Daher Tbm 910 vs Pilatus Pc 12 Ngx vs Piper M500 vs Piper M600 Sls
In category, the Daher TBM 910 and Piper M500 are fastest-oriented single‑engine turboprop personal/owner‑pilot aircraft, while the Piper M600 SLS sits a step up as a higher‑powered, more premium personal turboprop with advanced safety/automation features. The Pilatus PC‑12 NGX is in a larger “utility/executive” single‑engine turboprop category, designed to carry more people and baggage with a more versatile cabin. On range, the TBM 910 is generally the longest‑legged of this group and is optimized for high‑speed, long‑distance travel. The PC‑12 NGX and M600 SLS are typically in a similar long‑range bracket, well suited to cross‑country missions, with the PC‑12 often favored when payload and cabin volume matter more than outright speed. The M500 is usually the shortest‑range of the four, though still capable of solid cross‑country trips. For passenger capacity, the PC‑12 NGX typically carries the most (often up to about 8–10 seats depending on configuration), the M600 SLS commonly seats around 6, and the TBM 910 and M500 are usually configured around 4–6 seats.
| Spec | Daher TBM 910 | Pilatus PC-12 NGX | Piper M500 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.78 | $ 3.11 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 6 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Pilatus | Piper | Piper |
| Aircraft Name | TBM 910 | PC-12 NGX | M500 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1803 | 1000 | 1406 |
| DOC / nm / Seat | $ 0.56 | $ 0.46 | $ 0.78 | $ 0.55 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 2908 | — | 1698 | 2200 |
| Standard Cabin Seats | 4 | 6 | 4 | 4 |
| Direct Operating Cost | $ 744 | $ 793 | $ 579 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Honeywell Primus Apex | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 290 | 260 | 274 |
| Base Aircraft Price (USD) | $4,250,000 | $5,350,000 | $2,122,600 | $3,081,400 |
| Max Cabin Seats | — | 9 | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | Optional | No | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 5 | 5 |
| Galley Location | MID | — | MID | MID |
| Cabin Pressure (psi) | 6.2 | 5.8 | 5.5 | 5.6 |
| Galley / Refreshment | Refreshment Centre | No | Refreshment Centre | Refreshment Centre |
| Standard Cabin Seats | 4 | 6 | 4 | 4 |
| SL Cabin Altitude (ft) | 14390 | 13100 | 12600 | 12600 |
| Cargo Door | — | Yes | — | — |
| Max Cabin Seats | — | 9 | — | — |
| Lavatory Location | — | FWD | — | — |
| Max Cabin Altitude (ft) | — | — | 8244 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | No | No |
| Model | PT6A-66D | PT6E-67XP | PT6A-42A | PT6A-42A |
| TBO (hrs) | 3500 | 5000 | 3600 | 3600 |
| Horsepower | 850 | 1200 | 500 | 600 |
| Flat Rating | ISA + 49 | ISA + 35 | ISA + 55 | ISA + 55 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Burn (gph) | 37 | — | — | — |
| Fuel Capacity (gal) | 291 | — | 170 | 260 |
| Usable Fuel (gal) | — | 402 | — | — |
| Dimensions | ||||
| Length (ft) | 35.3 | 47.25 | 29.6 | 29.7 |
| Wingspan (ft) | 42.1 | 53.33 | 43.2 | 43.2 |
| Cabin Width (ft) | 4 | 5 | 4.1 | 4.1 |
| Cabin Height (ft) | 4.1 | 4.9 | 4 | 4 |
| Cabin Length (ft) | 13.4 | 16.9 | 12.3 | 12.3 |
| Overall Height (ft) | 14.3 | 14 | 11.3 | 11.3 |
| Cabin Volume (cu. ft) | 123 | — | 165 | 165 |
| Baggage Volume Int. (cu. ft) | 30 | 40 | 20 | 20 |
| Cabin Width - Floor (ft) | — | 4.25 | — | — |