Compare Beechcraft King Air 360ER vs Bombardier Global 5500 vs Dassault Falcon 6X vs Gulfstream G500
 |  |  |  | |
| Manufacturer | Beechcraft | Bombardier | Dassault Falcon | Gulfstream |
| Aircraft Type | KingAir 350ER | Global 5500 | 6X | G500 |
| Base Aircraft Price (USD) | $8,750,000 | $46,000,000 | $49,500,000 | $47,500,000 |
| Direct Operating Cost | $ 1,324 | $ 4,895 | $ 3,845 | $ 4,644 |
| DOC / nm | $ 4.37 | $ 9.49 | $ 7.74 | $ 9.00 |
| DOC / nm / Seat | $ 0.55 | $ 0.79 | $ 0.64 | $ 0.90 |
| Max Cruise Speed (ktas) | 303 | 504 | 516 | 516 |
| Max Range (nm) | 2338 | 5700 | 5500 | 5200 |
| Useful Load (lbs) | 6585 | - | - | 30650 |
| Total Seats | 10 | 14 | 17 | 12 |
| Cockpit | 2 | 2 | 3 | 2 |
| Standard Cabin Seats | 8 | 12 | 14 | 10 |
| Max Cabin Seats | 9 | 16 | 16 | 19 |
| Min Crew | 1 | 2 | 2 | 4 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy III | Gulfstream Symmetry Flight Deck |
| Flight Rules | IFR | - | - | - |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Weights | ||||
| MRAMP (lbs) | 16600 | 92750 | 77260 | 77250 |
| MTOW (lbs) | 16500 | 92500 | 77460 | 79600 |
| MLW (lbs) | 15675 | 78600 | 66190 | 64350 |
| MZFW (lbs) | 13000 | 58000 | 45920 | 52100 |
| BOW (lbs) | 10215 | 50861 | - | 46850 |
| BEW (lbs) | 9915 | - | - | - |
| Useful Load (lbs) | 6585 | - | - | 30650 |
| Max Payload (lbs) | 2785 | - | - | 5500 |
| Fuel Capacity (lbs) | 5192 | 39250 | 33790 | 28850 |
| Useful Load Max Fuel (lbs) | - | 7139 | - | - |
| Payload Max Fuel (lbs) | 1193 | - | - | 1800 |
| Max Baggage Weight (lbs) | 1150 | - | 2004 | 2250 |
| Dimensions | ||||
| Wingspan (ft) | 57.9 | 94 | 85.1 | 86.3 |
| Overall Height (ft) | 14.4 | 25.5 | 24.5 | 25.5 |
| Length (ft) | 46.7 | 96 | 84.3 | 91.2 |
| Cabin Height (ft) | 4.8 | 6.2 | 6.5 | 6.4 |
| Aisle Step (ft) | - | - | - | Flat Floor |
| Cabin Width (ft) | 4.5 | 8 | 8.5 | 7.6 |
| Cabin Width - Floor (ft) | 4.1 | - | 6.3 | 6.1 |
| Cabin Length (ft) | 19.5 | 40.8 | 40.4 | 41.5 |
| Cabin Length - Seating (ft) | 19.5 | - | 27.5 | 26.3 |
| Cabin Volume (cu. ft) | - | - | 1843 | - |
| Baggage Volume Int. (cu. ft) | 71 | - | 140 | 230 |
| Engine | ||||
| No. of Engines | 1 | 2 | 2 | 2 |
| Manufacturer | Beechcraft | Bombardier | Dassault Falcon | Gulfstream |
| Model | PT6A-60A | Pearl | PW812D | PW814GA |
| Horsepower | 1050 | - | - | - |
| Thrust (lbs) | - | 15125 | 14000 | 15144 |
| Flat Rating | ISA + 10 | - | ISA + 17 | ISA + 15 |
| FADEC | Yes | Yes | Yes | Yes |
| TBO (hrs) | 3600 | On-Condition | 5000 | 10000 |
| Fuel Capacity (gal) | 775 | - | - | - |
| Avionics | ||||
| Flight Deck | Rockwell Collins Pro Line Fusion | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy III | Gulfstream Symmetry Flight Deck |
| Flight Rules | IFR | - | - | - |
| FMS | 2 | 1 | 3 | 3 |
| Autopilot | 1 | 1 | 2 | 2 |
| PFD | 2 | 2 | 2 | 2 |
| MFD | 1 | 2 | 2 | 2 |
| GPS | 1 | 2 | 3 | 3 |
| AHRS | 1 | 2 | 1 | 1 |
| ADC | - | 2 | - | - |
| Transponder | 1 | 2 | 2 | 2 |
| VHF Com | 2 | 2 | 3 | 3 |
| VHF NAV | 2 | 2 | 3 | 3 |
| Cabin | ||||
| Total Seats | 10 | 14 | 17 | 12 |
| Cockpit | 2 | 2 | 3 | 2 |
| Standard Cabin Seats | 8 | 12 | 14 | 10 |
| Max Cabin Seats | 9 | 16 | 16 | 19 |
| Min Crew | 1 | 2 | 2 | 4 |
| Cargo Door | Optional | - | - | - |
| Lavatory | Yes (Belted Optional) | 2 Enclosed Flushing | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Lavatory Location | AFT | FWD / AFT | FWD / AFT | FWD / AFT |
| Galley / Refreshment | Refreshment Center | Galley | Galley | Galley |
| Galley Location | FWD | FWD | FWD | FWD |
| Crew Rest | - | No | No | No |
| Jump Seat | - | Yes | Yes | Yes |
| Max Cabin Altitude (ft) | - | - | 3900 | - |
| SL Cabin Altitude (ft) | - | - | 29200 | 31900 |
| Cabin Pressure (psi) | 6.5 | - | 10.2 | 10.7 |
| Other | ||||
| Prop Manufacturer | Hartzell | - | - | - |
| Prop Description | 4-Blade Constant Feathering Reverse | - | - | - |
| APU Manufacturer | - | - | - | - |
| APU Model | - | - | - | - |
| APU TBO (hrs) | - | - | - | - |
| Gear Type | Retractable | - | - | - |
| Warranty | ||||
| Airframe (Yrs) | - | 3 | 3 | 3 |
| Airframe (Hrs) | - | 1000 | 1000 | 1000 |
| Engine (Yrs) | - | 2 | 2 | 2 |
| Engine (Hrs) | - | 1000 | 1000 | 1000 |
| APU (Hrs) | - | 2000 | 2000 | 2000 |
| Performance | ||||
| Max Cruise Speed (Mach) | 0.58 | 0.88 | 0.9 | 0.9 |
| Max Cruise Speed (ktas) | 303 | 504 | 516 | 516 |
| Long Range Cruise (Mach) | - | 0.85 | 0.8 | 0.85 |
| Long Range Cruise (ktas) | 238 | 487 | 458 | 487 |
| Vref (kias) | 104 | - | 106 | - |
| Stall Speed - Clean (kias) | 82 | - | - | - |
| Max Range (nm) | 2338 | 5700 | 5500 | 5200 |
| Max Range Crew + 4 (nm) | 2271 | 5700 | 5500 | 5200 |
| Max Range Crew + 6 (nm) | - | 5700 | - | 5200 |
| Max Range Crew + 8 (nm) | - | 5700 | - | 5200 |
| Take-off FL (ft) | 4057 | 5490 | 5480 | 5200 |
| Take-Off (5000 / ISA + 10) | 7675 | - | 7815 | - |
| Landing Roll (ft) | - | 2207 | 2480 | 3100 |
| Landing >50ft Obst. (ft) | 2728 | - | - | - |
| Max Climb Rate (fpm) | 2400 | - | - | - |
| Service Ceiling (ft) | 35000 | 51000 | 51000 | 51000 |