Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are medium-heavy twin‑engine helicopters designed for offshore, SAR, and utility missions, offering similar categories and passenger capacities; both typically seat around 19 passengers in high-density layouts, with practical ranges commonly in the roughly 450–600 nautical mile class depending on payload and reserves. The MD Helicopters (McDonnell Douglas) 902 Explorer is a lighter twin‑engine helicopter aimed at EMS, law enforcement, and corporate shuttle roles; it carries fewer people, usually about 8–10 passengers, and has a shorter range, generally around 300–400 nautical miles. By contrast, the Beechcraft King Air 360ER is a fixed‑wing twin‑turboprop aircraft rather than a helicopter, optimized for fast point‑to‑point travel and endurance; it typically seats about 8–11 passengers and offers the longest range of the group, commonly on the order of 1,500+ nautical miles (mission dependent). Overall, King Air 360ER leads on range, H225 and S‑92 lead on lift and cabin capacity, and the 902 Explorer fits lighter, shorter‑range helicopter missions.
| Spec | AIRBUS H225 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Sikorsky |
| Aircraft Name | H225 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.94 |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7417 |
| Standard Cabin Seats | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $30,650,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 2100 | 2520 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | 684 | 760 |
| Dimensions | ||
| Length (ft) | 63.4 | — |
| Overall Height (ft) | 16.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |