Airport Engineering Wing loading of an aircraft is Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings 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 2 and 3 1,2 and 4 1,2,3 and 4 1,3, and 4 2 and 3 1,2 and 4 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Airport elevation is the reduced level above M.S.L. of Lowest point of the landing area 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to I.C.A.O. all markings on the runways are painted white and on taxiways Yellow Red Green Black Yellow Red Green Black ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The engine failure case for determining the basic runway length may require Either a clearway or a stop-way Either a clearway or a stop-way or both Only stop way Only clearway Either a clearway or a stop-way Either a clearway or a stop-way or both Only stop way Only clearway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of runway under standard conditions is 2000 m. The elevation of airport site is 300 m. Its reference temperature is 33.05°C. If the runway is to be constructed with an effective gradient of 0.25 percent, the corrected runway length will be 2600 m 2800 m 2500 m 2700 m 2600 m 2800 m 2500 m 2700 m ANSWER DOWNLOAD EXAMIANS APP
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