Airport Engineering The engine failure case for determining the basic runway length may require Only clearway Only stop way Either a clearway or a stop-way Either a clearway or a stop-way or both Only clearway Only stop way Either a clearway or a stop-way Either a clearway or a stop-way or both ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO recommendation, the rate of change of longitudinal gradient per 30 m length of vertical curve for A and B type of airports is limited to a maximum of 0.001 0.003 0.004 0.002 0.001 0.003 0.004 0.002 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The coordinates of the ends of a runway are (5000, 5000) and (8000, 7000). The co-ordinates of another runway are (4600, 5100) and (7000, 5300). The co-ordinates of the A.R.P. are (6500, 6000) (5800, 5200) (8000, 7000) (61500, 5600) (6500, 6000) (5800, 5200) (8000, 7000) (61500, 5600) ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The maximum length and pavement strength of the runway is that of B 3 A 1 G 7 B 2 B 3 A 1 G 7 B 2 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 30 m × 30 m 22.5 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
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