Airbus Helicopters H225 vs Beechcraft King Air 360 vs Beechcraft King Air 360er vs Bombardier Global 8000 vs Pilatus Pc 12 Ngx
The Airbus Helicopters H225 is a heavy, twin‑engine helicopter suited to offshore, search‑and‑rescue, and utility missions. It typically carries about 16–19 passengers in transport layouts and offers roughly 400–500 nautical miles of practical range, trading speed and range for vertical‑lift access. The Beechcraft King Air 360 is a twin‑turboprop business aircraft aimed at short to medium regional trips. It generally seats 6–9 passengers in executive configuration and flies about 1,800 nautical miles. The King Air 360ER keeps similar cabin capacity but extends endurance with additional fuel, pushing range to roughly 2,500 nautical miles, making it better for longer legs or loiter missions. The Bombardier Global 8000 is an ultra‑long‑range business jet built for intercontinental travel. It typically accommodates 8–19 passengers depending on layout and reaches about 8,000 nautical miles, far exceeding the turboprops in speed and nonstop distance. The Pilatus PC‑12 NGX is a single‑engine turboprop known for efficiency and rough‑field capability. It commonly carries 6–9 passengers and offers around 1,600–1,800 nautical miles of range.
| Spec | AIRBUS H225 | Beechcraft King Air 360 | Beechcraft King Air 360ER | Bombardier Global 8000 | Pilatus PC-12 NGX |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 4.20 | $ 4.37 | $ 9.50 | $ 2.78 |
| Min Crew | 2 | 1 | 1 | 4 | 1 |
| Total Seats | 21 | 10 | 10 | 19 | 8 |
| Flight Rules | IFR | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Beechcraft | Beechcraft | Bombardier | Pilatus |
| Aircraft Name | H225 | KingAir 350i | KingAir 350ER | Global 8000 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1560 | 2338 | 8000 | 1803 |
| DOC / nm / Seat | $ 0.99 | $ 0.53 | $ 0.55 | $ 0.79 | $ 0.46 |
| Max Cabin Seats | 28 | 9 | 9 | 19 | 9 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 5145 | 6585 | — | — |
| Standard Cabin Seats | 19 | 8 | 8 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 1,311 | $ 1,324 | $ 4,900 | $ 793 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Enhanced and Synthetic Vision Systems | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 142 | 312 | 303 | 626.7 | 290 |
| Base Aircraft Price (USD) | $ 29,500,000 | $7,650,000 | $8,750,000 | $78,000,000 | $5,350,000 |
| Aircraft Type | — | — | — | Business Jet | — |
| Max Passengers | — | — | — | 19 | — |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 4 | 1 |
| Total Seats | 21 | 10 | 10 | 19 | 8 |
| Max Cabin Seats | 28 | 9 | 9 | 19 | 9 |
| Standard Cabin Seats | 19 | 8 | 8 | 12 | 6 |
| Lavatory | — | Optional | Yes (Belted Optional) | 2 Enclosed Flushing | Optional |
| Galley Location | — | FWD | FWD | FWD | — |
| Lavatory Location | — | AFT | AFT | FWD / AFT | FWD |
| Cabin Pressure (psi) | — | 6.5 | 6.5 | — | 5.8 |
| Galley / Refreshment | — | Optional | Refreshment Center | Galley | No |
| Cargo Door | — | — | Optional | — | Yes |
| Crew Rest | — | — | — | Yes | — |
| Jump Seat | — | — | — | Yes | — |
| Max Cabin Altitude (ft) | — | — | — | 2,900 | — |
| SL Cabin Altitude (ft) | — | — | — | — | 13100 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6A-60A | PT6A-60A | Passport | PT6E-67XP |
| Fuel Type | JetFuel | — | — | — | — |
| TBO (hrs) | 3500 | 3600 | 3600 | On-Condition | 5000 |
| Horsepower | 2100 | 1050 | 1050 | — | 1200 |
| No. of Engines | 2 | 1 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 684 | 539 | 775 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 10 | ISA + 15 | ISA + 35 |
| Thrust (lbs) | — | — | — | 18920 | — |
| Usable Fuel (gal) | — | — | — | — | 402 |
| Dimensions | |||||
| Length (ft) | 63.4 | 46.7 | 46.7 | 111 | 47.25 |
| Overall Height (ft) | 16.3 | 14.4 | 14.4 | 27 | 14 |
| Rotor Diameter (ft) | 53.2 | — | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — | — |
| Wingspan (ft) | — | 57.9 | 57.9 | 104 | 53.33 |
| Cabin Width (ft) | — | 4.5 | 4.5 | 8 | 5 |
| Cabin Height (ft) | — | 4.8 | 4.8 | 6.2 | 4.9 |
| Cabin Length (ft) | — | 19.5 | 19.5 | 54.5 | 16.9 |
| Cabin Width - Floor (ft) | — | 4.1 | 4.1 | — | 4.25 |
| Cabin Length - Seating (ft) | — | 19.5 | 19.5 | — | — |
| Baggage Volume Int. (cu. ft) | — | 71 | 71 | — | 40 |