Airbus Helicopters H225 vs Embraer Legacy 650 E vs Pilatus Pc 24 vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are heavy, twin‑engine helicopters designed for offshore transport, search and rescue, and utility missions. They typically carry around 16–19 passengers in an airline-style layout (with higher-density options possible) and offer practical ranges on the order of roughly 450–600 nautical miles depending on payload, reserves, and mission equipment. Between the two, the S‑92 is often cited with slightly longer typical range, while the H225 is similarly positioned with strong lift and hot‑and‑high performance. The Embraer Legacy 650E is a long‑range business jet optimized for point‑to‑point travel at high speed and altitude. It generally seats about 13 passengers in executive configuration and has intercontinental-class range, roughly around 3,900 nautical miles, making it suited to nonstop transcontinental routes. The Pilatus PC‑24 is a light jet built for versatility, including operations from shorter and sometimes unpaved runways. It typically carries 6–10 passengers in executive layouts and has a midrange capability of about 2,000 nautical miles, bridging the gap between utility access and efficient regional-to-continental jet travel.
| Spec | AIRBUS H225 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Pilatus | Sikorsky |
| Aircraft Name | H225 | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 2076 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 28 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 6680 | 7417 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 142 | 440 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $11,800,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Max Cabin Seats | 28 | 10 | 19 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Lavatory | — | 1 Enclosed Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Cargo Door | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD | — |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Optional Refreshment Center | — |
| SL Cabin Altitude (ft) | — | 23500 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 |
| Horsepower | 2100 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 23 | — |
| Thrust (lbs) | — | 3435 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.2 | — |
| Overall Height (ft) | 16.3 | 17.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| Wingspan (ft) | — | 55.8 | — |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 5.6 | — |
| Cabin Height (ft) | — | 5.1 | — |
| Cabin Length (ft) | — | 23 | — |
| Cabin Width - Floor (ft) | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | 90 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |