Airport Engineering According to I.C.A.O. the recommended length of air ports is decided on Standard sea level temperature (15°C) Sea level elevation Effective gradient percentage All listed here Standard sea level temperature (15°C) Sea level elevation Effective gradient percentage All listed here ANSWER DOWNLOAD EXAMIANS APP
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. 0.0026 0.0043 0.0065 0.001 0.0026 0.0043 0.0065 0.001 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In instrument landing system 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 Localizer and L.M.M. are installed on one side and L.O.M. on the other side None of these 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 Localizer and L.M.M. are installed on one side and L.O.M. on the other side None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the runway at threshold is 290°, the runway number is W 20° N 290° 29° N 70° W W 20° N 290° 29° N 70° W 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 450 kmph and 500 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 500 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 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 horizontal and the fuselage axis 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 true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway ANSWER DOWNLOAD EXAMIANS APP
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