Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Sikorsky S 92
The Dassault Falcon 8X and Piaggio Avanti EVO are business airplanes, while the MD Helicopters (McDonnell Douglas) 902 Explorer and Sikorsky S-92 are helicopters aimed more at utility, corporate shuttle, and offshore or government missions. In range, the Falcon 8X is the clear leader, designed for intercontinental trips at roughly 6,400 nautical miles, enabling nonstop long-haul city pairs. The Avanti EVO is a shorter-range turboprop business aircraft, typically around 1,700–1,800 nautical miles, suited to regional missions with strong speed and efficiency for its class. Helicopters trade range for vertical lift and point-to-point access: the MD 902 Explorer commonly offers roughly 300–350 nautical miles depending on load and reserves, while the larger S-92 generally reaches about 500–600 nautical miles in typical configurations, especially in offshore roles. Passenger capacity follows a similar pattern: the Falcon 8X usually seats about 12–16 in executive layouts, the Avanti EVO about 7–9, the MD 902 about 7–8, and the S-92 about 19 passengers (often 18–19 in transport configurations).
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 17 | 8 | 21 |
| Manufacturer | Dassault Falcon | Piaggio | Sikorsky |
| Aircraft Name | 8X | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 | 439 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.94 |
| Max Cabin Seats | 16 | 7 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 36900 | 3775 | 7417 |
| Standard Cabin Seats | 14 | 6 | 19 |
| Direct Operating Cost | $ 3,805 | — | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | No | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | No | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 17 | 8 | 21 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 16 | 7 | 19 |
| Lavatory Location | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | 9 | — |
| Galley / Refreshment | Galley | No | — |
| Standard Cabin Seats | 14 | 6 | 19 |
| SL Cabin Altitude (ft) | 29200 | 24000 | — |
| Max Cabin Altitude (ft) | 3900 | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PW307D | PT6A–66B | CT7-8A |
| TBO (hrs) | On-Condition | 3600 | 4000 |
| Flat Rating | ISA + 17 | ISA + 28 | — |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 2 | 1 |
| Horsepower | — | 850 | 2520 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Type | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 80.2 | 47.3 | — |
| Wingspan (ft) | 86.3 | 47.1 | — |
| Cabin Width (ft) | 7.7 | 6.1 | — |
| Cabin Height (ft) | 6.2 | 5.8 | — |
| Cabin Length (ft) | 42.7 | 14.9 | — |
| Overall Height (ft) | 26.1 | 13.1 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | — | 775 |
| Cabin Width - Floor (ft) | 6.3 | 3.5 | — |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |