Beechcraft King Air 360er vs Bombardier Global 5500 vs Dassault Falcon 6x vs Gulfstream G500
The Beechcraft King Air 360ER is a twin‑turboprop aircraft typically used for short to medium missions, special operations, and regional business travel. It carries fewer passengers than the large business jets and, while efficient and versatile, has the shortest range of the group (roughly around 1,500–2,000 nm depending on mission and payload), generally seating about 6–9 passengers in executive layouts. The Bombardier Global 5500 is a large-cabin, long-range business jet designed for intercontinental flying, offering roughly ~5,900 nm range and typically accommodating around 12–16 passengers. The Dassault Falcon 6X is an ultra-long-range, large-cabin jet emphasizing cabin width and comfort, with about ~5,500 nm range and typical seating around 12–16 passengers. The Gulfstream G500 is a large-cabin jet positioned for long-range missions a step below the largest Gulfstreams, offering roughly ~5,300 nm range and commonly configured for about 12–16 passengers.
| Spec | Beechcraft King Air 360ER | Bombardier Global 5500 | Dassault Falcon 6X | Gulfstream G500 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 4.37 | $ 9.49 | $ 7.74 | $ 9.00 |
| Min Crew | 1 | 2 | 2 | 4 |
| Total Seats | 10 | 14 | 17 | 12 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Beechcraft | Bombardier | Dassault Falcon | Gulfstream |
| Aircraft Name | KingAir 350ER | Global 5500 | 6X | G500 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 2338 | 5900 | 5500 | 5200 |
| DOC / nm / Seat | $ 0.55 | $ 0.79 | $ 0.64 | $ 0.90 |
| Max Cabin Seats | 9 | 16 | 16 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6585 | — | — | 30650 |
| Standard Cabin Seats | 8 | 12 | 14 | 10 |
| Direct Operating Cost | $ 1,324 | $ 4,895 | $ 3,845 | $ 4,644 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy III | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 303 | 504 | 516 | 516 |
| Base Aircraft Price (USD) | $8,750,000 | $46,000,000 | $49,500,000 | $47,500,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Lavatory | Yes (Belted Optional) | 2 Enclosed Flushing | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Min Crew | 1 | 2 | 2 | 4 |
| Cargo Door | Optional | — | — | — |
| Total Seats | 10 | 14 | 17 | 12 |
| Galley Location | FWD | FWD | FWD | FWD |
| Max Cabin Seats | 9 | 16 | 16 | 19 |
| Lavatory Location | AFT | FWD / AFT | FWD / AFT | FWD / AFT |
| Cabin Pressure (psi) | 6.5 | — | 10.2 | 10.7 |
| Galley / Refreshment | Refreshment Center | Galley | Galley | Galley |
| Standard Cabin Seats | 8 | 12 | 14 | 10 |
| Crew Rest | — | No | No | No |
| Jump Seat | — | Yes | Yes | Yes |
| SL Cabin Altitude (ft) | — | — | 29200 | 31900 |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | Pearl | PW812D | PW814GA |
| TBO (hrs) | 3600 | On-Condition | 5000 | 10000 |
| Horsepower | 1050 | — | — | — |
| Flat Rating | ISA + 10 | — | ISA + 17 | ISA + 15 |
| No. of Engines | 1 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 775 | — | — | — |
| Thrust (lbs) | — | 15125 | 14000 | 15144 |
| Dimensions | ||||
| Length (ft) | 46.7 | 96 | 84.3 | 91.2 |
| Wingspan (ft) | 57.9 | 94 | 85.1 | 86.3 |
| Cabin Width (ft) | 4.5 | 8 | 8.5 | 7.6 |
| Cabin Height (ft) | 4.8 | 6.2 | 6.5 | 6.4 |
| Cabin Length (ft) | 19.5 | 40.8 | 40.4 | 41.5 |
| Overall Height (ft) | 14.4 | 25.5 | 24.5 | 25.5 |
| Cabin Width - Floor (ft) | 4.1 | — | 6.3 | 6.1 |
| Cabin Length - Seating (ft) | 19.5 | — | 27.5 | 26.3 |
| Baggage Volume Int. (cu. ft) | 71 | — | 140 | 230 |
| Cabin Volume (cu. ft) | — | — | 1843 | — |
| Aisle Step (ft) | — | — | — | Flat Floor |