Beechcraft Baron G58 vs Beechcraft Kingair Denali vs Cirrus Sf50 G2 vs Daher Tbm 940 vs Piper M500
The Beechcraft Baron G58 is a piston twin, typically used for short to medium missions. It generally offers the shortest range of this group (roughly 1,000–1,500 nm, depending on power settings and reserves) and usually carries 4–6 people in real-world travel comfort, with seating for up to six. The Piper M500 is a single‑engine turboprop, a step up in speed and altitude capability versus the Baron, with typical range around 1,000–1,300 nm and usually 4–5 passengers comfortably, with seating for up to five. The Daher TBM 940 is a high‑performance single‑engine turboprop, commonly flown for longer point‑to‑point trips. It typically ranges about 1,500–1,700 nm and can seat up to six, with 4–6 aboard depending on baggage and fuel. The Cirrus Vision Jet G2 is a single‑engine very light jet, usually around 1,200 nm range and seating for up to seven (including pilot), though payload often makes 4–5 passengers more typical. The Beechcraft King Air Denali is a pressurized single‑engine turboprop in the “large cabin” class, aimed at longer legs (about 1,500–1,600+ nm) and typically 6–9 passengers depending on configuration.
| Spec | Beechcraft Baron G58 | Beechcraft KingAir Denali | Daher TBM 940 | Piper M500 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | $ 4.08 | $ 2.25 | $ 3.11 |
| Total Seats | 6 | 11 | 6 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | GE® Aerospace | Daher TBM | Piper |
| Aircraft Name | Baron G58 | KingAir Denali | TBM 940 | M500 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 1600 | 1730 | 1000 |
| DOC / nm / Seat | $ 0.29 | $ 0.68 | $ 0.56 | $ 0.78 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1450 | 3280 | 2908 | 1698 |
| Standard Cabin Seats | 4 | 7 | 4 | 4 |
| Direct Operating Cost | $ 347 | $ 1,111 | $ 744 | $ 579 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 202 | 285 | 330 | 260 |
| Base Aircraft Price (USD) | $1,495,000 | $4,150,000 | $4,450,000 | $2,122,600 |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 9 | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 11 | 6 | 5 |
| Standard Cabin Seats | 4 | 7 | 4 | 4 |
| Lavatory | — | 1 Flushing | No | No |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 9 | — | — |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 5 | 6.2 | 5.5 |
| Galley / Refreshment | — | No | Refreshment Centre | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 11065 | 14390 | 12600 |
| Galley Location | — | — | MID | MID |
| Max Cabin Altitude (ft) | — | — | — | 8244 |
| Engine | ||||
| FADEC | No | — | Yes | No |
| Model | IO-550-C | Catalyst™ | PT6A-66D | PT6A-42A |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 1700 | — | 3500 | 3600 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 300 | — | 850 | 500 |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 2 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 194 | — | 291 | 170 |
| Flat Rating | — | — | ISA + 49 | ISA + 55 |
| Dimensions | ||||
| Length (ft) | 29.9 | 14.86 | 35.3 | 29.6 |
| Wingspan (ft) | 37.9 | 54.3 | 42.1 | 43.2 |
| Cabin Width (ft) | 3.5 | 4.5 | 4 | 4.1 |
| Cabin Height (ft) | 4.2 | 4.8 | 4.1 | 4 |
| Cabin Length (ft) | 12.6 | 12.6 | 13.4 | 12.3 |
| Overall Height (ft) | 9.8 | 4.65 | 14.3 | 11.3 |
| Cabin Volume (cu. ft) | 150 | — | 123 | 165 |
| Baggage Volume Int. (cu. ft) | 46 | 48 | 30 | 20 |
| Cabin Width - Floor (ft) | — | 4.1 | — | — |
| Cabin Length - Seating (ft) | — | 12.6 | — | — |