Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore, search‑and‑rescue, and utility roles where vertical lift matters more than speed. Its range is typically on the order of a few hundred nautical miles (roughly 400–500 nm depending on mission fit and reserves) and it commonly carries around 16–19 passengers in transport layouts, with higher capacity possible in denser configurations. The Beechcraft King Air 360ER is a long‑range twin‑turboprop business/utility aircraft, optimized for efficient regional travel and short or unimproved runways. It offers roughly 1,500–1,800 nm of range and typically seats about 6–9 passengers in executive configurations. The Dassault Falcon 8X is an ultra‑long‑range tri‑jet business aircraft designed for intercontinental missions. It reaches about 6,400–6,500 nm and usually carries around 12–16 passengers, emphasizing cabin comfort and range. The Pilatus PC‑24 is a light jet with “super versatile” operations, combining jet speed with rough‑field and short‑runway capability. Its range is roughly 2,000 nm and it typically seats about 6–10 passengers.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | $ 3.71 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Pilatus |
| Aircraft Name | H225 | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 6680 |
| Standard Cabin Seats | 19 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 6 |
| Max Cabin Seats | 28 | 16 | 10 |
| Standard Cabin Seats | 19 | 14 | 6 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Crew Rest | — | No | No |
| Jump Seat | — | Yes | No |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD |
| Cabin Pressure (psi) | — | 10.2 | 9.3 |
| Galley / Refreshment | — | Galley | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 29200 | 23500 |
| Max Cabin Altitude (ft) | — | 3900 | — |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | 6722 | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 80.2 | 52.2 |
| Overall Height (ft) | 16.3 | 26.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — |
| Wingspan (ft) | — | 86.3 | 55.8 |
| Cabin Width (ft) | — | 7.7 | 5.6 |
| Cabin Height (ft) | — | 6.2 | 5.1 |
| Cabin Length (ft) | — | 42.7 | 23 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | 29.2 | 17 |
| Baggage Volume Int. (cu. ft) | — | 140 | 90 |
| Aisle Step (ft) | — | — | Flat Floor |