Airbus Helicopters H145 vs Airbus Helicopters H225 vs Leonardo Aw169
Airbus Helicopters’ H145 and Leonardo’s AW169 sit in the light–intermediate twin-engine category, while the Airbus H225 is a heavy twin designed for higher payloads and longer offshore-style missions. In typical configurations, the H145 carries about 8–10 passengers and is optimized for short-to-medium ranges, commonly in the roughly 500–650 km class depending on fit, reserves, and mission profile. The AW169 is generally a step up in cabin volume within the same broad segment, often arranged for about 8–10 passengers as well, with a similar short-to-medium mission radius and typical ranges around 600–800 km depending on configuration. The H225 targets a different role: it commonly seats around 16–19 passengers and is built to cover longer legs, frequently quoted around 800–1,000+ km depending on tanks, payload, and reserves. Overall, H145 emphasizes versatility and compact footprint, AW169 emphasizes cabin and performance in the light-intermediate space, and H225 prioritizes capacity and range for heavier transport missions.
| Spec | AIRBUS H145 | AIRBUS H225 | AGUSTA / LEONARDO AW169 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | $ 20.87 | $ 11.84 |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 10 | 21 | 12 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo |
| Aircraft Name | H145 | H225 | AW169 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 454 | 440 |
| DOC / nm / Seat | $ 0.93 | $ 0.99 | $ 0.99 |
| Max Cabin Seats | 9 | 28 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 11929 | — |
| Standard Cabin Seats | 8 | 19 | 10 |
| Direct Operating Cost | $ 1,210 | $ 2,963 | $ 1,658 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 130 | 142 | 140 |
| Base Aircraft Price (USD) | $10,200,000 | $ 29,500,000 | $9,450,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 10 | 21 | 12 |
| Configuration | Green Interior | — | — |
| Max Cabin Seats | 9 | 28 | 10 |
| Standard Cabin Seats | 8 | 19 | 10 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2E | Makila 2A1 | PW210A |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 | 4000 |
| Horsepower | 894 | 2100 | 1000 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 684 | — |
| Dimensions | |||
| Length (ft) | 44.8 | 63.4 | 48.1 |
| Overall Height (ft) | 13 | 16.3 | 14.8 |
| Rotor Diameter (ft) | 36.1 | 53.2 | — |
| Cabin Volume (cu. ft) | 166 | 547 | 222.5 |
| Baggage Volume Ext. (cu. ft) | 46.8 | — | 49.5 |