Airport Engineering The length of clear zone for none instrument runway of a small aircraft is 300 m 600 m 750 m 150 m 300 m 600 m 750 m 150 m 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 : The ratio of arriving and departing aircrafts influences the airport capacity:Reason R : Landing operation is generally given priority over the taking off operation.Select your answer based on the coding system given below: Both A and R is true and 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 and 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 For the proposed air port, the survey project provides Master plan Topographic plan All listed here Grading plan Master plan Topographic plan All listed here Grading plan 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 172.5 m 145 m 162.5 m 152.5 m 172.5 m 145 m 162.5 m 152.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle 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 Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
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