Leonardo Aw189 vs Piper M600 Sls vs Sikorsky S 92
The Leonardo (Agusta) AW189 and Sikorsky S-92 are medium twin‑engine helicopters aimed at offshore, SAR, and utility missions, while the Piper M600 SLS is a single‑engine turboprop fixed‑wing aircraft optimized for personal and business travel. In range terms, the M600 SLS typically offers the longest point‑to‑point capability (roughly on the order of 1,000+ nautical miles depending on reserves and load), because fixed‑wing cruise efficiency is higher than rotorcraft. The AW189 and S-92 generally have shorter ranges than the Piper but are designed to lift and loiter, with typical mission radii suited to offshore legs rather than long nonstop travel; among the helicopters, the S-92 is often configured for longer overwater legs than many AW189 layouts, depending on tanks and payload. Passenger capacity differs sharply: the M600 SLS is usually flown with 1 pilot and up to 5 passengers (six seats total), the AW189 commonly seats around 16–19 passengers in high‑density transport configurations, and the larger S-92 is often configured around 19 passengers (with some layouts higher or lower based on role and equipment).
| Spec | AGUSTA / LEONARDO AW189 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Leonardo | Piper | Sikorsky |
| Aircraft Name | AW189 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1406 | 439 |
| DOC / nm / Seat | $ 0.74 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 19 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Standard Cabin Seats | 19 | 4 | 19 |
| Direct Operating Cost | $ 2,413 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 155 | 274 | 155 |
| Base Aircraft Price (USD) | $2,413,000 | $3,081,400 | $30,650,000 |
| Useful Load (lbs) | — | 2200 | 7417 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 5 | 21 |
| Max Cabin Seats | 19 | — | 19 |
| Standard Cabin Seats | 19 | 4 | 19 |
| 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 | Yes |
| Model | CT7-2E1 | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 3600 | 4000 |
| Horsepower | 1983 | 600 | 2520 |
| No. of Engines | 2 | 1 | 1 |
| Flat Rating | — | ISA + 55 | — |
| Fuel Capacity (gal) | — | 260 | 760 |
| Dimensions | |||
| Length (ft) | 57.8 | 29.7 | — |
| Overall Height (ft) | 16.6 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | 165 | 775 |
| Baggage Volume Ext. (cu. ft) | 85 | — | 140 |
| Wingspan (ft) | — | 43.2 | — |
| Cabin Width (ft) | — | 4.1 | — |
| Cabin Height (ft) | — | 4 | — |
| Cabin Length (ft) | — | 12.3 | — |
| Baggage Volume Int. (cu. ft) | — | 20 | — |