Airport Engineering The length of runway is increased per 300 m rise above M.S.L. 0.04 0.07 0.05 0.03 0.04 0.07 0.05 0.03 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If the monthly mean of average daily temperature for the hottest month of the year is 25°C and the monthly mean of the maximum daily temperature of the same month of the year is 46°C, the airport reference temperature is 48°C 32°C 35.5°C 25°C 48°C 32°C 35.5°C 25°C ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The engine failure case for determining the basic runway length may require Only stop way Either a clearway or a stop-way or both Either a clearway or a stop-way Only clearway Only stop way Either a clearway or a stop-way or both Either a clearway or a stop-way Only clearway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For the proposed runway stated in if the aerodrome reference temperature is 17.2°, the net designed length of the runway is 2816 m 3016 m 2916 m 2716 m 2816 m 3016 m 2916 m 2716 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: A is true but R is false 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 false but R is true A is true but R is false 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 false but R is true ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
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