Beechcraft Kingair Denali vs Cirrus Vision Jet G2 vs Daher Tbm 960
All three are single‑engine turbine aircraft but serve different niches. The Beechcraft Denali is a pressurized single‑engine turboprop positioned as a larger, utility‑oriented step above legacy light turboprops, intended to carry a typical executive load with room for baggage and optional high‑density seating. The Daher TBM 960 is also a pressurized single‑engine turboprop, but it emphasizes speed and efficient owner‑pilot touring; it generally carries fewer people than the Denali in typical layouts while delivering strong long‑range capability. The Cirrus Vision Jet G2 is a single‑engine very light jet, optimized for simplicity and short‑to‑medium trips with jet speeds, usually with the smallest practical payload and cabin volume of the three. In range, the TBM 960 is typically the longest‑legged, often around the ~1,700‑nautical‑mile class depending on reserves and conditions; the Denali is generally in the ~1,500‑nautical‑mile class as targeted; the Vision Jet G2 is usually shorter, commonly around ~1,200 nautical miles. In passenger capacity, the Denali is typically highest (often 6–9 seats depending on configuration), the Vision Jet G2 is commonly configured for 5 passengers plus a pilot (up to 7 seats including pilot), and the TBM 960 is usually 4–6 seats plus a pilot.
| Spec | Beechcraft KingAir Denali | Cirrus Vision Jet G2 | Daher TBM 960 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 2.37 | $ 2.25 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 11 | 5 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | GE® Aerospace | Cirrus | Daher TBM |
| Aircraft Name | KingAir Denali | SF50 G2 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1219 | 1730 |
| DOC / nm / Seat | $ 0.68 | $ 0.79 | $ 0.56 |
| Max Cabin Seats | 9 | 5 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3280 | 2450 | 2908 |
| Standard Cabin Seats | 7 | 3 | 4 |
| Direct Operating Cost | $ 1,111 | $ 711 | $ 744 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Cirrus Perspective Touch+ (G3000) | Garmin G3000 |
| Max Cruise Speed (ktas) | 285 | 311 | 330 |
| Base Aircraft Price (USD) | $4,150,000 | $2,315,000 | $4,450,000 |
| Aircraft Type | — | — | Turbo Prop |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | No |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 11 | 5 | 6 |
| Max Cabin Seats | 9 | 5 | — |
| Lavatory Location | AFT | — | — |
| Cabin Pressure (psi) | 5 | 6.4 | 6.2 |
| Galley / Refreshment | No | No | — |
| Standard Cabin Seats | 7 | 3 | 4 |
| SL Cabin Altitude (ft) | 11065 | — | 14390 |
| Galley Location | — | — | MID |
| Engine | |||
| Model | Catalyst™ | FJ33-5A | TBM 960 |
| No. of Engines | 1 | 1 | — |
| FADEC | — | Yes | Yes |
| TBO (hrs) | — | 4000 | 3500 |
| Flat Rating | — | ISA + 10 | ISA + 49 |
| Thrust (lbs) | — | 1846 | — |
| Fuel Burn (lbph) | — | 358 | — |
| Fuel Capacity (gal) | — | 320 | — |
| Horsepower | — | — | 850 |
| Dimensions | |||
| Length (ft) | 14.86 | 30.7 | 35.3 |
| Wingspan (ft) | 54.3 | 38.7 | 42.1 |
| Cabin Width (ft) | 4.5 | 5.1 | 4 |
| Cabin Height (ft) | 4.8 | — | 4.1 |
| Cabin Length (ft) | 12.6 | 11.5 | 13.4 |
| Overall Height (ft) | 4.65 | 10.9 | — |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | — |
| Cabin Length - Seating (ft) | 12.6 | 9.8 | — |
| Baggage Volume Int. (cu. ft) | 48 | 24 | — |
| Baggage Volume Ext. (cu. ft) | — | 30 | — |
| Cabin Volume (cu. ft) | — | — | 123 |