Compare Airbus Helicopters H145 vs Daher Kodiak 100 - Series III
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| Manufacturer | Airbus Helicopters | Daher |
| Aircraft Type | H145 | Kodiak 100 - Series II |
| Base Aircraft Price (USD) | $10,200,000 | $2,195,000 |
| Direct Operating Cost | $ 1,210 | $ 393 |
| DOC / nm | $ 9.31 | $ 2.15 |
| DOC / nm / Seat | $ 0.93 | $ 0.27 |
| Max Cruise Speed (ktas) | 130 | 183 |
| Max Range (nm) | 352 | 1132 |
| Useful Load (lbs) | 4200 | 3530 |
| Total Seats | 10 | 10 |
| Cockpit | 2 | 2 |
| Standard Cabin Seats | 8 | 8 |
| Max Cabin Seats | 9 | 8 |
| Min Crew | 1 | 1 |
| Flight Deck (Base Spec) | EFIS | Garmin G1000 NXi |
| Flight Rules | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | VERIFIED |
| Weights | ||
| MRAMP (lbs) | - | 7305 |
| MTOW (lbs) | 8378 | 7255 |
| MTOW External Load (lbs) | 8378 | - |
| Max External Load (lbs) | 3527 | - |
| MLW (lbs) | - | 7255 |
| MZFW (lbs) | - | 7071 |
| BOW (lbs) | - | 3955 |
| BEW (lbs) | 4231 | 3775 |
| Useful Load (lbs) | 4200 | 3530 |
| Max Payload (lbs) | - | 3300 |
| Fuel Capacity (lbs) | 1434 | 2144 |
| Useful Load Max Fuel (lbs) | 2492 | - |
| Payload Max Fuel (lbs) | - | 744 |
| Max Baggage Weight (lbs) | - | 200 |
| Dimensions | ||
| Wingspan (ft) | - | 45 |
| Rotor Diameter (ft) | 36.1 | - |
| Overall Height (ft) | 13 | 14.7 |
| Length (ft) | 44.8 | 34.2 |
| Cabin Height (ft) | - | 4.5 |
| Cabin Width (ft) | - | 4.8 |
| Cabin Length (ft) | - | 15.83 |
| Cabin Length - Seating (ft) | - | 12.7 |
| Cabin Volume (cu. ft) | 166 | - |
| Baggage Volume Int. (cu. ft) | - | 248 |
| Baggage Volume Ext. (cu. ft) | 46.8 | 63 |
| Engine | ||
| No. of Engines | 2 | 1 |
| Manufacturer | Airbus Helicopters | Daher |
| Model | Arriel 2E | PT6A-34 |
| Horsepower | 894 | 750 |
| Flat Rating | - | ISA + 7 |
| FADEC | Yes | Yes |
| TBO (hrs) | 4000 | 4000 |
| Fuel Type | JetFuel | - |
| Fuel Capacity (gal) | - | 320 |
| Usable Fuel (gal) | - | 315 |
| Fuel Burn (gph) | - | 48 |
| Fuel Burn (lbph) | - | 45 |
| Avionics | ||
| Flight Deck | EFIS | Garmin G1000 NXi |
| Flight Rules | IFR | IFR |
| Standby Instrument | Digital | 1 |
| Autopilot | 4-Axis | 1 |
| PFD | 2 | 2 |
| MFD | - | 1 |
| GPS | 1 | 2 |
| AHRS | 3 | - |
| Flight Director | - | 1 |
| Transponder | 1 | 1 |
| VHF Com | 1 | 2 |
| VHF NAV | 1 | 2 |
| Cabin | ||
| Total Seats | 10 | 10 |
| Cockpit | 2 | 2 |
| Standard Cabin Seats | 8 | 8 |
| Max Cabin Seats | 9 | 8 |
| Min Crew | 1 | 1 |
| Configuration | Green Interior | - |
| Cargo Door | - | Yes |
| Lavatory | - | No |
| Lavatory Location | - | N/A |
| Galley / Refreshment | - | No |
| Galley Location | - | N/A |
| Cabin Pressure (psi) | - | Un-Pressurized |
| Other | ||
| Prop Manufacturer | - | Hartzell |
| Prop Description | - | 4-Blade Constant Feathering |
| Prop Diameter | - | 96" |
| Prop TBO (hrs) | - | 4000 |
| Prop TBO (yrs) | - | 6 |
| Gear Type | Retractable Wheels | Fixed Steel Spring |
| Wheel Size | - | 29" |
| Rotorhead | 4-Blade Articulated | - |
| Tail Rotor | Enclosed Fenestron | - |
| 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) | 130 | 183 |
| Cruise Speed @ 85% (ktas) | - | 164 |
| Cruise Speed @ 75% (ktas) | - | 153 |
| Long Range Cruise (ktas) | 127 | 135 |
| Vref (kias) | - | 74 |
| Max Speed (Vne) | 143 | 182 |
| Stall Speed - Clean (kias) | - | 61 |
| Stall Speed - Flaps (kias) | - | 46 |
| Max Range (nm) | 352 | 1132 |
| Range @ 85% (nm) | - | 905 |
| Range @ 75% | - | 1024 |
| Range Seats Full (nm) | 352 | 594 |
| Max Range Crew + 4 (nm) | - | 1132 |
| Endurance (hrs) | 3.6 | 9.9 |
| Take-off Roll (ft) | - | 934 |
| Take-Off >50ft Obst. (ft) | - | 1467 |
| Take-Off (5000 / ISA + 10) | - | 2396 |
| Landing Roll (ft) | - | 765 |
| Landing >50ft Obst. (ft) | - | 1508 |
| Max Climb Rate (fpm) | 925 | 1340 |
| Service Ceiling (ft) | - | 25000 |
| Hover IGE (ft) | 12550 | - |
| Hover OGE (ft) | 8750 | - |