Piper M600 Sls vs Sikorsky S 92
The Piper M600 SLS and Sikorsky S-92 sit in entirely different aircraft categories. The M600 SLS is a single‑engine turboprop fixed‑wing airplane designed for owner‑pilots and small business travel, optimized for efficient point‑to‑point flights from runways. The S-92 is a twin‑engine, medium‑lift helicopter built for commercial and utility missions such as offshore transport, search and rescue, and VIP shuttle work, with the ability to operate without runways. In range terms, the M600 SLS typically offers longer point‑to‑point cruise range than a helicopter of similar size and is commonly quoted around roughly 1,400 nautical miles depending on payload and reserves, while an S-92 is generally in the several-hundred‑nautical‑mile class, often around 500–600 nautical miles depending on configuration and mission profile. Passenger capacity also differs substantially. The M600 SLS is usually configured for one pilot plus up to five passengers (about six seats total), whereas the S-92 commonly carries around 18–19 passengers plus crew, with layouts varying by operator.
| Spec | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piper | Sikorsky |
| Aircraft Name | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1406 | 439 |
| DOC / nm / Seat | $ 0.55 | $ 0.94 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2200 | 7417 |
| Standard Cabin Seats | 4 | 19 |
| Direct Operating Cost | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 274 | 155 |
| Base Aircraft Price (USD) | $3,081,400 | $30,650,000 |
| Max Cabin Seats | — | 19 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | — |
| Min Crew | 1 | 2 |
| Total Seats | 5 | 21 |
| Galley Location | MID | — |
| Cabin Pressure (psi) | 5.6 | — |
| Galley / Refreshment | Refreshment Centre | — |
| Standard Cabin Seats | 4 | 19 |
| SL Cabin Altitude (ft) | 12600 | — |
| Max Cabin Altitude (ft) | 8644 | — |
| Max Cabin Seats | — | 19 |
| Engine | ||
| FADEC | No | Yes |
| Model | PT6A-42A | CT7-8A |
| TBO (hrs) | 3600 | 4000 |
| Horsepower | 600 | 2520 |
| Flat Rating | ISA + 55 | — |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 260 | 760 |
| Fuel Type | — | JetFuel |
| Dimensions | ||
| Length (ft) | 29.7 | — |
| Wingspan (ft) | 43.2 | — |
| Cabin Width (ft) | 4.1 | — |
| Cabin Height (ft) | 4 | — |
| Cabin Length (ft) | 12.3 | — |
| Overall Height (ft) | 11.3 | 17.8 |
| Cabin Volume (cu. ft) | 165 | 775 |
| Baggage Volume Int. (cu. ft) | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | 140 |