Compare Piaggio Avanti EVO vs Piper Arrow
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| Manufacturer | Piaggio | Piper |
| Aircraft Type | Avanti EVO | Arrow |
| Base Aircraft Price (USD) | $ 7,695,000 | $765,000 |
| Direct Operating Cost | - | $ 221 |
| DOC / nm | - | $ 1.36 |
| DOC / nm / Seat | - | $ 0.23 |
| Max Cruise Speed (ktas) | 400 | 162 |
| Max Range (nm) | 1530 | 700 |
| Useful Load (lbs) | 3775 | 1191 |
| Total Seats | 8 | 6 |
| Cockpit | 2 | 2 |
| Standard Cabin Seats | 6 | 4 |
| Max Cabin Seats | 7 | - |
| Min Crew | 1 | - |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G1000 NXi |
| Flight Rules | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | Un-Verified |
| Weights | ||
| MRAMP (lbs) | 12150 | - |
| MTOW (lbs) | 12100 | 3800 |
| MLW (lbs) | 11500 | - |
| MZFW (lbs) | 9800 | - |
| BOW (lbs) | 8375 | - |
| BEW (lbs) | 8325 | 2625 |
| Useful Load (lbs) | 3775 | 1191 |
| Max Payload (lbs) | 1425 | - |
| Fuel Capacity (lbs) | 2802 | 648 |
| Useful Load Max Fuel (lbs) | - | 543 |
| Payload Max Fuel (lbs) | 973 | - |
| Max Baggage Weight (lbs) | 350 | - |
| Dimensions | ||
| Wingspan (ft) | 47.1 | 38.6 |
| Overall Height (ft) | 13.1 | 8.5 |
| Length (ft) | 47.3 | 27.6 |
| Cabin Height (ft) | 5.8 | - |
| Cabin Width (ft) | 6.1 | - |
| Cabin Width - Floor (ft) | 3.5 | - |
| Cabin Length (ft) | 14.9 | - |
| Baggage Volume Int. (cu. ft) | 35.2 | - |
| Engine | ||
| No. of Engines | 2 | 2 |
| Manufacturer | Piaggio | Piper |
| Model | PT6A–66B | O-360-AIH6 |
| Horsepower | 850 | 180 |
| Flat Rating | ISA + 28 | - |
| FADEC | Yes | No |
| TBO (hrs) | 3600 | 2000 |
| TBO (yrs) | - | 12 |
| Fuel Type | - | AvGas |
| Fuel Delivery | - | Carbureted |
| Fuel Capacity (gal) | - | 108 |
| Fuel Burn (gph) | 100 | - |
| Avionics | ||
| Flight Deck | Rockwell Collins Pro Line 21 | Garmin G1000 NXi |
| Flight Rules | IFR | IFR |
| Standby Instrument | - | Aspen Avionics EFD1000 |
| Autopilot | - | Garmin GFC 700 |
| PFD | - | 1 |
| MFD | - | 1 |
| GPS | - | 2 |
| Flight Director | - | 1 |
| Transponder | - | 1 |
| VHF Com | - | 1 |
| VHF NAV | - | 1 |
| Cabin | ||
| Total Seats | 8 | 6 |
| Cockpit | 2 | 2 |
| Standard Cabin Seats | 6 | 4 |
| Max Cabin Seats | 7 | - |
| Min Crew | 1 | - |
| Lavatory | No | - |
| Galley / Refreshment | No | - |
| Max Cabin Altitude (ft) | 6600 | - |
| SL Cabin Altitude (ft) | 24000 | - |
| Cabin Pressure (psi) | 9 | - |
| Other | ||
| Prop Manufacturer | Hartzell | Hartzell |
| Prop Description | Scimitar | 2-Blade Constant Feathering |
| Gear Type | Retractable | Retractable |
| Warranty | ||
| Airframe (Yrs) | - | 2 |
| Engine (Yrs) | - | 3 |
| Prop (Yrs) | - | 3 |
| Avionics (Yrs) | - | 2 |
| Performance | ||
| Max Cruise Speed (Mach) | 0.7 | - |
| Max Cruise Speed (ktas) | 400 | 162 |
| Long Range Cruise (ktas) | 318 | 162 |
| Max Range (nm) | 1530 | 700 |
| Take-off Roll (ft) | 3262 | 1100 |
| Take-Off >50ft Obst. (ft) | - | 2200 |
| Take-Off (5000 / ISA + 10) | 4700 | - |
| Landing Roll (ft) | - | 770 |
| Landing >50ft Obst. (ft) | 3282 | 1490 |
| Max Climb Rate (fpm) | 2770 | - |
| Service Ceiling (ft) | 41000 | 15000 |