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
Airport Elevation 1,200 ft. Altimeter 29.92 (standard). Temperature 28°C. Find: Density Altitude. Method: Align OAT (28°C) with Pressure Altitude (1,200). Read DA in the window: ~3,100 ft. Part 3: The Wind Triangle (The Hardest E6B Exercises) This is where most students quit. Solving for wind correction angle (WCA) and groundspeed (GS) requires visualizing vectors. Do these slowly, then speed up. Exercise 3.1: Finding Groundspeed & WCA (Given Course) The Standard Cross-Country Scenario: 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
Correction angle = (Distance off course / Distance flown) × 60
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Fuel burn = 9.5 GPH. Time en route = 2h 30m. Find: Total fuel. Method: Align 9.5 (outer) with the index (60). Find 150 minutes (2:30) on inner. Read outer = 23.75 gallons.