Airbus Helicopters H225 vs Enstrom 480b vs Sikorsky S 92
The Airbus H225, Enstrom 480B, and Sikorsky S-92 sit in very different helicopter categories. The Enstrom 480B is a light, single‑engine utility helicopter typically used for training, patrol, and short-range transport. It generally carries about 4–5 people including the pilot and has a comparatively short range, roughly a few hundred nautical miles depending on fuel and reserves. The Airbus H225 is a heavy, twin‑engine helicopter widely used for offshore energy support, search and rescue, and government missions. It offers long-range capability for its class, commonly on the order of roughly 450–600 nautical miles, and a typical passenger fit in the high teens, often around 16–19 passengers depending on configuration. The Sikorsky S‑92 is also a heavy, twin‑engine helicopter focused on offshore transport and SAR, with range broadly comparable to the H225 (often roughly 450–550 nautical miles) and a similar passenger capacity, commonly around 16–19. In general, the S‑92 and H225 compete directly in the heavy offshore category, while the 480B is in a much smaller light-utility segment.
| 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 |