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 0.001 0.0065 0.0043 0.0026 0.001 0.0065 0.0043 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle 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 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Load of the wings 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 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 Both A and R is true but R is not the correct explanation of A ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The height of the pilot's eye above the runway surface is assumed 1 m 3 m 5 m 4 m 1 m 3 m 5 m 4 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 60 m × 120 m 22.5 m × 22.5 m 30 m × 30 m 22.5 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 30 m × 30 m 22.5 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
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