Airbus Helicopters H225 vs Bell 525 Relentless vs Bombardier Global 7500 vs Dassault Falcon 8x
The Airbus H225 and Bell 525 Relentless are large, long‑range helicopters suited to offshore, search and rescue, and utility missions, while the Bombardier Global 7500 and Dassault Falcon 8X are ultra‑long‑range business jets optimized for intercontinental travel. In range, the Global 7500 leads at roughly 7,700 nautical miles, enabling nonstop city pairs such as New York–Hong Kong in favorable conditions. The Falcon 8X follows at about 6,450 nautical miles. By comparison, helicopter ranges are far shorter: the H225 is typically around 500–600 nautical miles depending on configuration and reserves, and the Bell 525 is in a similar class, roughly 500–600+ nautical miles, with strong hot‑and‑high and offshore performance emphasis. Passenger capacity also differs by category: the Global 7500 commonly seats about 14–19 in executive layouts (higher-density options exist), while the Falcon 8X typically seats about 12–16. The H225 can carry around 19 passengers in high-density transport (often fewer in missionized layouts), and the Bell 525 is generally configured for about 16–20 depending on interior and mission.
| Spec | AIRBUS H225 | Bell 525 Relentless | Bombardier Global 7500 | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 9.50 | $ 7.66 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 18 | 14 | 17 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Airbus Helicopters | Bell | Bombardier | Dassault Falcon |
| Aircraft Name | H225 | 525 Relentless | Global 7500 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 7700 | 6450 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.79 | $ 0.64 |
| Max Cabin Seats | 28 | 16 | 19 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | — | 36900 |
| Standard Cabin Seats | 19 | 16 | 12 | 14 |
| Direct Operating Cost | $ 2,963 | — | $ 4,900 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 160 | 516 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $75,000,000 | $ 62,500,000 |
| Aircraft Type | — | — | Business Jet | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 18 | 14 | 17 |
| Max Cabin Seats | 28 | 16 | 19 | 16 |
| Standard Cabin Seats | 19 | 16 | 12 | 14 |
| Lavatory | — | — | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Crew Rest | — | — | Yes | No |
| Jump Seat | — | — | Yes | Yes |
| Galley Location | — | — | FWD | FWD |
| Lavatory Location | — | — | FWD / AFT | FWD / AFT |
| Galley / Refreshment | — | — | Galley | Galley |
| Max Cabin Altitude (ft) | — | — | 4500 | 3900 |
| Cabin Pressure (psi) | — | — | — | 10.2 |
| SL Cabin Altitude (ft) | — | — | — | 29200 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Makila 2A1 | CT7-2F1 | Passport | PW307D |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | On-Condition | On-Condition |
| Horsepower | 2100 | 1800 | — | — |
| No. of Engines | 2 | 2 | 2 | 3 |
| Fuel Capacity (gal) | 684 | 641 | — | — |
| Flat Rating | — | — | ISA + 15 | ISA + 17 |
| Thrust (lbs) | — | — | 18920 | 6722 |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 111 | 80.2 |
| Overall Height (ft) | 16.3 | 18.18 | 27 | 26.1 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 1695 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 8 | 7.7 |
| Cabin Height (ft) | — | 4.5 | 6.2 | 6.2 |
| Cabin Length (ft) | — | 15.5 | 54.5 | 42.7 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 104 | 86.3 |
| Cabin Width - Floor (ft) | — | — | — | 6.3 |
| Cabin Length - Seating (ft) | — | — | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | — | — | 140 |