| Summary |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Total Seats | 8 | 6 | 8 | 17 | 21 |
| Flight Rules | IFR | — | IFR | IFR | IFR |
| Manufacturer | Piaggio | Pilatus | Pilatus | Leonardo | Leonardo |
| Aircraft Name | Avanti EVO | PC-24 | PC-12 NGX | AW139 | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 2076 | 1803 | 573 | 651 |
| Max Cabin Seats | 7 | 10 | 9 | 15 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3775 | 6680 | — | 4701 | — |
| Standard Cabin Seats | 6 | 6 | 6 | 15 | 19 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | Honeywell Primus Apex | EFIS | EFIS |
| Max Cruise Speed (ktas) | 400 | 440 | 290 | 165 | 155 |
| Base Aircraft Price (USD) | $ 7,695,000 | $11,800,000 | $5,350,000 | $15,900,000 | $2,413,000 |
| DOC / nm | — | $ 3.71 | $ 2.78 | $ 11.69 | $ 15.57 |
| DOC / nm / Seat | — | $ 0.62 | $ 0.46 | $ 0.69 | $ 0.74 |
| Direct Operating Cost | — | $ 1,619 | $ 793 | $ 1,929 | $ 2,413 |
| Cabin |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing | Optional | — | — |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Total Seats | 8 | 6 | 8 | 17 | 21 |
| Max Cabin Seats | 7 | 10 | 9 | 15 | 19 |
| Cabin Pressure (psi) | 9 | 9.3 | 5.8 | — | — |
| Galley / Refreshment | No | Optional Refreshment Center | No | — | — |
| Standard Cabin Seats | 6 | 6 | 6 | 15 | 19 |
| SL Cabin Altitude (ft) | 24000 | 23500 | 13100 | — | — |
| Max Cabin Altitude (ft) | 6600 | — | — | — | — |
| Crew Rest | — | No | — | — | — |
| Jump Seat | — | No | — | — | — |
| Cargo Door | — | Yes | Yes | — | — |
| Galley Location | — | FWD | — | — | — |
| Lavatory Location | — | FWD | FWD | — | — |
| Engine |
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | PT6A–66B | FJ44-4A-QPM | PT6E-67XP | PT6C-67C | CT7-2E1 |
| TBO (hrs) | 3600 | 5000 | 5000 | 5000 | 4000 |
| Horsepower | 850 | — | 1200 | 1679 | 1983 |
| Flat Rating | ISA + 28 | ISA + 23 | ISA + 35 | — | — |
| No. of Engines | 2 | 2 | 1 | 2 | 2 |
| Fuel Burn (gph) | 100 | — | — | — | — |
| Thrust (lbs) | — | 3435 | — | — | — |
| Usable Fuel (gal) | — | — | 402 | — | — |
| Fuel Type | — | — | — | JetFuel | JetFuel |
| Fuel Capacity (gal) | — | — | — | 414 | — |
| Dimensions |
| Length (ft) | 47.3 | 52.2 | 47.25 | 54.7 | 57.8 |
| Wingspan (ft) | 47.1 | 55.8 | 53.33 | — | — |
| Cabin Width (ft) | 6.1 | 5.6 | 5 | — | — |
| Cabin Height (ft) | 5.8 | 5.1 | 4.9 | — | — |
| Cabin Length (ft) | 14.9 | 23 | 16.9 | — | — |
| Overall Height (ft) | 13.1 | 17.4 | 14 | 16.4 | 16.6 |
| Cabin Width - Floor (ft) | 3.5 | 3.8 | 4.25 | — | — |
| Baggage Volume Int. (cu. ft) | 35.2 | 90 | 40 | — | — |
| Aisle Step (ft) | — | Flat Floor | — | — | — |
| Cabin Length - Seating (ft) | — | 17 | — | — | — |
| Rotor Diameter (ft) | — | — | — | 54.7 | 48 |
| Cabin Volume (cu. ft) | — | — | — | 282 | 395 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 120 | 85 |
