Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Aircraft rear loading door is far away from terminal building Hot blast is directed towards the terminal building All listed here Overall apron area required is more Aircraft rear loading door is far away from terminal building Hot blast is directed towards the terminal building All listed here Overall apron area required is more ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The thickness design of the pavement, is decided on the load carried by Main gears Nose wheel All listed here Tail wheel Main gears Nose wheel All listed here Tail wheel ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering An airport has 4 gates. If the weighted average gate occupancy time is 30 minutes and gate utilization factor is 0.5, then the capacity of the gate will be 16 aircrafts per hour 4 aircrafts per hour 1 aircraft per hour 2 aircrafts per hour 16 aircrafts per hour 4 aircrafts per hour 1 aircraft per hour 2 aircrafts per hour 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 (8000, 7000) (61500, 5600) (5800, 5200) (6500, 6000) (8000, 7000) (61500, 5600) (5800, 5200) (6500, 6000) 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: 1,2,3 and 4 1,3, and 4 1,2 and 4 2 and 3 1,2,3 and 4 1,3, and 4 1,2 and 4 2 and 3 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear ANSWER DOWNLOAD EXAMIANS APP
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