Airbus Helicopters H225 vs Daher Tbm 960 vs Dassault Falcon 8x
The Airbus H225 is a long‑range twin‑engine helicopter designed for missions such as offshore transport and search‑and‑rescue rather than point‑to‑point business travel. Its practical range is roughly in the 450–600 nautical mile class depending on payload and reserves, and it typically carries about 16–19 passengers in a transport configuration (fewer in VIP layouts). The Daher TBM 960 is a single‑engine turboprop airplane optimized for fast, efficient personal and light business travel. It offers an IFR range around 1,400–1,700 nautical miles depending on power settings and conditions, and it generally seats up to 6 passengers plus a pilot, with the most common real‑world load being 2–4 passengers plus bags. The Dassault Falcon 8X is an ultra‑long‑range tri‑jet business aircraft built for intercontinental missions. Its range is about 6,450 nautical miles, and typical cabin layouts accommodate about 12–16 passengers, with a maximum configuration around 19.
| 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 |