Online Ground School
Airline Transport and IATRA

Part 5: Navigation General

5-028. Determine the actual TAS on the basis of the following:

Indicated Airspeed: 240 kts
Airspeed Calibration Error: +2 kts
Compressibility Error: -10 kts
Indicated OAT: -28º C
Temperature Rise: +20º C
Cruising Altitude: FL 350

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