Compare Airbus Helicopters H145 vs Airbus Helicopters H155 vs Daher Kodiak 100 - Series III vs Pilatus PC-12 NGX
 |  |  |  | |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Daher | Pilatus |
| Aircraft Type | H145 | H155 | Kodiak 100 - Series II | PC-12 NGX |
| Base Aircraft Price (USD) | $10,200,000 | $14,800,000 | $2,195,000 | $5,350,000 |
| Direct Operating Cost | $ 1,210 | $ 1,593 | $ 393 | $ 793 |
| DOC / nm | $ 9.31 | $ 11.06 | $ 2.15 | $ 2.78 |
| DOC / nm / Seat | $ 0.93 | $ 0.74 | $ 0.27 | $ 0.46 |
| Max Cruise Speed (ktas) | 130 | 144 | 183 | 290 |
| Max Range (nm) | 352 | 423 | 1132 | 1866 |
| Useful Load (lbs) | 4200 | 4012 | 3530 | 3692 |
| Total Seats | 10 | 14 | 10 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 12 | 8 | 6 |
| Max Cabin Seats | 9 | 12 | 8 | 9 |
| Min Crew | 1 | 2 | 1 | 1 |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G1000 NXi | Honeywell Primus Apex |
| Flight Rules | IFR | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Weights | ||||
| MRAMP (lbs) | - | - | 7305 | 10495 |
| MTOW (lbs) | 8378 | 10846 | 7255 | 10450 |
| MTOW External Load (lbs) | 8378 | 10846 | - | - |
| Max External Load (lbs) | 3527 | 3527 | - | - |
| MLW (lbs) | - | - | 7255 | 9921 |
| MZFW (lbs) | - | - | 7071 | 9039 |
| BOW (lbs) | - | - | 3955 | 6803 |
| BEW (lbs) | 4231 | 5574 | 3775 | 6758 |
| Useful Load (lbs) | 4200 | 4012 | 3530 | 3692 |
| Max Payload (lbs) | - | - | 3300 | 2235 |
| Fuel Capacity (lbs) | 1434 | 1411 | 2144 | 2704 |
| Useful Load Max Fuel (lbs) | 2492 | 3661 | - | - |
| Payload Max Fuel (lbs) | - | - | 744 | 988 |
| Max Baggage Weight (lbs) | - | - | 200 | - |
| Dimensions | ||||
| Wingspan (ft) | - | - | 45 | 53.33 |
| Rotor Diameter (ft) | 36.1 | 41.1 | - | - |
| Overall Height (ft) | 13 | 14.3 | 14.7 | 14 |
| Length (ft) | 44.8 | 46.9 | 34.2 | 47.25 |
| Cabin Height (ft) | - | - | 4.5 | 4.9 |
| Cabin Width (ft) | - | - | 4.8 | 5 |
| Cabin Width - Floor (ft) | - | - | - | 4.25 |
| Cabin Length (ft) | - | - | 15.83 | 16.9 |
| Cabin Length - Seating (ft) | - | - | 12.7 | - |
| Cabin Volume (cu. ft) | 166 | 235.2 | - | - |
| Baggage Volume Int. (cu. ft) | - | - | 248 | 40 |
| Baggage Volume Ext. (cu. ft) | 46.8 | 88.3 | 63 | - |
| Engine | ||||
| No. of Engines | 2 | 2 | 1 | 1 |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Daher | Pilatus |
| Model | Arriel 2E | Arriel 2C2 | PT6A-34 | PT6E-67XP |
| Horsepower | 894 | 943 | 750 | 1200 |
| Flat Rating | - | - | ISA + 7 | ISA + 35 |
| FADEC | Yes | Yes | Yes | Yes |
| TBO (hrs) | 4000 | 4000 | 4000 | 5000 |
| Fuel Type | JetFuel | JetFuel | - | - |
| Fuel Capacity (gal) | - | 332 | 320 | - |
| Usable Fuel (gal) | - | - | 315 | 402 |
| Fuel Burn (gph) | - | - | 48 | - |
| Fuel Burn (lbph) | - | - | 45 | - |
| Avionics | ||||
| Flight Deck | EFIS | EFIS | Garmin G1000 NXi | Honeywell Primus Apex |
| Flight Rules | IFR | IFR | IFR | IFR |
| Standby Instrument | Digital | Digital | 1 | - |
| FMS | - | - | - | 1 |
| Autopilot | 4-Axis | 4-Axis | 1 | 1 |
| PFD | 2 | 2 | 2 | 2 |
| MFD | - | - | 1 | 1 |
| GPS | 1 | 1 | 2 | 1 |
| AHRS | 3 | 2 | - | 1 |
| Flight Director | - | - | 1 | - |
| ADC | - | 2 | - | - |
| Transponder | 1 | 1 | 1 | 1 |
| VHF Com | 1 | 1 | 2 | 2 |
| VHF NAV | 1 | 1 | 2 | 2 |
| Cabin | ||||
| Total Seats | 10 | 14 | 10 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 12 | 8 | 6 |
| Max Cabin Seats | 9 | 12 | 8 | 9 |
| Min Crew | 1 | 2 | 1 | 1 |
| Configuration | Green Interior | Green Interior | - | - |
| Cargo Door | - | - | Yes | Yes |
| Lavatory | - | - | No | Optional |
| Lavatory Location | - | - | N/A | FWD |
| Galley / Refreshment | - | - | No | No |
| Galley Location | - | - | N/A | - |
| SL Cabin Altitude (ft) | - | - | - | 13100 |
| Cabin Pressure (psi) | - | - | Un-Pressurized | 5.8 |
| Other | ||||
| Prop Manufacturer | - | - | Hartzell | Hartzell |
| Prop Description | - | - | 4-Blade Constant Feathering | 5-Blade Comp |
| Prop Diameter | - | - | 96" | - |
| Prop TBO (hrs) | - | - | 4000 | - |
| Prop TBO (yrs) | - | - | 6 | - |
| Gear Type | Retractable Wheels | Retractable Wheels | Fixed Steel Spring | Retractable |
| Wheel Size | - | - | 29" | - |
| Rotorhead | 4-Blade Articulated | 5-Blade Articulated | - | - |
| Tail Rotor | Enclosed Fenestron | 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 | 144 | 183 | 290 |
| Cruise Speed @ 85% (ktas) | - | - | 164 | - |
| Cruise Speed @ 75% (ktas) | - | - | 153 | - |
| Long Range Cruise (ktas) | 127 | 140 | 135 | 225 |
| Vref (kias) | - | - | 74 | - |
| Max Speed (Vne) | 143 | 175 | 182 | - |
| Stall Speed - Clean (kias) | - | - | 61 | - |
| Stall Speed - Flaps (kias) | - | - | 46 | 67 |
| Max Range (nm) | 352 | 423 | 1132 | 1866 |
| Range @ 85% (nm) | - | - | 905 | - |
| Range @ 75% | - | - | 1024 | - |
| Range Seats Full (nm) | 352 | 423 | 594 | - |
| Max Range Crew + 4 (nm) | - | - | 1132 | 1803 |
| Max Range Crew + 6 (nm) | - | - | - | 1568 |
| Max Range Crew + 8 (nm) | - | - | - | 1057 |
| Endurance (hrs) | 3.6 | 4 | 9.9 | - |
| Take-off Roll (ft) | - | - | 934 | - |
| Take-Off >50ft Obst. (ft) | - | - | 1467 | 2602 |
| Take-Off (5000 / ISA + 10) | - | - | 2396 | 4270 |
| Landing Roll (ft) | - | - | 765 | - |
| Landing >50ft Obst. (ft) | - | - | 1508 | 2170 |
| Max Climb Rate (fpm) | 925 | 1154 | 1340 | 1920 |
| Service Ceiling (ft) | - | - | 25000 | 30000 |
| Hover IGE (ft) | 12550 | 7050 | - | - |
| Hover OGE (ft) | 8750 | - | - | - |