Beechcraft Kingair Denali vs Daher Tbm 910 vs Pilatus 12
The Beechcraft Denali and the Daher TBM 910 sit in different turboprop categories, which drives most of their practical differences. The Denali is aimed at the larger single‑engine utility/cabin-class turboprop niche (a step toward “small twin” cabin comfort in a single), while the TBM 910 is a high‑performance, owner‑flown single focused on speed and efficient personal travel. On range, the TBM 910 typically offers longer real-world trip capability than most cabin-class singles in its size because it is optimized for fast, efficient cruise, making it well suited to longer nonstop business legs. The Denali is expected to deliver competitive range for its class, but its design emphasis on a larger cabin and higher payload flexibility can trade some maximum-range optimization versus the TBM’s performance-first approach. For passenger capacity, both are commonly operated with a pilot plus several passengers, but the Denali is generally positioned to accommodate more people more comfortably thanks to a larger cabin and a more utility-oriented interior, whereas the TBM 910 usually seats fewer and prioritizes travel speed over cabin volume.
| Spec | Beechcraft KingAir Denali | Daher TBM 910 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.08 | $ 2.25 |
| Min Crew | 1 | 1 |
| Total Seats | 11 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | GE® Aerospace | Daher TBM |
| Aircraft Name | KingAir Denali | TBM 910 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1730 |
| DOC / nm / Seat | $ 0.68 | $ 0.56 |
| Max Cabin Seats | 9 | — |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3280 | 2908 |
| Standard Cabin Seats | 7 | 4 |
| Direct Operating Cost | $ 1,111 | $ 744 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 285 | 330 |
| Base Aircraft Price (USD) | $4,150,000 | $4,250,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Flushing | No |
| Min Crew | 1 | 1 |
| Total Seats | 11 | 6 |
| Max Cabin Seats | 9 | — |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 5 | 6.2 |
| Galley / Refreshment | No | Refreshment Centre |
| Standard Cabin Seats | 7 | 4 |
| SL Cabin Altitude (ft) | 11065 | 14390 |
| Galley Location | — | MID |
| Engine | ||
| Model | Catalyst™ | PT6A-66D |
| No. of Engines | 1 | 1 |
| FADEC | — | Yes |
| TBO (hrs) | — | 3500 |
| Horsepower | — | 850 |
| Flat Rating | — | ISA + 49 |
| Fuel Burn (gph) | — | 37 |
| Fuel Capacity (gal) | — | 291 |
| Dimensions | ||
| Length (ft) | 14.86 | 35.3 |
| Wingspan (ft) | 54.3 | 42.1 |
| Cabin Width (ft) | 4.5 | 4 |
| Cabin Height (ft) | 4.8 | 4.1 |
| Cabin Length (ft) | 12.6 | 13.4 |
| Overall Height (ft) | 4.65 | 14.3 |
| Cabin Width - Floor (ft) | 4.1 | — |
| Cabin Length - Seating (ft) | 12.6 | — |
| Baggage Volume Int. (cu. ft) | 48 | 30 |
| Cabin Volume (cu. ft) | — | 123 |