Airbus Helicopters H225 vs Enstrom 480b vs Pilatus Pc 24
The Airbus H225 and Enstrom 480B are helicopters, while the Pilatus PC-24 is a fixed‑wing business jet, so their strengths differ sharply. The H225 is a large, long‑range twin‑engine transport helicopter suited to offshore and utility missions; it typically carries around 19 passengers (higher-density layouts can seat more) and offers roughly 450–600 nautical miles of range depending on payload, reserves, and configuration. The Enstrom 480B is a much smaller piston helicopter aimed at light utility and training; it generally seats 4–5 people and has a shorter range, commonly about 200–300 nautical miles. The Pilatus PC-24 is a light jet designed for fast point‑to‑point travel; it typically carries 6–10 passengers in executive layouts (up to about 11 in high-density seating) and has far greater range than either helicopter, roughly 1,800–2,000 nautical miles depending on load and conditions. Overall, the H225 prioritizes lift and vertical access, the 480B prioritizes simplicity and low capacity, and the PC-24 prioritizes speed and long-range passenger transport between runways.
| Spec | AIRBUS H225 | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 3.71 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Pilatus |
| Aircraft Name | H225 | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.62 |
| Max Cabin Seats | 28 | 10 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 6680 |
| Standard Cabin Seats | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $11,800,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Max Cabin Seats | 28 | 10 |
| Standard Cabin Seats | 19 | 6 |
| Lavatory | — | 1 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD |
| Cabin Pressure (psi) | — | 9.3 |
| Galley / Refreshment | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 23500 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 5000 |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 23 |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 63.4 | 52.2 |
| Overall Height (ft) | 16.3 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| Wingspan (ft) | — | 55.8 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width (ft) | — | 5.6 |
| Cabin Height (ft) | — | 5.1 |
| Cabin Length (ft) | — | 23 |
| Cabin Width - Floor (ft) | — | 3.8 |
| Cabin Length - Seating (ft) | — | 17 |
| Baggage Volume Int. (cu. ft) | — | 90 |