Airport Engineering In instrument landing system None of these L.O.M. and Localizer are installed on one side and L.M.M. on the other side Localizer and L.M.M. are installed on one side and L.O.M. on the other side L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side None of these L.O.M. and Localizer are installed on one side and L.M.M. on the other side Localizer and L.M.M. are installed on one side and L.O.M. on the other side L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO recommendation, minimum width of safety area for instrumental runway should be 150 m 78 m 450 m 300 m 150 m 78 m 450 m 300 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are 3 m and 30 m 4.2 m and 50 m 4.2 m and 30 m 3 m and 45 m 3 m and 30 m 4.2 m and 50 m 4.2 m and 30 m 3 m and 45 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The air is blowing at a speed of 75 knots in the direction of the aircraft flying at a ground speed of 775 knots. The air speed of the aircraft, is 775 knots 75 knots 675 knots 850 knots 775 knots 75 knots 675 knots 850 knots ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to maximum landing weight Less than empty operating weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Less than empty operating weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load 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 direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component 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 direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component ANSWER DOWNLOAD EXAMIANS APP
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