Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Embraer Legacy 650 E vs Sikorsky S 92
The Beechcraft King Air 360ER is a pressurized twin‑turboprop utility/business aircraft suited to short and regional missions; it typically seats about 6–9 passengers and offers roughly 1,500–1,800 nautical miles of range depending on fit and reserves. The Dassault Falcon 8X is an ultra‑long‑range tri‑jet business aircraft designed for intercontinental flying; it commonly carries about 12–16 passengers and can reach roughly 6,400–6,500 nautical miles. The Embraer Legacy 650E is a large‑cabin long‑range business jet positioned below the 8X in range but strong on cabin volume; it typically accommodates about 13–14 passengers with around 3,900 nautical miles of range. The Sikorsky S‑92 is a medium/heavy twin‑engine helicopter used for offshore transport, SAR, and VIP roles; it can be configured for about 12–19 passengers and offers roughly 500–600 nautical miles of range. Overall, the 8X leads in range, the Legacy 650E balances cabin and long‑range, the King Air 360ER is efficient for shorter runways and regional trips, and the S‑92 trades speed and range for vertical‑lift access.
| 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 |