Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Piper M600 Sls
The Agusta/Leonardo AW189 is a medium twin‑engine helicopter, optimized for vertical access and offshore or utility missions rather than speed. Its typical range is roughly 450–500 nautical miles depending on payload, and it generally carries about 12–16 passengers in a high‑density cabin (fewer in VIP or SAR fit). The Piaggio Avanti EVO is a pressurized twin‑turboprop aircraft aimed at fast regional travel; it typically offers about 1,400–1,700 nautical miles of range and usually seats 6–9 passengers in executive layouts. The Pilatus PC‑24 is a light jet designed for flexibility, including operations from shorter or semi‑prepared runways. It commonly provides around 1,800–2,000 nautical miles of range with typical seating of 6–10 passengers (higher maximum with optional configurations). The Piper M600 SLS is a single‑engine pressurized turboprop for owner‑operators, emphasizing simplicity and lower operating cost. Range is typically about 1,200–1,500 nautical miles, with seating generally 4–6 passengers plus a pilot, up to about 6 occupants total depending on configuration.
| Spec | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | — | $ 3.71 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Leonardo | Piaggio | Pilatus | Piper |
| Aircraft Name | AW189 | Avanti EVO | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1530 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.74 | — | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 19 | 7 | 10 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Standard Cabin Seats | 19 | 6 | 6 | 4 |
| Direct Operating Cost | $ 2,413 | — | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 155 | 400 | 440 | 274 |
| Base Aircraft Price (USD) | $2,413,000 | $ 7,695,000 | $11,800,000 | $3,081,400 |
| Useful Load (lbs) | — | 3775 | 6680 | 2200 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 | 5 |
| Max Cabin Seats | 19 | 7 | 10 | — |
| Standard Cabin Seats | 19 | 6 | 6 | 4 |
| Lavatory | — | No | 1 Enclosed Flushing | No |
| Cabin Pressure (psi) | — | 9 | 9.3 | 5.6 |
| Galley / Refreshment | — | No | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 24000 | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | 6600 | — | 8644 |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Cargo Door | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | CT7-2E1 | PT6A–66B | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | 3600 | 5000 | 3600 |
| Horsepower | 1983 | 850 | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Flat Rating | — | ISA + 28 | ISA + 23 | ISA + 55 |
| Fuel Burn (gph) | — | 100 | — | — |
| Thrust (lbs) | — | — | 3435 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 57.8 | 47.3 | 52.2 | 29.7 |
| Overall Height (ft) | 16.6 | 13.1 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 48 | — | — | — |
| Cabin Volume (cu. ft) | 395 | — | — | 165 |
| Baggage Volume Ext. (cu. ft) | 85 | — | — | — |
| Wingspan (ft) | — | 47.1 | 55.8 | 43.2 |
| Cabin Width (ft) | — | 6.1 | 5.6 | 4.1 |
| Cabin Height (ft) | — | 5.8 | 5.1 | 4 |
| Cabin Length (ft) | — | 14.9 | 23 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.5 | 3.8 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 90 | 20 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |