Beechcraft King Air 260 vs Cessna Grand Caravan Ex vs Daher Kodiak 100 Series Iii vs Pilatus Pc 12 Ngx vs Piper M350
By category, the Beechcraft King Air 260 is a pressurized twin‑turboprop business/utility aircraft, the Pilatus PC‑12 NGX is a pressurized single‑turboprop executive/utility aircraft, the Piper M350 is a pressurized piston‑single personal/business aircraft, and both the Cessna Grand Caravan EX and Daher Kodiak 100 Series III are unpressurized single‑turboprop utility/STOL aircraft optimized for short, rough-field work. In typical use, the PC‑12 NGX and King Air 260 generally offer the longest practical ranges in this group (often around the 1,500–1,800 nm class depending on payload and reserves), with the M350 usually somewhat shorter (roughly around 1,000–1,300 nm). The Grand Caravan EX and Kodiak are commonly operated at shorter ranges (often roughly 800–1,200 nm depending on configuration), prioritizing lift and field performance over long legs. For passenger capacity, the Caravan EX is usually the highest, commonly configured around 9 passengers (more in some utility layouts). The Kodiak is typically up to about 9. The PC‑12 often seats about 6–9 in executive configurations, while the King Air 260 commonly carries about 6–9 as well. The M350 is smaller, typically seating about 5–6.
| Spec | Beechcraft King Air 260 | Cessna Grand Caravan EX | Pilatus PC-12 NGX | Piper M350 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 3.15 | $ 2.78 | $ 1.34 |
| Min Crew | 1 | 1 | 1 | — |
| Total Seats | 8 | 10 | 8 | 6 |
| Flight Rules | IFR | VFR | IFR | VFR |
| Manufacturer | Beechcraft | Cessna | Pilatus | Piper |
| Aircraft Name | KingAir 250 | Grand Caravan EX | PC-12 NGX | M350 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 964 | 1803 | 1343 |
| DOC / nm / Seat | $ 0.72 | $ 0.39 | $ 0.46 | $ 0.22 |
| Max Cabin Seats | 8 | 12 | 9 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3760 | 3332 | — | 1308 |
| Standard Cabin Seats | 6 | 8 | 6 | 4 |
| Direct Operating Cost | $ 1,333 | $ 614 | $ 793 | $ 285 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Honeywell Primus Apex | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 310 | 195 | 290 | 213 |
| Base Aircraft Price (USD) | $6,450,000 | $2,695,000 | $5,350,000 | $1,195,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | Optional | — |
| Min Crew | 1 | 1 | 1 | — |
| Total Seats | 8 | 10 | 8 | 6 |
| Max Cabin Seats | 8 | 12 | 9 | — |
| Lavatory Location | AFT | — | FWD | — |
| Cabin Pressure (psi) | 6.5 | Un-Pressurized | 5.8 | 5.6 |
| Galley / Refreshment | No | No | No | — |
| Standard Cabin Seats | 6 | 8 | 6 | 4 |
| SL Cabin Altitude (ft) | 15293 | — | 13100 | — |
| Cargo Door | — | Yes | Yes | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PT6A-52 | PT6A-140 | PT6E-67XP | TIO-540-AE2A |
| TBO (hrs) | 3600 | 4000 | 5000 | 2000 |
| Horsepower | 850 | 867 | 1200 | 350 |
| Flat Rating | ISA + 37 | ISA + 24 | ISA + 35 | — |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 544 | 335 | — | 120 |
| Usable Fuel (gal) | — | — | 402 | — |
| Fuel Type | — | — | — | AvGas |
| TBO (yrs) | — | — | — | 12 |
| Fuel Delivery | — | — | — | Fuel Injected |
| Dimensions | ||||
| Length (ft) | 43.8 | 41.6 | 47.25 | 29 |
| Wingspan (ft) | 57.9 | 52.1 | 53.33 | 43 |
| Cabin Width (ft) | 4.5 | 5.4 | 5 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.5 | 4.9 | 4 |
| Cabin Length (ft) | 16.7 | 16.8 | 16.9 | 12.3 |
| Overall Height (ft) | 14.8 | 15.1 | 14 | 11.4 |
| Cabin Width - Floor (ft) | 4.1 | — | 4.25 | — |
| Cabin Length - Seating (ft) | 16.7 | — | — | — |
| Baggage Volume Int. (cu. ft) | 55 | 32 | 40 | 20 |
| Cabin Volume (cu. ft) | — | — | — | 165 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 13 |