Beechcraft King Air 360er vs Daher Tbm 960 vs Leonardo Aw139 vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360ER and Pilatus PC-12 NGX are pressurized single-aisle turboprop airplanes aimed at efficient regional missions, while the Daher TBM 960 is a high-speed, owner-flown oriented single-engine turboprop, and the Leonardo AW139 is a twin‑engine medium helicopter suited to point-to-point access without runways. On range, the King Air 360ER is generally the longest-legged of the airplanes (roughly up to about 1,800–2,000 nm depending on load and reserves). The PC-12 NGX typically sits next (about 1,500–1,800 nm), while the TBM 960 offers similar but often slightly lower practical range when flown fast (about 1,200–1,700 nm). The AW139’s range is markedly shorter (commonly around 500–700 nm, mission dependent). For passenger capacity, the King Air 360ER usually seats around 6–9, the PC-12 NGX around 6–10, and the TBM 960 typically 4–6 in comfort. The AW139 can carry more people than the fixed-wing types, commonly around 8–12 passengers in VIP/utility configurations, with higher-density layouts possible.
| Spec | Beechcraft King Air 360ER | Daher TBM 960 | AGUSTA / LEONARDO AW139 | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 2.25 | $ 11.69 | $ 2.78 |
| Min Crew | 1 | 1 | 2 | 1 |
| Total Seats | 10 | 6 | 17 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Leonardo | Pilatus |
| Aircraft Name | KingAir 350ER | TBM 960 | AW139 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 1730 | 573 | 1803 |
| DOC / nm / Seat | $ 0.55 | $ 0.56 | $ 0.69 | $ 0.46 |
| Max Cabin Seats | 9 | — | 15 | 9 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6585 | 2908 | 4701 | — |
| Standard Cabin Seats | 8 | 4 | 15 | 6 |
| Direct Operating Cost | $ 1,324 | $ 744 | $ 1,929 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | EFIS | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 303 | 330 | 165 | 290 |
| Base Aircraft Price (USD) | $8,750,000 | $4,450,000 | $15,900,000 | $5,350,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | No | — | Optional |
| Min Crew | 1 | 1 | 2 | 1 |
| Cargo Door | Optional | — | — | Yes |
| Total Seats | 10 | 6 | 17 | 8 |
| Galley Location | FWD | MID | — | — |
| Max Cabin Seats | 9 | — | 15 | 9 |
| Lavatory Location | AFT | — | — | FWD |
| Cabin Pressure (psi) | 6.5 | 6.2 | — | 5.8 |
| Galley / Refreshment | Refreshment Center | — | — | No |
| Standard Cabin Seats | 8 | 4 | 15 | 6 |
| SL Cabin Altitude (ft) | — | 14390 | — | 13100 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | TBM 960 | PT6C-67C | PT6E-67XP |
| TBO (hrs) | 3600 | 3500 | 5000 | 5000 |
| Horsepower | 1050 | 850 | 1679 | 1200 |
| Flat Rating | ISA + 10 | ISA + 49 | — | ISA + 35 |
| No. of Engines | 1 | — | 2 | 1 |
| Fuel Capacity (gal) | 775 | — | 414 | — |
| Fuel Type | — | — | JetFuel | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 46.7 | 35.3 | 54.7 | 47.25 |
| Wingspan (ft) | 57.9 | 42.1 | — | 53.33 |
| Cabin Width (ft) | 4.5 | 4 | — | 5 |
| Cabin Height (ft) | 4.8 | 4.1 | — | 4.9 |
| Cabin Length (ft) | 19.5 | 13.4 | — | 16.9 |
| Overall Height (ft) | 14.4 | — | 16.4 | 14 |
| Cabin Width - Floor (ft) | 4.1 | — | — | 4.25 |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | — | — | 40 |
| Cabin Volume (cu. ft) | — | 123 | 282 | — |
| Rotor Diameter (ft) | — | — | 54.7 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 120 | — |