Airport Engineering In instrument landing system None of these 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 L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side None of these 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 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 The length of runway under standard conditions is 2000 m. The elevation of airport site is 300 m. Its reference temperature is 33.05°C. If the runway is to be constructed with an effective gradient of 0.25 percent, the corrected runway length will be 2500 m 2800 m 2600 m 2700 m 2500 m 2800 m 2600 m 2700 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of clear zone for none instrument runway of a small aircraft is 150 m 750 m 300 m 600 m 150 m 750 m 300 m 600 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 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 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 2 aircrafts per hour 4 aircrafts per hour 16 aircrafts per hour 1 aircraft per hour 2 aircrafts per hour 4 aircrafts per hour 16 aircrafts per hour 1 aircraft per hour 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/total available H.P of engines Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Load of the wings ANSWER DOWNLOAD EXAMIANS APP
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