Beechcraft Baron G58 vs Beechcraft King Air 360 vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Beechcraft Baron G58 is a light piston twin suited to short-to-medium trips, typically carrying about 4–6 people, with a range roughly in the 1,000–1,300 nm class depending on payload and reserves. It’s generally the most economical and simplest of the group but also the least capable in speed, altitude, and cabin space. The Pilatus PC-12 NGX is a single-engine turboprop in the utility/executive category, commonly configured for about 6–9 passengers, and typically offers around 1,500–1,800 nm of range. It’s valued for efficiency, short-field capability, and cabin volume. The Beechcraft King Air 360 is a twin-engine turboprop with a more premium, higher-performance profile, often seating about 6–9 passengers in executive layouts, with range broadly similar to or slightly above the PC-12 class (around 1,500–1,800 nm), plus strong hot-and-high and redundancy advantages. The Pilatus PC-24 is a light jet, usually accommodating about 6–10 passengers, with range commonly around 1,800–2,000 nm; it adds jet speed and altitude while retaining notable runway flexibility for its class.
| Spec | Beechcraft Baron G58 | Beechcraft King Air 360 | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | $ 4.20 | $ 2.78 | $ 3.71 |
| Total Seats | 6 | 10 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Beechcraft | Beechcraft | Pilatus | Pilatus |
| Aircraft Name | Baron G58 | KingAir 350i | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 1560 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.29 | $ 0.53 | $ 0.46 | $ 0.62 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 1450 | 5145 | — | 6680 |
| Standard Cabin Seats | 4 | 8 | 6 | 6 |
| Direct Operating Cost | $ 347 | $ 1,311 | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 202 | 312 | 290 | 440 |
| Base Aircraft Price (USD) | $1,495,000 | $7,650,000 | $5,350,000 | $11,800,000 |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 9 | 9 | 10 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 10 | 8 | 6 |
| Standard Cabin Seats | 4 | 8 | 6 | 6 |
| Lavatory | — | Optional | Optional | 1 Enclosed Flushing |
| Min Crew | — | 1 | 1 | 1 |
| Galley Location | — | FWD | — | FWD |
| Max Cabin Seats | — | 9 | 9 | 10 |
| Lavatory Location | — | AFT | FWD | FWD |
| Cabin Pressure (psi) | — | 6.5 | 5.8 | 9.3 |
| Galley / Refreshment | — | Optional | No | Optional Refreshment Center |
| Cargo Door | — | — | Yes | Yes |
| SL Cabin Altitude (ft) | — | — | 13100 | 23500 |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Engine | ||||
| FADEC | No | Yes | Yes | Yes |
| Model | IO-550-C | PT6A-60A | PT6E-67XP | FJ44-4A-QPM |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 1700 | 3600 | 5000 | 5000 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 300 | 1050 | 1200 | — |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 2 | 1 | 1 | 2 |
| Fuel Capacity (gal) | 194 | 539 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 35 | ISA + 23 |
| Usable Fuel (gal) | — | — | 402 | — |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Length (ft) | 29.9 | 46.7 | 47.25 | 52.2 |
| Wingspan (ft) | 37.9 | 57.9 | 53.33 | 55.8 |
| Cabin Width (ft) | 3.5 | 4.5 | 5 | 5.6 |
| Cabin Height (ft) | 4.2 | 4.8 | 4.9 | 5.1 |
| Cabin Length (ft) | 12.6 | 19.5 | 16.9 | 23 |
| Overall Height (ft) | 9.8 | 14.4 | 14 | 17.4 |
| Cabin Volume (cu. ft) | 150 | — | — | — |
| Baggage Volume Int. (cu. ft) | 46 | 71 | 40 | 90 |
| Cabin Width - Floor (ft) | — | 4.1 | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | — | 19.5 | — | 17 |
| Aisle Step (ft) | — | — | — | Flat Floor |