Bell 525 Relentless vs Bombardier Global 7500 vs Dassault Falcon 8x vs Piaggio Avanti Evo
The Bell 525 Relentless is a super‑medium helicopter, optimized for vertical access to sites without runways. Its range is roughly in the 500–600 nautical mile class, and typical passenger capacity is about 12–16 depending on cabin layout. By contrast, the Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental missions, offering about 7,000+ nautical miles of range and commonly seating around 14–19 passengers in executive configurations. The Dassault Falcon 8X is also an ultra‑long‑range business jet, with slightly less range than the Global 7500 at roughly 6,400 nautical miles, and typically carries about 12–16 passengers with a focus on efficient trijet performance and runway flexibility. The Piaggio Avanti EVO sits in a different niche as a high‑speed turboprop, generally suited to regional missions; its range is around 1,500–1,800 nautical miles with a typical capacity of about 7–9 passengers. Overall, the Global 7500 and Falcon 8X dominate long‑haul jet travel, the Avanti EVO targets fast regional flying with turboprop economics, and the Bell 525 prioritizes access and landing flexibility over distance.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 17 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Bell | Bombardier | Dassault Falcon | Piaggio |
| Aircraft Name | 525 Relentless | Global 7500 | 8X | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 6450 | 1530 |
| Max Cabin Seats | 16 | 19 | 16 | 7 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — | 36900 | 3775 |
| Standard Cabin Seats | 16 | 12 | 14 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 516 | 516 | 400 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $ 62,500,000 | $ 7,695,000 |
| DOC / nm | — | $ 9.50 | $ 7.66 | — |
| Aircraft Type | — | Business Jet | — | — |
| DOC / nm / Seat | — | $ 0.79 | $ 0.64 | — |
| Direct Operating Cost | — | $ 4,900 | $ 3,805 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 17 | 8 |
| Max Cabin Seats | 16 | 19 | 16 | 7 |
| Standard Cabin Seats | 16 | 12 | 14 | 6 |
| Lavatory | — | 2 Enclosed Flushing | 2 Enclosed Flushing | No |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | Yes | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | FWD / AFT | — |
| Galley / Refreshment | — | Galley | Galley | No |
| Max Cabin Altitude (ft) | — | 4500 | 3900 | 6600 |
| Cabin Pressure (psi) | — | — | 10.2 | 9 |
| SL Cabin Altitude (ft) | — | — | 29200 | 24000 |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | Passport | PW307D | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | On-Condition | 3600 |
| Horsepower | 1800 | — | — | 850 |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 | ISA + 28 |
| Thrust (lbs) | — | 18920 | 6722 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 111 | 80.2 | 47.3 |
| Cabin Width (ft) | 7.58 | 8 | 7.7 | 6.1 |
| Cabin Height (ft) | 4.5 | 6.2 | 6.2 | 5.8 |
| Cabin Length (ft) | 15.5 | 54.5 | 42.7 | 14.9 |
| Overall Height (ft) | 18.18 | 27 | 26.1 | 13.1 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | — |
| Wingspan (ft) | — | 104 | 86.3 | 47.1 |
| Cabin Volume (cu. ft) | — | — | 1695 | — |
| Cabin Width - Floor (ft) | — | — | 6.3 | 3.5 |
| Cabin Length - Seating (ft) | — | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 35.2 |