Airport Engineering Pick up the component not applicable to aeroplanes Engines None of these Wings Air screw Engines None of these Wings Air screw 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 air is blowing at a speed of 75 knots in the direction of the aircraft flying at a ground speed of 775 knots. The air speed of the aircraft, is 75 knots 675 knots 850 knots 775 knots 75 knots 675 knots 850 knots 775 knots ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.75 0.4 0.5 0.6 0.75 0.4 0.5 0.6 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In instrument landing system L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side None of these Localizer and L.M.M. are installed on one side and L.O.M. on the other side L.O.M. and Localizer are installed on one side and L.M.M. on the other side L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side None of these Localizer and L.M.M. are installed on one side and L.O.M. on the other side L.O.M. and Localizer are installed on one side and L.M.M. on the other side ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight Less than the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
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