Beechcraft King Air 360 Er vs Pilatus Pc 24 vs Piper M600 Sls vs Sikorsky S 92
The Beechcraft King Air 360ER and Pilatus PC-24 are pressurized fixed‑wing business aircraft, while the Piper M600 SLS is a smaller pressurized single‑engine turboprop, and the Sikorsky S‑92 is a medium twin‑engine helicopter aimed at offshore, SAR, and VIP/utility roles. In range terms, the King Air 360ER is built for long turboprop legs, typically around 1,500–1,800 nautical miles depending on load and reserves, while the PC‑24 generally offers similar or somewhat greater reach, often around 1,700–2,000 nautical miles in typical mission profiles. The M600 SLS is shorter‑legged than the larger twins but still capable, commonly around 1,000–1,400 nautical miles. The S‑92’s range is much lower than the airplanes, typically roughly 500–700 nautical miles depending on tanks, payload, and reserves. For passengers, the King Air 360ER and PC‑24 usually seat about 6–10 in executive layouts (with the PC‑24 able to accommodate more in commuter configurations), the M600 SLS is generally 4–6 passengers plus a pilot, and the S‑92 commonly carries about 12–19 passengers depending on configuration.
| 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 |