Beechcraft King Air 360 Er vs Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Beechcraft King Air 360ER is a pressurized twin‑turboprop business/utility aircraft optimized for efficiency and short, rougher-field capability, with a typical range around 1,500–1,800 nautical miles and seating generally 6–9 passengers (higher in commuter layouts). The Leonardo AW189 is a twin‑engine medium helicopter aimed at offshore transport, SAR, and VIP missions; its practical range is typically about 450–500 nautical miles, with capacity commonly 12–16 passengers depending on configuration. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft focused on cruise speed and cabin comfort; it commonly offers roughly 1,500–1,800 nautical miles of range and usually seats 6–9 passengers. The Pilatus PC‑24 is a light business jet designed for versatile operations, including shorter runways; it delivers a longer typical range of about 1,900–2,000+ nautical miles and usually carries 6–10 passengers. Overall, the AW189 trades speed and range for vertical access, the King Air 360ER and Avanti EVO emphasize turboprop efficiency, and the PC‑24 leads on jet speed and longer reach.
| 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 |