Beechcraft King Air 360er vs Beechcraft Kingair Denali vs Pilatus Pc 12 Ngx vs Piper M600 Sls
In category, the Beechcraft King Air 360ER and Pilatus PC-12 NGX are pressurized turboprop business aircraft, with the King Air being a twin‑engine platform and the PC‑12 a single‑engine platform. The Piper M600 SLS is also a pressurized single‑engine turboprop but in a lighter, personal/owner‑pilot class. The Beechcraft King Air Denali is a newer, pressurized single‑engine turboprop positioned between the M600 and PC‑12/King Air in cabin and mission, depending on final configuration. For range, the King Air 360ER is generally the longest‑leg option among these, designed for extended missions; the PC‑12 NGX also offers long range but typically less than the 360ER. The Denali is expected to deliver competitive, long single‑engine turboprop range in the same general band as the PC‑12 class. The M600 SLS provides solid cross‑country range, but usually shorter than the larger PC‑12/Denali/360ER segment. For passenger capacity, the King Air 360ER typically carries the most (often up to around 9 passengers), the PC‑12 NGX and Denali commonly seat about 6 to 9 depending on layout, and the M600 SLS is usually configured for about 5 to 6.
| Spec | Beechcraft King Air 360ER | Beechcraft KingAir Denali | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 4.08 | $ 2.78 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 11 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | GE® Aerospace | Pilatus | Piper |
| Aircraft Name | KingAir 350ER | KingAir Denali | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 1600 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.55 | $ 0.68 | $ 0.46 | $ 0.55 |
| Max Cabin Seats | 9 | 9 | 9 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6585 | 3280 | — | 2200 |
| Standard Cabin Seats | 8 | 7 | 6 | 4 |
| Direct Operating Cost | $ 1,324 | $ 1,111 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 303 | 285 | 290 | 274 |
| Base Aircraft Price (USD) | $8,750,000 | $4,150,000 | $5,350,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | 1 Flushing | Optional | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | Optional | — | Yes | — |
| Total Seats | 10 | 11 | 8 | 5 |
| Galley Location | FWD | — | — | MID |
| Max Cabin Seats | 9 | 9 | 9 | — |
| Lavatory Location | AFT | AFT | FWD | — |
| Cabin Pressure (psi) | 6.5 | 5 | 5.8 | 5.6 |
| Galley / Refreshment | Refreshment Center | No | No | Refreshment Centre |
| Standard Cabin Seats | 8 | 7 | 6 | 4 |
| SL Cabin Altitude (ft) | — | 11065 | 13100 | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | — | Yes | No |
| Model | PT6A-60A | Catalyst™ | PT6E-67XP | PT6A-42A |
| TBO (hrs) | 3600 | — | 5000 | 3600 |
| Horsepower | 1050 | — | 1200 | 600 |
| Flat Rating | ISA + 10 | — | ISA + 35 | ISA + 55 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 775 | — | — | 260 |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 46.7 | 14.86 | 47.25 | 29.7 |
| Wingspan (ft) | 57.9 | 54.3 | 53.33 | 43.2 |
| Cabin Width (ft) | 4.5 | 4.5 | 5 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 | 4 |
| Cabin Length (ft) | 19.5 | 12.6 | 16.9 | 12.3 |
| Overall Height (ft) | 14.4 | 4.65 | 14 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 4.25 | — |
| Cabin Length - Seating (ft) | 19.5 | 12.6 | — | — |
| Baggage Volume Int. (cu. ft) | 71 | 48 | 40 | 20 |
| Cabin Volume (cu. ft) | — | — | — | 165 |