vs Airbus Helicopters H145 vs Airbus Helicopters H175
In category terms, a typical fixed‑wing aircraft (such as a turboprop or light jet) is optimized for point‑to‑point travel at higher speeds and altitudes from runways, while the Airbus Helicopters H145 is a light twin‑engine helicopter designed for short‑range missions with frequent stops and access to tight landing zones, and the H175 is a larger, medium twin‑engine helicopter aimed at heavier‑lift roles and longer sectors, often offshore. For range, fixed‑wing aircraft generally provide the longest legs, commonly several hundred to well over a thousand nautical miles depending on model and reserves, because they are more aerodynamically efficient in cruise. The H145 typically offers a few hundred nautical miles of practical range, while the H175 extends that into a higher bracket than the H145, commonly still within the helicopter “few hundred nautical miles” class but meaningfully longer and with more payload flexibility. On passenger capacity, many small fixed‑wing aircraft seat around 6–19 passengers (and larger airliners far more), the H145 commonly carries roughly 6–9 passengers in typical layouts, and the H175 generally accommodates more, often around 12–16 depending on configuration.
| Spec | AIRBUS H145 | AIRBUS H175 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 9.31 | $ 13.53 |
| Min Crew | 1 | 2 |
| Total Seats | 10 | 18 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H145 | H175 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 573 |
| DOC / nm / Seat | $ 0.93 | $ 0.75 |
| Max Cabin Seats | 9 | 18 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 6797 |
| Standard Cabin Seats | 8 | 16 |
| Direct Operating Cost | $ 1,210 | $ 2,016 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 130 | 149 |
| Base Aircraft Price (USD) | $10,200,000 | $17,900,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 10 | 18 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 9 | 18 |
| Standard Cabin Seats | 8 | 16 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Arriel 2E | PT6A-67E |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 |
| Horsepower | 894 | 1775 |
| No. of Engines | 2 | 2 |
| Dimensions | ||
| Length (ft) | 44.8 | 59.2 |
| Overall Height (ft) | 13 | 17.5 |
| Rotor Diameter (ft) | 36.1 | 48.5 |
| Cabin Volume (cu. ft) | 166 | 423.8 |
| Baggage Volume Ext. (cu. ft) | 46.8 | 81.9 |