Airbus Helicopters H225 vs Dassault Falcon 8x vs Embraer Legacy 650 E vs Piper M600 Sls
The Airbus H225 is a heavy, twin‑engine helicopter, suited to offshore and utility missions rather than long nonstop fixed‑wing travel. Its practical range is roughly around 500–700 nautical miles depending on payload and reserves, and it typically carries about 16–19 passengers (with layouts varying by mission and safety requirements). The Dassault Falcon 8X is an ultra‑long‑range large‑cabin business jet designed for intercontinental missions, with a range around 6,450 nautical miles and typical seating for about 12–16 passengers (certified higher, depending on configuration). The Embraer Legacy 650E is a large‑cabin, long‑range business jet positioned below the 8X for nonstop reach, offering about 3,900–4,000 nautical miles of range and typically seating around 13 passengers. The Piper M600 SLS is a single‑engine turboprop (personal/business aircraft), optimized for owner‑pilot operations and short to midrange trips, with roughly 1,400 nautical miles of range and seating for up to 6 occupants (commonly 5–6 including the 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 |