\f\f\f\fExercise 2: Airspeed Determination Givens: Altitude: FL310 (31,000 ft Pressure Altitude) Indicated Airspeed: 250 KIAS Indicated Outside Air Temperature (IOAT) or Total Temperature: -30 deg C Figure 2.1 for Atmosphere Figure 3.1 Position Errors Figure 3.2 Compressibility Errors Figure 11.2 or Tt = Ta (1 + .2M2) Temperature Ram Rise 1. Find CAS (Calibrated Airspeed in kts). 2. Find EAS (Equivalent Airspeed in kts). 3. Find Pressure Ratio: . 4. Find Mach. 5. Find Actual Outside Air Temperature (ambient temperature). 6. Find Temperature Ram Rise. 7. Find Density Ratio: . 8. Find TAS, True Airspeed in kts. 9. If you are landing into an airfield in mountainous terrain at a field elevation of 3,000 ft MSL (Mean Sea Level) and the field outside air temperature is -24 deg C, according to AC 91-XX Draft Appendix 2, how should you adjust your approach arrival procedures with a Final Approach Fix (FAF) at 5,000 ft MSL and your Minimum Descent Altitude (MDA) at 3500 ft MSL? ASCI 310: Aircraft Performance File name: Exercise_2