Cirrus Sf50 G2 vs Daher Tbm 910 vs Piper M500
The Cirrus Vision Jet G2, Daher TBM 910, and Piper M500 occupy different niches in the personal aircraft market. By category, the Vision Jet G2 is a single-engine very light jet designed for simplified jet ownership and typically flown at higher altitudes and speeds than the turboprops. The TBM 910 and M500 are single-engine turboprops; the TBM 910 is a higher-performance, faster cross-country platform, while the M500 is positioned as a more straightforward, value-oriented pressurized turboprop. On range, the TBM 910 generally offers the longest legs, commonly around 1,500–1,700 nautical miles depending on configuration and reserves. The Vision Jet G2 is typically in the middle, roughly around 1,000–1,200 nautical miles. The M500 is usually similar to or somewhat shorter than the Vision Jet, often around 1,000–1,300 nautical miles, again depending on load and conditions. For passenger capacity, all are usually configured for a pilot plus four to six occupants. The Vision Jet can seat up to seven (including an optional side-facing “jump seat”), while the TBM 910 and M500 are commonly six-seat cabins.
| Spec | Daher TBM 910 | 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 910 | 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 G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 330 | 260 |
| Base Aircraft Price (USD) | $4,250,000 | $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 Burn (gph) | 37 | — |
| 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 |