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 3016 m 2816 m 2916 m 2716 m 3016 m 2816 m 2916 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the All listed here Overall apron area required is more Aircraft rear loading door is far away from terminal building Hot blast is directed towards the terminal building All listed here Overall apron area required is more Aircraft rear loading door is far away from terminal building Hot blast is directed towards the terminal building ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for A, B, and C type of airports, maximum effective, transverse and longitudinal grades in percentage respectively are 1.5, 1.5 and 2.0 1.0, 1.5 and 1.5 2.0, 2.0 and 2.0 1.0, 1.5 and 2.0 1.5, 1.5 and 2.0 1.0, 1.5 and 1.5 2.0, 2.0 and 2.0 1.0, 1.5 and 2.0 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. 2 and 3 are correct 1 and 3 are correct 1, 2 and 3 are correct 1 and 2 are correct 2 and 3 are correct 1 and 3 are correct 1, 2 and 3 are correct 1 and 2 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Conical surface of the approach area rises outwards 1 in 10 1 in 25 1 in 20 1 in 15 1 in 10 1 in 25 1 in 20 1 in 15 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload ANSWER DOWNLOAD EXAMIANS APP
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