Beechcraft King Air 360 Er vs Bell 525 Relentless vs Dassault Falcon 8x vs Piaggio Avanti Evo
The Beechcraft King Air 360ER is a twin‑turboprop utility aircraft suited to short and unimproved runways; it typically carries about 6–9 passengers and offers long turboprop endurance, generally around 1,500–1,800 nautical miles depending on loading and reserves. The Piaggio Avanti EVO is also a turboprop, but optimized for speed and cabin comfort in a smaller business role; it commonly seats 6–7 passengers and has a range roughly in the 1,500–1,800 nautical mile class. The Dassault Falcon 8X is a long‑range, large‑cabin trijet business jet designed for intercontinental missions; it is typically configured for about 12–16 passengers and has an approximate range near 6,450 nautical miles. The Bell 525 Relentless is a super‑medium helicopter aimed at offshore, corporate, and special‑mission use; it commonly carries about 12–16 passengers and has a range on the order of 500–600 nautical miles, trading fixed‑wing speed and range for vertical‑lift flexibility.
| Spec | Bell 525 Relentless | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 17 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Dassault Falcon | Piaggio |
| Aircraft Name | 525 Relentless | 8X | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6450 | 1530 |
| Max Cabin Seats | 16 | 16 | 7 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 36900 | 3775 |
| Standard Cabin Seats | 16 | 14 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 516 | 400 |
| Base Aircraft Price (USD) | $15,000,000 | $ 62,500,000 | $ 7,695,000 |
| DOC / nm | — | $ 7.66 | — |
| DOC / nm / Seat | — | $ 0.64 | — |
| Direct Operating Cost | — | $ 3,805 | — |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 17 | 8 |
| Max Cabin Seats | 16 | 16 | 7 |
| Standard Cabin Seats | 16 | 14 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | 9 |
| Galley / Refreshment | — | Galley | No |
| SL Cabin Altitude (ft) | — | 29200 | 24000 |
| Max Cabin Altitude (ft) | — | 3900 | 6600 |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW307D | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | On-Condition | 3600 |
| Horsepower | 1800 | — | 850 |
| No. of Engines | 2 | 3 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 17 | ISA + 28 |
| Thrust (lbs) | — | 6722 | — |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 80.2 | 47.3 |
| Cabin Width (ft) | 7.58 | 7.7 | 6.1 |
| Cabin Height (ft) | 4.5 | 6.2 | 5.8 |
| Cabin Length (ft) | 15.5 | 42.7 | 14.9 |
| Overall Height (ft) | 18.18 | 26.1 | 13.1 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 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 |