Airbus Helicopters H225 vs Dassault Falcon 8x vs Piper M600 Sls
The Airbus H225 is a twin‑engine heavy helicopter, typically chosen for offshore, search‑and‑rescue, and utility missions where vertical lift and hover matter more than speed. Its range is generally in the few‑hundred‑nautical‑mile class (often roughly 400–600 nm depending on tanks and payload), and it can carry a large group, commonly around 19 passengers in high‑density seating, though layouts vary widely by mission. The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel. It offers about 6,000+ nm of range and usually seats about 12–16 passengers in typical executive configurations, prioritizing comfort, speed, and nonstop city‑pair flexibility. The Piper M600 SLS is a single‑engine turboprop, positioned as a high‑performance personal/corporate aircraft. Its range is roughly around 1,000–1,500 nm depending on reserves and payload, and it typically carries 5–6 occupants (one pilot plus passengers), trading cabin size and speed for lower operating cost and simpler ownership.
| 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 |