Piaggio Avanti Evo vs Pilatus Pc 24 vs Sikorsky S 92
The Piaggio Avanti EVO is best categorized as a high-speed, pressurized twin‑turboprop business aircraft, optimized for efficient regional trips. It typically offers the shortest range of the three, roughly in the 1,400–1,800 nautical mile class depending on payload and reserves, and is usually configured for about 6–8 passengers in an executive layout. The Pilatus PC‑24 is a light business jet designed for versatility, including operation from shorter or less‑prepared runways. It generally provides the longest range among these three, around the 2,000‑nautical‑mile class, and commonly carries about 6–10 passengers, with higher maximum seating possible in utility configurations. The Sikorsky S‑92 is a large, twin‑engine helicopter primarily used for offshore transport, SAR, and VIP missions where vertical lift matters more than cruise efficiency. Its range is typically shorter than the fixed‑wing aircraft (often roughly 500–600+ nautical miles, mission dependent), but it can carry the most people, commonly around 12–19 passengers in transport layouts (with variants accommodating more under certain certification and seating arrangements).
| 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 |