Airport Engineering The thickness design of the pavement, is decided on the load carried by All listed here Nose wheel Tail wheel Main gears All listed here Nose wheel Tail wheel Main gears ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 30 m × 30 m 22.5 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 30 m × 30 m 22.5 m × 30 m 22.5 m × 22.5 m 60 m × 120 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered 135° 13 Both (C) and (D) 31 135° 13 Both (C) and (D) 31 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The centre to centre spacing of heliport lighting along the periphery of landing and takeoff area should be 7.5 m 10.0 m 5.0 m 2.5 m 7.5 m 10.0 m 5.0 m 2.5 m 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 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 true but R is false A is false but R is true 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 true but R is false A is false but R is true 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 51 m 20 m 30 m 45 m 51 m 20 m 30 m 45 m ANSWER DOWNLOAD EXAMIANS APP
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