Given the following information, what is the Air distance (NAM) covered?
TAS: 120 kt
Headwind component: 20 kt
Ground Distance: 200 NGM
- TIME = NAM / TAS = NGM / GS
Solving for NAM and substituting the known values of the above equation, we get: NAM = NGM x TAS / GS = 200 NGM x 120 kt / (120 - 20) kt = 240 NAM.
OR
The flight time to cover 200 NGM is: Time = NGM / GS= 200 NM / (120 - 20) kt = 2 hr.
So, the Air distance will be: NAM = TAS x Time = 120 kt x 2 hr = 240 NAM.
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