Beechcraft Baron G58 vs Beechcraft King Air 260 vs Beechcraft Kingair Denali vs Pilatus Pc 12 Ngx
The Beechcraft Baron G58 is a piston twin best suited to short-to-medium trips and owner-pilot missions; it typically carries about five to six people in a club-style cabin and offers the shortest range of this group, roughly in the 1,000–1,500 nautical mile class depending on power and reserves. The Beechcraft King Air 260 is a pressurized twin‑turboprop in the light business/utility category, generally seating six to nine, with a longer practical range around 1,500–1,800 nautical miles and stronger all‑weather, high‑altitude capability than the Baron. The Beechcraft King Air Denali is a newer single‑engine turboprop aimed at the high‑performance utility/business segment; it’s designed to seat about six to nine with an anticipated range around 1,600 nautical miles, bridging capability between lighter King Air missions and PC‑12‑type roles. The Pilatus PC‑12 NGX is a mature single‑engine turboprop utility/business aircraft, typically configured for six to nine passengers, and commonly offers the longest real‑world range here, about 1,700–1,900 nautical miles, with strong short/rough-field flexibility.
| Spec | Beechcraft Baron G58 | Beechcraft King Air 260 | Beechcraft KingAir Denali | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | $ 4.30 | $ 4.08 | $ 2.78 |
| Total Seats | 6 | 8 | 11 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Beechcraft | GE® Aerospace | Pilatus |
| Aircraft Name | Baron G58 | KingAir 250 | KingAir Denali | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 1420 | 1600 | 1803 |
| DOC / nm / Seat | $ 0.29 | $ 0.72 | $ 0.68 | $ 0.46 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 1450 | 3760 | 3280 | — |
| Standard Cabin Seats | 4 | 6 | 7 | 6 |
| Direct Operating Cost | $ 347 | $ 1,333 | $ 1,111 | $ 793 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 202 | 310 | 285 | 290 |
| Base Aircraft Price (USD) | $1,495,000 | $6,450,000 | $4,150,000 | $5,350,000 |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 8 | 9 | 9 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 8 | 11 | 8 |
| Standard Cabin Seats | 4 | 6 | 7 | 6 |
| Lavatory | — | 1 Flushing | 1 Flushing | Optional |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 8 | 9 | 9 |
| Lavatory Location | — | AFT | AFT | FWD |
| Cabin Pressure (psi) | — | 6.5 | 5 | 5.8 |
| Galley / Refreshment | — | No | No | No |
| SL Cabin Altitude (ft) | — | 15293 | 11065 | 13100 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | No | Yes | — | Yes |
| Model | IO-550-C | PT6A-52 | Catalyst™ | PT6E-67XP |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 1700 | 3600 | — | 5000 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 300 | 850 | — | 1200 |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 2 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 194 | 544 | — | — |
| Flat Rating | — | ISA + 37 | — | ISA + 35 |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 29.9 | 43.8 | 14.86 | 47.25 |
| Wingspan (ft) | 37.9 | 57.9 | 54.3 | 53.33 |
| Cabin Width (ft) | 3.5 | 4.5 | 4.5 | 5 |
| Cabin Height (ft) | 4.2 | 4.8 | 4.8 | 4.9 |
| Cabin Length (ft) | 12.6 | 16.7 | 12.6 | 16.9 |
| Overall Height (ft) | 9.8 | 14.8 | 4.65 | 14 |
| Cabin Volume (cu. ft) | 150 | — | — | — |
| Baggage Volume Int. (cu. ft) | 46 | 55 | 48 | 40 |
| Cabin Width - Floor (ft) | — | 4.1 | 4.1 | 4.25 |
| Cabin Length - Seating (ft) | — | 16.7 | 12.6 | — |