Dassault Falcon 8x vs Gulfstream G700 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Dassault Falcon 8X, Gulfstream G700, and Piaggio Avanti EVO are fixed‑wing business aircraft, while the MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin‑engine helicopter used for corporate transport, public safety, and utility missions. In range, the Gulfstream G700 is the long‑haul leader at roughly 7,500 nautical miles, followed by the Falcon 8X at about 6,450 nautical miles; both are true intercontinental jets. The Piaggio Avanti EVO is a high‑performance turboprop suited to regional missions, typically around 1,700–1,800 nautical miles. The MD 902 Explorer has a much shorter helicopter range, commonly on the order of 300–400 nautical miles depending on configuration and reserves. For passenger capacity, the G700 generally accommodates about 13–19 passengers in a spacious cabin, the Falcon 8X commonly seats around 12–16, and the Avanti EVO typically carries about 7–9. The MD 902 Explorer usually seats 1–2 pilots plus roughly 6–7 passengers, varying with mission equipment.
| Spec | Dassault Falcon 8X | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 7.66 | — | — |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 17 | 16 | 8 |
| Manufacturer | Dassault Falcon | Gulfstream | Piaggio |
| Aircraft Name | 8X | G700 | Avanti EVO |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 6450 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.64 | — | — |
| Max Cabin Seats | 16 | 19 | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 36900 | — | 3775 |
| Standard Cabin Seats | 14 | 12 | 6 |
| Direct Operating Cost | $ 3,805 | — | — |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 516 | 516 | 400 |
| Base Aircraft Price (USD) | $ 62,500,000 | $78,000,000 | $ 7,695,000 |
| Flight Rules | — | — | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | No |
| Min Crew | 2 | 4 | 1 |
| Crew Rest | No | Optional | — |
| Jump Seat | Yes | Yes | — |
| Total Seats | 17 | 16 | 8 |
| Galley Location | FWD | FWD | — |
| Max Cabin Seats | 16 | 19 | 7 |
| Lavatory Location | FWD / AFT | FWD / AFT | — |
| Cabin Pressure (psi) | 10.2 | — | 9 |
| Galley / Refreshment | Galley | — | No |
| Standard Cabin Seats | 14 | 12 | 6 |
| SL Cabin Altitude (ft) | 29200 | — | 24000 |
| Max Cabin Altitude (ft) | 3900 | — | 6600 |
| Engine | |||
| FADEC | Yes | — | Yes |
| Model | PW307D | Pearl 700 | PT6A–66B |
| TBO (hrs) | On-Condition | On Condition | 3600 |
| Flat Rating | ISA + 17 | — | ISA + 28 |
| Thrust (lbs) | 6722 | 18250 | — |
| No. of Engines | 3 | 2 | 2 |
| Horsepower | — | — | 850 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 80.2 | 109.9 | 47.3 |
| Wingspan (ft) | 86.3 | 103 | 47.1 |
| Cabin Width (ft) | 7.7 | 8.2 | 6.1 |
| Cabin Height (ft) | 6.2 | 6.25 | 5.8 |
| Cabin Length (ft) | 42.7 | 56.9 | 14.9 |
| Overall Height (ft) | 26.1 | 25.4 | 13.1 |
| Cabin Volume (cu. ft) | 1695 | — | — |
| Cabin Width - Floor (ft) | 6.3 | — | 3.5 |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | 195 | 35.2 |
| Aisle Step (ft) | — | Flat Floor | — |