Compare Airbus Helicopters H130 vs Beechcraft King Air 360ER vs Dassault Falcon 8X vs Leonardo AW109 Trekker vs Leonardo AW119Kx
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| Manufacturer | Airbus Helicopters | Beechcraft | Dassault Falcon | Leonardo | Leonardo |
| Aircraft Type | H130 | KingAir 350ER | 8X | AW109 Trekker | AW119Kx |
| Base Aircraft Price (USD) | $3,450,000 | $8,750,000 | $ 62,500,000 | $6,950,000 | $3,850,000 |
| Direct Operating Cost | $ 640 | $ 1,324 | $ 3,805 | $ 1,125 | $ 885 |
| DOC / nm | $ 5.00 | $ 4.37 | $ 7.66 | $ 7.40 | $ 6.76 |
| DOC / nm / Seat | $ 0.71 | $ 0.55 | $ 0.64 | $ 0.93 | $ 0.84 |
| Max Cruise Speed (ktas) | 128 | 303 | 516 | 152 | 131 |
| Max Range (nm) | 333 | 2338 | 6450 | 450 | 515 |
| Useful Load (lbs) | 2299 | 6585 | 36900 | - | - |
| Total Seats | 7 | 10 | 17 | 8 | 8 |
| Cockpit | 3 | 2 | 3 | 2 | 2 |
| Standard Cabin Seats | 4 | 8 | 14 | 6 | 6 |
| Max Cabin Seats | 5 | 9 | 16 | 6 | 6 |
| Min Crew | 1 | 1 | 2 | 1 | 1 |
| Flight Deck (Base Spec) | Garmin G500H | Rockwell Collins Pro Line Fusion | Honeywell Primus EASy II | Genesys Aerosystems | Garmin G1000H |
| Flight Rules | VFR | IFR | - | VFR | VFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Weights | |||||
| MRAMP (lbs) | - | 16600 | 73200 | - | - |
| MTOW (lbs) | 5512 | 16500 | 73000 | 7000 | 6283 |
| MTOW External Load (lbs) | 6724 | - | - | - | - |
| Max External Load (lbs) | 3307 | - | - | - | - |
| MLW (lbs) | - | 15675 | 62400 | - | - |
| MZFW (lbs) | - | 13000 | 41000 | - | - |
| BOW (lbs) | - | 10215 | 36100 | - | - |
| BEW (lbs) | 3206 | 9915 | 36100 | - | - |
| Useful Load (lbs) | 2299 | 6585 | 36900 | - | - |
| Max Payload (lbs) | - | 2785 | 4560 | - | - |
| Fuel Capacity (lbs) | 858 | 5192 | 35141 | 1278 | - |
| Useful Load Max Fuel (lbs) | 1448 | - | - | - | - |
| Payload Max Fuel (lbs) | - | 1193 | 1759 | - | - |
| Max Baggage Weight (lbs) | - | 1150 | 2004 | - | - |
| Dimensions | |||||
| Wingspan (ft) | - | 57.9 | 86.3 | - | - |
| Rotor Diameter (ft) | 35.1 | - | - | 35.5 | 35.5 |
| Overall Height (ft) | 11.1 | 14.4 | 26.1 | 11.5 | 11.9 |
| Length (ft) | 41.5 | 46.7 | 80.2 | 42.5 | 42.5 |
| Cabin Height (ft) | - | 4.8 | 6.2 | - | - |
| Cabin Width (ft) | - | 4.5 | 7.7 | - | - |
| Cabin Width - Floor (ft) | - | 4.1 | 6.3 | - | - |
| Cabin Length (ft) | - | 19.5 | 42.7 | - | - |
| Cabin Length - Seating (ft) | - | 19.5 | 29.2 | - | - |
| Cabin Volume (cu. ft) | - | - | 1695 | - | - |
| Baggage Volume Int. (cu. ft) | - | 71 | 140 | - | - |
| Engine | |||||
| No. of Engines | 1 | 1 | 3 | 2 | 1 |
| Manufacturer | Airbus Helicopters | Beechcraft | Dassault Falcon | Leonardo | Leonardo |
| Model | Arriel 2D | PT6A-60A | PW307D | PW207C | PT6B-37A |
| Horsepower | 952 | 1050 | - | 735 | 917 |
| Thrust (lbs) | - | - | 6722 | - | - |
| Flat Rating | - | ISA + 10 | ISA + 17 | - | - |
| FADEC | Yes | Yes | Yes | Yes | Yes |
| TBO (hrs) | 5000 | 3600 | On-Condition | 4000 | 4500 |
| Fuel Type | JetFuel | - | - | JetFuel | JetFuel |
| Fuel Capacity (gal) | 143 | 775 | - | 152 | 160 |
| Avionics | |||||
| Flight Deck | Garmin G500H | Rockwell Collins Pro Line Fusion | Honeywell Primus EASy II | Genesys Aerosystems | Garmin G1000H |
| Flight Rules | VFR | IFR | - | VFR | VFR |
| Standby Instrument | Gyro / Analog | - | - | - | - |
| FMS | - | 2 | 3 | - | - |
| Autopilot | - | 1 | 2 | 1 | 1 |
| PFD | - | 2 | 2 | - | 2 |
| MFD | - | 1 | 2 | - | 1 |
| GPS | 1 | 1 | 3 | 2 | 1 |
| AHRS | - | 1 | 1 | - | - |
| Transponder | 1 | 1 | 2 | 2 | 1 |
| VHF Com | 1 | 2 | 3 | 2 | 1 |
| VHF NAV | 1 | 2 | 3 | 2 | 1 |
| Cabin | |||||
| Total Seats | 7 | 10 | 17 | 8 | 8 |
| Cockpit | 3 | 2 | 3 | 2 | 2 |
| Standard Cabin Seats | 4 | 8 | 14 | 6 | 6 |
| Max Cabin Seats | 5 | 9 | 16 | 6 | 6 |
| Min Crew | 1 | 1 | 2 | 1 | 1 |
| Cargo Door | - | Optional | - | - | - |
| Lavatory | - | Yes (Belted Optional) | 2 Enclosed Flushing | - | - |
| Lavatory Location | - | AFT | FWD / AFT | - | - |
| Galley / Refreshment | - | Refreshment Center | Galley | - | - |
| Galley Location | - | FWD | FWD | - | - |
| Crew Rest | - | - | No | - | - |
| Jump Seat | - | - | Yes | - | - |
| Max Cabin Altitude (ft) | - | - | 3900 | - | - |
| SL Cabin Altitude (ft) | - | - | 29200 | - | - |
| Cabin Pressure (psi) | - | 6.5 | 10.2 | - | - |
| Other | |||||
| Prop Manufacturer | - | Hartzell | - | - | - |
| Prop Description | - | 4-Blade Constant Feathering Reverse | - | - | - |
| APU Manufacturer | - | - | - | - | - |
| APU Model | - | - | - | - | - |
| APU TBO (hrs) | - | - | - | - | - |
| Gear Type | Low Skids | Retractable | - | Skids | Skids |
| Rotorhead | 3-Blade Articulated | - | - | 4-Blade Articulated | 4-Blade Articulated |
| Tail Rotor | Enclosed Fenestron | - | - | 2-Blade | 2-Blade |
| Warranty | |||||
| Airframe (Yrs) | - | - | 3 | - | - |
| Airframe (Hrs) | - | - | 1000 | - | - |
| Engine (Yrs) | - | - | 2 | - | - |
| Engine (Hrs) | - | - | 1000 | - | - |
| APU (Hrs) | - | - | 2000 | - | - |
| Performance | |||||
| Max Cruise Speed (Mach) | - | 0.58 | 0.9 | - | - |
| Max Cruise Speed (ktas) | 128 | 303 | 516 | 152 | 131 |
| Long Range Cruise (Mach) | - | - | 0.85 | - | - |
| Long Range Cruise (ktas) | 125 | 238 | 487 | 152 | 131 |
| Vref (kias) | - | 104 | 106 | - | - |
| Max Speed (Vne) | 155 | - | - | 152 | 152 |
| Stall Speed - Clean (kias) | - | 82 | - | - | - |
| Max Range (nm) | 333 | 2338 | 6450 | 450 | 515 |
| Range Seats Full (nm) | 333 | - | - | 450 | 515 |
| Max Range Crew + 4 (nm) | - | 2271 | 6450 | - | - |
| Endurance (hrs) | 4 | - | - | - | - |
| Take-off FL (ft) | - | 4057 | 5910 | - | - |
| Take-Off (5000 / ISA + 10) | - | 7675 | 8245 | - | - |
| Landing Roll (ft) | - | - | 2240 | - | - |
| Landing >50ft Obst. (ft) | - | 2728 | - | - | - |
| Max Climb Rate (fpm) | 1600 | 2400 | 2055 | - | - |
| Service Ceiling (ft) | - | 35000 | 51000 | - | 24000 |
| Hover IGE (ft) | 11250 | - | - | 15200 | 11000 |
| Hover OGE (ft) | 9700 | - | - | 9600 | 7300 |