Cessna 206 Turbo Stationair vs Diamond Aircraft Da62 vs Piper M350
The Cessna Turbo Stationair is best viewed as a rugged, utility-oriented single-engine aircraft that prioritizes versatility and short/rough-field capability over speed. Typical real-world range is roughly in the 700–900 nautical mile class depending on load and power settings, and it commonly seats six, with flexibility for cargo and mission equipment. The Diamond DA62 is a modern, efficient twin-engine aircraft aimed at comfortable family or business travel with added redundancy. It typically offers the longest legs of the three, often around 1,000–1,200 nautical miles in cruise profiles, and it is usually configured for seven seats, with a relatively spacious, automotive-like cabin feel. The Piper M350 is a pressurized, high-performance single designed for faster, higher-altitude personal and business travel. Its range commonly falls around 1,000–1,300 nautical miles depending on settings and payload, and seating is typically six. In category terms, it’s the most “travel-focused” and weather-capable thanks to pressurization, while the DA62 emphasizes twin safety and efficiency, and the Turbo Stationair emphasizes utility and access.
| Spec | Cessna Turbo Stationair | Diamond Aircraft DA62 | Piper M350 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 1.08 | $ 1.18 | $ 1.34 |
| Total Seats | 6 | 5 | 6 |
| Flight Rules | VFR | IFR | VFR |
| Manufacturer | Cessna | Diamond Aircraft | Piper |
| Aircraft Name | 206 Turbo Stationair | DA62 | M350 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 1283 | 1343 |
| DOC / nm / Seat | $ 0.18 | $ 0.24 | $ 0.22 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Standard Cabin Seats | 4 | 3 | 4 |
| Direct Operating Cost | $ 174 | $ 225 | $ 285 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 161 | 190 | 213 |
| Base Aircraft Price (USD) | $745,000 | $1,290,000 | $1,195,000 |
| Max Cabin Seats | — | 5 | — |
| Useful Load (lbs) | — | 1565 | 1308 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Total Seats | 6 | 5 | 6 |
| Standard Cabin Seats | 4 | 3 | 4 |
| Max Cabin Seats | — | 5 | — |
| Cabin Pressure (psi) | — | — | 5.6 |
| Engine | |||
| FADEC | No | Yes | No |
| Model | TIO-540-AJ1A | AE330 | TIO-540-AE2A |
| Fuel Type | AvGas | Diesel / Jet Fuel | AvGas |
| TBO (hrs) | 2000 | 1800 | 2000 |
| TBO (yrs) | 12 | — | 12 |
| Horsepower | 350 | 180 | 350 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Fuel Injected |
| No. of Engines | 1 | 2 | 1 |
| Fuel Capacity (gal) | 87 | 89 | 120 |
| Usable Fuel (gal) | — | 86 | — |
| Dimensions | |||
| Length (ft) | 28.3 | 30.1 | 29 |
| Wingspan (ft) | 36 | 47.8 | 43 |
| Cabin Width (ft) | 3.6 | — | 4.1 |
| Cabin Height (ft) | 4.2 | — | 4 |
| Cabin Length (ft) | 12.1 | — | 12.3 |
| Overall Height (ft) | 9.4 | 9.3 | 11.4 |
| Baggage Volume Int. (cu. ft) | 11 | — | 20 |
| Cabin Volume (cu. ft) | — | — | 165 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 |