Compare Airbus Helicopters H145 vs Bell 412EPi vs Leonardo AW169
 |  |  | |
| Manufacturer | Airbus Helicopters | Bell | Leonardo |
| Aircraft Type | H145 | 412EPi | AW169 |
| Base Aircraft Price (USD) | $10,200,000 | $ 12,500,000 | $9,450,000 |
| Direct Operating Cost | $ 1,210 | $ 1,487 | $ 1,658 |
| DOC / nm | $ 9.31 | $ 12.09 | $ 11.84 |
| DOC / nm / Seat | $ 0.93 | $ 0.86 | $ 0.99 |
| Max Cruise Speed (ktas) | 130 | 123 | 140 |
| Max Range (nm) | 352 | 363 | 440 |
| Useful Load (lbs) | 4200 | 4829 | - |
| Total Seats | 10 | 14 | 12 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 13 | 10 |
| Max Cabin Seats | 9 | 13 | 10 |
| Min Crew | 1 | 1 | 1 |
| Flight Deck (Base Spec) | EFIS | Bell BasiX-Pro | EFIS |
| Flight Rules | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Weights | |||
| MTOW (lbs) | 8378 | 11900 | 10141 |
| MTOW External Load (lbs) | 8378 | 11900 | - |
| Max External Load (lbs) | 3527 | 4500 | - |
| BEW (lbs) | 4231 | 7071 | - |
| Useful Load (lbs) | 4200 | 4829 | - |
| Fuel Capacity (lbs) | 1434 | 2214 | - |
| Useful Load Max Fuel (lbs) | 2492 | 2615 | - |
| Dimensions | |||
| Rotor Diameter (ft) | 36.1 | 46 | - |
| Width (ft) | - | 33 | - |
| Overall Height (ft) | 13 | 11.5 | 14.8 |
| Length (ft) | 44.8 | 52.1 | 48.1 |
| Cabin Volume (cu. ft) | 166 | 220 | 222.5 |
| Baggage Volume Ext. (cu. ft) | 46.8 | 28 | 49.5 |
| Engine | |||
| No. of Engines | 2 | 2 | 2 |
| Manufacturer | Airbus Helicopters | Bell | Leonardo |
| Model | Arriel 2E | PT6T-9 | PW210A |
| Horsepower | 894 | 1370 | 1000 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 4000 | 4000 | 4000 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| Fuel Capacity (gal) | - | 330.5 | - |
| Fuel Burn (gph) | - | 113 | - |
| Avionics | |||
| Flight Deck | EFIS | Bell BasiX-Pro | EFIS |
| Flight Rules | IFR | IFR | IFR |
| Standby Instrument | Digital | Gyro | - |
| FMS | - | 1 | 2 |
| Autopilot | 4-Axis | 1 x 3-Axis | 2 |
| PFD | 2 | 2 | - |
| MFD | - | 2 | - |
| GPS | 1 | 1 | 1 |
| AHRS | 3 | - | - |
| Flight Director | - | 2 | - |
| ADC | - | 2 | - |
| Transponder | 1 | 1 | 1 |
| VHF Com | 1 | 2 | 1 |
| VHF NAV | 1 | 2 | 1 |
| Cabin | |||
| Total Seats | 10 | 14 | 12 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 13 | 10 |
| Max Cabin Seats | 9 | 13 | 10 |
| Min Crew | 1 | 1 | 1 |
| Configuration | Green Interior | - | - |
| Other | |||
| Gear Type | Retractable Wheels | Low Skids | Retractable Wheels |
| Rotorhead | 4-Blade Articulated | 4-Blade Articulated | 5-Blade Articulated |
| Tail Rotor | Enclosed Fenestron | 2-Blade | 3-Blade |
| Warranty | |||
| Pilot Training Credits | - | 2 | - |
| MTX Training Credits | - | 1 | - |
| Airframe (Yrs) | - | 3 | - |
| Airframe (Hrs) | - | 1000 | - |
| Engine (Hrs) | - | 1000 | - |
| Performance | |||
| Max Cruise Speed (ktas) | 130 | 123 | 140 |
| Long Range Cruise (ktas) | 127 | 123 | 140 |
| Max Speed (Vne) | 143 | 140 | 165 |
| Max Range (nm) | 352 | 363 | 440 |
| Range Seats Full (nm) | 352 | 363 | 440 |
| Endurance (hrs) | 3.6 | 3.8 | - |
| Max Climb Rate (fpm) | 925 | 1600 | - |
| Service Ceiling (ft) | - | 15720 | - |
| Hover IGE (ft) | 12550 | 11400 | 14500 |
| Hover OGE (ft) | 8750 | 6700 | 11000 |