Airport Engineering In instrument landing system L.O.M. and Localizer are installed on one side and L.M.M. on the other side None of these L.O.M. and L.M.M. are installed on one side and Localizer antenna 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 Localizer are installed on one side and L.M.M. on the other side None of these L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side Localizer and L.M.M. are installed on one side and L.O.M. on the other side 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 4.2 m and 50 m 3 m and 45 m 4.2 m and 30 m 3 m and 30 m 4.2 m and 50 m 3 m and 45 m 4.2 m and 30 m 3 m and 30 m 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 A is false but R is true 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 true but R is false A is false but R is true 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering An airport has 4 gates. If the weighted average gate occupancy time is 30 minutes and gate utilization factor is 0.5, then the capacity of the gate will be 16 aircrafts per hour 2 aircrafts per hour 4 aircrafts per hour 1 aircraft per hour 16 aircrafts per hour 2 aircrafts per hour 4 aircrafts per hour 1 aircraft per hour ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For the proposed runway stated in if the aerodrome reference temperature is 17.2°, the net designed length of the runway is 2816 m 2916 m 3016 m 2716 m 2816 m 2916 m 3016 m 2716 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear ANSWER DOWNLOAD EXAMIANS APP
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