Airbus Helicopters H175 vs Airbus Helicopters H225
The Airbus Helicopters H175 and H225 sit in different weight classes and are typically chosen for different mission profiles. The H175 is generally considered a super-medium twin, optimized for efficient offshore transport, SAR, and utility roles where strong performance and lower operating weight are advantages. The H225 is a heavier twin (often classed as a heavy/long-range helicopter) aimed at higher payload missions such as offshore crew change to more distant fields, heavy utility work, and large-scale SAR. In range terms, the H225 is typically selected when longer legs and greater fuel/payload flexibility are priorities, while the H175 offers competitive offshore range in a smaller, more efficient package but is usually not positioned as the longest-range option between the two. For passenger capacity, the H225 generally accommodates more people in standard transport layouts, commonly around the high teens to low twenties depending on configuration, whereas the H175 is typically configured for fewer, often in the mid-to-high teens, again depending on seating standard and mission equipment.
| Spec | AIRBUS H175 | AIRBUS H225 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 13.53 | $ 20.87 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H175 | H225 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 454 |
| DOC / nm / Seat | $ 0.75 | $ 0.99 |
| Max Cabin Seats | 18 | 28 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 11929 |
| Standard Cabin Seats | 16 | 19 |
| Direct Operating Cost | $ 2,016 | $ 2,963 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 149 | 142 |
| Base Aircraft Price (USD) | $17,900,000 | $ 29,500,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 21 |
| Max Cabin Seats | 18 | 28 |
| Standard Cabin Seats | 16 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-67E | Makila 2A1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 3500 |
| Horsepower | 1775 | 2100 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | — | 684 |
| Dimensions | ||
| Length (ft) | 59.2 | 63.4 |
| Overall Height (ft) | 17.5 | 16.3 |
| Rotor Diameter (ft) | 48.5 | 53.2 |
| Cabin Volume (cu. ft) | 423.8 | 547 |
| Baggage Volume Ext. (cu. ft) | 81.9 | — |