Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Agusta/Leonardo AW189 is a twin‑engine medium helicopter, optimized for vertical access to offshore platforms, remote sites, and urban helipads where runways are unavailable. Its typical range is roughly 450–500 nautical miles depending on payload and reserves, and it commonly carries about 16–19 passengers in high‑density configurations (often fewer with executive interiors or mission equipment). The Piaggio Avanti EVO is a pressurized twin‑turboprop business aircraft intended for fast, efficient point‑to‑point travel between runways, including many shorter regional fields. Typical range is about 1,500–1,800 nautical miles, with seating usually 6–8 passengers in executive layout (up to around 9 depending on configuration). The Pilatus PC‑24 is a light business jet designed for runway flexibility, including many short and semi‑prepared strips, while offering jet speeds and cabin comfort. Typical range is around 1,800–2,000 nautical miles, with a common executive capacity of about 6–8 passengers (and higher in commuter-style layouts).
| Spec | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | — | $ 3.71 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Leonardo | Piaggio | Pilatus |
| Aircraft Name | AW189 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.74 | — | $ 0.62 |
| Max Cabin Seats | 19 | 7 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Standard Cabin Seats | 19 | 6 | 6 |
| Direct Operating Cost | $ 2,413 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 155 | 400 | 440 |
| Base Aircraft Price (USD) | $2,413,000 | $ 7,695,000 | $11,800,000 |
| Useful Load (lbs) | — | 3775 | 6680 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Max Cabin Seats | 19 | 7 | 10 |
| Standard Cabin Seats | 19 | 6 | 6 |
| Lavatory | — | No | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | 9 | 9.3 |
| Galley / Refreshment | — | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | CT7-2E1 | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 3600 | 5000 |
| Horsepower | 1983 | 850 | — |
| No. of Engines | 2 | 2 | 2 |
| Flat Rating | — | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | 100 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 57.8 | 47.3 | 52.2 |
| Overall Height (ft) | 16.6 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | — | — |
| Baggage Volume Ext. (cu. ft) | 85 | — | — |
| Wingspan (ft) | — | 47.1 | 55.8 |
| Cabin Width (ft) | — | 6.1 | 5.6 |
| Cabin Height (ft) | — | 5.8 | 5.1 |
| Cabin Length (ft) | — | 14.9 | 23 |
| Cabin Width - Floor (ft) | — | 3.5 | 3.8 |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 90 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | 17 |