Leonardo Aw189 vs Piaggio Avanti Evo vs Piper M600 Sls
The Agusta/Leonardo AW189 is a twin‑engine medium helicopter built for offshore, SAR, and utility roles. In typical passenger transport fit it carries roughly 16–18 passengers and trades cruise speed for the ability to land vertically and operate from confined sites; range is generally on the order of about 450–500 nautical miles depending on reserves, payload, and configuration. The Piaggio Avanti EVO is a pressurized twin‑turboprop business aircraft optimized for fast regional trips. It typically seats about 7–9 passengers and offers longer point‑to‑point range than the helicopter, commonly around 1,400–1,800 nautical miles, with higher cruise speed and lower operating flexibility compared with VTOL. The Piper M600 SLS is a single‑engine, pressurized turboprop positioned as a personal/business aircraft with advanced avionics and autoland capability. It generally carries about 5–6 passengers and has a range often cited around 1,400–1,500 nautical miles. Compared with the Avanti, it carries fewer people and uses one engine; compared with the AW189, it offers far greater range but requires runway access.
| Spec | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | — | $ 2.19 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Leonardo | Piaggio | Piper |
| Aircraft Name | AW189 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.74 | — | $ 0.55 |
| Max Cabin Seats | 19 | 7 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Standard Cabin Seats | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,413 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 155 | 400 | 274 |
| Base Aircraft Price (USD) | $2,413,000 | $ 7,695,000 | $3,081,400 |
| Useful Load (lbs) | — | 3775 | 2200 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 5 |
| Max Cabin Seats | 19 | 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 | CT7-2E1 | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 3600 | 3600 |
| Horsepower | 1983 | 850 | 600 |
| No. of Engines | 2 | 2 | 1 |
| Flat Rating | — | ISA + 28 | ISA + 55 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 57.8 | 47.3 | 29.7 |
| Overall Height (ft) | 16.6 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | — | 165 |
| Baggage Volume Ext. (cu. ft) | 85 | — | — |
| 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 |