Beechcraft King Air 260 vs Beechcraft King Air 360 vs Daher Kodiak 100 Series Iii vs Pilatus Pc 12 Ngx
In category, the Beechcraft King Air 260 and King Air 360 are twin‑engine pressurized turboprops aimed at corporate and utility missions, with the 360 positioned as the higher‑end, longer‑legged, more spacious variant. The Pilatus PC‑12 NGX is a single‑engine pressurized turboprop in the same general business/utility arena but optimized around single‑engine efficiency and a larger cabin. The Daher Kodiak 100 Series III is a single‑engine turboprop built primarily for rugged, short/rough‑field and utility roles, typically unpressurized and less business‑luxury focused than the others. On range, the Kodiak generally has the shortest legs of this group, suited to regional and remote operations. The King Air 260 offers solid mid‑to‑long range, while the King Air 360 typically extends range beyond the 260 depending on configuration. The PC‑12 NGX is generally competitive with, and often comparable to, the King Air 360 for longer trips, varying with payload and reserves. For passenger capacity, Kodiak commonly seats up to about 10, the King Air 260 and 360 are typically configured around 6–9, and the PC‑12 NGX often carries about 6–9 in executive layouts, with higher maximum seating possible in utility setups.
| Spec | Beechcraft King Air 260 | Beechcraft King Air 360 | Pilatus PC-12 NGX |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.20 | $ 2.78 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Beechcraft | Pilatus |
| Aircraft Name | KingAir 250 | KingAir 350i | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1560 | 1803 |
| DOC / nm / Seat | $ 0.72 | $ 0.53 | $ 0.46 |
| Max Cabin Seats | 8 | 9 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 5145 | — |
| Standard Cabin Seats | 6 | 8 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,311 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 310 | 312 | 290 |
| Base Aircraft Price (USD) | $6,450,000 | $7,650,000 | $5,350,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Flushing | Optional | Optional |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 8 |
| Max Cabin Seats | 8 | 9 | 9 |
| Lavatory Location | AFT | AFT | FWD |
| Cabin Pressure (psi) | 6.5 | 6.5 | 5.8 |
| Galley / Refreshment | No | Optional | No |
| Standard Cabin Seats | 6 | 8 | 6 |
| SL Cabin Altitude (ft) | 15293 | — | 13100 |
| Galley Location | — | FWD | — |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-52 | PT6A-60A | PT6E-67XP |
| TBO (hrs) | 3600 | 3600 | 5000 |
| Horsepower | 850 | 1050 | 1200 |
| Flat Rating | ISA + 37 | ISA + 10 | ISA + 35 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 544 | 539 | — |
| Usable Fuel (gal) | — | — | 402 |
| Dimensions | |||
| Length (ft) | 43.8 | 46.7 | 47.25 |
| Wingspan (ft) | 57.9 | 57.9 | 53.33 |
| Cabin Width (ft) | 4.5 | 4.5 | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 |
| Cabin Length (ft) | 16.7 | 19.5 | 16.9 |
| Overall Height (ft) | 14.8 | 14.4 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 4.25 |
| Cabin Length - Seating (ft) | 16.7 | 19.5 | — |
| Baggage Volume Int. (cu. ft) | 55 | 71 | 40 |