Pilatus Pc 24 vs Piper M600 Sls vs Sikorsky S 92
The Pilatus PC-24 is a twin‑engine light business jet designed for short to medium trips with jet speed and strong short/rough‑field capability. Typical range is roughly 1,900–2,000 nautical miles depending on load and conditions, and it commonly carries about 6–8 passengers in an executive layout (with higher maximum seating in commuter configurations). The Piper M600 SLS is a single‑engine turboprop aimed at owner‑pilots and efficient regional travel rather than pure speed. Its range is typically around 1,400–1,500 nautical miles, and it usually seats 4–6 passengers plus a pilot, favoring lower operating costs and access to smaller airports. The Sikorsky S‑92 is a large twin‑engine helicopter built for offshore transport, search and rescue, and utility missions where vertical lift matters more than speed or runway access. Its range is generally on the order of 500–600 nautical miles, and it can carry about 19 passengers in typical transport seating, trading distance and cruise efficiency for VTOL capability and mission flexibility.
| Spec | Pilatus PC-24 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 3.71 | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 6 | 6 | 21 |
| Manufacturer | Pilatus | Piper | Sikorsky |
| Aircraft Name | PC-24 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2076 | 1406 | 439 |
| DOC / nm / Seat | $ 0.62 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 10 | — | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6680 | 2200 | 7417 |
| Standard Cabin Seats | 6 | 4 | 19 |
| Direct Operating Cost | $ 1,619 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Pilatus ACE (Primus Apex) | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 440 | 274 | 155 |
| Base Aircraft Price (USD) | $11,800,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | No | — |
| Min Crew | 1 | 1 | 2 |
| Crew Rest | No | — | — |
| Jump Seat | No | — | — |
| Cargo Door | Yes | — | — |
| Total Seats | 6 | 5 | 21 |
| Galley Location | FWD | MID | — |
| Max Cabin Seats | 10 | — | 19 |
| Lavatory Location | FWD | — | — |
| Cabin Pressure (psi) | 9.3 | 5.6 | — |
| Galley / Refreshment | Optional Refreshment Center | Refreshment Centre | — |
| Standard Cabin Seats | 6 | 4 | 19 |
| SL Cabin Altitude (ft) | 23500 | 12600 | — |
| Max Cabin Altitude (ft) | — | 8644 | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | FJ44-4A-QPM | PT6A-42A | CT7-8A |
| TBO (hrs) | 5000 | 3600 | 4000 |
| Flat Rating | ISA + 23 | ISA + 55 | — |
| Thrust (lbs) | 3435 | — | — |
| No. of Engines | 2 | 1 | 1 |
| Horsepower | — | 600 | 2520 |
| Fuel Capacity (gal) | — | 260 | 760 |
| Fuel Type | — | — | JetFuel |
| Dimensions | |||
| Length (ft) | 52.2 | 29.7 | — |
| Wingspan (ft) | 55.8 | 43.2 | — |
| Aisle Step (ft) | Flat Floor | — | — |
| Cabin Width (ft) | 5.6 | 4.1 | — |
| Cabin Height (ft) | 5.1 | 4 | — |
| Cabin Length (ft) | 23 | 12.3 | — |
| Overall Height (ft) | 17.4 | 11.3 | 17.8 |
| Cabin Width - Floor (ft) | 3.8 | — | — |
| Cabin Length - Seating (ft) | 17 | — | — |
| Baggage Volume Int. (cu. ft) | 90 | 20 | — |
| Cabin Volume (cu. ft) | — | 165 | 775 |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |