Beechcraft King Air 260 vs Cessna Citation M2 vs Embraer Phenom 100ev vs Pilatus Pc 12 Ngx
The Beechcraft King Air 260 and Pilatus PC-12 NGX are pressurized turboprops, while the Cessna Citation M2 and Embraer Phenom 100EV are very light jets. In typical use, the PC-12 NGX generally offers the longest range of this group at roughly 1,700–1,800 nautical miles, with the King Air 260 close behind around 1,700 nm. The Phenom 100EV and Citation M2 usually come in shorter, commonly about 1,150–1,200 nm for the Phenom 100EV and about 1,300–1,550 nm for the M2 depending on configuration and reserves. For passenger capacity, the PC-12 NGX often seats 6–8 passengers in executive layouts (with higher-density options available), and the King Air 260 typically carries about 7–9. The Phenom 100EV is commonly arranged for 4–7, while the Citation M2 is usually configured for about 4–6. Overall, the jets emphasize speed and high-altitude cruise, while the turboprops emphasize cabin flexibility and strong short/rough-field capability.
| Spec | Beechcraft King Air 260 | Cessna Citation M2 | Embraer Phenom 100EV | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 3.45 | $ 2.84 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 7 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Beechcraft | Cessna Citation | Embraer | Pilatus |
| Aircraft Name | KingAir 250 | M2 | Phenom 100EV | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1400 | 1,178 | 1803 |
| DOC / nm / Seat | $ 0.72 | $ 0.58 | $ 0.71 | $ 0.46 |
| Max Cabin Seats | 8 | 7 | 7 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 3810 | 3451 | — |
| Standard Cabin Seats | 6 | 6 | 5 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,395 | $ 1,152 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 310 | 404 | 406 | 290 |
| Base Aircraft Price (USD) | $6,450,000 | $5,150,000 | $4,250,000 | $5,350,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Enclosed Belted Flushing | 1 Flushing | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 6 | 8 |
| Max Cabin Seats | 8 | 7 | 6 | 9 |
| Lavatory Location | AFT | AFT | AFT | FWD |
| Cabin Pressure (psi) | 6.5 | 8.5 | 8.3 | 5.8 |
| Galley / Refreshment | No | No | No | No |
| Standard Cabin Seats | 6 | 6 | 4 | 6 |
| SL Cabin Altitude (ft) | 15293 | 22027 | 21280 | 13100 |
| Crew Rest | — | No | No | — |
| Jump Seat | — | No | No | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-52 | FJ44-1AP-21 | PW617F1-E | PT6E-67XP |
| TBO (hrs) | 3600 | 3500 | 3500 | 5000 |
| Horsepower | 850 | — | — | 1200 |
| Flat Rating | ISA + 37 | ISA + 7 | ISA + 8 | ISA + 35 |
| No. of Engines | 1 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 544 | 492 | — | — |
| Thrust (lbs) | — | 1965 | 1730 | — |
| Fuel Burn (lbph) | — | 516 | 543 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 43.8 | 42.6 | 42.1 | 47.25 |
| Wingspan (ft) | 57.9 | 47.3 | 40.4 | 53.33 |
| Cabin Width (ft) | 4.5 | 4.8 | 5.1 | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 | 4.9 |
| Cabin Length (ft) | 16.7 | 11 | 11 | 16.9 |
| Overall Height (ft) | 14.8 | 14 | 14.3 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | 3.6 | 4.25 |
| Cabin Length - Seating (ft) | 16.7 | 8.8 | 9 | — |
| Baggage Volume Int. (cu. ft) | 55 | — | 10 | 40 |
| Aisle Step (ft) | — | 0.4 | 0.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 46 | 60 | — |