Airbus Helicopters H125 vs Airbus Helicopters H130 vs Pilatus Pc 12 Ngx vs Robinson Helicopters R66 Marine
In category, the Airbus H125 and H130 and the Robinson R66 Marine are single‑engine turbine helicopters, while the Pilatus PC‑12 NGX is a single‑engine turboprop fixed‑wing aircraft. For range, the PC‑12 NGX is in a different class, typically capable of well over 1,500 nautical miles, making it suited to longer intercity missions. The H125 and H130 generally offer mid‑hundreds of nautical miles of range, appropriate for regional hops, utility work, and tourism; the H130 is often optimized for quieter passenger operations, while the H125 is commonly chosen for higher‑power utility performance. The R66 Marine typically has the shortest range of the four, also in the mid‑hundreds of nautical miles, and is tailored for maritime environments (e.g., corrosion protection and mission equipment options) rather than maximum distance. For passenger capacity, the PC‑12 NGX typically seats one or two pilots plus up to about 8–9 passengers depending on configuration. The H130 is usually configured for up to around 7 passengers plus a pilot, the H125 for about 5–6 passengers plus a pilot, and the R66 Marine for about 4 passengers plus a pilot.
| Spec | AIRBUS H125 | AIRBUS H130 | Pilatus PC-12 NGX | ROBINSON R66 Marine |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 2.78 | $ 3.49 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 7 | 8 | 5 |
| Flight Rules | VFR | VFR | IFR | VFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Pilatus | Robinson Helicopters |
| Aircraft Name | H125 | H130 | PC-12 NGX | R66 Marine |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 333 | 1803 | 350 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.46 | $ 0.70 |
| Max Cabin Seats | 5 | 5 | 9 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | — | 1355 |
| Standard Cabin Seats | 4 | 4 | 6 | 3 |
| Direct Operating Cost | $ 627 | $ 640 | $ 793 | $ 384 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | Honeywell Primus Apex | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 128 | 290 | 110 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $5,350,000 | $ 965,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 7 | 8 | 5 |
| Max Cabin Seats | 5 | 5 | 9 | — |
| Standard Cabin Seats | 4 | 4 | 6 | 3 |
| Lavatory | — | — | Optional | — |
| Cargo Door | — | — | Yes | — |
| Lavatory Location | — | — | FWD | — |
| Cabin Pressure (psi) | — | — | 5.8 | — |
| Galley / Refreshment | — | — | No | — |
| SL Cabin Altitude (ft) | — | — | 13100 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Arriel 2D | Arriel 2D | PT6E-67XP | RR300 |
| Fuel Type | JetFuel | JetFuel | — | JetFuel |
| TBO (hrs) | 5000 | 5000 | 5000 | 2000 |
| Horsepower | 847 | 952 | 1200 | 300 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 143 | — | 73.6 |
| Flat Rating | — | — | ISA + 35 | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 42.5 | 41.5 | 47.25 | 38.3 |
| Overall Height (ft) | 10 | 11.1 | 14 | 11.4 |
| Rotor Diameter (ft) | 36.1 | 35.1 | — | 33 |
| Wingspan (ft) | — | — | 53.33 | — |
| Cabin Width (ft) | — | — | 5 | — |
| Cabin Height (ft) | — | — | 4.9 | — |
| Cabin Length (ft) | — | — | 16.9 | — |
| Cabin Width - Floor (ft) | — | — | 4.25 | — |
| Baggage Volume Int. (cu. ft) | — | — | 40 | — |
| Cabin Volume (cu. ft) | — | — | — | 50 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 18 |