Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 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 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 25 kmph 45 kmph 35 kmph 15 kmph 25 kmph 45 kmph 35 kmph 15 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.5 0.6 0.75 0.4 0.5 0.6 0.75 0.4 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to the International Civil Aviation Organization (I.C.A.O.), the runway lengths of aerodromes, have been coded by Last Seven English alphabets Seven English alphabets First seven natural numbers First Seven English alphabets Last Seven English alphabets Seven English alphabets First seven natural numbers First Seven English alphabets ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The engine failure case for determining the basic runway length may require Either a clearway or a stop-way or both Only stop way Either a clearway or a stop-way Only clearway Either a clearway or a stop-way or both Only stop way Either a clearway or a stop-way Only clearway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In an airport, if 4 groups of 5 gates each located well separated are considered for traffic and the future to present traffic ratio is 3, then the total requirement of future gates will be 36 68 44 32 36 68 44 32 ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS