Airport Engineering For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is 25 m 100 m 75 m 50 m 25 m 100 m 75 m 50 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine Direction of winds Strength of winds Height of air-crafts None of these Direction of winds Strength of winds Height of air-crafts None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The runway length after correcting for elevation and temperature is 2845 m. If the effective gradient on runway is 0.5 percent then the revised runway length will be 3130 m 2910 m 3030 m 2845 m 3130 m 2910 m 3030 m 2845 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered 31 Both (C) and (D) 135° 13 31 Both (C) and (D) 135° 13 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Less than empty operating weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Less than empty operating weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight 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: 2 and 3 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 ANSWER DOWNLOAD EXAMIANS APP
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