Piaggio Avanti Evo vs Piper Seminole
The Piaggio Avanti EVO and the Piper Arrow sit in very different categories. The Avanti EVO is a twin‑engine turboprop business aircraft designed for fast, high‑altitude corporate travel, typically operated with professional crew standards and offering a cabin sized for executive comfort. The Piper Arrow is a single‑engine, piston‑powered retractable‑gear general aviation airplane aimed at personal flying, training, and short cross‑country trips. In range, the Avanti EVO generally offers substantially longer legs and higher cruise speeds, making it better suited to city‑pair business missions without stops. The Arrow’s range is more modest and more sensitive to payload, winds, and power settings, and it is usually chosen for shorter trips where lower operating complexity and cost matter more than speed. Passenger capacity also differs. The Avanti EVO commonly carries around seven to eight occupants depending on configuration, while the Piper Arrow is typically a four‑seat aircraft, including the pilot, with practical seating and baggage limited by weight and balance.
| Spec | Piaggio Avanti EVO | Piper Arrow |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | — |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piaggio | Piper |
| Aircraft Name | Avanti EVO | Arrow |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 700 |
| Max Cabin Seats | 7 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3775 | 1191 |
| Standard Cabin Seats | 6 | 4 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 400 | 162 |
| Base Aircraft Price (USD) | $ 7,695,000 | $765,000 |
| DOC / nm | — | $ 1.36 |
| DOC / nm / Seat | — | $ 0.23 |
| Direct Operating Cost | — | $ 221 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | — |
| Min Crew | 1 | — |
| Total Seats | 8 | 6 |
| Max Cabin Seats | 7 | — |
| Cabin Pressure (psi) | 9 | — |
| Galley / Refreshment | No | — |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 24000 | — |
| Max Cabin Altitude (ft) | 6600 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | PT6A–66B | O-360-AIH6 |
| TBO (hrs) | 3600 | 2000 |
| Horsepower | 850 | 180 |
| Flat Rating | ISA + 28 | — |
| No. of Engines | 2 | 2 |
| Fuel Burn (gph) | 100 | — |
| Fuel Type | — | AvGas |
| TBO (yrs) | — | 12 |
| Fuel Delivery | — | Carbureted |
| Fuel Capacity (gal) | — | 108 |
| Dimensions | ||
| Length (ft) | 47.3 | 27.6 |
| Wingspan (ft) | 47.1 | 38.6 |
| Cabin Width (ft) | 6.1 | — |
| Cabin Height (ft) | 5.8 | — |
| Cabin Length (ft) | 14.9 | — |
| Overall Height (ft) | 13.1 | 8.5 |
| Cabin Width - Floor (ft) | 3.5 | — |
| Baggage Volume Int. (cu. ft) | 35.2 | — |