Cessna 206 Turbo Stationair vs Cessna Caravan vs Diamond Aircraft Da62
The Cessna Turbo Stationair (typically the turbocharged 206) is a rugged, piston single in the utility/“bush” category, suited to shorter strips and flexible loading. It usually carries about 5–6 passengers (often up to six seats including the pilot) and offers mid-range capability, commonly on the order of roughly 600–900 nautical miles depending on power setting, payload, and reserves. The Cessna Caravan (208 series) is a single‑engine turboprop designed for high payload and simple operations, widely used for charter, cargo, and remote access. Passenger seating is commonly around 9–14 (configuration dependent), and range is generally similar to or a bit better than the Stationair when loaded for typical missions, often roughly 700–1,000+ nautical miles, varying with variant and weight. The Diamond DA62 is a modern twin‑engine piston aircraft focused on efficient personal/business travel rather than heavy utility hauling. It typically seats 5–7 and is often comparable or better on range than the Stationair in cruise touring profiles, commonly around 1,000–1,200 nautical miles depending on configuration and reserves.
| Spec | Cessna Turbo Stationair | Cessna Caravan | Diamond Aircraft DA62 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 1.08 | $ 3.07 | $ 1.18 |
| Total Seats | 6 | 10 | 5 |
| Flight Rules | VFR | VFR | IFR |
| Manufacturer | Cessna | Cessna | Diamond Aircraft |
| Aircraft Name | 206 Turbo Stationair | Caravan | DA62 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 1070 | 1283 |
| DOC / nm / Seat | $ 0.18 | $ 0.38 | $ 0.24 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Standard Cabin Seats | 4 | 8 | 3 |
| Direct Operating Cost | $ 174 | $ 571 | $ 225 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 161 | 186 | 190 |
| Base Aircraft Price (USD) | $745,000 | $2,355,000 | $1,290,000 |
| Min Crew | — | 1 | — |
| Max Cabin Seats | — | 9 | 5 |
| Useful Load (lbs) | — | 3305 | 1565 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Total Seats | 6 | 10 | 5 |
| Standard Cabin Seats | 4 | 8 | 3 |
| Lavatory | — | No | — |
| Min Crew | — | 1 | — |
| Cargo Door | — | Yes | — |
| Max Cabin Seats | — | 9 | 5 |
| Cabin Pressure (psi) | — | Un-Pressurized | — |
| Galley / Refreshment | — | No | — |
| Engine | |||
| FADEC | No | Yes | Yes |
| Model | TIO-540-AJ1A | PT6A-114A | AE330 |
| Fuel Type | AvGas | — | Diesel / Jet Fuel |
| TBO (hrs) | 2000 | 3600 | 1800 |
| TBO (yrs) | 12 | — | — |
| Horsepower | 350 | 675 | 180 |
| Fuel Delivery | Fuel Injected | — | Fuel Injected |
| No. of Engines | 1 | 1 | 2 |
| Fuel Capacity (gal) | 87 | — | 89 |
| Flat Rating | — | ISA + 31 | — |
| Usable Fuel (gal) | — | — | 86 |
| Dimensions | |||
| Length (ft) | 28.3 | 37.6 | 30.1 |
| Wingspan (ft) | 36 | 52.1 | 47.8 |
| Cabin Width (ft) | 3.6 | 5.4 | — |
| Cabin Height (ft) | 4.2 | 4.5 | — |
| Cabin Length (ft) | 12.1 | 12.8 | — |
| Overall Height (ft) | 9.4 | 15 | 9.3 |
| Baggage Volume Int. (cu. ft) | 11 | 32 | — |