Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop fixed‑wing aircraft typically used for regional business travel, utility missions, and short to mid‑range operations from smaller airports. It offers a practical range on the order of roughly 1,500–1,800 nautical miles (depending on payload and conditions) and commonly carries about 6–9 passengers in a business layout. The Dassault Falcon 8X is a long‑range, large‑cabin tri‑jet business aircraft designed for intercontinental travel at higher speed and altitude. Its range is about 6,400–6,450 nautical miles, and it generally seats around 12–16 passengers, with maximum configurations higher. The Sikorsky S‑92 is a medium‑lift twin‑engine helicopter used for offshore transport, search and rescue, and VIP or utility roles where vertical takeoff and landing matters more than speed. Its range is far shorter, typically around 500–600 nautical miles, and it usually carries about 12–19 passengers depending on configuration.
| Spec | Dassault Falcon 8X | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 7.66 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 17 | 21 |
| Manufacturer | Dassault Falcon | Sikorsky |
| Aircraft Name | 8X | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.94 |
| Max Cabin Seats | 16 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 7417 |
| Standard Cabin Seats | 14 | 19 |
| Direct Operating Cost | $ 3,805 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $30,650,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | — |
| Min Crew | 2 | 2 |
| Crew Rest | No | — |
| Jump Seat | Yes | — |
| Total Seats | 17 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 16 | 19 |
| Lavatory Location | FWD / AFT | — |
| Cabin Pressure (psi) | 10.2 | — |
| Galley / Refreshment | Galley | — |
| Standard Cabin Seats | 14 | 19 |
| SL Cabin Altitude (ft) | 29200 | — |
| Max Cabin Altitude (ft) | 3900 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW307D | CT7-8A |
| TBO (hrs) | On-Condition | 4000 |
| Flat Rating | ISA + 17 | — |
| Thrust (lbs) | 6722 | — |
| No. of Engines | 3 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 80.2 | — |
| Wingspan (ft) | 86.3 | — |
| Cabin Width (ft) | 7.7 | — |
| Cabin Height (ft) | 6.2 | — |
| Cabin Length (ft) | 42.7 | — |
| Overall Height (ft) | 26.1 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | 775 |
| Cabin Width - Floor (ft) | 6.3 | — |
| Cabin Length - Seating (ft) | 29.2 | — |
| Baggage Volume Int. (cu. ft) | 140 | — |
| Baggage Volume Ext. (cu. ft) | — | 140 |