Piaggio Avanti Evo vs Piper Seneca
The Piaggio Avanti EVO and the Piper Seneca sit in different categories and are aimed at different missions. The Avanti EVO is a high-performance, pressurized twin‑turboprop business aircraft designed for fast, comfortable point‑to‑point travel at higher altitudes and speeds, typically used in executive and charter roles. The Piper Seneca is a pressurized (on most modern variants) twin‑piston light aircraft that emphasizes operating economy and training or personal/utility travel rather than outright performance. In range, the Avanti EVO generally offers longer legs, commonly around 1,500–1,800 nautical miles depending on payload, reserves, and cruise settings, making it better suited to frequent intercity trips without fuel stops. The Seneca’s typical range is shorter, often roughly 700–1,200 nautical miles depending on model, power settings, and payload, which fits regional missions and shorter hops. For passenger capacity, the Avanti EVO is usually configured for about 7–9 occupants (including crew, depending on layout), while the Seneca typically seats 5–7 total, with practical comfort often favoring fewer passengers plus baggage.
| Spec | Piaggio Avanti EVO | Piper Seneca |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | — |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piaggio | Piper |
| Aircraft Name | Avanti EVO | Seneca |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 828 |
| Max Cabin Seats | 7 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3775 | 1331 |
| Standard Cabin Seats | 6 | 4 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 400 | 200 |
| Base Aircraft Price (USD) | $ 7,695,000 | $1,095,000 |
| DOC / nm | — | $ 1.69 |
| DOC / nm / Seat | — | $ 0.28 |
| Direct Operating Cost | — | $ 337 |
| 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 | TSIO-360-RB |
| TBO (hrs) | 3600 | 1800 |
| Horsepower | 850 | 220 |
| Flat Rating | ISA + 28 | — |
| No. of Engines | 2 | 2 |
| Fuel Burn (gph) | 100 | — |
| Fuel Type | — | AvGas |
| Fuel Delivery | — | Fuel Injected |
| Fuel Capacity (gal) | — | 122 |
| Dimensions | ||
| Length (ft) | 47.3 | 28.6 |
| Wingspan (ft) | 47.1 | 39 |
| Cabin Width (ft) | 6.1 | — |
| Cabin Height (ft) | 5.8 | — |
| Cabin Length (ft) | 14.9 | — |
| Overall Height (ft) | 13.1 | 10 |
| Cabin Width - Floor (ft) | 3.5 | — |
| Baggage Volume Int. (cu. ft) | 35.2 | — |