Beechcraft King Air 360 vs Embraer Phenom 300e vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
By category, the Beechcraft King Air 360 and Pilatus PC-12 NGX are pressurized twin‑turboprop and single‑turboprop business aircraft respectively, optimized for short/rough-field flexibility and efficient regional missions. The Embraer Phenom 300E is a light business jet focused on higher cruise speeds and typical jet operating profiles, while the Pilatus PC-24 is a light “super versatile” jet designed to combine jet performance with the ability to use shorter runways than many peers. On range, the PC-12 NGX is typically the longest-legged of this group (roughly around 1,800+ nm), making it strong for longer nonstop legs at turboprop speeds. The King Air 360 and Phenom 300E are broadly similar in nominal range (often around the 1,500–1,800 nm class, depending on payload and reserves). The PC-24 generally sits in the same overall bracket (about 1,700–2,000 nm class) with variations by cabin load. For passenger capacity, all can be configured around six to eight passengers in typical executive layouts. The PC-12 NGX and King Air 360 can also be arranged for higher-density seating, while the PC-24’s cabin usually supports about eight to ten depending on configuration.
| Spec | Beechcraft King Air 360 | Embraer Phenom 300E | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 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 350i | Phenom 300E | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 2,010 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.53 | $ 0.55 | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 9 | 10 | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 5145 | 6914 | — | 6680 |
| Standard Cabin Seats | 8 | 6 | 6 | 6 |
| Direct Operating Cost | $ 1,311 | $ 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) | 312 | 464 | 290 | 440 |
| Base Aircraft Price (USD) | $7,650,000 | $9,650,000 | $5,350,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Optional | 1 Enclosed Flushing | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 1 |
| 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 | Optional | 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 |
| Cargo Door | — | — | Yes | Yes |
| 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) | 539 | — | — | — |
| 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 | — | — |