Beechcraft Kingair Denali vs Cirrus Vision Jet G2 vs Daher Kodiak 100 Series Iii vs Pilatus Pc 12 Ngx vs Piper M600 Sls
Category-wise, the Beechcraft Denali and Pilatus PC-12 NGX are pressurized, single‑engine turboprop business aircraft aimed at fast, high-altitude regional travel; the Piper M600 SLS is a smaller, owner-flown pressurized single turboprop; the Daher Kodiak 100 Series III is a utility/STOL turboprop optimized for short, rough strips and low‑altitude mission flexibility; and the Cirrus Vision Jet G2 is a single‑engine very light jet focused on simplicity and higher cruise speed rather than backcountry capability. On range, the PC-12 NGX and Denali generally sit at the top of this group among the turboprops for longer cross‑country legs, the M600 SLS is typically a step behind but still solid for regional trips, the Vision Jet G2 offers competitive range for a small jet but usually not as far as the longest‑leg turboprop missions, and the Kodiak’s range is typically the shortest because it prioritizes payload and short-field performance. For passenger capacity, the PC‑12 and Denali commonly accommodate the most in typical configurations, the Kodiak can also carry a large cabin load in commuter-style seating, while the M600 and Vision Jet G2 are oriented around fewer passengers in more personal owner-operator layouts.
| Spec | Beechcraft KingAir Denali | Cirrus Vision Jet G2 | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 2.37 | $ 2.78 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 5 | 8 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | GE® Aerospace | Cirrus | Pilatus | Piper |
| Aircraft Name | KingAir Denali | SF50 G2 | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1219 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.68 | $ 0.79 | $ 0.46 | $ 0.55 |
| Max Cabin Seats | 9 | 5 | 9 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3280 | 2450 | — | 2200 |
| Standard Cabin Seats | 7 | 3 | 6 | 4 |
| Direct Operating Cost | $ 1,111 | $ 711 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Cirrus Perspective Touch+ (G3000) | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 285 | 311 | 290 | 274 |
| Base Aircraft Price (USD) | $4,150,000 | $2,315,000 | $5,350,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | Optional | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 5 | 8 | 5 |
| Max Cabin Seats | 9 | 5 | 9 | — |
| Lavatory Location | AFT | — | FWD | — |
| Cabin Pressure (psi) | 5 | 6.4 | 5.8 | 5.6 |
| Galley / Refreshment | No | No | No | Refreshment Centre |
| Standard Cabin Seats | 7 | 3 | 6 | 4 |
| SL Cabin Altitude (ft) | 11065 | — | 13100 | 12600 |
| Cargo Door | — | — | Yes | — |
| Galley Location | — | — | — | MID |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| Model | Catalyst™ | FJ33-5A | PT6E-67XP | PT6A-42A |
| No. of Engines | 1 | 1 | 1 | 1 |
| FADEC | — | Yes | Yes | No |
| TBO (hrs) | — | 4000 | 5000 | 3600 |
| Flat Rating | — | ISA + 10 | ISA + 35 | ISA + 55 |
| Thrust (lbs) | — | 1846 | — | — |
| Fuel Burn (lbph) | — | 358 | — | — |
| Fuel Capacity (gal) | — | 320 | — | 260 |
| Horsepower | — | — | 1200 | 600 |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 14.86 | 30.7 | 47.25 | 29.7 |
| Wingspan (ft) | 54.3 | 38.7 | 53.33 | 43.2 |
| Cabin Width (ft) | 4.5 | 5.1 | 5 | 4.1 |
| Cabin Height (ft) | 4.8 | — | 4.9 | 4 |
| Cabin Length (ft) | 12.6 | 11.5 | 16.9 | 12.3 |
| Overall Height (ft) | 4.65 | 10.9 | 14 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | 4.25 | — |
| Cabin Length - Seating (ft) | 12.6 | 9.8 | — | — |
| Baggage Volume Int. (cu. ft) | 48 | 24 | 40 | 20 |
| Baggage Volume Ext. (cu. ft) | — | 30 | — | — |
| Cabin Volume (cu. ft) | — | — | — | 165 |