Beechcraft King Air 360 Er vs Bell 525 Relentless vs Bombardier Global 7500 vs Piaggio Avanti Evo
The Beechcraft King Air 360ER is a twin‑turboprop business/utility aircraft optimized for short and unimproved runways, typically carrying about 6–9 passengers with a long-range profile around 1,800–2,000 nautical miles depending on payload and reserves. The Piaggio Avanti EVO is also a twin‑turboprop, positioned as a fast, efficient executive aircraft; it commonly seats about 6–8 passengers and offers roughly 1,500–1,800 nautical miles of range. The Bell 525 Relentless is a super‑medium helicopter rather than a fixed‑wing aircraft, aimed at offshore and corporate missions; typical executive layouts carry about 12–16 passengers, with range on the order of roughly 500–600 nautical miles (highly configuration‑dependent). The Bombardier Global 7500 is an ultra‑long‑range business jet built for intercontinental travel, generally accommodating about 8–19 passengers in multiple cabin zones, with a published range of about 7,700 nautical miles, far exceeding the turboprops and the helicopter for nonstop distance.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Bombardier | Piaggio |
| Aircraft Name | 525 Relentless | Global 7500 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 1530 |
| Max Cabin Seats | 16 | 19 | 7 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — | 3775 |
| Standard Cabin Seats | 16 | 12 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 516 | 400 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $ 7,695,000 |
| DOC / nm | — | $ 9.50 | — |
| Aircraft Type | — | Business Jet | — |
| DOC / nm / Seat | — | $ 0.79 | — |
| Direct Operating Cost | — | $ 4,900 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 8 |
| Max Cabin Seats | 16 | 19 | 7 |
| Standard Cabin Seats | 16 | 12 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | Yes | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Galley / Refreshment | — | Galley | No |
| Max Cabin Altitude (ft) | — | 4500 | 6600 |
| Cabin Pressure (psi) | — | — | 9 |
| SL Cabin Altitude (ft) | — | — | 24000 |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | Passport | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | On-Condition | 3600 |
| Horsepower | 1800 | — | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 28 |
| Thrust (lbs) | — | 18920 | — |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 111 | 47.3 |
| Cabin Width (ft) | 7.58 | 8 | 6.1 |
| Cabin Height (ft) | 4.5 | 6.2 | 5.8 |
| Cabin Length (ft) | 15.5 | 54.5 | 14.9 |
| Overall Height (ft) | 18.18 | 27 | 13.1 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 104 | 47.1 |
| Cabin Width - Floor (ft) | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 |