Airbus Helicopters H225 vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Piper M600 Sls
The Airbus H225 is a twin‑engine helicopter aimed at offshore, SAR, and utility missions rather than point‑to‑point business travel. It typically carries a large cabin load (often around 16–19 passengers in transport layouts) but has a much shorter range than the jets and turboprops here, generally only a few hundred nautical miles depending on payload and reserves. The Dassault Falcon 8X is a long‑range, tri‑jet business aircraft optimized for intercontinental trips. It offers the greatest range of the group (roughly 6,000+ nautical miles) with a typical executive cabin for about 12–16 passengers, emphasizing comfort and nonstop city pairs. The Piaggio Avanti EVO is a fast twin‑turboprop business aircraft designed for efficient regional travel. It usually seats about 6–9 passengers and delivers midrange capability (roughly 1,200–1,700 nautical miles, mission‑dependent). The Piper M600 SLS is a single‑engine turboprop positioned for owner‑operators. It generally carries about 5–6 passengers plus a pilot, with range in the ballpark of 1,000–1,500 nautical miles depending on configuration.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | — | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 8 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Piaggio | Piper |
| Aircraft Name | H225 | 8X | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 7 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 3775 | 2200 |
| Standard Cabin Seats | 19 | 14 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 400 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $ 7,695,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 8 | 5 |
| Max Cabin Seats | 28 | 16 | 7 | — |
| Standard Cabin Seats | 19 | 14 | 6 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No | No |
| Crew Rest | — | No | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | MID |
| Lavatory Location | — | FWD / AFT | — | — |
| Cabin Pressure (psi) | — | 10.2 | 9 | 5.6 |
| Galley / Refreshment | — | Galley | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 29200 | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | 3900 | 6600 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | PW307D | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 | 3600 |
| Horsepower | 2100 | — | 850 | 600 |
| No. of Engines | 2 | 3 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 17 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | — | 6722 | — | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 47.3 | 29.7 |
| Overall Height (ft) | 16.3 | 26.1 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — | 165 |
| Wingspan (ft) | — | 86.3 | 47.1 | 43.2 |
| Cabin Width (ft) | — | 7.7 | 6.1 | 4.1 |
| Cabin Height (ft) | — | 6.2 | 5.8 | 4 |
| Cabin Length (ft) | — | 42.7 | 14.9 | 12.3 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.5 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 35.2 | 20 |