Airbus Helicopters H145 vs Beechcraft Baron G58 vs Beechcraft King Air 360 vs Pilatus Pc 12 Ngx
The Airbus Helicopters H145 is a light twin‑engine helicopter optimized for short‑range missions and point‑to‑point access where runways aren’t available. It typically carries about 1–2 pilots plus roughly 6–9 passengers depending on interior and mission equipment, with practical range generally a few hundred nautical miles (commonly around 300–400 nm). The Beechcraft Baron G58 is a piston‑twin airplane suited to personal and light business travel. It is usually configured for 1–2 pilots and about 4–5 passengers, with range typically in the 1,000–1,300 nm class depending on power settings and payload. The Pilatus PC‑12 NGX is a single‑engine turboprop business utility aircraft, commonly seating 1–2 pilots and about 6–9 passengers, with range often around 1,500–1,800 nm. The Beechcraft King Air 360 is a twin‑engine turboprop in a higher business class, generally carrying 1–2 pilots and about 6–9 passengers, with range broadly similar to or slightly above the PC‑12 in many configurations (often around 1,500–1,800 nm), while offering twin‑engine redundancy and more cabin/capability options.
| Spec | AIRBUS H145 | Beechcraft Baron G58 | Beechcraft King Air 360 | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | $ 1.72 | $ 4.20 | $ 2.78 |
| Min Crew | 1 | — | 1 | 1 |
| Total Seats | 10 | 6 | 10 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Beechcraft | Beechcraft | Pilatus |
| Aircraft Name | H145 | Baron G58 | KingAir 350i | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 1480 | 1560 | 1803 |
| DOC / nm / Seat | $ 0.93 | $ 0.29 | $ 0.53 | $ 0.46 |
| Max Cabin Seats | 9 | — | 9 | 9 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 4200 | 1450 | 5145 | — |
| Standard Cabin Seats | 8 | 4 | 8 | 6 |
| Direct Operating Cost | $ 1,210 | $ 347 | $ 1,311 | $ 793 |
| Flight Deck (Base Spec) | EFIS | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 130 | 202 | 312 | 290 |
| Base Aircraft Price (USD) | $10,200,000 | $1,495,000 | $7,650,000 | $5,350,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | — | 1 | 1 |
| Total Seats | 10 | 6 | 10 | 8 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 9 | — | 9 | 9 |
| Standard Cabin Seats | 8 | 4 | 8 | 6 |
| Lavatory | — | — | Optional | Optional |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | AFT | FWD |
| Cabin Pressure (psi) | — | — | 6.5 | 5.8 |
| Galley / Refreshment | — | — | Optional | No |
| Cargo Door | — | — | — | Yes |
| SL Cabin Altitude (ft) | — | — | — | 13100 |
| Engine | ||||
| FADEC | Yes | No | Yes | Yes |
| Model | Arriel 2E | IO-550-C | PT6A-60A | PT6E-67XP |
| Fuel Type | JetFuel | AvGas | — | — |
| TBO (hrs) | 4000 | 1700 | 3600 | 5000 |
| Horsepower | 894 | 300 | 1050 | 1200 |
| No. of Engines | 2 | 2 | 1 | 1 |
| TBO (yrs) | — | 12 | — | — |
| Fuel Delivery | — | Fuel Injected | — | — |
| Fuel Capacity (gal) | — | 194 | 539 | — |
| Flat Rating | — | — | ISA + 10 | ISA + 35 |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 44.8 | 29.9 | 46.7 | 47.25 |
| Overall Height (ft) | 13 | 9.8 | 14.4 | 14 |
| Rotor Diameter (ft) | 36.1 | — | — | — |
| Cabin Volume (cu. ft) | 166 | 150 | — | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | — | — | — |
| Wingspan (ft) | — | 37.9 | 57.9 | 53.33 |
| Cabin Width (ft) | — | 3.5 | 4.5 | 5 |
| Cabin Height (ft) | — | 4.2 | 4.8 | 4.9 |
| Cabin Length (ft) | — | 12.6 | 19.5 | 16.9 |
| Baggage Volume Int. (cu. ft) | — | 46 | 71 | 40 |
| Cabin Width - Floor (ft) | — | — | 4.1 | 4.25 |
| Cabin Length - Seating (ft) | — | — | 19.5 | — |