Piaggio Avanti Evo vs Pilatus Pc 24 vs Robinson R66
The Piaggio Avanti EVO and Pilatus PC-24 are pressurized business aircraft aimed at fast, weather-capable travel, while the Robinson R66 is a single‑engine turbine helicopter optimized for short-range point‑to‑point access and landing where runways are unavailable. In range, the PC-24 typically leads among the two fixed‑wings, commonly quoted around 2,000 nautical miles depending on load and reserves, while the Avanti EVO is usually in the roughly 1,500–1,800 nautical mile class. The R66 is much shorter-legged, generally a few hundred nautical miles (often around 300–350) before reserves, reflecting helicopter efficiency and typical mission profiles. For passenger capacity, the PC-24 is usually configured for about 6–10 passengers in executive layouts, the Avanti EVO commonly seats about 6–9, and the R66 is typically up to 4 passengers plus a pilot (about 5 seats total), with practical payload and comfort often reducing that. Overall, PC-24 emphasizes versatility and longer legs, Avanti EVO prioritizes speed and efficiency in the turboprop category, and R66 prioritizes access and vertical lift.
| Spec | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Piaggio | Pilatus |
| Aircraft Name | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 2076 |
| Max Cabin Seats | 7 | 10 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3775 | 6680 |
| Standard Cabin Seats | 6 | 6 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 400 | 440 |
| Base Aircraft Price (USD) | $ 7,695,000 | $11,800,000 |
| DOC / nm | — | $ 3.71 |
| DOC / nm / Seat | — | $ 0.62 |
| Direct Operating Cost | — | $ 1,619 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Max Cabin Seats | 7 | 10 |
| Cabin Pressure (psi) | 9 | 9.3 |
| Galley / Refreshment | No | Optional Refreshment Center |
| Standard Cabin Seats | 6 | 6 |
| SL Cabin Altitude (ft) | 24000 | 23500 |
| Max Cabin Altitude (ft) | 6600 | — |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A–66B | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 5000 |
| Horsepower | 850 | — |
| Flat Rating | ISA + 28 | ISA + 23 |
| No. of Engines | 2 | 2 |
| Fuel Burn (gph) | 100 | — |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 47.3 | 52.2 |
| Wingspan (ft) | 47.1 | 55.8 |
| Cabin Width (ft) | 6.1 | 5.6 |
| Cabin Height (ft) | 5.8 | 5.1 |
| Cabin Length (ft) | 14.9 | 23 |
| Overall Height (ft) | 13.1 | 17.4 |
| Cabin Width - Floor (ft) | 3.5 | 3.8 |
| Baggage Volume Int. (cu. ft) | 35.2 | 90 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Length - Seating (ft) | — | 17 |