Airbus Helicopters H225 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large, twin‑engine helicopters aimed at offshore transport, SAR, and heavy utility work. They sit in the same general category and typically offer similar mission reach, with practical ranges on the order of roughly 450–550 nautical miles depending on payload and reserves. Cabin capacity is also comparable: in airline-style seating they commonly carry about 16–19 passengers, and in high-density layouts can be configured for more. The MD Helicopters (McDonnell Douglas) 902 Explorer is a much lighter twin helicopter in a different class, optimized for law enforcement, EMS, and corporate shuttle roles. Its range is notably shorter than the H225/S‑92 group, often around 300–350 nautical miles, and it usually seats about 6–8 passengers. The Piaggio Avanti EVO is not a helicopter but a twin‑turboprop fixed‑wing business aircraft. Compared with the rotorcraft, it generally offers longer range—often around 1,400–1,700 nautical miles—and typically seats about 7–9 passengers, trading vertical-lift capability for speed and efficiency.
| 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 |