Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Daher Tbm 960 vs Dassault Falcon 8x
The Airbus H225 is a long‑range, heavy twin‑engine helicopter suited to offshore transport and utility missions rather than fixed‑wing business travel. It typically carries around 19 passengers in a high‑density layout and offers practical ranges on the order of roughly 400–600 nautical miles depending on payload, reserves, and mission profile. The Beechcraft King Air 360ER is a twin‑turboprop business/utility aircraft aimed at regional trips and remote airfields, usually configured for about 8–11 passengers, with an extended range roughly around 1,500–1,800 nautical miles. The Daher TBM 960 is a single‑engine turboprop optimized for speed and owner‑pilot efficiency, generally seating about 4–6 passengers (up to 6 plus pilot) and providing about 1,000–1,400 nautical miles of range depending on speed and payload. The Dassault Falcon 8X is an ultra‑long‑range tri‑jet business aircraft, typically carrying about 12–16 passengers in executive layouts and capable of roughly 6,450 nautical miles, enabling intercontinental nonstop missions.
| Spec | AIRBUS H225 | Daher TBM 960 | Dassault Falcon 8X |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 7.66 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 17 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Dassault Falcon |
| Aircraft Name | H225 | TBM 960 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.64 |
| Max Cabin Seats | 28 | — | 16 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 36900 |
| Standard Cabin Seats | 19 | 4 | 14 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 62,500,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 17 |
| Max Cabin Seats | 28 | — | 16 |
| Standard Cabin Seats | 19 | 4 | 14 |
| Lavatory | — | No | 2 Enclosed Flushing |
| Galley Location | — | MID | FWD |
| Cabin Pressure (psi) | — | 6.2 | 10.2 |
| SL Cabin Altitude (ft) | — | 14390 | 29200 |
| Crew Rest | — | — | No |
| Jump Seat | — | — | Yes |
| Lavatory Location | — | — | FWD / AFT |
| Galley / Refreshment | — | — | Galley |
| Max Cabin Altitude (ft) | — | — | 3900 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PW307D |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | On-Condition |
| Horsepower | 2100 | 850 | — |
| No. of Engines | 2 | — | 3 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 49 | ISA + 17 |
| Thrust (lbs) | — | — | 6722 |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | 80.2 |
| Overall Height (ft) | 16.3 | — | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 1695 |
| Wingspan (ft) | — | 42.1 | 86.3 |
| Cabin Width (ft) | — | 4 | 7.7 |
| Cabin Height (ft) | — | 4.1 | 6.2 |
| Cabin Length (ft) | — | 13.4 | 42.7 |
| Cabin Width - Floor (ft) | — | — | 6.3 |
| Cabin Length - Seating (ft) | — | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | — | 140 |