Compare Airbus Helicopters H160 vs Beechcraft King Air 360ER vs Leonardo AW169
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| Manufacturer | Airbus Helicopters | Beechcraft | Leonardo |
| Aircraft Type | H160 | KingAir 350ER | AW169 |
| Base Aircraft Price (USD) | $14,000,000 | $8,750,000 | $9,450,000 |
| Direct Operating Cost | - | $ 1,324 | $ 1,658 |
| DOC / nm | - | $ 4.37 | $ 11.84 |
| DOC / nm / Seat | - | $ 0.55 | $ 0.99 |
| Max Cruise Speed (ktas) | 155 | 303 | 140 |
| Max Range (nm) | 460 | 2338 | 440 |
| Useful Load (lbs) | 3992 | 6585 | - |
| Total Seats | 14 | 10 | 12 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 12 | 8 | 10 |
| Max Cabin Seats | 12 | 9 | 10 |
| Min Crew | 2 | 1 | 1 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line Fusion | EFIS |
| Flight Rules | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Weights | |||
| MRAMP (lbs) | - | 16600 | - |
| MTOW (lbs) | 12500 | 16500 | 10141 |
| MTOW External Load (lbs) | 12500 | - | - |
| Max External Load (lbs) | 3527 | - | - |
| MLW (lbs) | - | 15675 | - |
| MZFW (lbs) | - | 13000 | - |
| BOW (lbs) | - | 10215 | - |
| BEW (lbs) | 9348 | 9915 | - |
| Useful Load (lbs) | 3992 | 6585 | - |
| Max Payload (lbs) | - | 2785 | - |
| Fuel Capacity (lbs) | - | 5192 | - |
| Payload Max Fuel (lbs) | - | 1193 | - |
| Max Baggage Weight (lbs) | - | 1150 | - |
| Dimensions | |||
| Wingspan (ft) | - | 57.9 | - |
| Rotor Diameter (ft) | 45.2 | - | - |
| Overall Height (ft) | 13.1 | 14.4 | 14.8 |
| Length (ft) | 39.4 | 46.7 | 48.1 |
| Cabin Height (ft) | - | 4.8 | - |
| Cabin Width (ft) | - | 4.5 | - |
| Cabin Width - Floor (ft) | - | 4.1 | - |
| Cabin Length (ft) | - | 19.5 | - |
| Cabin Length - Seating (ft) | - | 19.5 | - |
| Cabin Volume (cu. ft) | - | - | 222.5 |
| Baggage Volume Int. (cu. ft) | - | 71 | - |
| Baggage Volume Ext. (cu. ft) | - | - | 49.5 |
| Engine | |||
| No. of Engines | 2 | 1 | 2 |
| Manufacturer | Airbus Helicopters | Beechcraft | Leonardo |
| Model | HE Arrano | PT6A-60A | PW210A |
| Horsepower | - | 1050 | 1000 |
| Flat Rating | - | ISA + 10 | - |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 4000 | 3600 | 4000 |
| Fuel Type | JetFuel | - | JetFuel |
| Fuel Capacity (gal) | - | 775 | - |
| Avionics | |||
| Flight Deck | EFIS | Rockwell Collins Pro Line Fusion | EFIS |
| Flight Rules | IFR | IFR | IFR |
| Standby Instrument | Digital | - | - |
| FMS | 1 | 2 | 2 |
| Autopilot | 4-Axis | 1 | 2 |
| PFD | 2 | 2 | - |
| MFD | - | 1 | - |
| GPS | 1 | 1 | 1 |
| AHRS | 2 | 1 | - |
| ADC | 1 | - | - |
| Transponder | 1 | 1 | 1 |
| VHF Com | 1 | 2 | 1 |
| VHF NAV | 1 | 2 | 1 |
| Cabin | |||
| Total Seats | 14 | 10 | 12 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 12 | 8 | 10 |
| Max Cabin Seats | 12 | 9 | 10 |
| Min Crew | 2 | 1 | 1 |
| Configuration | Green Interior | - | - |
| Cargo Door | - | Optional | - |
| Lavatory | - | Yes (Belted Optional) | - |
| Lavatory Location | - | AFT | - |
| Galley / Refreshment | - | Refreshment Center | - |
| Galley Location | - | FWD | - |
| Cabin Pressure (psi) | - | 6.5 | - |
| Other | |||
| Prop Manufacturer | - | Hartzell | - |
| Prop Description | - | 4-Blade Constant Feathering Reverse | - |
| Gear Type | Retractable Wheels | Retractable | Retractable Wheels |
| Rotorhead | 5-Blade Articulated | - | 5-Blade Articulated |
| Tail Rotor | Enclosed Fenestron | - | 3-Blade |
| Performance | |||
| Max Cruise Speed (Mach) | - | 0.58 | - |
| Max Cruise Speed (ktas) | 155 | 303 | 140 |
| Long Range Cruise (ktas) | 155 | 238 | 140 |
| Vref (kias) | - | 104 | - |
| Max Speed (Vne) | 175 | - | 165 |
| Stall Speed - Clean (kias) | - | 82 | - |
| Max Range (nm) | 460 | 2338 | 440 |
| Range Seats Full (nm) | 460 | - | 440 |
| Max Range Crew + 4 (nm) | - | 2271 | - |
| Take-off FL (ft) | - | 4057 | - |
| Take-Off (5000 / ISA + 10) | - | 7675 | - |
| Landing >50ft Obst. (ft) | - | 2728 | - |
| Max Climb Rate (fpm) | 1750 | 2400 | - |
| Service Ceiling (ft) | 19357 | 35000 | - |
| Hover IGE (ft) | 9200 | - | 14500 |
| Hover OGE (ft) | 6500 | - | 11000 |