Beechcraft Baron G58 vs Cessna 206 Turbo Stationair vs Piper M350
The Beechcraft Baron G58 is a piston twin aimed at owner-operators who prioritize redundancy and speed in the personal and light business category. It typically seats five to six people depending on configuration, and offers a solid mid-range cross-country capability, generally around 900–1,300 nautical miles with reserves depending on power settings and payload. The Cessna Turbo Stationair is a high-wing, turbocharged single positioned as a rugged utility and family/business traveler with strong short/rough-field flexibility. It commonly seats six, can be configured for more utility-focused loading, and its range is usually in a similar or slightly shorter band than the Baron, often roughly 700–1,200 nautical miles depending on model year, tanks, and load. The Piper M350 is a pressurized, turbocharged single designed for higher-altitude, all-weather personal and business travel. It generally seats six, and tends to deliver the longest practical range of the three, often around 1,000–1,400 nautical miles, with the added comfort and capability of pressurization for longer trips.
| Spec | Beechcraft Baron G58 | Cessna Turbo Stationair | Piper M350 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | $ 1.08 | $ 1.34 |
| Total Seats | 6 | 6 | 6 |
| Flight Rules | IFR | VFR | VFR |
| Manufacturer | Beechcraft | Cessna | Piper |
| Aircraft Name | Baron G58 | 206 Turbo Stationair | M350 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 703 | 1343 |
| DOC / nm / Seat | $ 0.29 | $ 0.18 | $ 0.22 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 1450 | — | 1308 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Direct Operating Cost | $ 347 | $ 174 | $ 285 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 202 | 161 | 213 |
| Base Aircraft Price (USD) | $1,495,000 | $745,000 | $1,195,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Total Seats | 6 | 6 | 6 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Cabin Pressure (psi) | — | — | 5.6 |
| Engine | |||
| FADEC | No | No | No |
| Model | IO-550-C | TIO-540-AJ1A | TIO-540-AE2A |
| Fuel Type | AvGas | AvGas | AvGas |
| TBO (hrs) | 1700 | 2000 | 2000 |
| TBO (yrs) | 12 | 12 | 12 |
| Horsepower | 300 | 350 | 350 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Fuel Injected |
| No. of Engines | 2 | 1 | 1 |
| Fuel Capacity (gal) | 194 | 87 | 120 |
| Dimensions | |||
| Length (ft) | 29.9 | 28.3 | 29 |
| Wingspan (ft) | 37.9 | 36 | 43 |
| Cabin Width (ft) | 3.5 | 3.6 | 4.1 |
| Cabin Height (ft) | 4.2 | 4.2 | 4 |
| Cabin Length (ft) | 12.6 | 12.1 | 12.3 |
| Overall Height (ft) | 9.8 | 9.4 | 11.4 |
| Cabin Volume (cu. ft) | 150 | — | 165 |
| Baggage Volume Int. (cu. ft) | 46 | 11 | 20 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 |