Airbus Helicopters H215 vs Airbus Helicopters H225
The Airbus Helicopters H215 and H225 are both medium twin-engine helicopters derived from the Super Puma family, but they sit in different performance tiers. The H215 is generally positioned as a cost-effective, multi-role medium transport helicopter suited to utility, firefighting, and passenger transfer missions where acquisition and operating economics are prioritized. The H225 is typically considered the higher-capability, long-range variant, commonly selected for demanding offshore transport and search-and-rescue profiles that benefit from greater payload and system sophistication. In range, the H225 is usually cited with a longer mission radius and more endurance than the H215, making it better suited to extended overwater or remote-area operations. In passenger capacity, both can be configured for around the high teens to low twenties depending on layout, but the H225 is more often offered and operated in higher-density passenger configurations, while the H215 is frequently configured for flexible utility roles and mixed cabin arrangements.
| 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 |