Airport Engineering Total correction for elevation, temperature and gradient for a runway should not be more than 0.15 0.35 0.2 0.25 0.15 0.35 0.2 0.25 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 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 0.004 0.003 0.002 0.001 0.004 0.003 0.002 0.001 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to I.C.A.O. the recommended length of air ports is decided on All listed here Sea level elevation Effective gradient percentage Standard sea level temperature (15°C) All listed here Sea level elevation Effective gradient percentage Standard sea level temperature (15°C) 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 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 Between the direction of wind and the longitudinal axis of the runway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Two single runways may be arranged so as to have X-shape All listed here T-shape L-shape X-shape All listed here T-shape L-shape ANSWER DOWNLOAD EXAMIANS APP
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