Airbus Helicopters H145 vs Airbus Helicopters H225
The Airbus Helicopters H145 and H225 sit in different weight and mission categories. The H145 is a light twin‑engine helicopter commonly used for emergency medical services, law enforcement, corporate transport, and utility work where agility, lower operating costs, and access to tighter landing areas matter. The H225 is a heavy twin‑engine helicopter designed for high‑payload, long‑endurance missions such as offshore oil and gas transport, search and rescue, and other roles requiring greater lift and cabin volume. In range, the H145 typically supports medium‑range operations, suited to regional point‑to‑point flights and frequent short sectors. The H225 generally offers longer range and greater endurance, making it better aligned with extended overwater legs and missions that demand more fuel and payload margin. For passenger capacity, the H145 is usually configured for smaller groups, often around 8 to 10 passengers depending on layout and mission equipment. The H225 is built to carry larger passenger loads, commonly in the high‑teens to low‑20s in offshore-style seating, again depending on configuration and regulatory requirements.
| Spec | AIRBUS H145 | AIRBUS H225 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 9.31 | $ 20.87 |
| Min Crew | 1 | 2 |
| Total Seats | 10 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H145 | H225 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 454 |
| DOC / nm / Seat | $ 0.93 | $ 0.99 |
| Max Cabin Seats | 9 | 28 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 11929 |
| Standard Cabin Seats | 8 | 19 |
| Direct Operating Cost | $ 1,210 | $ 2,963 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 130 | 142 |
| Base Aircraft Price (USD) | $10,200,000 | $ 29,500,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 10 | 21 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 9 | 28 |
| Standard Cabin Seats | 8 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Arriel 2E | Makila 2A1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 |
| Horsepower | 894 | 2100 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | — | 684 |
| Dimensions | ||
| Length (ft) | 44.8 | 63.4 |
| Overall Height (ft) | 13 | 16.3 |
| Rotor Diameter (ft) | 36.1 | 53.2 |
| Cabin Volume (cu. ft) | 166 | 547 |
| Baggage Volume Ext. (cu. ft) | 46.8 | — |