Airbus Helicopters H125 vs Airbus Helicopters H130 vs Robinson Helicopters R44 Raven Ii vs Robinson Helicopters R66
The Airbus Helicopters H125 and H130 are light single‑engine turbine helicopters, while the Robinson R44 Raven II is a light piston helicopter and the Robinson R66 is a light single‑engine turbine. In typical use, the H125 is the more utilitarian “workhorse” in the group, widely configured for external‑load and high‑altitude operations; the H130 is oriented more toward passenger comfort and sightseeing with a quieter cabin. The R44 Raven II is generally the lowest‑cost category here, commonly used for training and private flying; the R66 steps up in performance and turbine smoothness while remaining smaller and simpler than the Airbus models. For range, these aircraft broadly overlap, but the turbine models (H125, H130, and R66) are often operated at longer legs and higher cruise speeds than the piston R44; exact range varies heavily with tanks, payload, and reserves. For passenger capacity, the H125 typically seats about five to six occupants, the H130 about six to seven, the R44 up to four, and the R66 up to five (including the pilot).
| Spec | AIRBUS H125 | AIRBUS H130 | ROBINSON R44 Raven II | ROBINSON R66 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | — | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 2.36 | $ 3.49 |
| Min Crew | 1 | 1 | — | 1 |
| Total Seats | 6 | 7 | 4 | 5 |
| Flight Rules | VFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Robinson Helicopters | Robinson Helicopters |
| Aircraft Name | H125 | H130 | R44 Raven II | R66 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 333 | 300 | 350 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.59 | $ 0.70 |
| Max Cabin Seats | 5 | 5 | — | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | 995 | 1355 |
| Standard Cabin Seats | 4 | 4 | — | 3 |
| Direct Operating Cost | $ 627 | $ 640 | $ 257 | $ 384 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 128 | 109 | 110 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $ 490,000 | $ 920,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | — | 2 |
| Min Crew | 1 | 1 | — | 1 |
| Total Seats | 6 | 7 | 4 | 5 |
| Max Cabin Seats | 5 | 5 | — | — |
| Standard Cabin Seats | 4 | 4 | — | 3 |
| Engine | ||||
| FADEC | Yes | Yes | No | No |
| Model | Arriel 2D | Arriel 2D | IO-540 | RR300 |
| Fuel Type | JetFuel | JetFuel | AvGas | JetFuel |
| TBO (hrs) | 5000 | 5000 | 2200 | 2000 |
| Horsepower | 847 | 952 | 245 | 300 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 143 | 29.5 | 73.6 |
| TBO (yrs) | — | — | 12 | — |
| Fuel Delivery | — | — | Fuel Injected | — |
| Dimensions | ||||
| Length (ft) | 42.5 | 41.5 | 38.3 | 38.3 |
| Overall Height (ft) | 10 | 11.1 | 10.8 | 11.4 |
| Rotor Diameter (ft) | 36.1 | 35.1 | 33 | 33 |
| Baggage Volume Int. (cu. ft) | — | — | 2.5 | — |
| Cabin Volume (cu. ft) | — | — | — | 50 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 18 |