Cirrus Sf50 G2 vs Daher Tbm 940 vs Piper M500
The Cirrus Vision Jet G2 is a single‑engine very light jet aimed at owner‑pilots wanting jet speed and simplicity. It typically seats up to seven (including the pilot, with a smaller rear seat), and offers a practical range of roughly 1,000–1,200 nautical miles depending on load and reserves. The Daher TBM 940 is a high‑performance single‑engine turboprop, often considered a step up in cruise speed and overall capability versus many personal aircraft. It generally carries four to six people in comfort (up to six seats plus pilot, depending on configuration) and delivers about 1,400–1,700 nautical miles of range, again varying with payload and conditions. The Piper M500 is a single‑engine turboprop positioned as a more accessible entry into the pressurized turboprop category. It typically seats five to six (including the pilot) and offers around 1,000–1,300 nautical miles of range. In short, the Vision Jet emphasizes jet experience with moderate range, the TBM 940 leads in speed and longer legs, and the M500 focuses on value and straightforward turboprop capability.
| Spec | Daher TBM 940 | Piper M500 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.25 | $ 3.11 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Daher TBM | Piper |
| Aircraft Name | TBM 940 | M500 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1000 |
| DOC / nm / Seat | $ 0.56 | $ 0.78 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | 1698 |
| Standard Cabin Seats | 4 | 4 |
| Direct Operating Cost | $ 744 | $ 579 |
| Flight Deck (Base Spec) | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 330 | 260 |
| Base Aircraft Price (USD) | $4,450,000 | $2,122,600 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | No |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 5 |
| Galley Location | MID | MID |
| Cabin Pressure (psi) | 6.2 | 5.5 |
| Galley / Refreshment | Refreshment Centre | Refreshment Centre |
| Standard Cabin Seats | 4 | 4 |
| SL Cabin Altitude (ft) | 14390 | 12600 |
| Max Cabin Altitude (ft) | — | 8244 |
| Engine | ||
| FADEC | Yes | No |
| Model | PT6A-66D | PT6A-42A |
| TBO (hrs) | 3500 | 3600 |
| Horsepower | 850 | 500 |
| Flat Rating | ISA + 49 | ISA + 55 |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 291 | 170 |
| Dimensions | ||
| Length (ft) | 35.3 | 29.6 |
| Wingspan (ft) | 42.1 | 43.2 |
| Cabin Width (ft) | 4 | 4.1 |
| Cabin Height (ft) | 4.1 | 4 |
| Cabin Length (ft) | 13.4 | 12.3 |
| Overall Height (ft) | 14.3 | 11.3 |
| Cabin Volume (cu. ft) | 123 | 165 |
| Baggage Volume Int. (cu. ft) | 30 | 20 |