Compare Airbus Helicopters H160 vs Beechcraft Bonanza G36 vs Cessna Skylane vs Sikorsky S-76D
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| Manufacturer | Airbus Helicopters | Beechcraft | Cessna | Sikorsky |
| Aircraft Type | H160 | Bonanza G36 | 182 Skylane | S-76D |
| Base Aircraft Price (USD) | $14,000,000 | $925,000 | $530,000 | $14,900,000 |
| Direct Operating Cost | - | $ 204 | $ 146 | $ 1,781 |
| DOC / nm | - | $ 1.16 | $ 1.01 | $ 11.49 |
| DOC / nm / Seat | - | $ 0.19 | $ 0.25 | $ 0.96 |
| Max Cruise Speed (ktas) | 155 | 176 | 145 | 155 |
| Max Range (nm) | 460 | 920 | 915 | 441 |
| Useful Load (lbs) | 3992 | 1050 | - | - |
| Total Seats | 14 | 6 | 4 | 12 |
| Cockpit | 2 | 2 | - | 2 |
| Standard Cabin Seats | 12 | 4 | - | 10 |
| Max Cabin Seats | 12 | - | - | 10 |
| Min Crew | 2 | - | - | 2 |
| Flight Deck (Base Spec) | EFIS | Garmin G1000 NXi | Garmin G1000 NXi | Thales TopDeck |
| Flight Rules | IFR | VFR | VFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Weights | ||||
| MTOW (lbs) | 12500 | 3650 | 3100 | 11700 |
| MTOW External Load (lbs) | 12500 | - | - | - |
| Max External Load (lbs) | 3527 | - | - | - |
| MLW (lbs) | - | 3650 | 2950 | - |
| BEW (lbs) | 9348 | 2600 | - | - |
| Useful Load (lbs) | 3992 | 1050 | - | - |
| Fuel Capacity (lbs) | - | 444 | 522 | 296 |
| Useful Load Max Fuel (lbs) | - | 606 | - | - |
| Max Baggage Weight (lbs) | - | 70 | 200 | - |
| Dimensions | ||||
| Wingspan (ft) | - | 33.5 | 36 | - |
| Rotor Diameter (ft) | 45.2 | - | - | 44 |
| Overall Height (ft) | 13.1 | 8.6 | 9.4 | 14.5 |
| Length (ft) | 39.4 | 27.5 | 29 | 52.5 |
| Cabin Height (ft) | - | 4.2 | 4.1 | - |
| Cabin Width (ft) | - | 3.5 | 3.5 | - |
| Cabin Length (ft) | - | 12.6 | 11.2 | - |
| Cabin Volume (cu. ft) | - | 100 | - | - |
| Baggage Volume Int. (cu. ft) | - | 10 | 32 | - |
| Engine | ||||
| No. of Engines | 2 | 1 | 1 | 1 |
| Manufacturer | Airbus Helicopters | Beechcraft | Cessna | Sikorsky |
| Model | HE Arrano | IO-550-B | IO-540-AB1A5 | PW210S |
| Horsepower | - | 300 | 245 | 1077 |
| FADEC | Yes | No | No | Yes |
| TBO (hrs) | 4000 | 1700 | 2000 | 4000 |
| TBO (yrs) | - | 12 | 12 | - |
| Fuel Type | JetFuel | AvGas | AvGas | JetFuel |
| Fuel Delivery | - | Fuel Injected | Fuel Injected | - |
| Fuel Capacity (gal) | - | 74 | 87 | 296 |
| Avionics | ||||
| Flight Deck | EFIS | Garmin G1000 NXi | Garmin G1000 NXi | Thales TopDeck |
| Flight Rules | IFR | VFR | VFR | IFR |
| Standby Instrument | Digital | - | - | - |
| FMS | 1 | - | - | 1 |
| Autopilot | 4-Axis | Garmin GFC 700 | Garmin GFC 700 | 1 |
| PFD | 2 | 1 | 1 | 2 |
| MFD | - | 1 | 1 | 2 |
| GPS | 1 | - | - | 1 |
| AHRS | 2 | - | - | - |
| ADC | 1 | - | - | - |
| Transponder | 1 | 1 | 1 | 1 |
| VHF Com | 1 | 1 | 1 | 1 |
| VHF NAV | 1 | 1 | 1 | 1 |
| Cabin | ||||
| Total Seats | 14 | 6 | 4 | 12 |
| Cockpit | 2 | 2 | - | 2 |
| Standard Cabin Seats | 12 | 4 | - | 10 |
| Max Cabin Seats | 12 | - | - | 10 |
| Min Crew | 2 | - | - | 2 |
| Configuration | Green Interior | - | - | - |
| Other | ||||
| Prop Manufacturer | - | Hartzell | McCauley | - |
| Prop Description | - | 3-Blade Constant | 3-Blade Constant | - |
| Gear Type | Retractable Wheels | Retractable | Float | High Skids |
| Float Type | - | - | Amphib | - |
| Rotorhead | 5-Blade Articulated | - | - | 4-Blade Articulated |
| Tail Rotor | Enclosed Fenestron | - | - | 4-Blade |
| Performance | ||||
| Max Cruise Speed (ktas) | 155 | 176 | 145 | 155 |
| Long Range Cruise (ktas) | 155 | 137 | - | 155 |
| Max Speed (Vne) | 175 | - | - | - |
| Stall Speed - Clean (kias) | - | 59 | 49 | - |
| Max Range (nm) | 460 | 920 | 915 | 441 |
| Range Seats Full (nm) | 460 | - | - | 441 |
| Take-off Roll (ft) | - | 1913 | 1514 | - |
| Landing Roll (ft) | - | 1450 | 1350 | - |
| Max Climb Rate (fpm) | 1750 | 1230 | 924 | - |
| Service Ceiling (ft) | 19357 | 18500 | 18100 | - |
| Hover IGE (ft) | 9200 | - | - | - |
| Hover OGE (ft) | 6500 | - | - | - |