Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 60 m × 120 m 22.5 m × 30 m 22.5 m × 22.5 m 30 m × 30 m 60 m × 120 m 22.5 m × 30 m 22.5 m × 22.5 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to empty operating weight Less than empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Equal to empty operating weight Less than empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load 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 1,3, and 4 2 and 3 1,2,3 and 4 1,2 and 4 1,3, and 4 2 and 3 1,2,3 and 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 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 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 From the end of an instrumental runway, the approach surface rises outwards 1 in 50 1 in 30 1 in 40 1 in 20 1 in 50 1 in 30 1 in 40 1 in 20 ANSWER DOWNLOAD EXAMIANS APP
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