Beechcraft King Air 360er vs Daher Tbm 910 vs Daher Tbm 960 vs Pilatus Pc 12 Ngx
All four are pressurized turboprops aimed at owner-operators and small-business missions, but they split into two categories. The Beechcraft King Air 360ER and Pilatus PC-12 NGX are larger “utility/light business” turboprops, while the Daher TBM 910 and TBM 960 are “high-performance single-engine” turboprops optimized for speed and efficiency. On range, the King Air 360ER is the standout for long legs, commonly cited around 1,800–2,000 nm depending on payload and reserves. The PC-12 NGX is also a long-range aircraft, typically around 1,600–1,800 nm. The TBM 910 and TBM 960 generally offer shorter but still substantial range, often about 1,400–1,700 nm depending on cruise settings and loading, with the 960 broadly similar in reach but optimized with updated systems and performance. On passenger capacity, the King Air 360ER typically seats the most in practical use, commonly 7–9 (up to about 11 with certain configurations). The PC-12 NGX is usually 6–9 (maximum around 10). The TBM 910 and TBM 960 are typically 4–6 passengers plus the pilot.
| Spec | Beechcraft King Air 360ER | Daher TBM 910 | Daher TBM 960 | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 2.25 | $ 2.25 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 6 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Daher TBM | Pilatus |
| Aircraft Name | KingAir 350ER | TBM 910 | TBM 960 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 1730 | 1730 | 1803 |
| DOC / nm / Seat | $ 0.55 | $ 0.56 | $ 0.56 | $ 0.46 |
| Max Cabin Seats | 9 | — | — | 9 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6585 | 2908 | 2908 | — |
| Standard Cabin Seats | 8 | 4 | 4 | 6 |
| Direct Operating Cost | $ 1,324 | $ 744 | $ 744 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Garmin G3000 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 303 | 330 | 330 | 290 |
| Base Aircraft Price (USD) | $8,750,000 | $4,250,000 | $4,450,000 | $5,350,000 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | No | No | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | Optional | — | — | Yes |
| Total Seats | 10 | 6 | 6 | 8 |
| Galley Location | FWD | MID | MID | — |
| Max Cabin Seats | 9 | — | — | 9 |
| Lavatory Location | AFT | — | — | FWD |
| Cabin Pressure (psi) | 6.5 | 6.2 | 6.2 | 5.8 |
| Galley / Refreshment | Refreshment Center | Refreshment Centre | — | No |
| Standard Cabin Seats | 8 | 4 | 4 | 6 |
| SL Cabin Altitude (ft) | — | 14390 | 14390 | 13100 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | PT6A-66D | TBM 960 | PT6E-67XP |
| TBO (hrs) | 3600 | 3500 | 3500 | 5000 |
| Horsepower | 1050 | 850 | 850 | 1200 |
| Flat Rating | ISA + 10 | ISA + 49 | ISA + 49 | ISA + 35 |
| No. of Engines | 1 | 1 | — | 1 |
| Fuel Capacity (gal) | 775 | 291 | — | — |
| Fuel Burn (gph) | — | 37 | — | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 46.7 | 35.3 | 35.3 | 47.25 |
| Wingspan (ft) | 57.9 | 42.1 | 42.1 | 53.33 |
| Cabin Width (ft) | 4.5 | 4 | 4 | 5 |
| Cabin Height (ft) | 4.8 | 4.1 | 4.1 | 4.9 |
| Cabin Length (ft) | 19.5 | 13.4 | 13.4 | 16.9 |
| Overall Height (ft) | 14.4 | 14.3 | — | 14 |
| Cabin Width - Floor (ft) | 4.1 | — | — | 4.25 |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | 30 | — | 40 |
| Cabin Volume (cu. ft) | — | 123 | 123 | — |