Beechcraft King Air 360er vs Cessna Grand Caravan Ex vs Pilatus Pc 12 Ngx vs Piper M600 Sls
The Beechcraft King Air 360ER is a twin‑engine turboprop in the light business/utility category, oriented toward higher speed, redundancy, and special‑mission flexibility. It typically offers a long range on the order of roughly 1,500–1,800 nautical miles depending on configuration, and commonly seats about 6–9 passengers in executive layouts, with more in high‑density commuter arrangements. The Cessna Grand Caravan EX is a single‑engine utility turboprop optimized for rugged, short/rough‑field operations and cargo/passenger versatility. Its range is generally around 900–1,200 nautical miles, and it is often configured for up to about 9 passengers (or substantial cargo). The Pilatus PC‑12 NGX is a single‑engine high‑performance turboprop positioned as a premium “single‑engine business aircraft,” blending speed and comfort with good field performance. Typical range is about 1,500–1,800 nautical miles, with common seating around 6–9 passengers. The Piper M600 SLS is a smaller single‑engine personal/business turboprop. It usually has shorter range than the PC‑12/King Air (roughly 1,200–1,500 nautical miles) and typically seats about 4–6 passengers.
| Spec | Beechcraft King Air 360ER | Cessna Grand Caravan EX | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 3.15 | $ 2.78 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 10 | 8 | 6 |
| Flight Rules | IFR | VFR | IFR | IFR |
| Manufacturer | Beechcraft | Cessna | Pilatus | Piper |
| Aircraft Name | KingAir 350ER | Grand Caravan EX | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 964 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.55 | $ 0.39 | $ 0.46 | $ 0.55 |
| Max Cabin Seats | 9 | 12 | 9 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6585 | 3332 | — | 2200 |
| Standard Cabin Seats | 8 | 8 | 6 | 4 |
| Direct Operating Cost | $ 1,324 | $ 614 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 303 | 195 | 290 | 274 |
| Base Aircraft Price (USD) | $8,750,000 | $2,695,000 | $5,350,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | No | Optional | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | Optional | Yes | Yes | — |
| Total Seats | 10 | 10 | 8 | 5 |
| Galley Location | FWD | — | — | MID |
| Max Cabin Seats | 9 | 12 | 9 | — |
| Lavatory Location | AFT | — | FWD | — |
| Cabin Pressure (psi) | 6.5 | Un-Pressurized | 5.8 | 5.6 |
| Galley / Refreshment | Refreshment Center | No | No | Refreshment Centre |
| Standard Cabin Seats | 8 | 8 | 6 | 4 |
| SL Cabin Altitude (ft) | — | — | 13100 | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PT6A-60A | PT6A-140 | PT6E-67XP | PT6A-42A |
| TBO (hrs) | 3600 | 4000 | 5000 | 3600 |
| Horsepower | 1050 | 867 | 1200 | 600 |
| Flat Rating | ISA + 10 | ISA + 24 | ISA + 35 | ISA + 55 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 775 | 335 | — | 260 |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 46.7 | 41.6 | 47.25 | 29.7 |
| Wingspan (ft) | 57.9 | 52.1 | 53.33 | 43.2 |
| Cabin Width (ft) | 4.5 | 5.4 | 5 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.5 | 4.9 | 4 |
| Cabin Length (ft) | 19.5 | 16.8 | 16.9 | 12.3 |
| Overall Height (ft) | 14.4 | 15.1 | 14 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — | 4.25 | — |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | 32 | 40 | 20 |
| Cabin Volume (cu. ft) | — | — | — | 165 |