Piaggio Avanti Evo vs Pilatus Pc 24 vs Piper M600 Sls vs Robinson R66
The Piaggio Avanti EVO and Pilatus PC-24 sit in the fast, pressurized, turbine business-aircraft category, while the Piper M600 SLS is a single-engine pressurized turboprop aimed at owner-operators, and the Robinson R66 is a light turbine helicopter optimized for short-range, point-to-point flexibility. For range, the PC-24 typically leads among these, designed for longer trips with jet speeds and the ability to use shorter or rougher runways; the Avanti EVO is also long-legged for a turboprop and is competitive on many missions, though generally behind the PC-24 at maximum range. The M600 SLS offers solid cross-country range but is usually shorter-range than the two larger, twin-engine business aircraft. The R66 has the shortest range, reflecting helicopter fuel fractions and speed, but compensates with vertical access. For passenger capacity, the PC-24 generally carries the most in typical configurations, followed by the Avanti EVO; the M600 SLS usually seats fewer, and the R66 commonly carries a small group, often around four to five passengers plus a pilot depending on configuration and fuel.
| Spec | Piaggio Avanti EVO | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 6 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Piaggio | Pilatus | Piper |
| Aircraft Name | Avanti EVO | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 2076 | 1406 |
| Max Cabin Seats | 7 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3775 | 6680 | 2200 |
| Standard Cabin Seats | 6 | 6 | 4 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 400 | 440 | 274 |
| Base Aircraft Price (USD) | $ 7,695,000 | $11,800,000 | $3,081,400 |
| DOC / nm | — | $ 3.71 | $ 2.19 |
| DOC / nm / Seat | — | $ 0.62 | $ 0.55 |
| Direct Operating Cost | — | $ 1,619 | $ 603 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing | No |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 6 | 5 |
| Max Cabin Seats | 7 | 10 | — |
| Cabin Pressure (psi) | 9 | 9.3 | 5.6 |
| Galley / Refreshment | No | Optional Refreshment Center | Refreshment Centre |
| Standard Cabin Seats | 6 | 6 | 4 |
| 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 | No |
| Model | PT6A–66B | FJ44-4A-QPM | PT6A-42A |
| TBO (hrs) | 3600 | 5000 | 3600 |
| Horsepower | 850 | — | 600 |
| Flat Rating | ISA + 28 | ISA + 23 | ISA + 55 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Burn (gph) | 100 | — | — |
| Thrust (lbs) | — | 3435 | — |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 47.3 | 52.2 | 29.7 |
| 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 |
| Overall Height (ft) | 13.1 | 17.4 | 11.3 |
| 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 | — |
| Cabin Volume (cu. ft) | — | — | 165 |