Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Subsonic Sonic Mach Super-sonic Subsonic Sonic Mach Super-sonic 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 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 4.2 m and 50 m 3 m and 45 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of a runway under standard atmospheric conditions is 1800 m. If the actual reduced level of the site is 1200 m, the design length of the runway is 2560 m 2660 m 2360 m 2460 m 2560 m 2660 m 2360 m 2460 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO recommendation, the rate of change of longitudinal gradient per 30 m length of vertical curve for A and B type of airports is limited to a maximum of 0.004 0.001 0.003 0.002 0.004 0.001 0.003 0.002 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Aircraft rear loading door is far away from terminal building All listed here Overall apron area required is more Hot blast is directed towards the terminal building Aircraft rear loading door is far away from terminal building All listed here Overall apron area required is more Hot blast is directed towards the terminal building ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to maximum landing weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to maximum landing weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight ANSWER DOWNLOAD EXAMIANS APP
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