Dassault Falcon 8x vs Enstrom 480b vs Leonardo Aw189 vs Sikorsky S 92
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for high‑speed intercontinental travel, with an advertised range around 6,450 nautical miles and typical seating for about 12–16 passengers depending on cabin layout. The Enstrom 480B is a light, single‑engine piston helicopter oriented toward short‑range utility and training missions, with range roughly in the 200–300 nautical mile class and passenger capacity typically 4 (pilot plus three). The Agusta/Leonardo AW189 is a super‑medium twin‑engine helicopter built for offshore and SAR/utility roles, offering roughly 450–500 nautical miles of range (mission dependent) and commonly configured for about 16–19 passengers. The Sikorsky S‑92 is a larger heavy twin‑engine helicopter optimized for offshore transport and search and rescue, with range commonly around 500 nautical miles (configuration dependent) and typical passenger seating in the 19‑passenger class. Overall, the Falcon 8X dominates range and cruise speed, while the AW189 and S‑92 trade speed for vertical lift and mission flexibility, and the 480B sits at the small end for capacity and endurance.
| 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 |