Beechcraft King Air 360 vs Beechcraft Kingair Denali vs Embraer Phenom 100ev vs Pilatus Pc 12 Ngx
In category, the Beechcraft King Air 360 and Pilatus PC-12 NGX are pressurized single/dual‑engine turboprop business aircraft (the King Air is twin‑turboprop; the PC‑12 is single‑turboprop) optimized for short fields and flexible regional missions. The Beechcraft King Air Denali is a newer‑generation single‑engine turboprop positioned between traditional utility turboprops and light business aircraft. The Embraer Phenom 100EV is a very light jet, prioritizing higher cruise speeds and jet operating characteristics over rough/short‑field versatility. On range, the PC‑12 NGX and King Air 360 generally sit in the ~1,600–1,800+ nm class depending on payload and reserves, while the Denali is designed to be competitive in the high‑1,000‑nm turboprop segment (often cited around ~1,600 nm). The Phenom 100EV typically offers shorter legs than these long‑range turboprops, roughly in the ~1,100–1,200 nm class. For passenger capacity, the King Air 360 commonly seats about 6–9, the Denali about 6–8, the PC‑12 NGX about 6–10 (with high‑density options), and the Phenom 100EV typically 4–7 in executive layouts.
| Spec | Beechcraft King Air 360 | Beechcraft KingAir Denali | Embraer Phenom 100EV | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 4.08 | $ 2.84 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 11 | 7 | 8 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Beechcraft | GE® Aerospace | Embraer | Pilatus |
| Aircraft Name | KingAir 350i | KingAir Denali | Phenom 100EV | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 1600 | 1,178 | 1803 |
| DOC / nm / Seat | $ 0.53 | $ 0.68 | $ 0.71 | $ 0.46 |
| Max Cabin Seats | 9 | 9 | 7 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 5145 | 3280 | 3451 | — |
| Standard Cabin Seats | 8 | 7 | 5 | 6 |
| Direct Operating Cost | $ 1,311 | $ 1,111 | $ 1,152 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 312 | 285 | 406 | 290 |
| Base Aircraft Price (USD) | $7,650,000 | $4,150,000 | $4,250,000 | $5,350,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Optional | 1 Flushing | 1 Flushing | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 11 | 6 | 8 |
| Galley Location | FWD | — | — | — |
| Max Cabin Seats | 9 | 9 | 6 | 9 |
| Lavatory Location | AFT | AFT | AFT | FWD |
| Cabin Pressure (psi) | 6.5 | 5 | 8.3 | 5.8 |
| Galley / Refreshment | Optional | No | No | No |
| Standard Cabin Seats | 8 | 7 | 4 | 6 |
| SL Cabin Altitude (ft) | — | 11065 | 21280 | 13100 |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | PT6A-60A | Catalyst™ | PW617F1-E | PT6E-67XP |
| TBO (hrs) | 3600 | — | 3500 | 5000 |
| Horsepower | 1050 | — | — | 1200 |
| Flat Rating | ISA + 10 | — | ISA + 8 | ISA + 35 |
| No. of Engines | 1 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 539 | — | — | — |
| Thrust (lbs) | — | — | 1730 | — |
| Fuel Burn (lbph) | — | — | 543 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 46.7 | 14.86 | 42.1 | 47.25 |
| Wingspan (ft) | 57.9 | 54.3 | 40.4 | 53.33 |
| Cabin Width (ft) | 4.5 | 4.5 | 5.1 | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.9 | 4.9 |
| Cabin Length (ft) | 19.5 | 12.6 | 11 | 16.9 |
| Overall Height (ft) | 14.4 | 4.65 | 14.3 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 3.6 | 4.25 |
| Cabin Length - Seating (ft) | 19.5 | 12.6 | 9 | — |
| Baggage Volume Int. (cu. ft) | 71 | 48 | 10 | 40 |
| Aisle Step (ft) | — | — | 0.3 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 60 | — |