Bell 525 Relentless vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Pilatus Pc 24
The Bell 525 Relentless is a fly-by-wire civil helicopter, best suited to vertical-access missions (offshore, medical, executive point-to-point) rather than long-range city-pair travel. Its typical range is roughly in the 500–600 nautical mile class with reserves, and it usually carries around 12–16 passengers depending on configuration. The Dassault Falcon 8X is a long-range, large-cabin trijet business jet optimized for intercontinental legs. It offers about 6,000+ nautical miles of range and commonly accommodates 12–16 passengers in executive layouts (with higher-density options possible). The Piaggio Avanti EVO is a twin-turboprop business aircraft focused on speed and efficiency for regional routes. It typically offers around 1,500–1,800 nautical miles of range and seats about 7–9 passengers. The Pilatus PC-24 is a light business jet designed for versatility, including operation from shorter or semi-prepared runways. Its range is generally around 2,000 nautical miles, and it typically carries 6–10 passengers (with commuter-style seating options up to about 11).
| Spec | Bell 525 Relentless | Dassault Falcon 8X | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 17 | 8 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Bell | Dassault Falcon | Piaggio | Pilatus |
| Aircraft Name | 525 Relentless | 8X | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6450 | 1530 | 2076 |
| Max Cabin Seats | 16 | 16 | 7 | 10 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | 36900 | 3775 | 6680 |
| Standard Cabin Seats | 16 | 14 | 6 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 516 | 400 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $ 62,500,000 | $ 7,695,000 | $11,800,000 |
| DOC / nm | — | $ 7.66 | — | $ 3.71 |
| DOC / nm / Seat | — | $ 0.64 | — | $ 0.62 |
| Direct Operating Cost | — | $ 3,805 | — | $ 1,619 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 17 | 8 | 6 |
| Max Cabin Seats | 16 | 16 | 7 | 10 |
| Standard Cabin Seats | 16 | 14 | 6 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No | 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 | 9.3 |
| Galley / Refreshment | — | Galley | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 29200 | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | 3900 | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | PW307D | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | 3600 | 5000 |
| Horsepower | 1800 | — | 850 | — |
| No. of Engines | 2 | 3 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 17 | ISA + 28 | ISA + 23 |
| Thrust (lbs) | — | 6722 | — | 3435 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 80.2 | 47.3 | 52.2 |
| Cabin Width (ft) | 7.58 | 7.7 | 6.1 | 5.6 |
| Cabin Height (ft) | 4.5 | 6.2 | 5.8 | 5.1 |
| Cabin Length (ft) | 15.5 | 42.7 | 14.9 | 23 |
| Overall Height (ft) | 18.18 | 26.1 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | — |
| Wingspan (ft) | — | 86.3 | 47.1 | 55.8 |
| Cabin Volume (cu. ft) | — | 1695 | — | — |
| Cabin Width - Floor (ft) | — | 6.3 | 3.5 | 3.8 |
| Cabin Length - Seating (ft) | — | 29.2 | — | 17 |
| Baggage Volume Int. (cu. ft) | — | 140 | 35.2 | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |