Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
By category, the Piaggio Avanti EVO is a twin‑engine turboprop positioned as a high‑speed executive aircraft; the Pilatus PC‑12 NGX is a single‑engine turboprop optimized for utility, short/rough-field flexibility, and owner-operator efficiency; and the Pilatus PC‑24 is a twin‑engine light business jet designed for higher cruise speeds and jet comfort while retaining strong runway versatility. On range, the Avanti EVO and PC‑12 NGX are broadly comparable in typical real-world mission profiles, both suited to medium-length business trips, with the PC‑12 NGX often marketed around roughly 1,800 nautical miles depending on payload and reserves and the Avanti EVO in a similar general bracket. The PC‑24 generally offers a longer jet-class reach, commonly quoted around roughly 2,000 nautical miles depending on configuration and mission assumptions. For passenger capacity, all three are usually arranged for about six to eight passengers in executive layouts. The PC‑12 NGX can be configured for higher-density seating than typical business layouts, while the PC‑24 often carries around eight to ten in many business configurations, with maximum layouts varying by operator and certification basis.
| Spec | Piaggio Avanti EVO | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Piaggio | Pilatus | Pilatus |
| Aircraft Name | Avanti EVO | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 1803 | 2076 |
| Max Cabin Seats | 7 | 9 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3775 | — | 6680 |
| Standard Cabin Seats | 6 | 6 | 6 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 400 | 290 | 440 |
| Base Aircraft Price (USD) | $ 7,695,000 | $5,350,000 | $11,800,000 |
| DOC / nm | — | $ 2.78 | $ 3.71 |
| DOC / nm / Seat | — | $ 0.46 | $ 0.62 |
| Direct Operating Cost | — | $ 793 | $ 1,619 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 6 |
| Max Cabin Seats | 7 | 9 | 10 |
| Cabin Pressure (psi) | 9 | 5.8 | 9.3 |
| Galley / Refreshment | No | No | Optional Refreshment Center |
| Standard Cabin Seats | 6 | 6 | 6 |
| SL Cabin Altitude (ft) | 24000 | 13100 | 23500 |
| Max Cabin Altitude (ft) | 6600 | — | — |
| Cargo Door | — | Yes | Yes |
| Lavatory Location | — | FWD | FWD |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Galley Location | — | — | FWD |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A–66B | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 5000 | 5000 |
| Horsepower | 850 | 1200 | — |
| Flat Rating | ISA + 28 | ISA + 35 | ISA + 23 |
| No. of Engines | 2 | 1 | 2 |
| Fuel Burn (gph) | 100 | — | — |
| Usable Fuel (gal) | — | 402 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 47.3 | 47.25 | 52.2 |
| Wingspan (ft) | 47.1 | 53.33 | 55.8 |
| Cabin Width (ft) | 6.1 | 5 | 5.6 |
| Cabin Height (ft) | 5.8 | 4.9 | 5.1 |
| Cabin Length (ft) | 14.9 | 16.9 | 23 |
| Overall Height (ft) | 13.1 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 3.5 | 4.25 | 3.8 |
| Baggage Volume Int. (cu. ft) | 35.2 | 40 | 90 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | 17 |