Airbus Helicopters H225 vs Dassault Falcon 8x vs Piper M600 Sls vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Dassault Falcon 8X and Piper M600 SLS are fixed‑wing aircraft, so their strengths differ sharply. For category, the H225 is a large, twin‑engine heavy helicopter suited to offshore, SAR, and utility missions; the R66 is a light single‑engine turbine helicopter aimed at personal, training, and light commercial use. The Falcon 8X is an ultra‑long‑range tri‑jet business aircraft designed for intercontinental travel, whereas the M600 SLS is a single‑engine turboprop personal/business aircraft optimized for simpler operations and shorter business trips. On range, the Falcon 8X is the clear leader at roughly 6,450 nautical miles, enabling nonstop long‑haul routes. The M600 SLS is typically around 1,600 nautical miles. Helicopters trail fixed‑wing aircraft: the H225 is roughly in the 450–500 nautical mile class (mission dependent), and the R66 is typically around 300–350 nautical miles. For passenger capacity, the H225 can carry a large cabin load, commonly up to about 19 passengers, the Falcon 8X typically seats around 12–16, the M600 SLS usually carries up to 5 passengers plus a pilot, and the R66 seats about 4 passengers plus a pilot.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | $ 2.19 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Piper |
| Aircraft Name | H225 | 8X | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 2200 |
| Standard Cabin Seats | 19 | 14 | 4 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 5 |
| Max Cabin Seats | 28 | 16 | — |
| Standard Cabin Seats | 19 | 14 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | 5.6 |
| Galley / Refreshment | — | Galley | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 29200 | 12600 |
| Max Cabin Altitude (ft) | — | 3900 | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | PW307D | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | — | 600 |
| No. of Engines | 2 | 3 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 17 | ISA + 55 |
| Thrust (lbs) | — | 6722 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 80.2 | 29.7 |
| Overall Height (ft) | 16.3 | 26.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | 165 |
| Wingspan (ft) | — | 86.3 | 43.2 |
| Cabin Width (ft) | — | 7.7 | 4.1 |
| Cabin Height (ft) | — | 6.2 | 4 |
| Cabin Length (ft) | — | 42.7 | 12.3 |
| Cabin Width - Floor (ft) | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 20 |