Beechcraft Kingair 250 vs Daher Tbm 910 vs Pilatus Pc 12 Ngx
The Beechcraft King Air 260 is a twin‑engine turboprop positioned as a short‑ to mid‑range business and utility aircraft, valued for redundancy and strong all‑weather, multi‑mission capability. Its typical range is in the roughly 1,500–1,700 nautical mile class depending on load and conditions, and it generally accommodates about six to nine passengers in executive layouts, with maximum seating varying by configuration. The Daher TBM 910 is a single‑engine turboprop optimized for speed and efficient point‑to‑point travel in the light business category. It typically offers the longest range of the three—around the 1,700–1,900 nautical mile class—and usually carries four to six passengers comfortably (often up to six seats plus a pilot, depending on interior). The Pilatus PC‑12 NGX is a larger single‑engine turboprop in the utility/executive category, known for cabin volume, cargo flexibility, and unimproved‑strip capability. Its range is generally similar to the King Air 260 (about 1,500–1,800 nautical miles), but it usually offers the highest practical passenger and cabin capacity, commonly six to nine passengers with options for more in commuter-style seating.
| Spec | Daher TBM 910 | Pilatus PC-12 NGX |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.78 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Daher TBM | Pilatus |
| Aircraft Name | TBM 910 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1803 |
| DOC / nm / Seat | $ 0.56 | $ 0.46 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | — |
| Standard Cabin Seats | 4 | 6 |
| Direct Operating Cost | $ 744 | $ 793 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 330 | 290 |
| Base Aircraft Price (USD) | $4,250,000 | $5,350,000 |
| Max Cabin Seats | — | 9 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | Optional |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 8 |
| Galley Location | MID | — |
| Cabin Pressure (psi) | 6.2 | 5.8 |
| Galley / Refreshment | Refreshment Centre | No |
| Standard Cabin Seats | 4 | 6 |
| SL Cabin Altitude (ft) | 14390 | 13100 |
| Cargo Door | — | Yes |
| Max Cabin Seats | — | 9 |
| Lavatory Location | — | FWD |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-66D | PT6E-67XP |
| TBO (hrs) | 3500 | 5000 |
| Horsepower | 850 | 1200 |
| Flat Rating | ISA + 49 | ISA + 35 |
| No. of Engines | 1 | 1 |
| Fuel Burn (gph) | 37 | — |
| Fuel Capacity (gal) | 291 | — |
| Usable Fuel (gal) | — | 402 |
| Dimensions | ||
| Length (ft) | 35.3 | 47.25 |
| Wingspan (ft) | 42.1 | 53.33 |
| Cabin Width (ft) | 4 | 5 |
| Cabin Height (ft) | 4.1 | 4.9 |
| Cabin Length (ft) | 13.4 | 16.9 |
| Overall Height (ft) | 14.3 | 14 |
| Cabin Volume (cu. ft) | 123 | — |
| Baggage Volume Int. (cu. ft) | 30 | 40 |
| Cabin Width - Floor (ft) | — | 4.25 |