Compare Airbus ACJ350 vs Airbus Helicopters H145 vs Leonardo AW139
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| Manufacturer | Airbus | Airbus Helicopters | Leonardo |
| Aircraft Type | ACJ350 | H145 | AW139 |
| Base Aircraft Price (USD) | $366,000,000 | $10,200,000 | $15,900,000 |
| Direct Operating Cost | - | $ 1,210 | $ 1,929 |
| DOC / nm | - | $ 9.31 | $ 11.69 |
| DOC / nm / Seat | - | $ 0.93 | $ 0.69 |
| Max Cruise Speed (ktas) | 470 | 130 | 165 |
| Max Range (nm) | 11100 | 352 | 573 |
| Useful Load (lbs) | 32500 | 4200 | 4701 |
| Total Seats | 12 | 10 | 17 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | - | 8 | 15 |
| Max Cabin Seats | 35 | 9 | 15 |
| Min Crew | 4 | 1 | 2 |
| Flight Deck (Base Spec) | Thales | EFIS | EFIS |
| Flight Rules | - | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Weights | |||
| MTOW (lbs) | 172400 | 8378 | 15430 |
| MTOW External Load (lbs) | - | 8378 | - |
| Max External Load (lbs) | - | 3527 | - |
| MLW (lbs) | 140850 | - | - |
| MZFW (lbs) | 116850 | - | - |
| BOW (lbs) | 102000 | - | 9409 |
| BEW (lbs) | - | 4231 | 7985 |
| Useful Load (lbs) | 32500 | 4200 | 4701 |
| Fuel Capacity (lbs) | 66000 | 1434 | 3276 |
| Useful Load Max Fuel (lbs) | - | 2492 | 1937 |
| Dimensions | |||
| Wingspan (ft) | 212 ft 5 in | - | - |
| Rotor Diameter (ft) | - | 36.1 | 54.7 |
| Overall Height (ft) | 55 ft 11 in | 13 | 16.4 |
| Length (ft) | 219 ft 2 in | 44.8 | 54.7 |
| Cabin Width (ft) | 167 ft 5 in | - | - |
| Cabin Width - Floor (ft) | 2,905 sq ft | - | - |
| Cabin Length (ft) | 167 ft 5 in | - | - |
| Cabin Volume (cu. ft) | 30,162 cu ft | 166 | 282 |
| Baggage Volume Ext. (cu. ft) | - | 46.8 | 120 |
| Engine | |||
| No. of Engines | - | 2 | 2 |
| Manufacturer | Airbus | Airbus Helicopters | Leonardo |
| Model | Trent XWB 84 | Arriel 2E | PT6C-67C |
| Horsepower | - | 894 | 1679 |
| FADEC | - | Yes | Yes |
| TBO (hrs) | - | 4000 | 5000 |
| Fuel Type | - | JetFuel | JetFuel |
| Fuel Capacity (gal) | 43985 | - | 414 |
| Avionics | |||
| Flight Deck | - | EFIS | EFIS |
| Flight Rules | - | IFR | IFR |
| Standby Instrument | - | Digital | - |
| FMS | - | - | 2 |
| Autopilot | - | 4-Axis | 2 |
| PFD | - | 2 | - |
| GPS | - | 1 | 1 |
| AHRS | - | 3 | - |
| Transponder | - | 1 | 1 |
| VHF Com | - | 1 | 1 |
| VHF NAV | - | 1 | 1 |
| Cabin | |||
| Total Seats | 12 | 10 | 17 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | - | 8 | 15 |
| Max Cabin Seats | 35 | 9 | 15 |
| Min Crew | 4 | 1 | 2 |
| Configuration | - | Green Interior | - |
| Other | |||
| Gear Type | - | Retractable Wheels | Retractable Wheels |
| Rotorhead | - | 4-Blade Articulated | 5-Blade Articulated |
| Tail Rotor | - | Enclosed Fenestron | 4-Blade |
| Performance | |||
| Max Cruise Speed (ktas) | 470 | 130 | 165 |
| Long Range Cruise (ktas) | - | 127 | 140 |
| Max Speed (Vne) | - | 143 | 167 |
| Max Range (nm) | 11100 | 352 | 573 |
| Range Seats Full (nm) | - | 352 | 302 |
| Endurance (hrs) | - | 3.6 | - |
| Max Climb Rate (fpm) | - | 925 | 2140 |
| Service Ceiling (ft) | - | - | 20000 |
| Hover IGE (ft) | - | 12550 | 15360 |
| Hover OGE (ft) | - | 8750 | 8130 |