Airbus Helicopters H225 vs Bombardier Global 7500 vs Dassault Falcon 8x vs Pilatus Pc 24
The Airbus H225 is a long‑range, twin‑engine helicopter aimed at offshore, SAR, and utility missions rather than point‑to‑point business travel. Its typical practical range is roughly 500–700 nautical miles depending on payload and reserves, and it can carry about 16–19 passengers in transport seating (more in high‑density layouts). The Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental city pairs. It offers about 7,700 nautical miles of range and typically seats 8–19 passengers depending on cabin configuration. The Dassault Falcon 8X is also an ultra‑long‑range business jet, optimized for efficiency and access to shorter runways. Its range is about 6,450 nautical miles, with typical seating around 8–16 passengers. The Pilatus PC‑24 is a light/super‑light business jet with strong short/rough‑field capability. Its range is roughly 2,000 nautical miles (varies by payload) and it typically carries 6–10 passengers, with higher‑density commuter layouts possible.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 7.66 | $ 3.71 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 17 | 6 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Bombardier | Dassault Falcon | Pilatus |
| Aircraft Name | H225 | Global 7500 | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 6450 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.64 | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | — | 36900 | 6680 |
| Standard Cabin Seats | 19 | 12 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 3,805 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $ 62,500,000 | $11,800,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 17 | 6 |
| Max Cabin Seats | 28 | 19 | 16 | 10 |
| Standard Cabin Seats | 19 | 12 | 14 | 6 |
| Lavatory | — | 2 Enclosed Flushing | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Crew Rest | — | Yes | No | No |
| Jump Seat | — | Yes | Yes | No |
| Galley Location | — | FWD | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD / AFT | FWD |
| Galley / Refreshment | — | Galley | Galley | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | 4500 | 3900 | — |
| Cabin Pressure (psi) | — | — | 10.2 | 9.3 |
| SL Cabin Altitude (ft) | — | — | 29200 | 23500 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 5000 |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | 18920 | 6722 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 80.2 | 52.2 |
| Overall Height (ft) | 16.3 | 27 | 26.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | — |
| Wingspan (ft) | — | 104 | 86.3 | 55.8 |
| Cabin Width (ft) | — | 8 | 7.7 | 5.6 |
| Cabin Height (ft) | — | 6.2 | 6.2 | 5.1 |
| Cabin Length (ft) | — | 54.5 | 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 |