Compare Airbus Helicopters H130 vs Airbus Helicopters H160 vs Leonardo AW609 Tiltrotor vs Sikorsky S-76D vs Sikorsky S-92
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| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo | Sikorsky | Sikorsky |
| Aircraft Type | H130 | H160 | AW609 Tiltrotor | S-76D | S-92 |
| Base Aircraft Price (USD) | $3,450,000 | $14,000,000 | $20,000,000 | $14,900,000 | $30,650,000 |
| Direct Operating Cost | $ 640 | - | - | $ 1,781 | $ 3,068 |
| DOC / nm | $ 5.00 | - | - | $ 11.49 | $ 19.79 |
| DOC / nm / Seat | $ 0.71 | - | - | $ 0.96 | $ 0.94 |
| Max Cruise Speed (ktas) | 128 | 155 | - | 155 | 155 |
| Max Range (nm) | 333 | 460 | - | 441 | 439 |
| Useful Load (lbs) | 2299 | 3992 | - | - | 7417 |
| Total Seats | 7 | 14 | - | 12 | 21 |
| Cockpit | 3 | 2 | - | 2 | 2 |
| Standard Cabin Seats | 4 | 12 | - | 10 | 19 |
| Max Cabin Seats | 5 | 12 | - | 10 | 19 |
| Min Crew | 1 | 2 | - | 2 | 2 |
| Flight Deck (Base Spec) | Garmin G500H | EFIS | - | Thales TopDeck | EFIS |
| Flight Rules | VFR | IFR | - | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | - | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | Un-Verified | - | Un-Verified | Un-Verified |
| Weights | |||||
| MTOW (lbs) | 5512 | 12500 | - | 11700 | 26500 |
| MTOW External Load (lbs) | 6724 | 12500 | - | - | - |
| Max External Load (lbs) | 3307 | 3527 | - | - | - |
| BOW (lbs) | - | - | - | - | 19083 |
| BEW (lbs) | 3206 | 9348 | - | - | - |
| Useful Load (lbs) | 2299 | 3992 | - | - | 7417 |
| Fuel Capacity (lbs) | 858 | - | - | 296 | 5092 |
| Useful Load Max Fuel (lbs) | 1448 | - | - | - | 2325 |
| Dimensions | |||||
| Rotor Diameter (ft) | 35.1 | 45.2 | - | 44 | - |
| Overall Height (ft) | 11.1 | 13.1 | - | 14.5 | 17.8 |
| Length (ft) | 41.5 | 39.4 | - | 52.5 | - |
| Cabin Volume (cu. ft) | - | - | - | - | 775 |
| Baggage Volume Ext. (cu. ft) | - | - | - | - | 140 |
| Engine | |||||
| No. of Engines | 1 | 2 | - | 1 | 1 |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo | Sikorsky | Sikorsky |
| Model | Arriel 2D | HE Arrano | - | PW210S | CT7-8A |
| Horsepower | 952 | - | - | 1077 | 2520 |
| FADEC | Yes | Yes | - | Yes | Yes |
| TBO (hrs) | 5000 | 4000 | - | 4000 | 4000 |
| Fuel Type | JetFuel | JetFuel | - | JetFuel | JetFuel |
| Fuel Capacity (gal) | 143 | - | - | 296 | 760 |
| Avionics | |||||
| Flight Deck | Garmin G500H | EFIS | - | Thales TopDeck | EFIS |
| Flight Rules | VFR | IFR | - | IFR | IFR |
| Standby Instrument | Gyro / Analog | Digital | - | - | - |
| FMS | - | 1 | - | 1 | 1 |
| Autopilot | - | 4-Axis | - | 1 | 1 |
| PFD | - | 2 | - | 2 | 2 |
| MFD | - | - | - | 2 | 2 |
| GPS | 1 | 1 | - | 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 | 7 | 14 | - | 12 | 21 |
| Cockpit | 3 | 2 | - | 2 | 2 |
| Standard Cabin Seats | 4 | 12 | - | 10 | 19 |
| Max Cabin Seats | 5 | 12 | - | 10 | 19 |
| Min Crew | 1 | 2 | - | 2 | 2 |
| Configuration | - | Green Interior | - | - | - |
| Other | |||||
| Gear Type | Low Skids | Retractable Wheels | - | High Skids | High Skids |
| Rotorhead | 3-Blade Articulated | 5-Blade Articulated | - | 4-Blade Articulated | 5-Blade Articulated |
| Tail Rotor | Enclosed Fenestron | Enclosed Fenestron | - | 4-Blade | 4-Blade |
| Performance | |||||
| Max Cruise Speed (ktas) | 128 | 155 | - | 155 | 155 |
| Long Range Cruise (ktas) | 125 | 155 | - | 155 | 155 |
| Max Speed (Vne) | 155 | 175 | - | - | - |
| Max Range (nm) | 333 | 460 | - | 441 | 439 |
| Range Seats Full (nm) | 333 | 460 | - | 441 | 322 |
| Endurance (hrs) | 4 | - | - | - | - |
| Max Climb Rate (fpm) | 1600 | 1750 | - | - | 1600 |
| Service Ceiling (ft) | - | 19357 | - | - | - |
| Hover IGE (ft) | 11250 | 9200 | - | - | - |
| Hover OGE (ft) | 9700 | 6500 | - | - | - |