Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with Asphaltic concrete Rubberised tar concrete All listed here Plain concrete Asphaltic concrete Rubberised tar concrete All listed here Plain concrete 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 1500 m 1000 m 1200 m 800 m 1500 m 1000 m 1200 m 800 m 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 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 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of a runway under standard atmospheric conditions is 1800 m. If the actual reduced level of the site is 1200 m, the design length of the runway is 2660 m 2460 m 2360 m 2560 m 2660 m 2460 m 2360 m 2560 m 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 500 kmph and 500 kmph 450 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 450 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 450 kmph 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
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