Airbus Helicopters H225 vs Embraer Legacy 650 E vs Enstrom 480b vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter designed for offshore, search‑and‑rescue, and utility missions rather than point‑to‑point business travel. It typically carries a large cabin load (often well over a dozen passengers depending on interior and mission fit) and offers medium helicopter range, generally a few hundred nautical miles with reserves, optimized for lifting and endurance more than speed. The Embraer Legacy 650E is a long‑range large‑cabin business jet built for intercity and intercontinental missions. It commonly seats around 13 passengers in executive configuration and can fly roughly 3,900 nautical miles, emphasizing comfort, baggage volume, and nonstop range. The Enstrom 480B is a light single‑engine piston helicopter suited to training, patrol, and short utility flights. It typically carries about 4–5 occupants and has short‑to‑moderate helicopter range, roughly a few hundred nautical miles. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft. It generally seats up to 6 and offers midrange capability, about 1,400 nautical miles, balancing efficiency with cabin comfort.
| Spec | AIRBUS H225 | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.19 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piper |
| Aircraft Name | H225 | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.55 |
| Max Cabin Seats | 28 | — |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2200 |
| Standard Cabin Seats | 19 | 4 |
| Direct Operating Cost | $ 2,963 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $3,081,400 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 5 |
| Max Cabin Seats | 28 | — |
| Standard Cabin Seats | 19 | 4 |
| Lavatory | — | No |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 5.6 |
| Galley / Refreshment | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 12600 |
| Max Cabin Altitude (ft) | — | 8644 |
| Engine | ||
| FADEC | Yes | No |
| Model | Makila 2A1 | PT6A-42A |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3600 |
| Horsepower | 2100 | 600 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | 684 | 260 |
| Flat Rating | — | ISA + 55 |
| Dimensions | ||
| Length (ft) | 63.4 | 29.7 |
| Overall Height (ft) | 16.3 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 165 |
| Wingspan (ft) | — | 43.2 |
| Cabin Width (ft) | — | 4.1 |
| Cabin Height (ft) | — | 4 |
| Cabin Length (ft) | — | 12.3 |
| Baggage Volume Int. (cu. ft) | — | 20 |