Airbus Helicopters H225 vs Embraer Legacy 650 E vs Piaggio Avanti Evo vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter designed for offshore and utility missions rather than point‑to‑point executive travel. Its practical range is roughly in the 400–500 nautical mile class depending on payload and reserves, and it typically carries around 16–19 passengers in transport seating (fewer in VIP layouts). The Embraer Legacy 650E is a large‑cabin long‑range business jet, built for intercity and transcontinental flights, offering about 3,900 nautical miles of range and seating commonly for 13–14 passengers (up to about 19 certified, depending on configuration). The Piaggio Avanti EVO is a fast twin‑turboprop with a smaller cabin than the Legacy, optimized for efficiency and short‑field flexibility, delivering roughly 1,500–1,800 nautical miles of range and usually seating 6–9 passengers. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑operators, with about 1,400–1,500 nautical miles of range and typically 4–6 passengers plus a pilot, prioritizing simplicity and operating cost over cabin size.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio | Piper |
| Aircraft Name | H225 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.55 |
| Max Cabin Seats | 28 | 7 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 3775 | 2200 |
| Standard Cabin Seats | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 400 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 8 | 5 |
| Max Cabin Seats | 28 | 7 | — |
| Standard Cabin Seats | 19 | 6 | 4 |
| Lavatory | — | No | No |
| Cabin Pressure (psi) | — | 9 | 5.6 |
| Galley / Refreshment | — | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | 6600 | 8644 |
| Galley Location | — | — | MID |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3600 | 3600 |
| Horsepower | 2100 | 850 | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 28 | ISA + 55 |
| Fuel Burn (gph) | — | 100 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 47.3 | 29.7 |
| Overall Height (ft) | 16.3 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 |
| Wingspan (ft) | — | 47.1 | 43.2 |
| Cabin Width (ft) | — | 6.1 | 4.1 |
| Cabin Height (ft) | — | 5.8 | 4 |
| Cabin Length (ft) | — | 14.9 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 20 |