Airbus Helicopters H135 vs Airbus Helicopters H155 vs Airbus Helicopters H175 vs Airbus Helicopters H225
The Airbus Helicopters H135 is a light twin in the entry/EMS and training category, optimized for short to medium missions. It typically carries about five to seven passengers (depending on interior fit) and offers roughly a 300–350 nm class range. The H155 sits in the light‑intermediate segment, aimed at corporate and offshore shuttle work; it generally accommodates around eight to twelve passengers and provides a longer, mid‑400 nm class range. The H175 is a super‑medium helicopter designed largely for offshore transport and SAR; it commonly seats about sixteen passengers in an offshore layout (or fewer in VIP/SAR configurations) and delivers roughly a 500+ nm class range. The H225 (Super Puma family) is a heavy twin intended for high‑capacity offshore, SAR, and utility roles; it typically carries around nineteen passengers and offers about a 450–500+ nm class range depending on fuel and mission equipment. Across the lineup, capability scales from the H135’s compact efficiency to the H225’s lift and cabin volume, with the H175 often balancing range, payload, and operating cost in the offshore-focused middle.
| Spec | AIRBUS H135 | AIRBUS H155 | AIRBUS H175 | AIRBUS H225 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 6.33 | $ 11.06 | $ 13.53 | $ 20.87 |
| Min Crew | 1 | 2 | 2 | 2 |
| Total Seats | 9 | 14 | 18 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H135 | H155 | H175 | H225 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 342 | 423 | 573 | 454 |
| DOC / nm / Seat | $ 0.79 | $ 0.74 | $ 0.75 | $ 0.99 |
| Max Cabin Seats | 7 | 12 | 18 | 28 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3124 | 4012 | 6797 | 11929 |
| Standard Cabin Seats | 7 | 12 | 16 | 19 |
| Direct Operating Cost | $ 861 | $ 1,593 | $ 2,016 | $ 2,963 |
| Flight Deck (Base Spec) | Helionix | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 136 | 144 | 149 | 142 |
| Base Aircraft Price (USD) | $6,150,000 | $14,800,000 | $17,900,000 | $ 29,500,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 2 | 2 |
| Total Seats | 9 | 14 | 18 | 21 |
| Configuration | Green Interior | Green Interior | — | — |
| Max Cabin Seats | 7 | 12 | 18 | 28 |
| Standard Cabin Seats | 7 | 12 | 16 | 19 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Arrius 2B2+ | Arriel 2C2 | PT6A-67E | Makila 2A1 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 3500 | 3500 |
| Horsepower | 660 | 943 | 1775 | 2100 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 332 | — | 684 |
| Dimensions | ||||
| Length (ft) | 33.5 | 46.9 | 59.2 | 63.4 |
| Overall Height (ft) | 12.6 | 14.3 | 17.5 | 16.3 |
| Rotor Diameter (ft) | 34 | 41.1 | 48.5 | 53.2 |
| Cabin Volume (cu. ft) | 173 | 235.2 | 423.8 | 547 |
| Baggage Volume Ext. (cu. ft) | — | 88.3 | 81.9 | — |