Airport Engineering Pick up the component not applicable to aeroplanes None of these Air screw Engines Wings None of these Air screw Engines Wings 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 0.6 0.5 0.75 0.4 0.6 0.5 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The threshold markings are All listed here 1 m clear space between adjacent Placed symmetrically on either side of the runway centre line 4 m wide All listed here 1 m clear space between adjacent Placed symmetrically on either side of the runway centre line 4 m wide ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The runway orientation is made so that landing and takeoff are Against the wind direction None of these Perpendicular to wind direction Along the wind direction Against the wind direction None of these Perpendicular to wind direction Along the wind direction 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 and 2 are correct 1, 2 and 3 are correct 2 and 3 are correct 1 and 3 are correct 1 and 2 are correct 1, 2 and 3 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component ANSWER DOWNLOAD EXAMIANS APP
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