Airbus Helicopters H225 vs Embraer Legacy 650 E vs Leonardo Aw189 vs Piper M600 Sls
The Airbus H225 and Leonardo AW189 are large, twin‑engine helicopters suited to offshore, SAR, and utility missions. Their practical range is broadly similar—typically a few hundred nautical miles depending on payload and reserves—while passenger capacity is high for rotorcraft, commonly in the mid‑teens to around twenty in high‑density seating; the H225 is generally the larger/heavier-lift option, with the AW189 slightly smaller but still in the same class. The Embraer Legacy 650E is a long‑range business jet, optimized for fast point‑to‑point travel. It has far greater range than the helicopters, typically in the several‑thousand‑nautical‑mile class, and carries roughly a dozen to low‑teens passengers in an executive layout. The Piper M600 SLS is a single‑engine turboprop, a much smaller category aimed at owner‑pilots and short to mid‑range trips. Its range is typically around the low‑thousands of nautical miles (mission‑dependent), with seating generally up to six including the pilot.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Piper |
| Aircraft Name | H225 | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | $ 0.55 |
| Max Cabin Seats | 28 | 19 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 2200 |
| Standard Cabin Seats | 19 | 19 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 155 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 5 |
| Max Cabin Seats | 28 | 19 | — |
| Standard Cabin Seats | 19 | 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 | Yes | No |
| Model | Makila 2A1 | CT7-2E1 | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 3600 |
| Horsepower | 2100 | 1983 | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | — | ISA + 55 |
| Dimensions | |||
| Length (ft) | 63.4 | 57.8 | 29.7 |
| Overall Height (ft) | 16.3 | 16.6 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 48 | — |
| Cabin Volume (cu. ft) | 547 | 395 | 165 |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |
| Wingspan (ft) | — | — | 43.2 |
| Cabin Width (ft) | — | — | 4.1 |
| Cabin Height (ft) | — | — | 4 |
| Cabin Length (ft) | — | — | 12.3 |
| Baggage Volume Int. (cu. ft) | — | — | 20 |