Dassault Falcon 8x vs Leonardo Aw189 vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Dassault Falcon 8X is a long-range, intercontinental business jet, optimized for fast point‑to‑point travel between major cities. It typically carries about 12–16 passengers in executive seating and offers roughly 6,000–6,400 nautical miles of range, far exceeding either helicopter, but it requires runways and airport infrastructure. The Leonardo AW189 is a medium twin‑engine helicopter aimed at offshore, SAR, and corporate/VIP missions where vertical access matters. It generally seats about 16–19 passengers in high‑density layouts (fewer in VIP) with an approximate range around 450–500 nautical miles depending on load and reserves, trading speed and distance for direct site access. The MD Helicopters (McDonnell Douglas) MD 902 Explorer is a lighter twin helicopter designed for utility, EMS, and law‑enforcement roles, notable for its NOTAR anti‑torque system. It typically carries around 7–10 passengers and has a shorter range, commonly about 300–350 nautical miles, making it best for regional missions rather than offshore or long‑distance travel.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 |
| Min Crew | 2 | 1 |
| Total Seats | 17 | 21 |
| Manufacturer | Dassault Falcon | Leonardo |
| Aircraft Name | 8X | AW189 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 |
| Max Cabin Seats | 16 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | — |
| Standard Cabin Seats | 14 | 19 |
| Direct Operating Cost | $ 3,805 | $ 2,413 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | — |
| Min Crew | 2 | 1 |
| 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 | CT7-2E1 |
| TBO (hrs) | On-Condition | 4000 |
| Flat Rating | ISA + 17 | — |
| Thrust (lbs) | 6722 | — |
| No. of Engines | 3 | 2 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 1983 |
| 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 |
| Cabin Volume (cu. ft) | 1695 | 395 |
| 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 |