Beechcraft King Air 360 Er vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Sikorsky S 92
The Beechcraft King Air 360ER and Piaggio Avanti EVO are pressurized twin‑turboprop airplanes aimed at efficient short‑to‑midrange travel. The King Air 360ER is generally positioned for longer endurance within the turboprop class, often planned around roughly 1,500–1,800 nautical miles depending on payload and reserves, and typically carries about 6–9 passengers in executive layouts. The Avanti EVO is a fast turboprop optimized for speed and fuel efficiency, commonly planned around roughly 1,400–1,700 nautical miles, with a typical cabin fit of about 6–7 passengers. The Pilatus PC‑24 is a twin‑jet light business aircraft, offering higher cruise speeds and longer legs than most turboprops; typical range planning is roughly 1,800–2,000 nautical miles with 6–10 passengers depending on configuration. The Sikorsky S‑92 is a large twin‑engine helicopter, focused on offshore, SAR, and VIP transport rather than fixed‑wing efficiency. Its range is much shorter, commonly around 500–600 nautical miles, but it can carry far more people, typically about 19 passengers in transport layouts (fewer in VIP).
| 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 |