Airbus Helicopters H225 vs Dassault Falcon 8x vs Enstrom 480b vs Pilatus Pc 24
The Airbus H225 and Enstrom 480B are helicopters, while the Dassault Falcon 8X and Pilatus PC-24 are fixed‑wing business jets. The H225 is a large, long‑range twin‑engine helicopter typically used for offshore transport, SAR, and utility missions; it generally carries around 16–19 passengers in transport seating and has a practical range on the order of roughly 400–500 nautical miles depending on reserves and configuration. The Enstrom 480B is a light single‑engine helicopter aimed at training and personal/utility use; it usually seats 4–5 and has a much shorter range, roughly 250–350 nautical miles. The Falcon 8X is an ultra‑long‑range large‑cabin business jet, typically configured for about 12–16 passengers, with intercontinental range around 6,400 nautical miles. The Pilatus PC‑24 is a “super versatile” light jet designed for short/rough-field capability; it typically carries 6–10 passengers and offers a mid‑range capability of roughly 2,000 nautical miles, bridging the gap between helicopters and long‑range jets in access and flexibility.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | $ 3.71 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Pilatus |
| Aircraft Name | H225 | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 6680 |
| Standard Cabin Seats | 19 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 6 |
| Max Cabin Seats | 28 | 16 | 10 |
| Standard Cabin Seats | 19 | 14 | 6 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Crew Rest | — | No | No |
| Jump Seat | — | Yes | No |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD |
| Cabin Pressure (psi) | — | 10.2 | 9.3 |
| Galley / Refreshment | — | Galley | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 29200 | 23500 |
| Max Cabin Altitude (ft) | — | 3900 | — |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | 6722 | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 80.2 | 52.2 |
| Overall Height (ft) | 16.3 | 26.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — |
| Wingspan (ft) | — | 86.3 | 55.8 |
| Cabin Width (ft) | — | 7.7 | 5.6 |
| Cabin Height (ft) | — | 6.2 | 5.1 |
| Cabin Length (ft) | — | 42.7 | 23 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | 29.2 | 17 |
| Baggage Volume Int. (cu. ft) | — | 140 | 90 |
| Aisle Step (ft) | — | — | Flat Floor |