Beechcraft King Air 360er vs Embraer Phenom 300e vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Beechcraft King Air 360ER and Pilatus PC-12 NGX are pressurized single/dual‑engine turboprops, typically categorized as utility/corporate turboprops, while the Embraer Phenom 300E is a light jet and the Pilatus PC-24 is a “super versatile” light/medium business jet designed for rough-field flexibility. In range, the King Air 360ER is generally the longest-legged of the group, optimized for extended missions, with the PC-12 NGX also offering strong long-range capability for a single-engine turboprop. The Phenom 300E typically delivers solid light-jet range suited to regional point-to-point flying, while the PC-24 usually sits in a similar general bracket but emphasizes runway performance and mission versatility as much as outright distance. For passenger capacity, the Phenom 300E commonly seats around 6–8, the King Air 360ER often accommodates about 7–9 in typical executive layouts, the PC-12 NGX is usually configured around 6–9, and the PC-24 generally seats about 6–10 depending on layout and options.
| Spec | Beechcraft King Air 360ER | Embraer Phenom 300E | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 3.88 | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 10 | 8 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Beechcraft | Embraer | Pilatus | Pilatus |
| Aircraft Name | KingAir 350ER | Phenom 300E | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 2,010 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.55 | $ 0.55 | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 9 | 10 | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6585 | 6914 | — | 6680 |
| Standard Cabin Seats | 8 | 6 | 6 | 6 |
| Direct Operating Cost | $ 1,324 | $ 1,758 | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Prodigy Touch (G3000) | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 303 | 464 | 290 | 440 |
| Base Aircraft Price (USD) | $8,750,000 | $9,650,000 | $5,350,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | 1 Enclosed Flushing | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | Optional | — | Yes | Yes |
| Total Seats | 10 | 9 | 8 | 6 |
| Galley Location | FWD | FWD | — | FWD |
| Max Cabin Seats | 9 | 9 | 9 | 10 |
| Lavatory Location | AFT | AFT | FWD | FWD |
| Cabin Pressure (psi) | 6.5 | 9.4 | 5.8 | 9.3 |
| Galley / Refreshment | Refreshment Center | Galley | No | Optional Refreshment Center |
| Standard Cabin Seats | 8 | 7 | 6 | 6 |
| Crew Rest | — | No | — | No |
| Jump Seat | — | No | — | No |
| SL Cabin Altitude (ft) | — | 25560 | 13100 | 23500 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | Canada PW535E1 | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 5000 | 5000 | 5000 |
| Horsepower | 1050 | — | 1200 | — |
| Flat Rating | ISA + 10 | ISA + 15 | ISA + 35 | ISA + 23 |
| No. of Engines | 1 | 2 | 1 | 2 |
| Fuel Capacity (gal) | 775 | — | — | — |
| Thrust (lbs) | — | 3360 | — | 3435 |
| Fuel Burn (lbph) | — | 757 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 46.7 | 51.2 | 47.25 | 52.2 |
| Wingspan (ft) | 57.9 | 52.16 | 53.33 | 55.8 |
| Cabin Width (ft) | 4.5 | 5.1 | 5 | 5.6 |
| Cabin Height (ft) | 4.8 | 4.9 | 4.9 | 5.1 |
| Cabin Length (ft) | 19.5 | 17.2 | 16.9 | 23 |
| Overall Height (ft) | 14.4 | 16.75 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 4.1 | 3.6 | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | 19.5 | 14.8 | — | 17 |
| Baggage Volume Int. (cu. ft) | 71 | 10 | 40 | 90 |
| Aisle Step (ft) | — | 0.3 | — | Flat Floor |
| Baggage Volume Ext. (cu. ft) | — | 74 | — | — |