Airbus Helicopters H225 vs Daher Tbm 960 vs Dassault Falcon 8x vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Daher TBM 960 and Dassault Falcon 8X are fixed‑wing airplanes. The H225 is a large twin‑engine rotorcraft used for offshore transport and SAR; it typically carries roughly 16–19 passengers and offers a practical range on the order of about 400–500 nautical miles depending on configuration. The Robinson R66 is a light single‑engine helicopter aimed at utility and private use; it generally seats 4–5 and has a shorter range, roughly 300–350 nautical miles. The TBM 960 is a single‑engine turboprop airplane optimized for fast owner‑operation; it usually carries 4–6 passengers (up to about 6–7 seats including pilot) and can reach roughly 1,400–1,700 nautical miles. The Falcon 8X is a long‑range tri‑jet business aircraft designed for intercontinental missions; it commonly carries 8–14 passengers depending on cabin layout and has a range around 6,000+ nautical miles, far exceeding the others.
| 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 |