Airport Engineering The total length of a runway is 1000 m. The elevation at distance 0,200 m, 400 m, 600 m, 800 m and 1000 m are 100.0 m, 99.2 m, 101.0 m, 101.8 m, 101.4 m and 101.0 m respectively. The effective gradient of runway will be. 0.001 0.0043 0.0065 0.0026 0.001 0.0043 0.0065 0.0026 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with Asphaltic concrete All listed here Rubberised tar concrete Plain concrete Asphaltic concrete All listed here Rubberised tar concrete Plain concrete 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 From the end of an instrumental runway, the approach surface rises outwards 1 in 50 1 in 20 1 in 40 1 in 30 1 in 50 1 in 20 1 in 40 1 in 30 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 0.003 0.004 0.002 0.001 0.003 0.004 0.002 0.001 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS