Airbus Helicopters H130 vs Robinson Helicopters R44 Cadet
The Airbus Helicopters H130 and the Robinson Helicopters R44 Cadet sit in different light-helicopter categories and are typically used for different missions. The H130 is a light single‑engine turbine helicopter, commonly positioned as a higher-end aircraft for passenger transport, sightseeing, and utility roles where turbine performance and cabin comfort are priorities. The R44 Cadet is a light single‑engine piston helicopter, generally viewed as a cost-conscious platform aimed more at training and basic transport. In range, the H130 typically offers a longer, more flexible practical reach than the R44 Cadet, helped by turbine power margins and mission-oriented fuel options, though exact numbers vary by configuration, payload, and reserves. The R44 Cadet’s range is adequate for local and regional flying but is usually more limited compared with turbine singles like the H130. For passenger capacity, the H130 is commonly configured to carry a pilot plus up to six passengers (seven seats total), whereas the R44 Cadet is typically configured for a pilot plus three passengers (four seats total), reflecting its training-focused, lighter-weight design.
| Spec | AIRBUS H130 | ROBINSON R44 Cadet |
|---|---|---|
| Summary | ||
| Cockpit | 3 | — |
| DOC / nm | $ 5.00 | $ 2.22 |
| Min Crew | 1 | — |
| Total Seats | 7 | 2 |
| Flight Rules | VFR | VFR |
| Manufacturer | Airbus Helicopters | Robinson Helicopters |
| Aircraft Name | H130 | R44 Cadet |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 333 | 300 |
| DOC / nm / Seat | $ 0.71 | $ 1.11 |
| Max Cabin Seats | 5 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2299 | 763 |
| Standard Cabin Seats | 4 | — |
| Direct Operating Cost | $ 640 | $ 238 |
| Flight Deck (Base Spec) | Garmin G500H | Gyro / Analog |
| Max Cruise Speed (ktas) | 128 | 107 |
| Base Aircraft Price (USD) | $3,450,000 | $344,000 |
| Cabin | ||
| Cockpit | 3 | — |
| Min Crew | 1 | — |
| Total Seats | 7 | 2 |
| Max Cabin Seats | 5 | — |
| Standard Cabin Seats | 4 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | Arriel 2D | O-540 |
| Fuel Type | JetFuel | AvGas |
| TBO (hrs) | 5000 | 2200 |
| Horsepower | 952 | 210 |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 143 | 29.5 |
| TBO (yrs) | — | 12 |
| Fuel Delivery | — | Carbureted |
| Dimensions | ||
| Length (ft) | 41.5 | 38.3 |
| Overall Height (ft) | 11.1 | 10.8 |
| Rotor Diameter (ft) | 35.1 | 33 |
| Baggage Volume Int. (cu. ft) | — | 2.5 |