Beechcraft Kingair Denali vs Cessna Skycourier vs Pilatus Pc 12 Ngx
In category terms, the Beechcraft Denali and Pilatus PC-12 NGX are best viewed as single‑engine turboprop business/utility aircraft aimed at executive travel and premium, flexible missions, while the Cessna SkyCourier is a purpose-built utility turboprop (typically twin‑engine) optimized for short-haul cargo and regional shuttle work rather than owner-flown business transport. On range, the PC-12 NGX generally leads the group, widely used for longer point-to-point trips and often cited around the ~1,700–1,800 nm class depending on payload and reserves. The Denali is positioned to be competitive in the same general bracket but is typically described as somewhat shorter than the PC‑12 on long-range missions, with published targets often around the ~1,600 nm class. The SkyCourier is optimized for shorter regional legs; its practical range is commonly around the ~900–1,200 nm class depending on configuration and load. For passenger capacity, the PC-12 NGX and Denali commonly seat about 6–9 passengers in executive layouts. The SkyCourier can carry more people in commuter form, typically around 19 passengers, and is especially strong in cargo-oriented configurations.
| Spec | Beechcraft KingAir Denali | Cessna SkyCourier | Pilatus PC-12 NGX |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | — | $ 2.78 |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 11 | 21 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | GE® Aerospace | Cessna | Pilatus |
| Aircraft Name | KingAir Denali | SkyCourier | PC-12 NGX |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 1600 | 900 | 1803 |
| DOC / nm / Seat | $ 0.68 | — | $ 0.46 |
| Max Cabin Seats | 9 | 19 | 9 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3280 | — | — |
| Standard Cabin Seats | 7 | 19 | 6 |
| Direct Operating Cost | $ 1,111 | — | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Gyro / Analog | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 285 | 200 | 290 |
| Base Aircraft Price (USD) | $4,150,000 | $7,375,000 | $5,350,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | Optional |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 11 | 21 | 8 |
| Max Cabin Seats | 9 | 19 | 9 |
| Lavatory Location | AFT | — | FWD |
| Cabin Pressure (psi) | 5 | Un-Pressurized | 5.8 |
| Galley / Refreshment | No | No | No |
| Standard Cabin Seats | 7 | 19 | 6 |
| SL Cabin Altitude (ft) | 11065 | — | 13100 |
| Cargo Door | — | Yes | Yes |
| Engine | |||
| Model | Catalyst™ | PT6A-65SC | PT6E-67XP |
| No. of Engines | 1 | 1 | 1 |
| FADEC | — | Yes | Yes |
| TBO (hrs) | — | 6000 | 5000 |
| Horsepower | — | 1100 | 1200 |
| Flat Rating | — | — | ISA + 35 |
| Usable Fuel (gal) | — | — | 402 |
| Dimensions | |||
| Length (ft) | 14.86 | 54.9 | 47.25 |
| Wingspan (ft) | 54.3 | 72 | 53.33 |
| Cabin Width (ft) | 4.5 | — | 5 |
| Cabin Height (ft) | 4.8 | — | 4.9 |
| Cabin Length (ft) | 12.6 | — | 16.9 |
| Overall Height (ft) | 4.65 | 19.8 | 14 |
| Cabin Width - Floor (ft) | 4.1 | — | 4.25 |
| Cabin Length - Seating (ft) | 12.6 | — | — |
| Baggage Volume Int. (cu. ft) | 48 | — | 40 |