Beechcraft King Air 360 vs Daher Tbm 960 vs Leonardo Aw109 Grand New vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360 and Pilatus PC-12 NGX are pressurized single-/twin‑turboprop business aircraft suited to short and medium regional missions, while the Daher TBM 960 is a high‑performance single‑turboprop optimized for fast owner‑pilot travel, and the Leonardo AW109 Grand New is a light twin‑engine helicopter focused on point‑to‑point access and vertical operations. In range, the TBM 960 typically leads among the fixed‑wing options at roughly 1,500–1,700 nm depending on configuration, followed by the PC‑12 NGX around 1,500 nm. The King Air 360 is generally in the ~1,300–1,500 nm class, varying with payload and reserves. The AW109 Grand New’s range is much shorter in absolute terms, commonly around 400–500 nm, reflecting helicopter performance and reserves. For passenger capacity, the King Air 360 and PC‑12 NGX usually seat about 6–9 passengers in executive layouts, with the PC‑12 also offering higher-density commuter or utility configurations. The TBM 960 is typically 4–6 passengers plus pilot. The AW109 Grand New generally carries about 6–7 passengers plus one or two pilots.
| Spec | Beechcraft King Air 360 | Daher TBM 960 | AGUSTA / LEONARDO AW109 Grand New | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 2.25 | $ 7.31 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 8 | 8 |
| Flight Rules | IFR | IFR | VFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Leonardo | Pilatus |
| Aircraft Name | KingAir 350i | TBM 960 | AW109 Grand New | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 1730 | 464 | 1803 |
| DOC / nm / Seat | $ 0.53 | $ 0.56 | $ 0.91 | $ 0.46 |
| Max Cabin Seats | 9 | — | 6 | 9 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 5145 | 2908 | — | — |
| Standard Cabin Seats | 8 | 4 | 6 | 6 |
| Direct Operating Cost | $ 1,311 | $ 744 | $ 1,140 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | EFIS | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 312 | 330 | 156 | 290 |
| Base Aircraft Price (USD) | $7,650,000 | $4,450,000 | $ 7,800,000 | $5,350,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Optional | No | — | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 8 | 8 |
| Galley Location | FWD | MID | — | — |
| Max Cabin Seats | 9 | — | 6 | 9 |
| Lavatory Location | AFT | — | — | FWD |
| Cabin Pressure (psi) | 6.5 | 6.2 | — | 5.8 |
| Galley / Refreshment | Optional | — | — | No |
| Standard Cabin Seats | 8 | 4 | 6 | 6 |
| SL Cabin Altitude (ft) | — | 14390 | — | 13100 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | TBM 960 | PW207C | PT6E-67XP |
| TBO (hrs) | 3600 | 3500 | 4000 | 5000 |
| Horsepower | 1050 | 850 | 735 | 1200 |
| Flat Rating | ISA + 10 | ISA + 49 | — | ISA + 35 |
| No. of Engines | 1 | — | 2 | 1 |
| Fuel Capacity (gal) | 539 | — | 152 | — |
| Fuel Type | — | — | JetFuel | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 46.7 | 35.3 | 42.5 | 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 | — | 11.5 | 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 | — | — |
| Rotor Diameter (ft) | — | — | 35.5 | — |