Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 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 22.5 m × 30 m 22.5 m × 22.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The fuse large includes Pilot's cabin All listed here Passengers chamber Tail of aircraft Pilot's cabin All listed here Passengers chamber Tail of aircraft ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Airport elevation is the reduced level above M.S.L. of Highest point of the landing area None of these Control tower Lowest point of the landing area Highest point of the landing area None of these Control tower Lowest point of the landing area ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 45 kmph 15 kmph 25 kmph 35 kmph 45 kmph 15 kmph 25 kmph 35 kmph 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 1.5 1.5, 1.5 and 2.0 1.0, 1.5 and 2.0 2.0, 2.0 and 2.0 1.0, 1.5 and 1.5 1.5, 1.5 and 2.0 1.0, 1.5 and 2.0 2.0, 2.0 and 2.0 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Which of the following factors are taken into account for estimating the runway length required for aircraft landing?1. Normal maximum temperature2. Airport elevation3. Maximum landing weight4. Effective runway gradientSelect the correct answer using the codes given below Codes: 1,2 and 4 2 and 3 1,3, and 4 1,2,3 and 4 1,2 and 4 2 and 3 1,3, and 4 1,2,3 and 4 ANSWER DOWNLOAD EXAMIANS APP
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