Airbus Helicopters H215 vs Airbus Helicopters H225 vs Sikorsky S 92"
The Airbus H215 (AS332 L1e) is typically positioned as a medium-class utility helicopter. In most configurations it carries fewer passengers than the larger heavy models, commonly around the high‑teens to low‑20s depending on seating, fuel and mission kit. Its practical range is generally in the several-hundred‑nautical‑mile class, optimized for cost-effective transport, utility and some offshore support. The Airbus H225 (EC725/AS332 L2e family) is a heavier, higher‑powered development aimed squarely at heavy-lift and offshore transport. It usually offers higher passenger capacity than the H215, often low‑to‑mid 20s in transport layouts, and it tends to provide longer range or better payload‑range tradeoffs, especially with auxiliary tanks, making it a frequent choice for longer offshore legs and SAR. The Sikorsky S‑92 sits in the same heavy, offshore-optimized category as the H225. It is widely used for oil and gas passenger transport, commonly configured for about 19 passengers in typical offshore seating, with range likewise in the several-hundred‑nautical‑mile bracket. Operationally, H225 and S‑92 are closest peers, while H215 is generally the lighter, lower-capacity option.
| Spec | AIRBUS H215 | AIRBUS H225 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 19.07 | $ 20.87 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H215 | H225 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 468 | 454 |
| DOC / nm / Seat | $ 0.91 | $ 0.99 |
| Max Cabin Seats | 22 | 28 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 8903 | 11929 |
| Standard Cabin Seats | 19 | 19 |
| Direct Operating Cost | $ 2,708 | $ 2,963 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 142 |
| Base Aircraft Price (USD) | $27,500,000 | $ 29,500,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Max Cabin Seats | 22 | 28 |
| Standard Cabin Seats | 19 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 1A1 | Makila 2A1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3000 | 3500 |
| Horsepower | 1820 | 2100 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 540 | 684 |
| Dimensions | ||
| Length (ft) | 61.4 | 63.4 |
| Overall Height (ft) | 16.2 | 16.3 |
| Rotor Diameter (ft) | 51.2 | 53.2 |
| Cabin Volume (cu. ft) | 473.9 | 547 |