Beechcraft King Air 360 Er vs Embraer Legacy 650 E vs Pilatus Pc 24 vs Sikorsky S 92
The Beechcraft King Air 360ER is a pressurized twin‑turboprop typically used for regional corporate and utility missions, offering roughly 1,500–1,800 nautical miles of range and usually seating about 6–9 passengers in executive layouts. The Pilatus PC‑24 is a light business jet designed for versatility, including operation from shorter or less‑prepared runways, with about 2,000 nautical miles of range and generally 6–10 passengers depending on configuration. The Embraer Legacy 650E is a large‑cabin long‑range business jet aimed at intercontinental-style missions, providing around 3,900 nautical miles of range and commonly accommodating 10–13 passengers in a high-comfort cabin. The Sikorsky S‑92 is a medium heavy twin‑engine helicopter focused on offshore, VIP, and search-and-rescue roles; it trades speed and range for vertical lift capability, typically offering about 500–600 nautical miles of range and seating often around 12–19 passengers depending on interior and mission equipment. Overall, the Legacy 650E leads on range and cabin size, the PC‑24 balances jet performance with field capability, the King Air 360ER emphasizes efficient regional turboprop operations, and the S‑92 uniquely enables point-to-point access without runways.
| Spec | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.71 | $ 19.79 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 21 |
| Manufacturer | Pilatus | Sikorsky |
| Aircraft Name | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2076 | 439 |
| DOC / nm / Seat | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 10 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6680 | 7417 |
| Standard Cabin Seats | 6 | 19 |
| Direct Operating Cost | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 440 | 155 |
| Base Aircraft Price (USD) | $11,800,000 | $30,650,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | — |
| Min Crew | 1 | 2 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Cargo Door | Yes | — |
| Total Seats | 6 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 10 | 19 |
| Lavatory Location | FWD | — |
| Cabin Pressure (psi) | 9.3 | — |
| Galley / Refreshment | Optional Refreshment Center | — |
| Standard Cabin Seats | 6 | 19 |
| SL Cabin Altitude (ft) | 23500 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | 5000 | 4000 |
| Flat Rating | ISA + 23 | — |
| Thrust (lbs) | 3435 | — |
| No. of Engines | 2 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 52.2 | — |
| Wingspan (ft) | 55.8 | — |
| Aisle Step (ft) | Flat Floor | — |
| Cabin Width (ft) | 5.6 | — |
| Cabin Height (ft) | 5.1 | — |
| Cabin Length (ft) | 23 | — |
| Overall Height (ft) | 17.4 | 17.8 |
| Cabin Width - Floor (ft) | 3.8 | — |
| Cabin Length - Seating (ft) | 17 | — |
| Baggage Volume Int. (cu. ft) | 90 | — |
| Cabin Volume (cu. ft) | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |