Beechcraft King Air 260 vs Embraer Phenom 100ev
The Beechcraft King Air 260 and Embraer Phenom 100EV sit in different categories despite overlapping mission profiles. The King Air 260 is a twin‑turboprop business aircraft optimized for versatility, including shorter or less‑prepared runways and operations where prop efficiency and ruggedness matter. The Phenom 100EV is a very light jet focused on higher cruise speeds and a more “jet-like” point‑to‑point experience on typical paved runways. On range, the King Air 260 is generally in the mid‑1,000‑nautical‑mile class (around 1,700 nm depending on configuration and reserves), while the Phenom 100EV is typically in the ~1,100–1,200 nm class. In practical trip planning, both cover many regional missions, but the King Air often offers more flexibility when alternates and payload are prioritized. For passenger capacity, the King Air 260 commonly seats about 7 to 9 passengers in executive layouts, whereas the Phenom 100EV is usually configured for about 4 to 7 passengers, often with a more compact cabin but faster cruise.
| Spec | Beechcraft King Air 260 | Embraer Phenom 100EV |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.30 | $ 2.84 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 7 |
| Flight Rules | IFR | — |
| Manufacturer | Beechcraft | Embraer |
| Aircraft Name | KingAir 250 | Phenom 100EV |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1,178 |
| DOC / nm / Seat | $ 0.72 | $ 0.71 |
| Max Cabin Seats | 8 | 7 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 3451 |
| Standard Cabin Seats | 6 | 5 |
| Direct Operating Cost | $ 1,333 | $ 1,152 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Prodigy Touch (G3000) |
| Max Cruise Speed (ktas) | 310 | 406 |
| Base Aircraft Price (USD) | $6,450,000 | $4,250,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Flushing | 1 Flushing |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Max Cabin Seats | 8 | 6 |
| Lavatory Location | AFT | AFT |
| Cabin Pressure (psi) | 6.5 | 8.3 |
| Galley / Refreshment | No | No |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 15293 | 21280 |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-52 | PW617F1-E |
| TBO (hrs) | 3600 | 3500 |
| Horsepower | 850 | — |
| Flat Rating | ISA + 37 | ISA + 8 |
| No. of Engines | 1 | 2 |
| Fuel Capacity (gal) | 544 | — |
| Thrust (lbs) | — | 1730 |
| Fuel Burn (lbph) | — | 543 |
| Dimensions | ||
| Length (ft) | 43.8 | 42.1 |
| Wingspan (ft) | 57.9 | 40.4 |
| Cabin Width (ft) | 4.5 | 5.1 |
| Cabin Height (ft) | 4.8 | 4.9 |
| Cabin Length (ft) | 16.7 | 11 |
| Overall Height (ft) | 14.8 | 14.3 |
| Cabin Width - Floor (ft) | 4.1 | 3.6 |
| Cabin Length - Seating (ft) | 16.7 | 9 |
| Baggage Volume Int. (cu. ft) | 55 | 10 |
| Aisle Step (ft) | — | 0.3 |
| Baggage Volume Ext. (cu. ft) | — | 60 |