Airbus Helicopters H125 vs Airbus Helicopters H135 vs Airbus Helicopters H145 vs Airbus Helicopters H160 vs Airbus Helicopters H225
Airbus Helicopters’ H125 is a single‑engine light utility helicopter, typically used for training, tourism, and aerial work; it carries about 5–6 passengers (plus pilot) and offers a moderate range suited to short regional missions. The H135 is a light twin, optimized for EMS, law enforcement, and corporate flying; it generally seats around 5–7 passengers and provides similar short‑to‑medium range with twin‑engine redundancy. The H145 is a larger light twin with a more spacious cabin and higher payload, commonly configured for EMS and utility roles; it typically carries about 7–9 passengers and delivers a solid medium range. The H160 is a medium twin designed for higher speed, comfort, and efficiency in corporate and offshore roles; it usually accommodates roughly 10–12 passengers and offers longer medium‑range capability. The H225 is a heavy twin for offshore transport and SAR, carrying about 16–19 passengers and providing the longest range of this group, suited to extended overwater and high‑payload missions.
| Spec | AIRBUS H125 | AIRBUS H135 | AIRBUS H145 | AIRBUS H160 | AIRBUS H225 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 6.33 | $ 9.31 | — | $ 20.87 |
| Min Crew | 1 | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 9 | 10 | 14 | 21 |
| Flight Rules | VFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H125 | H135 | H145 | H160 | H225 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 342 | 352 | 460 | 454 |
| DOC / nm / Seat | $ 0.77 | $ 0.79 | $ 0.93 | — | $ 0.99 |
| Max Cabin Seats | 5 | 7 | 9 | 12 | 28 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 3124 | 4200 | 3992 | 11929 |
| Standard Cabin Seats | 4 | 7 | 8 | 12 | 19 |
| Direct Operating Cost | $ 627 | $ 861 | $ 1,210 | — | $ 2,963 |
| Flight Deck (Base Spec) | Garmin G500H | Helionix | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 136 | 136 | 130 | 155 | 142 |
| Base Aircraft Price (USD) | $3,200,000 | $6,150,000 | $10,200,000 | $14,000,000 | $ 29,500,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 9 | 10 | 14 | 21 |
| Max Cabin Seats | 5 | 7 | 9 | 12 | 28 |
| Standard Cabin Seats | 4 | 7 | 8 | 12 | 19 |
| Configuration | — | Green Interior | Green Interior | Green Interior | — |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | Arrius 2B2+ | Arriel 2E | HE Arrano | Makila 2A1 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 4000 | 4000 | 3500 |
| Horsepower | 847 | 660 | 894 | — | 2100 |
| No. of Engines | 1 | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 143 | — | — | — | 684 |
| Dimensions | |||||
| Length (ft) | 42.5 | 33.5 | 44.8 | 39.4 | 63.4 |
| Overall Height (ft) | 10 | 12.6 | 13 | 13.1 | 16.3 |
| Rotor Diameter (ft) | 36.1 | 34 | 36.1 | 45.2 | 53.2 |
| Cabin Volume (cu. ft) | — | 173 | 166 | — | 547 |
| Baggage Volume Ext. (cu. ft) | — | — | 46.8 | — | — |