Cessna 208b Grand Caravan Ex vs Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for short and rough-field operations; it typically carries about 9–14 passengers and offers a moderate range around roughly 900–1,200 nm depending on load and reserves. The Dassault Falcon 8X is a long‑range tri‑jet business jet designed for intercontinental missions; it usually seats about 12–16 passengers in executive layouts and can reach roughly 6,400–6,500 nm. The MD Helicopters (McDonnell Douglas) 902 Explorer is a twin‑engine light helicopter for short‑range shuttle, patrol, and EMS-type roles; it generally seats about 6–8 occupants total and has a range on the order of roughly 300–400 nm. The Piaggio Avanti EVO is a high‑speed twin turboprop business aircraft positioned between utility turboprops and light jets; it commonly accommodates about 7–9 passengers and offers a range around roughly 1,500–1,800 nm. Overall, the Falcon 8X leads by far in range and high-end cabin travel, the Avanti EVO balances speed and efficiency for regional business trips, the Grand Caravan EX prioritizes payload and access, and the 902 Explorer specializes in vertical lift with the shortest range.
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 7.66 | — |
| Min Crew | 2 | 1 |
| Total Seats | 17 | 8 |
| Manufacturer | Dassault Falcon | Piaggio |
| Aircraft Name | 8X | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 |
| DOC / nm / Seat | $ 0.64 | — |
| Max Cabin Seats | 16 | 7 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 3775 |
| Standard Cabin Seats | 14 | 6 |
| Direct Operating Cost | $ 3,805 | — |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 516 | 400 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | No |
| Min Crew | 2 | 1 |
| Crew Rest | No | — |
| Jump Seat | Yes | — |
| Total Seats | 17 | 8 |
| Galley Location | FWD | — |
| Max Cabin Seats | 16 | 7 |
| Lavatory Location | FWD / AFT | — |
| Cabin Pressure (psi) | 10.2 | 9 |
| Galley / Refreshment | Galley | No |
| Standard Cabin Seats | 14 | 6 |
| SL Cabin Altitude (ft) | 29200 | 24000 |
| Max Cabin Altitude (ft) | 3900 | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW307D | PT6A–66B |
| TBO (hrs) | On-Condition | 3600 |
| Flat Rating | ISA + 17 | ISA + 28 |
| Thrust (lbs) | 6722 | — |
| No. of Engines | 3 | 2 |
| Horsepower | — | 850 |
| Fuel Burn (gph) | — | 100 |
| 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 |
| 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 | 35.2 |