Compare Airbus Helicopters H125 vs Airbus Helicopters H145 vs Pilatus PC-12 NGX
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| Manufacturer | Airbus Helicopters | Airbus Helicopters | Pilatus |
| Aircraft Type | H125 | H145 | PC-12 NGX |
| Base Aircraft Price (USD) | $3,200,000 | $10,200,000 | $5,350,000 |
| Direct Operating Cost | $ 627 | $ 1,210 | $ 793 |
| DOC / nm | $ 4.61 | $ 9.31 | $ 2.78 |
| DOC / nm / Seat | $ 0.77 | $ 0.93 | $ 0.46 |
| Max Cruise Speed (ktas) | 136 | 130 | 290 |
| Max Range (nm) | 341 | 352 | 1866 |
| Useful Load (lbs) | 2189 | 4200 | 3692 |
| Total Seats | 6 | 10 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 4 | 8 | 6 |
| Max Cabin Seats | 5 | 9 | 9 |
| Min Crew | 1 | 1 | 1 |
| Flight Deck (Base Spec) | Garmin G500H | EFIS | Honeywell Primus Apex |
| Flight Rules | VFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Weights | |||
| MRAMP (lbs) | - | - | 10495 |
| MTOW (lbs) | 4960 | 8378 | 10450 |
| MTOW External Load (lbs) | 6172 | 8378 | - |
| Max External Load (lbs) | 3086 | 3527 | - |
| MLW (lbs) | - | - | 9921 |
| MZFW (lbs) | - | - | 9039 |
| BOW (lbs) | - | - | 6803 |
| BEW (lbs) | 2816 | 4231 | 6758 |
| Useful Load (lbs) | 2189 | 4200 | 3692 |
| Max Payload (lbs) | - | - | 2235 |
| Fuel Capacity (lbs) | 858 | 1434 | 2704 |
| Useful Load Max Fuel (lbs) | 1551 | 2492 | - |
| Payload Max Fuel (lbs) | - | - | 988 |
| Dimensions | |||
| Wingspan (ft) | - | - | 53.33 |
| Rotor Diameter (ft) | 36.1 | 36.1 | - |
| Overall Height (ft) | 10 | 13 | 14 |
| Length (ft) | 42.5 | 44.8 | 47.25 |
| Cabin Height (ft) | - | - | 4.9 |
| Cabin Width (ft) | - | - | 5 |
| Cabin Width - Floor (ft) | - | - | 4.25 |
| Cabin Length (ft) | - | - | 16.9 |
| Cabin Volume (cu. ft) | - | 166 | - |
| Baggage Volume Int. (cu. ft) | - | - | 40 |
| Baggage Volume Ext. (cu. ft) | - | 46.8 | - |
| Engine | |||
| No. of Engines | 1 | 2 | 1 |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Pilatus |
| Model | Arriel 2D | Arriel 2E | PT6E-67XP |
| Horsepower | 847 | 894 | 1200 |
| Flat Rating | - | - | ISA + 35 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 5000 | 4000 | 5000 |
| Fuel Type | JetFuel | JetFuel | - |
| Fuel Capacity (gal) | 143 | - | - |
| Usable Fuel (gal) | - | - | 402 |
| Avionics | |||
| Flight Deck | Garmin G500H | EFIS | Honeywell Primus Apex |
| Flight Rules | VFR | IFR | IFR |
| Standby Instrument | Gyro / Analog | Digital | - |
| FMS | - | - | 1 |
| Autopilot | - | 4-Axis | 1 |
| PFD | - | 2 | 2 |
| MFD | - | - | 1 |
| GPS | - | 1 | 1 |
| AHRS | - | 3 | 1 |
| Transponder | 1 | 1 | 1 |
| VHF Com | 1 | 1 | 2 |
| VHF NAV | 1 | 1 | 2 |
| Cabin | |||
| Total Seats | 6 | 10 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 4 | 8 | 6 |
| Max Cabin Seats | 5 | 9 | 9 |
| Min Crew | 1 | 1 | 1 |
| Configuration | - | Green Interior | - |
| Cargo Door | - | - | Yes |
| Lavatory | - | - | Optional |
| Lavatory Location | - | - | FWD |
| Galley / Refreshment | - | - | No |
| SL Cabin Altitude (ft) | - | - | 13100 |
| Cabin Pressure (psi) | - | - | 5.8 |
| Other | |||
| Prop Manufacturer | - | - | Hartzell |
| Prop Description | - | - | 5-Blade Comp |
| Gear Type | High Skids | Retractable Wheels | Retractable |
| Rotorhead | 3-Blade Articulated | 4-Blade Articulated | - |
| Tail Rotor | 2-Blade | Enclosed Fenestron | - |
| Performance | |||
| Max Cruise Speed (ktas) | 136 | 130 | 290 |
| Long Range Cruise (ktas) | 130 | 127 | 225 |
| Max Speed (Vne) | 155 | 143 | - |
| Stall Speed - Flaps (kias) | - | - | 67 |
| Max Range (nm) | 341 | 352 | 1866 |
| Range Seats Full (nm) | 336 | 352 | - |
| Max Range Crew + 4 (nm) | - | - | 1803 |
| Max Range Crew + 6 (nm) | - | - | 1568 |
| Max Range Crew + 8 (nm) | - | - | 1057 |
| Endurance (hrs) | 4.5 | 3.6 | - |
| Take-Off >50ft Obst. (ft) | - | - | 2602 |
| Take-Off (5000 / ISA + 10) | - | - | 4270 |
| Landing >50ft Obst. (ft) | - | - | 2170 |
| Max Climb Rate (fpm) | 1773 | 925 | 1920 |
| Service Ceiling (ft) | - | - | 30000 |
| Hover IGE (ft) | 13250 | 12550 | - |
| Hover OGE (ft) | 11150 | 8750 | - |