Beechcraft King Air 360 vs Pilatus Pc 12 Ngx vs Piper M350 vs Piper M600 Sls
The Beechcraft King Air 360 and Pilatus PC-12 NGX sit in the high-end turboprop category, while the Piper M600 SLS is a lighter, single‑engine turboprop and the Piper M350 is a pressurized piston single. In typical mission use, the King Air 360 offers strong all‑around performance with a common real‑world range around roughly 1,500–1,800 nm depending on load and reserves, and it generally carries about 6–9 passengers in executive seating. The PC‑12 NGX is also long‑legged, often quoted around about 1,700–1,800 nm, and usually seats about 6–9, with notable cabin and cargo flexibility for a single‑engine turboprop. The M600 SLS targets owner‑operators needing turboprop speed and simplicity; its typical range is roughly 1,200–1,400 nm with seating commonly around 4–6 passengers. The M350 emphasizes efficiency and lower operating costs in the pressurized piston class, with a typical range roughly 1,000–1,300 nm and usually 4–5 passengers plus pilot, depending on configuration and payload.
| Spec | Beechcraft King Air 360 | Pilatus PC-12 NGX | Piper M350 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 2.78 | $ 1.34 | $ 2.19 |
| Min Crew | 1 | 1 | — | 1 |
| Total Seats | 10 | 8 | 6 | 6 |
| Flight Rules | IFR | IFR | VFR | IFR |
| Manufacturer | Beechcraft | Pilatus | Piper | Piper |
| Aircraft Name | KingAir 350i | PC-12 NGX | M350 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 1803 | 1343 | 1406 |
| DOC / nm / Seat | $ 0.53 | $ 0.46 | $ 0.22 | $ 0.55 |
| Max Cabin Seats | 9 | 9 | — | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 5145 | — | 1308 | 2200 |
| Standard Cabin Seats | 8 | 6 | 4 | 4 |
| Direct Operating Cost | $ 1,311 | $ 793 | $ 285 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 312 | 290 | 213 | 274 |
| Base Aircraft Price (USD) | $7,650,000 | $5,350,000 | $1,195,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Optional | Optional | — | No |
| Min Crew | 1 | 1 | — | 1 |
| Total Seats | 10 | 8 | 6 | 5 |
| Galley Location | FWD | — | — | MID |
| Max Cabin Seats | 9 | 9 | — | — |
| Lavatory Location | AFT | FWD | — | — |
| Cabin Pressure (psi) | 6.5 | 5.8 | 5.6 | 5.6 |
| Galley / Refreshment | Optional | No | — | Refreshment Centre |
| Standard Cabin Seats | 8 | 6 | 4 | 4 |
| Cargo Door | — | Yes | — | — |
| SL Cabin Altitude (ft) | — | 13100 | — | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | No | No |
| Model | PT6A-60A | PT6E-67XP | TIO-540-AE2A | PT6A-42A |
| TBO (hrs) | 3600 | 5000 | 2000 | 3600 |
| Horsepower | 1050 | 1200 | 350 | 600 |
| Flat Rating | ISA + 10 | ISA + 35 | — | ISA + 55 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 539 | — | 120 | 260 |
| Usable Fuel (gal) | — | 402 | — | — |
| Fuel Type | — | — | AvGas | — |
| TBO (yrs) | — | — | 12 | — |
| Fuel Delivery | — | — | Fuel Injected | — |
| Dimensions | ||||
| Length (ft) | 46.7 | 47.25 | 29 | 29.7 |
| Wingspan (ft) | 57.9 | 53.33 | 43 | 43.2 |
| Cabin Width (ft) | 4.5 | 5 | 4.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.9 | 4 | 4 |
| Cabin Length (ft) | 19.5 | 16.9 | 12.3 | 12.3 |
| Overall Height (ft) | 14.4 | 14 | 11.4 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | 4.25 | — | — |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | 40 | 20 | 20 |
| Cabin Volume (cu. ft) | — | — | 165 | 165 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 | — |