apron area required is more 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 135° 13 31 Both (C) and (D) 135° 13 31 Both (C) and (D) ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle 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 true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway 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 true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The thickness design of the pavement, is decided on the load carried by Nose wheel Tail wheel All listed here Main gears Nose wheel Tail wheel All listed here Main gears ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Load of the wings ANSWER DOWNLOAD EXAMIANS APP
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