Beechcraft King Air 260 vs Beechcraft Kingair Denali vs Daher Tbm 910 vs Pilatus Pc 12 Ngx
In category, the Beechcraft King Air 260 is a twin‑engine turboprop, typically chosen for redundancy, short/medium missions, and flexible utility. The Beechcraft King Air Denali is a newer‑generation single‑engine turboprop positioned as a modern, high‑performance alternative with simplified operations compared with twins. The Daher TBM 910 is also a single‑engine turboprop, oriented toward fast, owner‑pilot travel and efficient point‑to‑point flying. The Pilatus PC‑12 NGX is a single‑engine turboprop known for rugged utility, cabin volume, and operating from shorter or less‑developed runways. On range, the TBM 910 generally emphasizes longer, faster business trips for its size class, while the PC‑12 NGX also offers long range but often with greater payload flexibility. The King Air 260 typically covers solid mid‑range missions with twin‑engine capability, and the Denali is aimed at competitive long‑range single‑engine missions, though final figures depend on certification and configuration. For passenger capacity, the PC‑12 NGX and King Air 260 commonly seat more passengers in typical layouts than the TBM 910, while the Denali is expected to fall in the same general mid‑cabin class as other premium singles, with seating driven by interior choices.
| Spec | Beechcraft King Air 260 | Beechcraft KingAir Denali | Daher TBM 910 | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.08 | $ 2.25 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 11 | 6 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | GE® Aerospace | Daher TBM | Pilatus |
| Aircraft Name | KingAir 250 | KingAir Denali | TBM 910 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1600 | 1730 | 1803 |
| DOC / nm / Seat | $ 0.72 | $ 0.68 | $ 0.56 | $ 0.46 |
| Max Cabin Seats | 8 | 9 | — | 9 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3760 | 3280 | 2908 | — |
| Standard Cabin Seats | 6 | 7 | 4 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,111 | $ 744 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 310 | 285 | 330 | 290 |
| Base Aircraft Price (USD) | $6,450,000 | $4,150,000 | $4,250,000 | $5,350,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Flushing | No | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 11 | 6 | 8 |
| Max Cabin Seats | 8 | 9 | — | 9 |
| Lavatory Location | AFT | AFT | — | FWD |
| Cabin Pressure (psi) | 6.5 | 5 | 6.2 | 5.8 |
| Galley / Refreshment | No | No | Refreshment Centre | No |
| Standard Cabin Seats | 6 | 7 | 4 | 6 |
| SL Cabin Altitude (ft) | 15293 | 11065 | 14390 | 13100 |
| Galley Location | — | — | MID | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | PT6A-52 | Catalyst™ | PT6A-66D | PT6E-67XP |
| TBO (hrs) | 3600 | — | 3500 | 5000 |
| Horsepower | 850 | — | 850 | 1200 |
| Flat Rating | ISA + 37 | — | ISA + 49 | ISA + 35 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 544 | — | 291 | — |
| Fuel Burn (gph) | — | — | 37 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 43.8 | 14.86 | 35.3 | 47.25 |
| Wingspan (ft) | 57.9 | 54.3 | 42.1 | 53.33 |
| Cabin Width (ft) | 4.5 | 4.5 | 4 | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.1 | 4.9 |
| Cabin Length (ft) | 16.7 | 12.6 | 13.4 | 16.9 |
| Overall Height (ft) | 14.8 | 4.65 | 14.3 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | — | 4.25 |
| Cabin Length - Seating (ft) | 16.7 | 12.6 | — | — |
| Baggage Volume Int. (cu. ft) | 55 | 48 | 30 | 40 |
| Cabin Volume (cu. ft) | — | — | 123 | — |