Airport Engineering Pick up the correct abbreviation from the following: L.O.M. (low powered outer marker) All listed here V.H.F. (very high frequency) L.M.M. (low powered middle marker) L.O.M. (low powered outer marker) All listed here V.H.F. (very high frequency) L.M.M. (low powered middle marker) ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The cruising speed of the aircraft is 500 kmph. If there is a head wind of 50 kmph, then the air speed and ground speed of the aircraft respectively will be 500 kmph and 450 kmph 500 kmph and 500 kmph 450 kmph and 450 kmph 450 kmph and 500 kmph 500 kmph and 450 kmph 500 kmph and 500 kmph 450 kmph and 450 kmph 450 kmph and 500 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Sonic Mach Subsonic Super-sonic Sonic Mach Subsonic Super-sonic ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Airport elevation is the reduced level above M.S.L. of Control tower Lowest point of the landing area None of these Highest point of the landing area Control tower Lowest point of the landing area None of these Highest point of the landing area 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 and 3 are correct 2 and 3 are correct 1, 2 and 3 are correct 1 and 2 are correct 1 and 3 are correct 2 and 3 are correct 1, 2 and 3 are correct 1 and 2 are correct 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