Airbus Helicopters H225 vs Beechcraft King Air 360er vs Bombardier Global 8000 vs Pilatus Pc 12 Ngx
The Airbus Helicopters H225 is a long‑range twin‑engine helicopter typically used for offshore transport, SAR, and utility missions. Compared with fixed‑wing aircraft, its category prioritizes vertical lift and hovering; its practical range is shorter than business aircraft, and typical passenger loads are in the mid‑teens depending on cabin fit. The Beechcraft King Air 360ER is a twin‑turboprop business/utility airplane optimized for efficiency and short/rougher runway access. It offers a longer range than most helicopters and generally carries about 6–11 passengers in executive layouts (higher in commuter configurations). The Pilatus PC‑12 NGX is a single‑turboprop utility/business aircraft known for rugged-field capability and low operating cost. Its range is broadly comparable to the King Air class, and it typically seats about 6–10 passengers in executive configurations. The Bombardier Global 8000 is an ultra‑long‑range business jet, delivering by far the greatest range of the four and a higher-speed intercontinental mission profile, with typical seating around 8–19 depending on cabin configuration.
| Spec | AIRBUS H225 | Beechcraft King Air 360ER | Bombardier Global 8000 | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 4.37 | $ 9.50 | $ 2.78 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 21 | 10 | 19 | 8 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Beechcraft | Bombardier | Pilatus |
| Aircraft Name | H225 | KingAir 350ER | Global 8000 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 2338 | 8000 | 1803 |
| DOC / nm / Seat | $ 0.99 | $ 0.55 | $ 0.79 | $ 0.46 |
| Max Cabin Seats | 28 | 9 | 19 | 9 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6585 | — | — |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 1,324 | $ 4,900 | $ 793 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line Fusion | Enhanced and Synthetic Vision Systems | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 142 | 303 | 626.7 | 290 |
| Base Aircraft Price (USD) | $ 29,500,000 | $8,750,000 | $78,000,000 | $5,350,000 |
| Aircraft Type | — | — | Business Jet | — |
| Max Passengers | — | — | 19 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 21 | 10 | 19 | 8 |
| Max Cabin Seats | 28 | 9 | 19 | 9 |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Lavatory | — | Yes (Belted Optional) | 2 Enclosed Flushing | Optional |
| Cargo Door | — | Optional | — | Yes |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | AFT | FWD / AFT | FWD |
| Cabin Pressure (psi) | — | 6.5 | — | 5.8 |
| Galley / Refreshment | — | Refreshment Center | Galley | No |
| Crew Rest | — | — | Yes | — |
| Jump Seat | — | — | Yes | — |
| Max Cabin Altitude (ft) | — | — | 2,900 | — |
| SL Cabin Altitude (ft) | — | — | — | 13100 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6A-60A | Passport | PT6E-67XP |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3600 | On-Condition | 5000 |
| Horsepower | 2100 | 1050 | — | 1200 |
| No. of Engines | 2 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 684 | 775 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 15 | ISA + 35 |
| Thrust (lbs) | — | — | 18920 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 63.4 | 46.7 | 111 | 47.25 |
| Overall Height (ft) | 16.3 | 14.4 | 27 | 14 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 57.9 | 104 | 53.33 |
| Cabin Width (ft) | — | 4.5 | 8 | 5 |
| Cabin Height (ft) | — | 4.8 | 6.2 | 4.9 |
| Cabin Length (ft) | — | 19.5 | 54.5 | 16.9 |
| Cabin Width - Floor (ft) | — | 4.1 | — | 4.25 |
| Cabin Length - Seating (ft) | — | 19.5 | — | — |
| Baggage Volume Int. (cu. ft) | — | 71 | — | 40 |