Final answer:
The calculated calibrated airspeed of the aircraft is 220 knots, obtained by correcting the indicated airspeed of 225 knots by the position error of -5 knots.
Step-by-step explanation:
The student's question pertains to an ICeT problem which involves calculating the aircraft's calibrated airspeed. The given parameters are a pressure altitude of 14,000 ft, an indicated airspeed of 225 knots, and a position error of -5 knots. The calibrated airspeed is simply the indicated airspeed corrected for position error.
To determine the calibrated airspeed, we apply the following steps:
- Start with the indicated airspeed (IAS): 225 knots.
- Adjust for position error: Since the position error is -5 knots, we subtract this from the indicated airspeed. 225 knots - 5 knots = 220 knots.
- The result is the calibrated airspeed (CAS): 220 knots.
Therefore, the aircraft's calibrated airspeed is 220 knots.