Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Subsonic Mach Super-sonic Sonic Subsonic Mach Super-sonic Sonic ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If the width of the approach area near the runway end is 150 m, the width of the approach area at a distance of 3 kilometers from runway end will be 1500 m 800 m 1200 m 1000 m 1500 m 800 m 1200 m 1000 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with Rubberised tar concrete Asphaltic concrete Plain concrete All listed here Rubberised tar concrete Asphaltic concrete Plain concrete All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Consider the following statements regarding ICAO recommendation for correction to basic runway length of these statements1. The basic runway length should be increased at the rate of 7 percent per 300 m rise in elevation above the mean sea level.2. The basic runway length after having been corrected for elevation should be further increased at the rate of 1 percent for every 1°C rise in airport reference temperature above the standard atmospheric temperature at that elevation.3. The runway length after having been corrected for elevation and temperature should be further increased at the rate of 20% for every 1 percent of effective gradient. 1, 2 and 3 are correct 1 and 3 are correct 1 and 2 are correct 2 and 3 are correct 1, 2 and 3 are correct 1 and 3 are correct 1 and 2 are correct 2 and 3 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The centre to centre spacing of heliport lighting along the periphery of landing and takeoff area should be 2.5 m 10.0 m 5.0 m 7.5 m 2.5 m 10.0 m 5.0 m 7.5 m 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 2716 m 2816 m 2916 m 3016 m 2716 m 2816 m 2916 m 3016 m ANSWER DOWNLOAD EXAMIANS APP