Leonardo Aw189 vs Piper M600 Sls vs Robinson R66
The Agusta/Leonardo AW189 and Robinson R66 are helicopters, while the Piper M600 SLS is a single‑engine fixed‑wing turboprop, so their strengths differ by mission. The AW189 is a medium twin‑engine helicopter suited to offshore, SAR, and utility transport, typically offering the most passenger capacity of the three (commonly up to the mid‑teens in high‑density layouts, with fewer in executive configuration) and solid all‑around range for a helicopter. The Robinson R66 is a light single‑engine helicopter aimed at lower-cost operations; it carries fewer people (pilot plus up to four passengers) and generally has the shortest range and payload capability here, but offers rotorcraft access and flexibility. The Piper M600 SLS is optimized for point‑to‑point travel; it typically carries one pilot plus up to five passengers and, compared with either helicopter, usually delivers substantially longer range and higher cruise speed, making it better for regional trips between runways rather than landing close to the destination.
| Spec | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 15.57 | $ 2.19 |
| Min Crew | 1 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Leonardo | Piper |
| Aircraft Name | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1406 |
| DOC / nm / Seat | $ 0.74 | $ 0.55 |
| Max Cabin Seats | 19 | — |
| OEM Verification | Un-Verified | VERIFIED |
| Standard Cabin Seats | 19 | 4 |
| Direct Operating Cost | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 155 | 274 |
| Base Aircraft Price (USD) | $2,413,000 | $3,081,400 |
| Useful Load (lbs) | — | 2200 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 21 | 5 |
| Max Cabin Seats | 19 | — |
| 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 | CT7-2E1 | PT6A-42A |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | 3600 |
| Horsepower | 1983 | 600 |
| No. of Engines | 2 | 1 |
| Flat Rating | — | ISA + 55 |
| Fuel Capacity (gal) | — | 260 |
| Dimensions | ||
| Length (ft) | 57.8 | 29.7 |
| Overall Height (ft) | 16.6 | 11.3 |
| Rotor Diameter (ft) | 48 | — |
| Cabin Volume (cu. ft) | 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 |