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Airport Engineering

Airport Engineering
An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as

Sonic
Super-sonic
Mach
Subsonic

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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

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Airport Engineering
According to I.C.A.O. the recommended length of air ports is decided on

Sea level elevation
Standard sea level temperature (15°C)
All listed here
Effective gradient percentage

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Airport Engineering
The reduced level of the proposed site of an air port is 2500 m above M.S.L. If the recommended length by I.C.A.O. for the runway at sea level is 2500 m, the required length of the runway is

2500 m
3725 m
3250 m
3000 m

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Airport Engineering
The total length of a runway is 1000 m. The elevation at distance 0,200 m, 400 m, 600 m, 800 m and 1000 m are 100.0 m, 99.2 m, 101.0 m, 101.8 m, 101.4 m and 101.0 m respectively. The effective gradient of runway will be.

0.0043
0.0065
0.001
0.0026

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Airport Engineering
The length of runway is increased per 300 m rise above M.S.L.

0.04
0.07
0.05
0.03

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