Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Pilatus Pc 24 vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft optimized for regional missions; it offers roughly 1,800 nautical miles of range and typically carries about 6 to 9 passengers in an executive layout. The Dassault Falcon 8X is a long‑range tri‑jet business jet in a higher category, designed for intercontinental travel; it can fly about 6,450 nautical miles and commonly seats around 12 to 16 passengers depending on cabin configuration. The Pilatus PC‑24 is a light business jet valued for versatility and short/rough‑field capability; it provides approximately 2,000 nautical miles of range and usually accommodates about 6 to 10 passengers in corporate use (with higher-density layouts possible). The Sikorsky S‑92 is a large twin‑engine helicopter used for offshore, VIP, and utility transport; its range is typically around 500 nautical miles (mission and fuel-fit dependent) and it generally carries about 12 to 19 passengers. Overall, the Falcon 8X leads on range and cabin size, the King Air 360ER and PC‑24 cover medium-range business needs with different performance tradeoffs, and the S‑92 trades speed and range for vertical access.
| Spec | Dassault Falcon 8X | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 17 | 6 | 21 |
| Manufacturer | Dassault Falcon | Pilatus | Sikorsky |
| Aircraft Name | 8X | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 2076 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 16 | 10 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 6680 | 7417 |
| Standard Cabin Seats | 14 | 6 | 19 |
| Direct Operating Cost | $ 3,805 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 516 | 440 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $11,800,000 | $30,650,000 |
| Flight Rules | — | — | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Flushing | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | No | No | — |
| Jump Seat | Yes | No | — |
| Total Seats | 17 | 6 | 21 |
| Galley Location | FWD | FWD | — |
| Max Cabin Seats | 16 | 10 | 19 |
| Lavatory Location | FWD / AFT | FWD | — |
| Cabin Pressure (psi) | 10.2 | 9.3 | — |
| Galley / Refreshment | Galley | Optional Refreshment Center | — |
| Standard Cabin Seats | 14 | 6 | 19 |
| SL Cabin Altitude (ft) | 29200 | 23500 | — |
| Max Cabin Altitude (ft) | 3900 | — | — |
| Cargo Door | — | Yes | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PW307D | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | On-Condition | 5000 | 4000 |
| Flat Rating | ISA + 17 | ISA + 23 | — |
| Thrust (lbs) | 6722 | 3435 | — |
| No. of Engines | 3 | 2 | 1 |
| Fuel Type | — | — | JetFuel |
| Horsepower | — | — | 2520 |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 80.2 | 52.2 | — |
| Wingspan (ft) | 86.3 | 55.8 | — |
| Cabin Width (ft) | 7.7 | 5.6 | — |
| Cabin Height (ft) | 6.2 | 5.1 | — |
| Cabin Length (ft) | 42.7 | 23 | — |
| Overall Height (ft) | 26.1 | 17.4 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | — | 775 |
| Cabin Width - Floor (ft) | 6.3 | 3.8 | — |
| Cabin Length - Seating (ft) | 29.2 | 17 | — |
| Baggage Volume Int. (cu. ft) | 140 | 90 | — |
| Aisle Step (ft) | — | Flat Floor | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |