Airbus Helicopters H225 vs Embraer Legacy 650 E vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are large twin‑engine helicopters, best categorized for offshore transport, search and rescue, and utility/VIP missions where vertical access matters more than speed or altitude. Both typically carry around 16–19 passengers in transport layouts (fewer in VIP), with practical ranges commonly in the ~450–550 nautical mile class depending on payload, reserves, and configuration; the S‑92 is often cited slightly higher, while the H225 can vary widely by mission kit and weights. The Embraer Legacy 650E is a long‑range, large‑cabin business jet optimized for point‑to‑point travel at high speed and altitude. It generally seats 13–14 passengers, with a range around 3,900–4,000 nautical miles, enabling intercontinental legs. The Piaggio Avanti EVO is a twin‑turboprop business aircraft in the light/midsize category, trading jet‑like cruise efficiency for shorter‑field flexibility. It typically seats 7–9 passengers, with range roughly 1,500–1,800 nautical miles, ideal for regional and intra‑continental routes.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio | Sikorsky |
| Aircraft Name | H225 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.94 |
| Max Cabin Seats | 28 | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 | 7417 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 400 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Max Cabin Seats | 28 | 7 | 19 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Lavatory | — | No | — |
| Cabin Pressure (psi) | — | 9 | — |
| Galley / Refreshment | — | No | — |
| SL Cabin Altitude (ft) | — | 24000 | — |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 3600 | 4000 |
| Horsepower | 2100 | 850 | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 28 | — |
| Fuel Burn (gph) | — | 100 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 47.3 | — |
| Overall Height (ft) | 16.3 | 13.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| Wingspan (ft) | — | 47.1 | — |
| Cabin Width (ft) | — | 6.1 | — |
| Cabin Height (ft) | — | 5.8 | — |
| Cabin Length (ft) | — | 14.9 | — |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |