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.
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.
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: e6b flight computer exercises
Exercise 2.1: 6. ~105 kts 7. ~161 kts 8. ~83 kts (density altitude ~2,800 ft)
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. Fuel burn = 9
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.
When you sit for your FAA Knowledge Test, you will not fear the word problems. When you fly your first solo cross-country, you will correct for wind without second-guessing. And when the DPE (Designated Pilot Examiner) hands you a diversion scenario, you will smile, spin the wheel, and answer in 20 seconds. Method: Align 9
Correction angle = (Distance off course / Distance flown) × 60