Piaggio Avanti Evo vs Pilatus Pc 24 vs Robinson R66 vs Sikorsky S 92
The Piaggio Avanti EVO and Pilatus PC-24 are fixed-wing business aircraft, while the Robinson R66 and Sikorsky S-92 are helicopters aimed at very different missions and budgets. The Avanti EVO is a fast turboprop executive aircraft typically carrying about 6–7 passengers (up to around 9 in high-density layouts) with roughly 1,700–1,800 nautical miles of range, emphasizing speed and cabin comfort. The PC-24 is a light jet designed for versatility and short/rough-field capability, usually seating about 6–8 passengers (often up to 10) with about 2,000 nautical miles of range, generally offering the longest reach of this group. The Robinson R66 is a light single-engine turbine helicopter, commonly configured for 4 passengers plus a pilot, with an approximate 300 nautical mile range, suited to short regional hops and utility flying. The Sikorsky S-92 is a large twin-engine helicopter used for offshore transport, SAR, and VIP roles, typically carrying around 19 passengers (plus crew) with roughly 500–600 nautical miles of range, prioritizing payload, safety, and all-weather capability over speed and distance.
| Spec | Piaggio Avanti EVO | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 8 | 6 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Piaggio | Pilatus | Sikorsky |
| Aircraft Name | Avanti EVO | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 2076 | 439 |
| Max Cabin Seats | 7 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3775 | 6680 | 7417 |
| Standard Cabin Seats | 6 | 6 | 19 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 400 | 440 | 155 |
| Base Aircraft Price (USD) | $ 7,695,000 | $11,800,000 | $30,650,000 |
| DOC / nm | — | $ 3.71 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.62 | $ 0.94 |
| Direct Operating Cost | — | $ 1,619 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing | — |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 8 | 6 | 21 |
| Max Cabin Seats | 7 | 10 | 19 |
| Cabin Pressure (psi) | 9 | 9.3 | — |
| Galley / Refreshment | No | Optional Refreshment Center | — |
| Standard Cabin Seats | 6 | 6 | 19 |
| 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 | PT6A–66B | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | 3600 | 5000 | 4000 |
| Horsepower | 850 | — | 2520 |
| Flat Rating | ISA + 28 | ISA + 23 | — |
| No. of Engines | 2 | 2 | 1 |
| Fuel Burn (gph) | 100 | — | — |
| Thrust (lbs) | — | 3435 | — |
| Fuel Type | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 47.3 | 52.2 | — |
| 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 | — |
| Overall Height (ft) | 13.1 | 17.4 | 17.8 |
| 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 | — |
| Cabin Volume (cu. ft) | — | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |