Compare Airbus Helicopters H125 vs Daher Kodiak 100 - Series III vs Daher TBM 960 vs Leonardo AW119Kx
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| Manufacturer | Airbus Helicopters | Daher | Daher TBM | Leonardo |
| Aircraft Type | H125 | Kodiak 100 - Series II | TBM 960 | AW119Kx |
| Base Aircraft Price (USD) | $3,200,000 | $2,195,000 | $4,450,000 | $3,850,000 |
| Direct Operating Cost | $ 627 | $ 393 | $ 744 | $ 885 |
| DOC / nm | $ 4.61 | $ 2.15 | $ 2.25 | $ 6.76 |
| DOC / nm / Seat | $ 0.77 | $ 0.27 | $ 0.56 | $ 0.84 |
| Max Cruise Speed (ktas) | 136 | 183 | 330 | 131 |
| Max Range (nm) | 341 | 1132 | 1730 | 515 |
| Useful Load (lbs) | 2189 | 3530 | 2601 | - |
| Total Seats | 6 | 10 | 6 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 4 | 8 | 4 | 6 |
| Max Cabin Seats | 5 | 8 | - | 6 |
| Min Crew | 1 | 1 | 1 | 1 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000 NXi | Garmin G3000 | Garmin G1000H |
| Flight Rules | VFR | IFR | IFR | VFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Weights | ||||
| MRAMP (lbs) | - | 7305 | 7430 | - |
| MTOW (lbs) | 4960 | 7255 | 7394 | 6283 |
| MTOW External Load (lbs) | 6172 | - | - | - |
| Max External Load (lbs) | 3086 | - | - | - |
| MLW (lbs) | - | 7255 | 7024 | - |
| MZFW (lbs) | - | 7071 | 6032 | - |
| BOW (lbs) | - | 3955 | 4629 | - |
| BEW (lbs) | 2816 | 3775 | - | - |
| Useful Load (lbs) | 2189 | 3530 | 2601 | - |
| Max Payload (lbs) | - | 3300 | 1403 | - |
| Fuel Capacity (lbs) | 858 | 2144 | 2017 | - |
| Useful Load Max Fuel (lbs) | 1551 | - | - | - |
| Payload Max Fuel (lbs) | - | 744 | 891 | - |
| Max Baggage Weight (lbs) | - | 200 | 507 | - |
| Dimensions | ||||
| Wingspan (ft) | - | 45 | 42.1 | - |
| Rotor Diameter (ft) | 36.1 | - | - | 35.5 |
| Overall Height (ft) | 10 | 14.7 | - | 11.9 |
| Length (ft) | 42.5 | 34.2 | 35.3 | 42.5 |
| Cabin Height (ft) | - | 4.5 | 4.1 | - |
| Cabin Width (ft) | - | 4.8 | 4 | - |
| Cabin Length (ft) | - | 15.83 | 13.4 | - |
| Cabin Length - Seating (ft) | - | 12.7 | - | - |
| Cabin Volume (cu. ft) | - | - | 123 | - |
| Baggage Volume Int. (cu. ft) | - | 248 | - | - |
| Baggage Volume Ext. (cu. ft) | - | 63 | - | - |
| Engine | ||||
| No. of Engines | 1 | 1 | - | 1 |
| Manufacturer | Airbus Helicopters | Daher | Daher TBM | Leonardo |
| Model | Arriel 2D | PT6A-34 | TBM 960 | PT6B-37A |
| Horsepower | 847 | 750 | 850 | 917 |
| Flat Rating | - | ISA + 7 | ISA + 49 | - |
| FADEC | Yes | Yes | Yes | Yes |
| TBO (hrs) | 5000 | 4000 | 3500 | 4500 |
| Fuel Type | JetFuel | - | - | JetFuel |
| Fuel Capacity (gal) | 143 | 320 | - | 160 |
| Usable Fuel (gal) | - | 315 | - | - |
| Fuel Burn (gph) | - | 48 | - | - |
| Fuel Burn (lbph) | - | 45 | - | - |
| Avionics | ||||
| Flight Deck | Garmin G500H | Garmin G1000 NXi | Garmin G3000 | Garmin G1000H |
| Flight Rules | VFR | IFR | IFR | VFR |
| Standby Instrument | Gyro / Analog | 1 | - | - |
| Autopilot | - | 1 | 1 | 1 |
| PFD | - | 2 | 2 | 2 |
| MFD | - | 1 | 1 | 1 |
| GPS | - | 2 | 1 | 1 |
| Flight Director | - | 1 | - | - |
| Transponder | 1 | 1 | 1 | 1 |
| VHF Com | 1 | 2 | 2 | 1 |
| VHF NAV | 1 | 2 | 2 | 1 |
| Cabin | ||||
| Total Seats | 6 | 10 | 6 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 4 | 8 | 4 | 6 |
| Max Cabin Seats | 5 | 8 | - | 6 |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | - | Yes | - | - |
| Lavatory | - | No | No | - |
| Lavatory Location | - | N/A | - | - |
| Galley / Refreshment | - | No | - | - |
| Galley Location | - | N/A | MID | - |
| SL Cabin Altitude (ft) | - | - | 14390 | - |
| Cabin Pressure (psi) | - | Un-Pressurized | 6.2 | - |
| Other | ||||
| Prop Manufacturer | - | Hartzell | - | - |
| Prop Description | - | 4-Blade Constant Feathering | - | - |
| Prop Diameter | - | 96" | - | - |
| Prop TBO (hrs) | - | 4000 | - | - |
| Prop TBO (yrs) | - | 6 | - | - |
| Gear Type | High Skids | Fixed Steel Spring | Retractable | Skids |
| Wheel Size | - | 29" | - | - |
| Rotorhead | 3-Blade Articulated | - | - | 4-Blade Articulated |
| Tail Rotor | 2-Blade | - | - | 2-Blade |
| Warranty | ||||
| Airframe (Yrs) | - | 2 | - | - |
| Airframe (Hrs) | - | 1000 | - | - |
| Engine (Yrs) | - | N/A | - | - |
| Engine (Hrs) | - | 1000 | - | - |
| Prop (Yrs) | - | 5 | - | - |
| Prop (Hrs) | - | 1000 | - | - |
| Avionics (Yrs) | - | 2 | - | - |
| Performance | ||||
| Max Cruise Speed (ktas) | 136 | 183 | 330 | 131 |
| Cruise Speed @ 85% (ktas) | - | 164 | - | - |
| Cruise Speed @ 75% (ktas) | - | 153 | - | - |
| Long Range Cruise (ktas) | 130 | 135 | 252 | 131 |
| Vref (kias) | - | 74 | - | - |
| Max Speed (Vne) | 155 | 182 | - | 152 |
| Stall Speed - Clean (kias) | - | 61 | - | - |
| Stall Speed - Flaps (kias) | - | 46 | - | - |
| Max Range (nm) | 341 | 1132 | 1730 | 515 |
| Range @ 85% (nm) | - | 905 | 1440 | - |
| Range @ 75% | - | 1024 | 1594 | - |
| Range Seats Full (nm) | 336 | 594 | - | 515 |
| Max Range Crew + 4 (nm) | - | 1132 | - | - |
| Endurance (hrs) | 4.5 | 9.9 | - | - |
| Take-off Roll (ft) | - | 934 | - | - |
| Take-Off >50ft Obst. (ft) | - | 1467 | 2380 | - |
| Take-Off (5000 / ISA + 10) | - | 2396 | 3475 | - |
| Landing Roll (ft) | - | 765 | - | - |
| Landing >50ft Obst. (ft) | - | 1508 | 2430 | - |
| Max Climb Rate (fpm) | 1773 | 1340 | - | - |
| Service Ceiling (ft) | - | 25000 | 31000 | 24000 |
| Hover IGE (ft) | 13250 | - | - | 11000 |
| Hover OGE (ft) | 11150 | - | - | 7300 |