Beechcraft King Air 360er vs Cessna Grand Caravan Ex vs Diamond Aircraft Da42 Vi vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360ER and Pilatus PC‑12 NGX sit in the pressurized, higher-performance turboprop class, while the Cessna Grand Caravan EX is a simpler utility turboprop optimized for short, rough-field hauling, and the Diamond DA42 VI is a lighter twin‑piston aircraft suited to smaller groups and efficient regional travel. In range, the King Air 360ER is typically the longest‑legged of this set, designed for extended missions; the PC‑12 NGX is also long‑range and close behind, depending on load and conditions. The Grand Caravan EX generally offers moderate range focused on practical payload rather than long legs. The DA42 VI tends to have respectable but shorter range than the large turboprops. For passenger capacity, the Grand Caravan EX usually carries the most in typical commuter configurations (often up to around 9 passengers), the PC‑12 NGX commonly seats about 6 to 9, and the King Air 360ER is typically configured around 6 to 9 in executive layouts. The DA42 VI is usually a 4‑ to 5‑seat aircraft.
| Spec | Beechcraft King Air 360ER | Cessna Grand Caravan EX | Diamond Aircraft DA42 VI | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | — | 2 |
| DOC / nm | $ 4.37 | $ 3.15 | $ 1.11 | $ 2.78 |
| Min Crew | 1 | 1 | — | 1 |
| Total Seats | 10 | 10 | 4 | 8 |
| Flight Rules | IFR | VFR | IFR | IFR |
| Manufacturer | Beechcraft | Cessna | Diamond Aircraft | Pilatus |
| Aircraft Name | KingAir 350ER | Grand Caravan EX | DA42 VI | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 964 | 1273 | 1803 |
| DOC / nm / Seat | $ 0.55 | $ 0.39 | $ 0.28 | $ 0.46 |
| Max Cabin Seats | 9 | 12 | — | 9 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6585 | 3332 | 1298 | — |
| Standard Cabin Seats | 8 | 8 | — | 6 |
| Direct Operating Cost | $ 1,324 | $ 614 | $ 211 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Garmin G1000 NXi | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 303 | 195 | 190 | 290 |
| Base Aircraft Price (USD) | $8,750,000 | $2,695,000 | $869,000 | $5,350,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | — | 2 |
| Lavatory | Yes (Belted Optional) | No | — | Optional |
| Min Crew | 1 | 1 | — | 1 |
| Cargo Door | Optional | Yes | — | Yes |
| Total Seats | 10 | 10 | 4 | 8 |
| Galley Location | FWD | — | — | — |
| Max Cabin Seats | 9 | 12 | — | 9 |
| Lavatory Location | AFT | — | — | FWD |
| Cabin Pressure (psi) | 6.5 | Un-Pressurized | — | 5.8 |
| Galley / Refreshment | Refreshment Center | No | — | No |
| Standard Cabin Seats | 8 | 8 | — | 6 |
| SL Cabin Altitude (ft) | — | — | — | 13100 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | PT6A-140 | AE300 | PT6E-67XP |
| TBO (hrs) | 3600 | 4000 | 1800 | 5000 |
| Horsepower | 1050 | 867 | 168 | 1200 |
| Flat Rating | ISA + 10 | ISA + 24 | — | ISA + 35 |
| No. of Engines | 1 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 775 | 335 | 79.4 | — |
| Fuel Type | — | — | Diesel / Jet Fuel | — |
| Fuel Delivery | — | — | Fuel Injected | — |
| Usable Fuel (gal) | — | — | 76.4 | 402 |
| Dimensions | ||||
| Length (ft) | 46.7 | 41.6 | 28.1 | 47.25 |
| Wingspan (ft) | 57.9 | 52.1 | 44.5 | 53.33 |
| Cabin Width (ft) | 4.5 | 5.4 | — | 5 |
| Cabin Height (ft) | 4.8 | 4.5 | — | 4.9 |
| Cabin Length (ft) | 19.5 | 16.8 | — | 16.9 |
| Overall Height (ft) | 14.4 | 15.1 | 8.2 | 14 |
| Cabin Width - Floor (ft) | 4.1 | — | — | 4.25 |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | 32 | — | 40 |