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 51 m 45 m 20 m 30 m 51 m 45 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is More than the maximum structural landing weight Equal to the empty operating weight plus the payload Equal to the maximum structural landing weight Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the empty operating weight plus the payload Equal to the maximum structural landing weight Less than the maximum structural landing weight 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 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 A is false but R is true ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Overall apron area required is more All listed here Aircraft rear loading door is far away from terminal building Hot blast is directed towards the terminal building Overall apron area required is more All listed here Aircraft rear loading door is far away from terminal building Hot blast is directed towards the terminal building ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 15 kmph 45 kmph 25 kmph 35 kmph 15 kmph 45 kmph 25 kmph 35 kmph 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 500 kmph and 450 kmph 450 kmph and 450 kmph 450 kmph and 500 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 450 kmph 450 kmph and 500 kmph ANSWER DOWNLOAD EXAMIANS APP
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