Beechcraft Bonanza G36 vs Cessna 206 Turbo Stationair vs Piper M350 vs Piper M600 Sls
In category, the Beechcraft Bonanza G36 is a high-performance, single‑engine piston aircraft (typically normally aspirated), suited to efficient personal and business travel. The Cessna Turbo Stationair is also a single‑engine piston aircraft but optimized for utility and load-carrying, with turbocharging helping it maintain performance at altitude. The Piper M350 is a pressurized, turbocharged single‑engine piston step-up, aimed at higher-altitude, more weather-capable traveling. The Piper M600 SLS moves into the single‑engine turboprop category, with substantially higher cruise speed and climb performance, plus more advanced automation. On range, the Bonanza G36 generally offers solid cross-country capability but is typically shorter-legged than the pressurized M350 and especially the M600 SLS. The Turbo Stationair’s range can be competitive depending on configuration and power settings, but it’s often chosen more for mission flexibility than maximum speed or distance. The M350 commonly provides longer, higher-altitude legs than the non-pressurized pistons, while the M600 SLS typically delivers the longest practical range of the group. For passenger capacity, the Bonanza G36 and M350 are commonly six-seat aircraft, the Turbo Stationair is often configured for six (sometimes more depending on version), and the M600 SLS typically seats up to six.
| Spec | Beechcraft Bonanza G36 | Cessna Turbo Stationair | Piper M350 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.16 | $ 1.08 | $ 1.34 | $ 2.19 |
| Total Seats | 6 | 6 | 6 | 6 |
| Flight Rules | VFR | VFR | VFR | IFR |
| Manufacturer | Beechcraft | Cessna | Piper | Piper |
| Aircraft Name | Bonanza G36 | 206 Turbo Stationair | M350 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 920 | 703 | 1343 | 1406 |
| DOC / nm / Seat | $ 0.19 | $ 0.18 | $ 0.22 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1050 | — | 1308 | 2200 |
| Standard Cabin Seats | 4 | 4 | 4 | 4 |
| Direct Operating Cost | $ 204 | $ 174 | $ 285 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 176 | 161 | 213 | 274 |
| Base Aircraft Price (USD) | $925,000 | $745,000 | $1,195,000 | $3,081,400 |
| Min Crew | — | — | — | 1 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 6 | 6 | 5 |
| Standard Cabin Seats | 4 | 4 | 4 | 4 |
| 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 | No | No | No |
| Model | IO-550-B | TIO-540-AJ1A | TIO-540-AE2A | PT6A-42A |
| Fuel Type | AvGas | AvGas | AvGas | — |
| TBO (hrs) | 1700 | 2000 | 2000 | 3600 |
| TBO (yrs) | 12 | 12 | 12 | — |
| Horsepower | 300 | 350 | 350 | 600 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Fuel Injected | — |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 74 | 87 | 120 | 260 |
| Flat Rating | — | — | — | ISA + 55 |
| Dimensions | ||||
| Length (ft) | 27.5 | 28.3 | 29 | 29.7 |
| Wingspan (ft) | 33.5 | 36 | 43 | 43.2 |
| Cabin Width (ft) | 3.5 | 3.6 | 4.1 | 4.1 |
| Cabin Height (ft) | 4.2 | 4.2 | 4 | 4 |
| Cabin Length (ft) | 12.6 | 12.1 | 12.3 | 12.3 |
| Overall Height (ft) | 8.6 | 9.4 | 11.4 | 11.3 |
| Cabin Volume (cu. ft) | 100 | — | 165 | 165 |
| Baggage Volume Int. (cu. ft) | 10 | 11 | 20 | 20 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 | — |