Airbus Helicopters H125 vs Airbus Helicopters H130 vs Airbus Helicopters H135 vs Airbus Helicopters H145 vs Airbus Helicopters H175
Airbus Helicopters’ H125 and H130 sit in the light single‑engine category. The H125 is a rugged utility helicopter with a moderate range and typically carries about 5–6 passengers plus a pilot, while the H130 is a comfort‑oriented light single with similar general range but a roomier cabin, commonly seating up to 6–7 passengers plus a pilot depending on configuration. The H135 and H145 are light twin‑engine helicopters aimed at passenger transport and EMS; both offer greater redundancy and generally longer or comparable practical ranges than the light singles, with the H135 typically configured for about 5–7 passengers plus pilot(s) and the larger‑cabin H145 often carrying about 7–9 passengers plus pilot(s). The H175 is a super‑medium twin‑engine helicopter designed for offshore and longer‑distance missions, delivering the greatest range in this group and the highest capacity, commonly around 12–16 passengers depending on layout. Overall, capability, range, and passenger capacity generally step up from H125/H130 to H135/H145, and peak with the H175.
| Spec | AIRBUS H125 | AIRBUS H130 | AIRBUS H135 | AIRBUS H145 | AIRBUS H175 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 3 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 6.33 | $ 9.31 | $ 13.53 |
| Min Crew | 1 | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 7 | 9 | 10 | 18 |
| Flight Rules | VFR | VFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H125 | H130 | H135 | H145 | H175 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 333 | 342 | 352 | 573 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.79 | $ 0.93 | $ 0.75 |
| Max Cabin Seats | 5 | 5 | 7 | 9 | 18 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | 3124 | 4200 | 6797 |
| Standard Cabin Seats | 4 | 4 | 7 | 8 | 16 |
| Direct Operating Cost | $ 627 | $ 640 | $ 861 | $ 1,210 | $ 2,016 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | Helionix | EFIS | EFIS |
| Max Cruise Speed (ktas) | 136 | 128 | 136 | 130 | 149 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $6,150,000 | $10,200,000 | $17,900,000 |
| Cabin | |||||
| Cockpit | 2 | 3 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 7 | 9 | 10 | 18 |
| Max Cabin Seats | 5 | 5 | 7 | 9 | 18 |
| Standard Cabin Seats | 4 | 4 | 7 | 8 | 16 |
| Configuration | — | — | Green Interior | Green Interior | — |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | Arriel 2D | Arrius 2B2+ | Arriel 2E | PT6A-67E |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 5000 | 4000 | 4000 | 3500 |
| Horsepower | 847 | 952 | 660 | 894 | 1775 |
| No. of Engines | 1 | 1 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 143 | 143 | — | — | — |
| Dimensions | |||||
| Length (ft) | 42.5 | 41.5 | 33.5 | 44.8 | 59.2 |
| Overall Height (ft) | 10 | 11.1 | 12.6 | 13 | 17.5 |
| Rotor Diameter (ft) | 36.1 | 35.1 | 34 | 36.1 | 48.5 |
| Cabin Volume (cu. ft) | — | — | 173 | 166 | 423.8 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 46.8 | 81.9 |