Airbus Helicopters H125 vs Pilatus Pc 12 Ngx
The Airbus Helicopters H125 is a single‑engine light utility helicopter designed for vertical takeoff and landing, short-hop transport, aerial work, and access to unimproved sites. The Pilatus PC‑12 NGX is a single‑engine turboprop fixed‑wing airplane optimized for longer cross‑country travel from short runways, with higher cruise speed and greater payload efficiency over distance. In range, the PC‑12 NGX generally offers substantially longer legs, typically on the order of roughly 1,500–1,800 nautical miles depending on load and reserves, making it better suited to regional or intercity missions. The H125’s range is much shorter, commonly around roughly 300–350 nautical miles depending on configuration and conditions, but it can reach places without runways and hover for specialized tasks. For passenger capacity, an H125 is usually configured for about 1 pilot plus up to 5–6 passengers (layout dependent). A PC‑12 NGX typically carries 1–2 pilots with about 6–9 passengers in executive or commuter interiors, with more cabin space and baggage volume for longer trips.
| Spec | AIRBUS H125 | Pilatus PC-12 NGX |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.61 | $ 2.78 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 8 |
| Flight Rules | VFR | IFR |
| Manufacturer | Airbus Helicopters | Pilatus |
| Aircraft Name | H125 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 1803 |
| DOC / nm / Seat | $ 0.77 | $ 0.46 |
| Max Cabin Seats | 5 | 9 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 2189 | — |
| Standard Cabin Seats | 4 | 6 |
| Direct Operating Cost | $ 627 | $ 793 |
| Flight Deck (Base Spec) | Garmin G500H | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 136 | 290 |
| Base Aircraft Price (USD) | $3,200,000 | $5,350,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 8 |
| Max Cabin Seats | 5 | 9 |
| Standard Cabin Seats | 4 | 6 |
| 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 |
| Model | Arriel 2D | PT6E-67XP |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 5000 | 5000 |
| Horsepower | 847 | 1200 |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 143 | — |
| Flat Rating | — | ISA + 35 |
| Usable Fuel (gal) | — | 402 |
| Dimensions | ||
| Length (ft) | 42.5 | 47.25 |
| Overall Height (ft) | 10 | 14 |
| Rotor Diameter (ft) | 36.1 | — |
| 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 |