Piper M500 vs Cirrus Sf50 G2 vs Daher Tbm 940
The Piper M500 is a single‑engine turboprop positioned as an owner‑flown personal and business aircraft, typically offering a practical range around 1,000–1,300 nautical miles depending on payload and reserves, and seating generally for five to six occupants in a pressurized cabin. The Daher TBM 940 is also a single‑engine turboprop but sits in a higher performance tier, commonly delivering roughly 1,400–1,700 nautical miles of range in typical cruise planning, with seating usually for up to six (often arranged as four to six plus pilot), emphasizing speed, avionics, and efficiency for longer legs. The Cirrus SF50 Vision Jet G2 is a single‑engine very light jet, trading some turboprop short‑field utility for jet smoothness and higher-altitude cruise; its typical range is roughly 1,100–1,200 nautical miles, and it is commonly configured for five passengers plus a pilot (with certain configurations accommodating up to seven total seats). Overall, the TBM 940 tends to lead on range and cruise capability, the M500 targets accessible turboprop ownership, and the SF50 G2 provides entry‑level jet experience with competitive passenger flexibility.
| 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 |