Beechcraft Kingair Denali vs Cirrus Vision Jet G2 vs Daher Tbm 960 vs Piper M500
The Beechcraft Denali and Piper M500 are single‑engine turboprops aimed at efficient owner‑pilot travel, while the Daher TBM 960 is a higher‑performance single‑engine turboprop and the Cirrus Vision Jet G2 is a single‑engine very light jet. In range terms, the TBM 960 generally leads this group at roughly 1,700–1,800 nm depending on conditions, the Denali is positioned around the mid‑1,500 nm class, the M500 is typically around 1,000–1,200 nm, and the Vision Jet G2 is usually around 1,200 nm. For passenger capacity, the Denali is designed as a larger‑cabin turboprop typically configured for about 6–9 occupants including the pilot, the TBM 960 commonly seats 5–6 plus a pilot (often marketed as up to 6–7 total depending on seating choices), the M500 is generally a 5–6 seat aircraft including the pilot, and the Vision Jet G2 is typically configured for 4–5 passengers plus a pilot, with an option for small additional seating but with practical limits set by payload and mission length.
| Spec | Beechcraft KingAir Denali | Cirrus Vision Jet G2 | Daher TBM 960 | Piper M500 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 2.37 | $ 2.25 | $ 3.11 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 5 | 6 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | GE® Aerospace | Cirrus | Daher TBM | Piper |
| Aircraft Name | KingAir Denali | SF50 G2 | TBM 960 | M500 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1219 | 1730 | 1000 |
| DOC / nm / Seat | $ 0.68 | $ 0.79 | $ 0.56 | $ 0.78 |
| Max Cabin Seats | 9 | 5 | — | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3280 | 2450 | 2908 | 1698 |
| Standard Cabin Seats | 7 | 3 | 4 | 4 |
| Direct Operating Cost | $ 1,111 | $ 711 | $ 744 | $ 579 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Cirrus Perspective Touch+ (G3000) | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 285 | 311 | 330 | 260 |
| Base Aircraft Price (USD) | $4,150,000 | $2,315,000 | $4,450,000 | $2,122,600 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | No | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 5 | 6 | 5 |
| Max Cabin Seats | 9 | 5 | — | — |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 5 | 6.4 | 6.2 | 5.5 |
| Galley / Refreshment | No | No | — | Refreshment Centre |
| Standard Cabin Seats | 7 | 3 | 4 | 4 |
| SL Cabin Altitude (ft) | 11065 | — | 14390 | 12600 |
| Galley Location | — | — | MID | MID |
| Max Cabin Altitude (ft) | — | — | — | 8244 |
| Engine | ||||
| Model | Catalyst™ | FJ33-5A | TBM 960 | PT6A-42A |
| No. of Engines | 1 | 1 | — | 1 |
| FADEC | — | Yes | Yes | No |
| TBO (hrs) | — | 4000 | 3500 | 3600 |
| Flat Rating | — | ISA + 10 | ISA + 49 | ISA + 55 |
| Thrust (lbs) | — | 1846 | — | — |
| Fuel Burn (lbph) | — | 358 | — | — |
| Fuel Capacity (gal) | — | 320 | — | 170 |
| Horsepower | — | — | 850 | 500 |
| Dimensions | ||||
| Length (ft) | 14.86 | 30.7 | 35.3 | 29.6 |
| Wingspan (ft) | 54.3 | 38.7 | 42.1 | 43.2 |
| Cabin Width (ft) | 4.5 | 5.1 | 4 | 4.1 |
| Cabin Height (ft) | 4.8 | — | 4.1 | 4 |
| Cabin Length (ft) | 12.6 | 11.5 | 13.4 | 12.3 |
| Overall Height (ft) | 4.65 | 10.9 | — | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | — | — |
| Cabin Length - Seating (ft) | 12.6 | 9.8 | — | — |
| Baggage Volume Int. (cu. ft) | 48 | 24 | — | 20 |
| Baggage Volume Ext. (cu. ft) | — | 30 | — | — |
| Cabin Volume (cu. ft) | — | — | 123 | 165 |