Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Robinson R66
The Leonardo AW189 and Robinson R66 are helicopters, while the Piaggio Avanti EVO and Pilatus PC-24 are fixed‑wing aircraft. In category, the AW189 is a super‑medium, twin‑engine utility helicopter suited to offshore, SAR, and corporate shuttle work; the R66 is a light, single‑engine turbine helicopter aimed at simpler, shorter missions. The Avanti EVO is a fast, pressurized twin‑turboprop business aircraft optimized for efficient point‑to‑point travel, whereas the PC‑24 is a light business jet designed for higher speed and the ability to operate from shorter or less‑prepared runways than many jets. In range, the PC‑24 generally offers the longest reach at roughly 2,000 nautical miles, the Avanti EVO is typically in the upper‑1,000‑nautical‑mile class, the AW189 is commonly several hundred nautical miles (often around 400–500 nm depending on load), and the R66 is shorter still, typically a few hundred nautical miles. For passenger capacity, the PC‑24 and Avanti EVO are usually configured for about 6–9 passengers, the AW189 can carry a larger cabin load (often 12–16+ depending on layout), and the R66 is typically 4 passengers plus a pilot.
| 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 |