E6b Flight Computer Exercises ✓

Pressure Altitude = 8,500 ft. Temperature = +15°C. CAS = 110 kts. Find: TAS. E6B Method: Move the density altitude window so 8,500 ft aligns with 15°C. Read the "True Airspeed" correction: ~124 kts.

Exercise 2.1: 6. ~105 kts 7. ~161 kts 8. ~83 kts (density altitude ~2,800 ft) e6b flight computer exercises

Correction angle = (Distance off course / Distance flown) × 60 Pressure Altitude = 8,500 ft

6. PA 6,000 ft, Temp 10°C, CAS 95 kts → TAS? 7. PA 12,000 ft, Temp -5°C, CAS 145 kts → TAS? 8. PA 2,000 ft, Temp 30°C, CAS 80 kts → TAS? (High DA warning) Exercise 2.2: Finding Density Altitude Directly Goal: Know your aircraft’s takeoff performance. Find: TAS

4. Burn 12.2 GPH, Time 1h 45m → Gallons? 5. Burn 8.7 GPH, Distance 260 NM, GS 104 kts → Total fuel? (Hint: Find time first, then fuel) Part 2: Speed & Density Altitude Exercises Density altitude kills performance. These exercises force you to calibrate your thinking from indicated to true airspeed. Exercise 2.1: True Airspeed (TAS) from Calibrated (CAS) Formula: TAS = CAS × √(Sea Level Density / Actual Density) – or use the E6B window.

Groundspeed (GS) = 120 knots. Time = 1 hour 45 minutes. Find: Distance traveled. E6B Method: Rotate inner scale so 120 (outer) aligns with the index (60 minutes). Find 1:45 (105 minutes) on the inner scale. Read outer scale = 210 nautical miles.

9. TC 180°, TAS 130, Wind 240°/20 kts → WCA? GS? 10. TC 045°, TAS 95, Wind 090°/15 kts → WCA? GS? 11. TC 310°, TAS 150, Wind 290°/35 kts → WCA? (Crosswind component high) Exercise 3.2: Finding Wind (When aloft) Advanced skill: You don't know the wind, but you know your heading and track.