Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/ wing area ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If the width of the approach area near the runway end is 150 m, the width of the approach area at a distance of 3 kilometers from runway end will be 800 m 1200 m 1500 m 1000 m 800 m 1200 m 1500 m 1000 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Assertion A : Airport capacity during IFR conditions is usually less than that during VFR conditions.Reason R: During clear weather condition (VFR), the aircrafts on final approach to runway can be spaced closer during poor visibility conditions.Select your answer based on the coding system given below: Both A and R is true but R is not the correct explanation of A Both A and R is true and R is the correct explanation of A A is false but R is true A is true but R is false Both A and R is true but R is not the correct explanation of A Both A and R is true and R is the correct explanation of A A is false but R is true A is true but R is false ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the true speed of the aircraft and the crosswind component 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 direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component 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 direction of wind and the longitudinal axis of the runway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If lift off distance of an craft is 2000 m, the clear way at the end of the runway should not be less than 152.5 m 172.5 m 145 m 162.5 m 152.5 m 172.5 m 145 m 162.5 m ANSWER DOWNLOAD EXAMIANS APP
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