Airbus Helicopters H225 vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters optimized for offshore transport, SAR, and utility work, trading speed for vertical lift and access to confined sites. The H225 typically offers roughly 450–550 nautical miles of range and seats about 16–19 passengers in common layouts, while the S‑92 is in a similar category with about 480–550 nautical miles and usually around 19 seats. The Piaggio Avanti EVO is a fast pressurized twin‑turboprop airplane aimed at executive and regional missions; it generally carries 6–9 passengers and can reach about 1,200–1,400 nautical miles, with higher cruise speeds than most turboprops. The Pilatus PC‑24 is a light twin‑jet designed for short and unimproved runways and flexible airfield access; it typically seats 6–10 passengers and offers about 1,700–2,000 nautical miles depending on payload and reserves, combining jet speed with rugged-field capability. Overall, the helicopters lead in access and lifting, while the Avanti and PC‑24 lead in range and cruise efficiency.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 8 | 6 | 21 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Piaggio | Pilatus | Sikorsky |
| Aircraft Name | H225 | Avanti EVO | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 2076 | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 28 | 7 | 10 | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 | 6680 | 7417 |
| Standard Cabin Seats | 19 | 6 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 142 | 400 | 440 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $11,800,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 8 | 6 | 21 |
| Max Cabin Seats | 28 | 7 | 10 | 19 |
| Standard Cabin Seats | 19 | 6 | 6 | 19 |
| Lavatory | — | No | 1 Enclosed Flushing | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | — |
| Galley / Refreshment | — | No | Optional Refreshment Center | — |
| 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 | Yes |
| Model | Makila 2A1 | PT6A–66B | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 3600 | 5000 | 4000 |
| Horsepower | 2100 | 850 | — | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 28 | ISA + 23 | — |
| Fuel Burn (gph) | — | 100 | — | — |
| Thrust (lbs) | — | — | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 47.3 | 52.2 | — |
| Overall Height (ft) | 16.3 | 13.1 | 17.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 775 |
| 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 | — |
| 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 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |