Beechcraft King Air 360 vs Beechcraft King Air 360er vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Beechcraft King Air 360 and 360ER are twin‑turboprop utility/business aircraft in the same family; the standard 360 typically offers roughly 1,500–1,800 nm range and is commonly configured for about 6–9 passengers, while the 360ER is optimized for endurance with auxiliary fuel, stretching range to about 2,000–2,500 nm with similar seating but sometimes trading payload for fuel on longer legs. The Pilatus PC‑12 NGX is a single‑engine turboprop, positioned as a versatile owner‑flown/corporate platform with strong short‑field capability; it generally carries about 6–9 passengers and typically delivers around 1,700–1,900 nm range depending on load and reserves. The Pilatus PC‑24 is a light jet (twin‑engine) aimed at faster point‑to‑point travel and jet comfort, usually seating about 6–10 passengers, with typical range around 1,900–2,200 nm. In broad terms, the King Airs emphasize twin‑turboprop redundancy and cabin utility, the PC‑12 emphasizes efficiency and simplicity, and the PC‑24 emphasizes speed and jet mission profiles.
| Spec | Beechcraft King Air 360 | Beechcraft King Air 360ER | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 4.37 | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 10 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Beechcraft | Beechcraft | Pilatus | Pilatus |
| Aircraft Name | KingAir 350i | KingAir 350ER | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 2338 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.53 | $ 0.55 | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 9 | 9 | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 5145 | 6585 | — | 6680 |
| Standard Cabin Seats | 8 | 8 | 6 | 6 |
| Direct Operating Cost | $ 1,311 | $ 1,324 | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 312 | 303 | 290 | 440 |
| Base Aircraft Price (USD) | $7,650,000 | $8,750,000 | $5,350,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Optional | Yes (Belted Optional) | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 10 | 8 | 6 |
| Galley Location | FWD | FWD | — | FWD |
| Max Cabin Seats | 9 | 9 | 9 | 10 |
| Lavatory Location | AFT | AFT | FWD | FWD |
| Cabin Pressure (psi) | 6.5 | 6.5 | 5.8 | 9.3 |
| Galley / Refreshment | Optional | Refreshment Center | No | Optional Refreshment Center |
| Standard Cabin Seats | 8 | 8 | 6 | 6 |
| Cargo Door | — | Optional | Yes | Yes |
| SL Cabin Altitude (ft) | — | — | 13100 | 23500 |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | PT6A-60A | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 3600 | 5000 | 5000 |
| Horsepower | 1050 | 1050 | 1200 | — |
| Flat Rating | ISA + 10 | ISA + 10 | ISA + 35 | ISA + 23 |
| No. of Engines | 1 | 1 | 1 | 2 |
| Fuel Capacity (gal) | 539 | 775 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Length (ft) | 46.7 | 46.7 | 47.25 | 52.2 |
| Wingspan (ft) | 57.9 | 57.9 | 53.33 | 55.8 |
| Cabin Width (ft) | 4.5 | 4.5 | 5 | 5.6 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 | 5.1 |
| Cabin Length (ft) | 19.5 | 19.5 | 16.9 | 23 |
| Overall Height (ft) | 14.4 | 14.4 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | 19.5 | 19.5 | — | 17 |
| Baggage Volume Int. (cu. ft) | 71 | 71 | 40 | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |