Beechcraft King Air 360 Er vs Bell 525 Relentless vs Dassault Falcon 8x
The Beechcraft King Air 360ER is a twin‑turboprop utility/business aircraft suited to short and medium trips and operations from smaller airfields. It typically carries about 6 to 9 passengers in corporate layouts (with higher-density options possible) and offers an extended range on the order of roughly 1,800 to 2,000 nautical miles, depending on payload and conditions. The Bell 525 Relentless is a long‑range, fly‑by‑wire commercial/VIP helicopter. Its strength is point‑to‑point access to heliports and remote sites rather than speed or altitude. Cabin configurations vary, but it generally accommodates about 12 to 16 passengers, with range typically around 500 to 600 nautical miles. The Dassault Falcon 8X is an ultra‑long‑range tri‑jet business aircraft designed for intercontinental missions at high speed and altitude. It commonly seats about 12 to 16 passengers in executive layouts and is rated for roughly 6,400 nautical miles, enabling nonstop city pairs that are beyond the reach of the turboprop and far beyond the helicopter.
| Spec | Bell 525 Relentless | Dassault Falcon 8X |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 17 |
| Flight Rules | IFR | — |
| Manufacturer | Bell | Dassault Falcon |
| Aircraft Name | 525 Relentless | 8X |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6450 |
| Max Cabin Seats | 16 | 16 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 36900 |
| Standard Cabin Seats | 16 | 14 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 160 | 516 |
| Base Aircraft Price (USD) | $15,000,000 | $ 62,500,000 |
| DOC / nm | — | $ 7.66 |
| DOC / nm / Seat | — | $ 0.64 |
| Direct Operating Cost | — | $ 3,805 |
| Cabin | ||
| Cockpit | 2 | 3 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 17 |
| Max Cabin Seats | 16 | 16 |
| Standard Cabin Seats | 16 | 14 |
| Lavatory | — | 2 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD / AFT |
| Cabin Pressure (psi) | — | 10.2 |
| Galley / Refreshment | — | Galley |
| SL Cabin Altitude (ft) | — | 29200 |
| Max Cabin Altitude (ft) | — | 3900 |
| Engine | ||
| FADEC | Dual-Channel | Yes |
| Model | CT7-2F1 | PW307D |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | On-Condition |
| Horsepower | 1800 | — |
| No. of Engines | 2 | 3 |
| Fuel Capacity (gal) | 641 | — |
| Flat Rating | — | ISA + 17 |
| Thrust (lbs) | — | 6722 |
| Dimensions | ||
| Width (ft) | 25.77 | — |
| Length (ft) | 61.58 | 80.2 |
| Cabin Width (ft) | 7.58 | 7.7 |
| Cabin Height (ft) | 4.5 | 6.2 |
| Cabin Length (ft) | 15.5 | 42.7 |
| Overall Height (ft) | 18.18 | 26.1 |
| Rotor Diameter (ft) | 54.5 | — |
| Baggage Volume Ext. (cu. ft) | 128 | — |
| Wingspan (ft) | — | 86.3 |
| Cabin Volume (cu. ft) | — | 1695 |
| Cabin Width - Floor (ft) | — | 6.3 |
| Cabin Length - Seating (ft) | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | 140 |