Airbus Helicopters H175 vs Airbus Helicopters H215
The Airbus Helicopters H175 is a modern medium-class twin-engine helicopter, while the H215 (also known historically as the AS332 L1 Super Puma) is a larger, heavy/medium-heavy twin-engine helicopter derived from an earlier generation design. In practical category terms, the H175 typically targets the “super-medium” segment for offshore transport, search and rescue, and utility missions where high comfort and efficiency are priorities, whereas the H215 is generally positioned as a more traditional heavy utility and transport platform with strong lifting capability and a focus on rugged multi-role operations. On range, the H175 is usually considered the longer-legged aircraft in typical offshore configurations, benefiting from newer aerodynamics and systems, while the H215’s range is more dependent on configuration and mission equipment and is often somewhat shorter in comparable setups. For passenger capacity, the H175 is commonly arranged around 16–18 passengers in offshore seating, while the H215 is generally capable of carrying more, often around 19–24 passengers depending on layout and weight limits.
| Spec | AIRBUS H175 | AIRBUS H215 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 13.53 | $ 19.07 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H175 | H215 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 468 |
| DOC / nm / Seat | $ 0.75 | $ 0.91 |
| Max Cabin Seats | 18 | 22 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 8903 |
| Standard Cabin Seats | 16 | 19 |
| Direct Operating Cost | $ 2,016 | $ 2,708 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 149 | 142 |
| Base Aircraft Price (USD) | $17,900,000 | $27,500,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 21 |
| Max Cabin Seats | 18 | 22 |
| Standard Cabin Seats | 16 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-67E | Makila 1A1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 3000 |
| Horsepower | 1775 | 1820 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | — | 540 |
| Dimensions | ||
| Length (ft) | 59.2 | 61.4 |
| Overall Height (ft) | 17.5 | 16.2 |
| Rotor Diameter (ft) | 48.5 | 51.2 |
| Cabin Volume (cu. ft) | 423.8 | 473.9 |
| Baggage Volume Ext. (cu. ft) | 81.9 | — |