Airport Engineering The maximum value of the angle of turning of the nose gear large jet aircrafts, is limited to 20° 30° 60° 45° 20° 30° 60° 45° 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: A is false but R is true Both A and R is true and R is not the correct explanation of A A is true but R is false Both A and R is true and R is the correct explanation of A A is false but R is true Both A and R is true and R is not the correct explanation of A A is true but R is false Both A and R is true and R is the correct explanation of A 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: A is false but R is true Both A and R is true and R is the correct explanation of A Both A and R is true but R is not the correct explanation of A A is true but R is false A is false but R is true Both A and R is true and R is the correct explanation of A Both A and R is true but R is not the correct explanation of A A is true but R is false ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In approach areas of runways equipped with instrumental landing facilities any object within 4.5 km distance from runway end shall be considered as an obstruction if its height is more than 20 m 30 m 45 m 51 m 20 m 30 m 45 m 51 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ 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 1200 m 800 m 1500 m 1000 m 1200 m 800 m 1500 m 1000 m ANSWER DOWNLOAD EXAMIANS APP
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