Beechcraft King Air 260 vs Beechcraft King Air 360er vs Embraer Phenom 300e vs Pilatus Pc 12 Ngx
The Beechcraft King Air 260, King Air 360ER, Embraer Phenom 300E, and Pilatus PC-12 NGX span three distinct categories. The King Air 260 and 360ER are twin‑engine turboprops aimed at flexible short- to mid-range missions with strong short-field and all-weather utility; the 360ER is the longer‑legged, higher‑end variant. The PC‑12 NGX is a single‑engine turboprop optimized for versatility and rugged/short runways, while the Phenom 300E is a light jet focused on higher cruise speed and typical jet operations. In range, the Phenom 300E and King Air 360ER generally lead: the Phenom 300E is typically around 2,000 nm class, and the 360ER is also in the roughly 2,000+ nm class depending on configuration and reserves. The PC‑12 NGX commonly sits around the ~1,800 nm class, while the King Air 260 is usually shorter, around the ~1,700 nm class. For passenger capacity, all can be configured for about 6 to 9 passengers in typical executive layouts. The PC‑12 NGX can be arranged for more seats in commuter-style configurations, while the Phenom 300E is usually capped lower by cabin size despite strong performance.
| Spec | Beechcraft King Air 260 | Beechcraft King Air 360ER | Embraer Phenom 300E | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.37 | $ 3.88 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 10 | 8 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Beechcraft | Beechcraft | Embraer | Pilatus |
| Aircraft Name | KingAir 250 | KingAir 350ER | Phenom 300E | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 2338 | 2,010 | 1803 |
| DOC / nm / Seat | $ 0.72 | $ 0.55 | $ 0.55 | $ 0.46 |
| Max Cabin Seats | 8 | 9 | 10 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 6585 | 6914 | — |
| Standard Cabin Seats | 6 | 8 | 6 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,324 | $ 1,758 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 310 | 303 | 464 | 290 |
| Base Aircraft Price (USD) | $6,450,000 | $8,750,000 | $9,650,000 | $5,350,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | Yes (Belted Optional) | 1 Enclosed Flushing | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 9 | 8 |
| Max Cabin Seats | 8 | 9 | 9 | 9 |
| Lavatory Location | AFT | AFT | AFT | FWD |
| Cabin Pressure (psi) | 6.5 | 6.5 | 9.4 | 5.8 |
| Galley / Refreshment | No | Refreshment Center | Galley | No |
| Standard Cabin Seats | 6 | 8 | 7 | 6 |
| SL Cabin Altitude (ft) | 15293 | — | 25560 | 13100 |
| Cargo Door | — | Optional | — | Yes |
| Galley Location | — | FWD | FWD | — |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-52 | PT6A-60A | Canada PW535E1 | PT6E-67XP |
| TBO (hrs) | 3600 | 3600 | 5000 | 5000 |
| Horsepower | 850 | 1050 | — | 1200 |
| Flat Rating | ISA + 37 | ISA + 10 | ISA + 15 | ISA + 35 |
| No. of Engines | 1 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 544 | 775 | — | — |
| Thrust (lbs) | — | — | 3360 | — |
| Fuel Burn (lbph) | — | — | 757 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 43.8 | 46.7 | 51.2 | 47.25 |
| Wingspan (ft) | 57.9 | 57.9 | 52.16 | 53.33 |
| Cabin Width (ft) | 4.5 | 4.5 | 5.1 | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 | 4.9 |
| Cabin Length (ft) | 16.7 | 19.5 | 17.2 | 16.9 |
| Overall Height (ft) | 14.8 | 14.4 | 16.75 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 3.6 | 4.25 |
| Cabin Length - Seating (ft) | 16.7 | 19.5 | 14.8 | — |
| Baggage Volume Int. (cu. ft) | 55 | 71 | 10 | 40 |
| Aisle Step (ft) | — | — | 0.3 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 74 | — |