Airbus Helicopters H125 vs Robinson Helicopters R66 Marine
The Airbus Helicopters H125 and the Robinson Helicopters R66 Marine sit in different parts of the light single‑engine market. The H125 is a higher‑performance light utility helicopter commonly used for commercial work such as aerial services, external load, and operations in hot‑and‑high environments, whereas the R66 Marine is a lighter, more cost‑focused turbine helicopter tailored for private, training, and light utility use, with marine‑oriented equipment aimed at overwater operations. In range, the H125 is generally competitive and often longer‑legged depending on fuel configuration, while the R66 Marine typically offers a solid but more modest range consistent with its smaller size and power class; real‑world endurance for either varies significantly with payload, speed, and reserves. For passenger capacity, the H125 typically accommodates a pilot plus up to five passengers in standard seating, making it a common choice when you need more seats and payload margin. The R66 Marine is usually configured for a pilot plus up to four passengers, which fits smaller groups and lighter mission profiles.
| Spec | AIRBUS H125 | ROBINSON R66 Marine |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.61 | $ 3.49 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 5 |
| Flight Rules | VFR | VFR |
| Manufacturer | Airbus Helicopters | Robinson Helicopters |
| Aircraft Name | H125 | R66 Marine |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 350 |
| DOC / nm / Seat | $ 0.77 | $ 0.70 |
| Max Cabin Seats | 5 | — |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2189 | 1355 |
| Standard Cabin Seats | 4 | 3 |
| Direct Operating Cost | $ 627 | $ 384 |
| Flight Deck (Base Spec) | Garmin G500H | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 110 |
| Base Aircraft Price (USD) | $3,200,000 | $ 965,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 5 |
| Max Cabin Seats | 5 | — |
| Standard Cabin Seats | 4 | 3 |
| Engine | ||
| FADEC | Yes | No |
| Model | Arriel 2D | RR300 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 2000 |
| Horsepower | 847 | 300 |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 143 | 73.6 |
| Dimensions | ||
| Length (ft) | 42.5 | 38.3 |
| Overall Height (ft) | 10 | 11.4 |
| Rotor Diameter (ft) | 36.1 | 33 |
| Cabin Volume (cu. ft) | — | 50 |
| Baggage Volume Ext. (cu. ft) | — | 18 |