Dassault Falcon 8x vs Leonardo Aw189 vs Robinson R66 vs Sikorsky S 92
The Dassault Falcon 8X is a long‑range, large‑cabin business jet, built for intercontinental missions. It typically carries about 12–16 passengers in executive layouts (up to 19) and offers roughly 6,400 nautical miles of range, making it suited to nonstop city‑pair travel across oceans. The Leonardo (Agusta) AW189 is a super‑medium, twin‑engine helicopter aimed at offshore and utility work. It generally seats around 16–19 passengers in high‑density configurations (often fewer in VIP) with an approximate range on the order of 450–500 nautical miles, varying strongly with payload and reserves. The Robinson R66 is a light, single‑engine helicopter primarily for short hops, training, and light utility. It typically carries 4 passengers plus a pilot (five seats total) and has a range roughly around 300 nautical miles. The Sikorsky S‑92 is a heavy, twin‑engine helicopter optimized for offshore transport and SAR. It commonly carries about 19 passengers (with higher‑density options) and offers roughly 500–600 nautical miles of range depending on configuration.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 17 | 21 | 21 |
| Manufacturer | Dassault Falcon | Leonardo | Sikorsky |
| Aircraft Name | 8X | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 16 | 19 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 36900 | — | 7417 |
| Standard Cabin Seats | 14 | 19 | 19 |
| Direct Operating Cost | $ 3,805 | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | No | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 17 | 21 | 21 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 16 | 19 | 19 |
| Lavatory Location | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | — | — |
| Galley / Refreshment | Galley | — | — |
| Standard Cabin Seats | 14 | 19 | 19 |
| SL Cabin Altitude (ft) | 29200 | — | — |
| Max Cabin Altitude (ft) | 3900 | — | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PW307D | CT7-2E1 | CT7-8A |
| TBO (hrs) | On-Condition | 4000 | 4000 |
| Flat Rating | ISA + 17 | — | — |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 2 | 1 |
| Fuel Type | — | JetFuel | JetFuel |
| Horsepower | — | 1983 | 2520 |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 80.2 | 57.8 | — |
| Wingspan (ft) | 86.3 | — | — |
| Cabin Width (ft) | 7.7 | — | — |
| Cabin Height (ft) | 6.2 | — | — |
| Cabin Length (ft) | 42.7 | — | — |
| Overall Height (ft) | 26.1 | 16.6 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | 395 | 775 |
| Cabin Width - Floor (ft) | 6.3 | — | — |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | — | — |
| Rotor Diameter (ft) | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | 140 |