Compare Airbus Helicopters H145 vs Beechcraft Baron G58 vs Beechcraft King Air 360 vs Pilatus PC-12 NGX
 |  |  |  | |
| Manufacturer | Airbus Helicopters | Beechcraft | Beechcraft | Pilatus |
| Aircraft Type | H145 | Baron G58 | KingAir 350i | PC-12 NGX |
| Base Aircraft Price (USD) | $10,200,000 | $1,495,000 | $7,650,000 | $5,350,000 |
| Direct Operating Cost | $ 1,210 | $ 347 | $ 1,311 | $ 793 |
| DOC / nm | $ 9.31 | $ 1.72 | $ 4.20 | $ 2.78 |
| DOC / nm / Seat | $ 0.93 | $ 0.29 | $ 0.53 | $ 0.46 |
| Max Cruise Speed (ktas) | 130 | 202 | 312 | 290 |
| Max Range (nm) | 352 | 1480 | 1560 | 1866 |
| Useful Load (lbs) | 4200 | 1450 | 5145 | 3692 |
| Total Seats | 10 | 6 | 10 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 4 | 8 | 6 |
| Max Cabin Seats | 9 | - | 9 | 9 |
| Min Crew | 1 | - | 1 | 1 |
| Flight Deck (Base Spec) | EFIS | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | 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) | - | - | 15100 | 10495 |
| MTOW (lbs) | 8378 | 5500 | 15000 | 10450 |
| MTOW External Load (lbs) | 8378 | - | - | - |
| Max External Load (lbs) | 3527 | - | - | - |
| MLW (lbs) | - | 5400 | 15000 | 9921 |
| MZFW (lbs) | - | - | 12500 | 9039 |
| BOW (lbs) | - | - | 9955 | 6803 |
| BEW (lbs) | 4231 | 4050 | 9855 | 6758 |
| Useful Load (lbs) | 4200 | 1450 | 5145 | 3692 |
| Max Payload (lbs) | - | - | 2545 | 2235 |
| Fuel Capacity (lbs) | 1434 | 1164 | 3611 | 2704 |
| Useful Load Max Fuel (lbs) | 2492 | 286 | - | - |
| Payload Max Fuel (lbs) | - | - | 1534 | 988 |
| Max Baggage Weight (lbs) | - | 420 | 1150 | - |
| Dimensions | ||||
| Wingspan (ft) | - | 37.9 | 57.9 | 53.33 |
| Rotor Diameter (ft) | 36.1 | - | - | - |
| Overall Height (ft) | 13 | 9.8 | 14.4 | 14 |
| Length (ft) | 44.8 | 29.9 | 46.7 | 47.25 |
| Cabin Height (ft) | - | 4.2 | 4.8 | 4.9 |
| Cabin Width (ft) | - | 3.5 | 4.5 | 5 |
| Cabin Width - Floor (ft) | - | - | 4.1 | 4.25 |
| Cabin Length (ft) | - | 12.6 | 19.5 | 16.9 |
| Cabin Length - Seating (ft) | - | - | 19.5 | - |
| Cabin Volume (cu. ft) | 166 | 150 | - | - |
| Baggage Volume Int. (cu. ft) | - | 46 | 71 | 40 |
| Baggage Volume Ext. (cu. ft) | 46.8 | - | - | - |
| Engine | ||||
| No. of Engines | 2 | 2 | 1 | 1 |
| Manufacturer | Airbus Helicopters | Beechcraft | Beechcraft | Pilatus |
| Model | Arriel 2E | IO-550-C | PT6A-60A | PT6E-67XP |
| Horsepower | 894 | 300 | 1050 | 1200 |
| Flat Rating | - | - | ISA + 10 | ISA + 35 |
| FADEC | Yes | No | Yes | Yes |
| TBO (hrs) | 4000 | 1700 | 3600 | 5000 |
| TBO (yrs) | - | 12 | - | - |
| Fuel Type | JetFuel | AvGas | - | - |
| Fuel Delivery | - | Fuel Injected | - | - |
| Fuel Capacity (gal) | - | 194 | 539 | - |
| Usable Fuel (gal) | - | - | - | 402 |
| Avionics | ||||
| Flight Deck | EFIS | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex |
| Flight Rules | IFR | IFR | IFR | IFR |
| Standby Instrument | Digital | - | - | - |
| FMS | - | - | 2 | 1 |
| Autopilot | 4-Axis | Garmin GFC 700 | 1 | 1 |
| PFD | 2 | 1 | 2 | 2 |
| MFD | - | 1 | 1 | 1 |
| GPS | 1 | 1 | 1 | 1 |
| AHRS | 3 | - | 1 | 1 |
| Transponder | 1 | 1 | 1 | 1 |
| VHF Com | 1 | 1 | 2 | 2 |
| VHF NAV | 1 | 1 | 2 | 2 |
| Cabin | ||||
| Total Seats | 10 | 6 | 10 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 4 | 8 | 6 |
| Max Cabin Seats | 9 | - | 9 | 9 |
| Min Crew | 1 | - | 1 | 1 |
| Configuration | Green Interior | - | - | - |
| Cargo Door | - | - | - | Yes |
| Lavatory | - | - | Optional | Optional |
| Lavatory Location | - | - | AFT | FWD |
| Galley / Refreshment | - | - | Optional | No |
| Galley Location | - | - | FWD | - |
| SL Cabin Altitude (ft) | - | - | - | 13100 |
| Cabin Pressure (psi) | - | - | 6.5 | 5.8 |
| Other | ||||
| Prop Manufacturer | - | McCauley | Hartzell | Hartzell |
| Prop Description | - | 3-Blade Constant | 4-Blade Constant Feathering Reverse | 5-Blade Comp |
| Gear Type | Retractable Wheels | Retractable | Retractable | Retractable |
| Rotorhead | 4-Blade Articulated | - | - | - |
| Tail Rotor | Enclosed Fenestron | - | - | - |
| Performance | ||||
| Max Cruise Speed (Mach) | - | - | 0.58 | - |
| Max Cruise Speed (ktas) | 130 | 202 | 312 | 290 |
| Long Range Cruise (ktas) | 127 | 163 | 235 | 225 |
| Vref (kias) | - | - | 100 | - |
| Max Speed (Vne) | 143 | - | - | - |
| Stall Speed - Clean (kias) | - | 73 | 82 | - |
| Stall Speed - Flaps (kias) | - | - | - | 67 |
| Max Range (nm) | 352 | 1480 | 1560 | 1866 |
| Range Seats Full (nm) | 352 | - | - | - |
| Max Range Crew + 4 (nm) | - | - | 1533 | 1803 |
| Max Range Crew + 6 (nm) | - | - | - | 1568 |
| Max Range Crew + 8 (nm) | - | - | - | 1057 |
| Endurance (hrs) | 3.6 | - | - | - |
| Take-off FL (ft) | - | - | 3300 | - |
| Take-off Roll (ft) | - | 2345 | - | - |
| Take-Off >50ft Obst. (ft) | - | - | - | 2602 |
| Take-Off (5000 / ISA + 10) | - | - | 5376 | 4270 |
| Landing Roll (ft) | - | 2490 | - | - |
| Landing >50ft Obst. (ft) | - | - | 2692 | 2170 |
| Max Climb Rate (fpm) | 925 | 1700 | 2731 | 1920 |
| Service Ceiling (ft) | - | 20688 | 35000 | 30000 |
| Hover IGE (ft) | 12550 | - | - | - |
| Hover OGE (ft) | 8750 | - | - | - |