Cessna 206 Turbo Stationair vs Cirrus Sr22t G6 vs Diamond Aircraft Da62 vs Piper M350 vs Piper M600 Sls
The Cessna Turbo Stationair (pressurized 206/207-class utility single) is primarily a rugged, short‑field hauler; it typically carries about 5–6 people with flexible loading, and offers moderate cross‑country range that is generally shorter than the faster pressurized singles. The Cirrus SR22T G6 is a high‑performance, unpressurized piston single optimized for speed and personal travel; it seats up to 5, with a solid mid‑to‑long range that suits regional to longer trips. The Diamond DA62 is a modern, efficient twin piston aimed at comfortable family and light business travel; it commonly seats 5–7 and provides long range with strong redundancy and excellent fuel efficiency. The Piper M350 is a pressurized piston single positioned for frequent IFR and higher‑altitude cruising; it seats 6 and usually delivers longer range than most unpressurized pistons with greater weather flexibility. The Piper M600 SLS is a pressurized turbine single built for fast, high‑altitude business travel; it seats 6 and typically offers the longest range and highest cruise capability of this group.
| Spec | Cessna Turbo Stationair | Diamond Aircraft DA62 | Piper M350 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.08 | $ 1.18 | $ 1.34 | $ 2.19 |
| Total Seats | 6 | 5 | 6 | 6 |
| Flight Rules | VFR | IFR | VFR | IFR |
| Manufacturer | Cessna | Diamond Aircraft | Piper | Piper |
| Aircraft Name | 206 Turbo Stationair | DA62 | M350 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 1283 | 1343 | 1406 |
| DOC / nm / Seat | $ 0.18 | $ 0.24 | $ 0.22 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Standard Cabin Seats | 4 | 3 | 4 | 4 |
| Direct Operating Cost | $ 174 | $ 225 | $ 285 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 161 | 190 | 213 | 274 |
| Base Aircraft Price (USD) | $745,000 | $1,290,000 | $1,195,000 | $3,081,400 |
| Max Cabin Seats | — | 5 | — | — |
| Useful Load (lbs) | — | 1565 | 1308 | 2200 |
| Min Crew | — | — | — | 1 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 5 | 6 | 5 |
| Standard Cabin Seats | 4 | 3 | 4 | 4 |
| Max Cabin Seats | — | 5 | — | — |
| Cabin Pressure (psi) | — | — | 5.6 | 5.6 |
| Lavatory | — | — | — | No |
| Min Crew | — | — | — | 1 |
| Galley Location | — | — | — | MID |
| Galley / Refreshment | — | — | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | — | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | No | Yes | No | No |
| Model | TIO-540-AJ1A | AE330 | TIO-540-AE2A | PT6A-42A |
| Fuel Type | AvGas | Diesel / Jet Fuel | AvGas | — |
| TBO (hrs) | 2000 | 1800 | 2000 | 3600 |
| TBO (yrs) | 12 | — | 12 | — |
| Horsepower | 350 | 180 | 350 | 600 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Fuel Injected | — |
| No. of Engines | 1 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 87 | 89 | 120 | 260 |
| Usable Fuel (gal) | — | 86 | — | — |
| Flat Rating | — | — | — | ISA + 55 |
| Dimensions | ||||
| Length (ft) | 28.3 | 30.1 | 29 | 29.7 |
| Wingspan (ft) | 36 | 47.8 | 43 | 43.2 |
| Cabin Width (ft) | 3.6 | — | 4.1 | 4.1 |
| Cabin Height (ft) | 4.2 | — | 4 | 4 |
| Cabin Length (ft) | 12.1 | — | 12.3 | 12.3 |
| Overall Height (ft) | 9.4 | 9.3 | 11.4 | 11.3 |
| Baggage Volume Int. (cu. ft) | 11 | — | 20 | 20 |
| Cabin Volume (cu. ft) | — | — | 165 | 165 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 | — |