Airport Engineering The engine failure case for determining the basic runway length may require Only stop way Only clearway Either a clearway or a stop-way or both Either a clearway or a stop-way Only stop way Only clearway Either a clearway or a stop-way or both Either a clearway or a stop-way ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the runway at threshold is 290°, the runway number is N 70° W 290° 29° W 20° N N 70° W 290° 29° W 20° N ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to I.C.A.O. the slope of transitional surface at right angles to the centre line of runway, is kept 1 in 6 1 in 7 1 in 5 1 in 4 1 in 6 1 in 7 1 in 5 1 in 4 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for A, B, and C type of airports, maximum effective, transverse and longitudinal grades in percentage respectively are 1.0, 1.5 and 2.0 2.0, 2.0 and 2.0 1.5, 1.5 and 2.0 1.0, 1.5 and 1.5 1.0, 1.5 and 2.0 2.0, 2.0 and 2.0 1.5, 1.5 and 2.0 1.0, 1.5 and 1.5 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 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 Both A and R is true but R is not the correct explanation of A 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/ 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 Load of the wings Gross total weight of the aircraft/total available H.P of engines ANSWER DOWNLOAD EXAMIANS APP
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