Beechcraft King Air 360er vs Daher Tbm 960 vs Leonardo Aw109 Grand New vs Leonardo Aw139 vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360ER and Pilatus PC-12 NGX are pressurized single-/twin‑turboprop business aircraft suited to flexible regional missions. The King Air 360ER is a twin‑engine turboprop with a long-range “ER” focus, generally offering roughly 1,500–1,800 nm capability depending on load and reserves, and typically seats about 6–9 passengers in executive layouts. The PC‑12 NGX is a single‑engine turboprop known for efficiency and short/rough‑field versatility, commonly offering about 1,500–1,800 nm range and typically 6–9 passengers, with higher-density configurations possible. The Daher TBM 960 is a high‑performance single‑engine turboprop optimized for speed with a smaller cabin; it typically carries about 4–6 passengers and offers roughly 1,200–1,700 nm range depending on profile. The Leonardo AW109 Grand New and AW139 are twin‑engine helicopters. The AW109 is a light helicopter with typical ranges around 400–500 nm and usually 5–7 passengers in VIP use. The AW139 is a medium helicopter with greater cabin volume, typically 6–12 passengers, and about 500–700 nm range depending on configuration.
| Spec | Beechcraft King Air 360ER | Daher TBM 960 | AGUSTA / LEONARDO AW109 Grand New | AGUSTA / LEONARDO AW139 | Pilatus PC-12 NGX |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 2.25 | $ 7.31 | $ 11.69 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Total Seats | 10 | 6 | 8 | 17 | 8 |
| Flight Rules | IFR | IFR | VFR | IFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Leonardo | Leonardo | Pilatus |
| Aircraft Name | KingAir 350ER | TBM 960 | AW109 Grand New | AW139 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 1730 | 464 | 573 | 1803 |
| DOC / nm / Seat | $ 0.55 | $ 0.56 | $ 0.91 | $ 0.69 | $ 0.46 |
| Max Cabin Seats | 9 | — | 6 | 15 | 9 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6585 | 2908 | — | 4701 | — |
| Standard Cabin Seats | 8 | 4 | 6 | 15 | 6 |
| Direct Operating Cost | $ 1,324 | $ 744 | $ 1,140 | $ 1,929 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | EFIS | EFIS | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 303 | 330 | 156 | 165 | 290 |
| Base Aircraft Price (USD) | $8,750,000 | $4,450,000 | $ 7,800,000 | $15,900,000 | $5,350,000 |
| Aircraft Type | — | Turbo Prop | — | — | — |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | No | — | — | Optional |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Cargo Door | Optional | — | — | — | Yes |
| Total Seats | 10 | 6 | 8 | 17 | 8 |
| Galley Location | FWD | MID | — | — | — |
| Max Cabin Seats | 9 | — | 6 | 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 | 6 | 15 | 6 |
| SL Cabin Altitude (ft) | — | 14390 | — | — | 13100 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | TBM 960 | PW207C | PT6C-67C | PT6E-67XP |
| TBO (hrs) | 3600 | 3500 | 4000 | 5000 | 5000 |
| Horsepower | 1050 | 850 | 735 | 1679 | 1200 |
| Flat Rating | ISA + 10 | ISA + 49 | — | — | ISA + 35 |
| No. of Engines | 1 | — | 2 | 2 | 1 |
| Fuel Capacity (gal) | 775 | — | 152 | 414 | — |
| Fuel Type | — | — | JetFuel | JetFuel | — |
| Usable Fuel (gal) | — | — | — | — | 402 |
| Dimensions | |||||
| Length (ft) | 46.7 | 35.3 | 42.5 | 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 | — | 11.5 | 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) | — | — | 35.5 | 54.7 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 120 | — |