Beechcraft King Air 360er vs Dassault Falcon 7x vs Embraer Praetor 500 vs Piaggio Avanti Evo
By category, the Beechcraft King Air 360ER and Piaggio Avanti EVO are pressurized twin‑turboprops, typically used for short‑to‑medium missions with strong short/rough‑field capability, while the Embraer Praetor 500 is a super‑midsize business jet and the Dassault Falcon 7X is a long‑range, large‑cabin tri‑jet. On range, the Falcon 7X leads comfortably, designed for true intercontinental trips at roughly 5,900–6,000 nm class capability. The Praetor 500 follows as a transcontinental performer around the 3,300–3,400 nm class. The King Air 360ER offers long endurance for a turboprop, generally in the ~1,800–2,000+ nm class depending on configuration and reserves, while the Avanti EVO is typically shorter, around the ~1,500–1,800 nm class. On passenger capacity, the Falcon 7X commonly seats about 12–16 in a large cabin. The Praetor 500 is usually configured for about 8–9. The King Air 360ER typically carries about 6–9. The Avanti EVO generally seats about 7–9, with a compact cabin but efficient cruise for a turboprop.
| Spec | Beechcraft King Air 360ER | Dassault Falcon 7X | Embraer Praetor 500 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 7.75 | $ 6.02 | — |
| Min Crew | 1 | 2 | 2 | 1 |
| Total Seats | 10 | 17 | 9 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Beechcraft | Dassault Falcon | Embraer | Piaggio |
| Aircraft Name | KingAir 350ER | 7X | Praetor 500 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 5950 | 3340 | 1530 |
| DOC / nm / Seat | $ 0.55 | $ 0.65 | $ 0.86 | — |
| Max Cabin Seats | 9 | 16 | 9 | 7 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6585 | 33600 | — | 3775 |
| Standard Cabin Seats | 8 | 14 | 7 | 6 |
| Direct Operating Cost | $ 1,324 | $ 3,850 | $ 2,779 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Honeywell Primus EASy II | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 303 | 516 | 466 | 400 |
| Base Aircraft Price (USD) | $8,750,000 | $53,800,000 | $16,995,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | No |
| Min Crew | 1 | 2 | 2 | 1 |
| Cargo Door | Optional | — | — | — |
| Total Seats | 10 | 17 | 9 | 8 |
| Galley Location | FWD | FWD | FWD | — |
| Max Cabin Seats | 9 | 16 | 9 | 7 |
| Lavatory Location | AFT | FWD / AFT | AFT | — |
| Cabin Pressure (psi) | 6.5 | 10.2 | 9.7 | 9 |
| Galley / Refreshment | Refreshment Center | Galley | Galley | No |
| Standard Cabin Seats | 8 | 14 | 7 | 6 |
| Crew Rest | — | No | No | — |
| Jump Seat | — | Yes | No | — |
| SL Cabin Altitude (ft) | — | 29200 | 27110 | 24000 |
| Max Cabin Altitude (ft) | — | 3900 | 5800 | 6600 |
| Connectivity | — | — | Gogo AVANCE L5 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | PW307A | HTF7500E | PT6A–66B |
| TBO (hrs) | 3600 | 7200 | On-Condition | 3600 |
| Horsepower | 1050 | — | — | 850 |
| Flat Rating | ISA + 10 | ISA + 17 | ISA + 18 | ISA + 28 |
| No. of Engines | 1 | 3 | 2 | 2 |
| Fuel Capacity (gal) | 775 | — | — | — |
| Thrust (lbs) | — | 6402 | 6540 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 46.7 | 76.7 | 64.6 | 47.3 |
| Wingspan (ft) | 57.9 | 86 | 70.5 | 47.1 |
| Cabin Width (ft) | 4.5 | 7.7 | 6.9 | 6.1 |
| Cabin Height (ft) | 4.8 | 6.2 | 6 | 5.8 |
| Cabin Length (ft) | 19.5 | 39.1 | 20.6 | 14.9 |
| Overall Height (ft) | 14.4 | 25.7 | 21.1 | 13.1 |
| Cabin Width - Floor (ft) | 4.1 | 6.3 | 4.7 | 3.5 |
| Cabin Length - Seating (ft) | 19.5 | 26.2 | 17.4 | — |
| Baggage Volume Int. (cu. ft) | 71 | 140 | 40 | 35.2 |
| Cabin Volume (cu. ft) | — | 1552 | — | — |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Baggage Volume Ext. (cu. ft) | — | — | 110 | — |