Beechcraft King Air 360 vs Beechcraft King Air 360er vs Beechcraft Kingair Denali vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360 is a pressurized twin‑turboprop positioned as a premium short‑to‑mid range utility and business aircraft, typically configured for about six to nine passengers depending on interior and mission fit. The King Air 360ER keeps the same general category and cabin concept but is optimized for endurance; it trades some payload flexibility for substantially more range, making it better suited to long overwater legs, remote-region operations, and missions where refueling options are limited, while still generally seating in the same broad six‑to‑nine passenger band. The Beechcraft King Air Denali is a newer clean‑sheet single‑engine turboprop aimed at the high‑performance, owner‑operator/business segment; it targets a similar passenger count to a well‑appointed PC‑12 class aircraft, generally around six to nine, with range intended to compete in the long‑leg single‑engine turboprop market. The Pilatus PC‑12 NGX is the established benchmark in that single‑engine category, commonly configured for six to nine passengers, and offers long range for a single‑turboprop, typically exceeding the standard King Air 360 but generally trailing the 360ER’s maximum endurance-focused capability.
| Spec | Beechcraft King Air 360 | Beechcraft King Air 360ER | Beechcraft KingAir Denali | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 4.37 | $ 4.08 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 10 | 11 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Beechcraft | GE® Aerospace | Pilatus |
| Aircraft Name | KingAir 350i | KingAir 350ER | KingAir Denali | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 2338 | 1600 | 1803 |
| DOC / nm / Seat | $ 0.53 | $ 0.55 | $ 0.68 | $ 0.46 |
| Max Cabin Seats | 9 | 9 | 9 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 5145 | 6585 | 3280 | — |
| Standard Cabin Seats | 8 | 8 | 7 | 6 |
| Direct Operating Cost | $ 1,311 | $ 1,324 | $ 1,111 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 312 | 303 | 285 | 290 |
| Base Aircraft Price (USD) | $7,650,000 | $8,750,000 | $4,150,000 | $5,350,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Optional | Yes (Belted Optional) | 1 Flushing | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 10 | 11 | 8 |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 9 | 9 | 9 | 9 |
| Lavatory Location | AFT | AFT | AFT | FWD |
| Cabin Pressure (psi) | 6.5 | 6.5 | 5 | 5.8 |
| Galley / Refreshment | Optional | Refreshment Center | No | No |
| Standard Cabin Seats | 8 | 8 | 7 | 6 |
| Cargo Door | — | Optional | — | Yes |
| SL Cabin Altitude (ft) | — | — | 11065 | 13100 |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | PT6A-60A | PT6A-60A | Catalyst™ | PT6E-67XP |
| TBO (hrs) | 3600 | 3600 | — | 5000 |
| Horsepower | 1050 | 1050 | — | 1200 |
| Flat Rating | ISA + 10 | ISA + 10 | — | ISA + 35 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 539 | 775 | — | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 46.7 | 46.7 | 14.86 | 47.25 |
| Wingspan (ft) | 57.9 | 57.9 | 54.3 | 53.33 |
| Cabin Width (ft) | 4.5 | 4.5 | 4.5 | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.8 | 4.9 |
| Cabin Length (ft) | 19.5 | 19.5 | 12.6 | 16.9 |
| Overall Height (ft) | 14.4 | 14.4 | 4.65 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 4.1 | 4.25 |
| Cabin Length - Seating (ft) | 19.5 | 19.5 | 12.6 | — |
| Baggage Volume Int. (cu. ft) | 71 | 71 | 48 | 40 |