Airbus Helicopters H175 vs Airbus Helicopters H215 vs Airbus Helicopters H225 vs Leonardo Aw169
The Airbus Helicopters H175 and H225 sit in the “super-medium” and “heavy” offshore/utility class respectively, while the Airbus H215 is a “medium” helicopter derived from the Super Puma family, and the Leonardo AW169 is a “light-intermediate” twin aimed at EMS, corporate and utility roles. In range terms, the H225 is generally the longest-legged of the four (often configured for long offshore sectors), with the H175 close behind and also optimized for offshore endurance; the H215 typically offers solid medium-class range but is usually shorter than H175/H225 in comparable mission fits. The AW169, being smaller and lighter, normally has the shortest range of the group, though it can still cover substantial regional legs depending on tanks and payload. Passenger capacity follows the same size ladder: AW169 commonly seats around 8–10 passengers in typical layouts, the H175 around 16–18, the H215 roughly 19–22, and the H225 typically about 19–24, with exact figures varying by certification, seating density, fuel, and mission equipment.
| Spec | AIRBUS H175 | AIRBUS H215 | AIRBUS H225 | AGUSTA / LEONARDO AW169 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 13.53 | $ 19.07 | $ 20.87 | $ 11.84 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 21 | 21 | 12 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Leonardo |
| Aircraft Name | H175 | H215 | H225 | AW169 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 468 | 454 | 440 |
| DOC / nm / Seat | $ 0.75 | $ 0.91 | $ 0.99 | $ 0.99 |
| Max Cabin Seats | 18 | 22 | 28 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 8903 | 11929 | — |
| Standard Cabin Seats | 16 | 19 | 19 | 10 |
| Direct Operating Cost | $ 2,016 | $ 2,708 | $ 2,963 | $ 1,658 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 149 | 142 | 142 | 140 |
| Base Aircraft Price (USD) | $17,900,000 | $27,500,000 | $ 29,500,000 | $9,450,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 21 | 21 | 12 |
| Max Cabin Seats | 18 | 22 | 28 | 10 |
| Standard Cabin Seats | 16 | 19 | 19 | 10 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-67E | Makila 1A1 | Makila 2A1 | PW210A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 3000 | 3500 | 4000 |
| Horsepower | 1775 | 1820 | 2100 | 1000 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 540 | 684 | — |
| Dimensions | ||||
| Length (ft) | 59.2 | 61.4 | 63.4 | 48.1 |
| Overall Height (ft) | 17.5 | 16.2 | 16.3 | 14.8 |
| Rotor Diameter (ft) | 48.5 | 51.2 | 53.2 | — |
| Cabin Volume (cu. ft) | 423.8 | 473.9 | 547 | 222.5 |
| Baggage Volume Ext. (cu. ft) | 81.9 | — | — | 49.5 |