Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Load of the wings ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with Plain concrete Asphaltic concrete Rubberised tar concrete All listed here Plain concrete Asphaltic concrete Rubberised tar concrete All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Total correction for elevation, temperature and gradient for a runway should not be more than 0.25 0.15 0.2 0.35 0.25 0.15 0.2 0.35 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The reduced level of the proposed site of an air port is 2500 m above M.S.L. If the recommended length by I.C.A.O. for the runway at sea level is 2500 m, the required length of the runway is 3000 m 3250 m 2500 m 3725 m 3000 m 3250 m 2500 m 3725 m 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 2700 m 2800 m 2500 m 2600 m 2700 m 2800 m 2500 m 2600 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 1 aircraft per hour 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 ANSWER DOWNLOAD EXAMIANS APP
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