Calibrated airspeed is primarily corrected for which of the following?

Calibrated airspeed is defined as the indicated airspeed of an aircraft, corrected for instrument errors and position errors. Instrument errors can occur due to inaccuracies in the speed measuring devices, while position errors arise from the airflow around the aircraft's pitot-static system. These errors are significant because they can lead to misleading indications of the aircraft's actual performance.

When pilots refer to calibrated airspeed, they are relying on a figure that provides a more accurate representation of the aircraft's true airspeed than indicated airspeed does. This accuracy is crucial during critical phases of flight, such as takeoff, landing, and maneuvers where precise speed control is necessary for safety and performance.

In contrast, the other options do not relate directly to the specific adjustments made in calculating calibrated airspeed. Altitude and climb rate primarily affect true airspeed calculations, while wind and temperature influences are more relevant to groundspeed and performance calculations, and speed and angle of attack pertain to different aerodynamic concepts.