Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Robinson R66 vs Sikorsky S 92
The Beechcraft King Air 360ER is a pressurized twin‑turboprop business aircraft suited to short and mid‑range missions, typically carrying about 6 to 9 passengers, with an approximate maximum range around 1,500 nautical miles depending on payload and reserves. The Dassault Falcon 8X is a long‑range trijet business jet designed for intercontinental travel, commonly configured for roughly 12 to 16 passengers, with a maximum range near 6,450 nautical miles. The Robinson R66 is a light single‑engine turbine helicopter aimed at short‑haul utility and executive hops, generally carrying 4 passengers plus a pilot, with an approximate range around 300 nautical miles. The Sikorsky S‑92 is a medium/heavy twin‑engine helicopter used for offshore transport, SAR, and VIP roles, typically seating about 16 to 19 passengers (higher in some layouts) with a practical range on the order of 500 nautical miles depending on configuration. Overall, the Falcon 8X leads on range, the S‑92 leads on helicopter passenger lift, the King Air balances efficiency and runway flexibility, and the R66 is best for short, point‑to‑point rotorcraft 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 |