Daher Tbm 910 vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Daher TBM 910 is a single‑engine turboprop optimized for owner‑pilot efficiency and speed, fitting the personal and light business travel category. It offers a typical IFR range on the order of about 1,500–1,700 nautical miles depending on reserves, payload, and cruise settings, and is generally configured for around 4–6 passengers plus a pilot (with maximum seating typically higher but more constrained by comfort and weight). The Pilatus PC‑12 NGX is also a single‑engine turboprop, but it sits a class above in cabin volume and utility, often used as a corporate shuttle and rugged utility platform. Its typical range is broadly similar, roughly about 1,500–1,800 nautical miles, but it can comfortably carry more people and bags, commonly 6–9 passengers plus a pilot. The Pilatus PC‑24 is a light jet, aimed at faster point‑to‑point business missions and “jet to more places” operations. Its range is typically around 1,800–2,000 nautical miles, and it usually seats about 6–8 passengers plus crew, trading turboprop field performance for higher cruise speed and jet comfort.
| Spec | Daher TBM 910 | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Daher TBM | Pilatus | Pilatus |
| Aircraft Name | TBM 910 | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.56 | $ 0.46 | $ 0.62 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 2908 | — | 6680 |
| Standard Cabin Seats | 4 | 6 | 6 |
| Direct Operating Cost | $ 744 | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 330 | 290 | 440 |
| Base Aircraft Price (USD) | $4,250,000 | $5,350,000 | $11,800,000 |
| Max Cabin Seats | — | 9 | 10 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 6 |
| Galley Location | MID | — | FWD |
| Cabin Pressure (psi) | 6.2 | 5.8 | 9.3 |
| Galley / Refreshment | Refreshment Centre | No | Optional Refreshment Center |
| Standard Cabin Seats | 4 | 6 | 6 |
| SL Cabin Altitude (ft) | 14390 | 13100 | 23500 |
| Cargo Door | — | Yes | Yes |
| Max Cabin Seats | — | 9 | 10 |
| Lavatory Location | — | FWD | FWD |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-66D | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 3500 | 5000 | 5000 |
| Horsepower | 850 | 1200 | — |
| Flat Rating | ISA + 49 | ISA + 35 | ISA + 23 |
| No. of Engines | 1 | 1 | 2 |
| Fuel Burn (gph) | 37 | — | — |
| Fuel Capacity (gal) | 291 | — | — |
| Usable Fuel (gal) | — | 402 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 35.3 | 47.25 | 52.2 |
| Wingspan (ft) | 42.1 | 53.33 | 55.8 |
| Cabin Width (ft) | 4 | 5 | 5.6 |
| Cabin Height (ft) | 4.1 | 4.9 | 5.1 |
| Cabin Length (ft) | 13.4 | 16.9 | 23 |
| Overall Height (ft) | 14.3 | 14 | 17.4 |
| Cabin Volume (cu. ft) | 123 | — | — |
| Baggage Volume Int. (cu. ft) | 30 | 40 | 90 |
| Cabin Width - Floor (ft) | — | 4.25 | 3.8 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | 17 |