Given a true course of 017°, wind velocity of 340° at 30 knots, and a true airspeed of 420 knots, calculate the wind correction angle and ground speed.
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FLIGHT PLANNING
Given a true course of 017°, wind velocity of 340° at 30 knots, and a true airspeed of 420 knots, calculate the wind correction angle and ground speed.
What is the true track if you are flying a constant heading of 252°, with a variation of 22°E, a deviation of 3°W, and an INS drift of 9° to the right?
A twin-jet airplane is flying from point K (35°N, 048°W) and must consider rerouting to one of three fields due to a non-mechanical event. The flight conditions are: - from K to A (distance 847NM, headwind component = 18kt) - from K to B (distance 1112NM, tailwind component = 120kt) - from K to C (distance 883NM, wind component = 0) Given an airplane true airspeed of 460 kt, which field can be reached the fastest?