Beechcraft Baron G58 vs Daher Tbm 960 vs Piper M600 Sls
The Beechcraft Baron G58 is a piston-powered, twin‑engine light aircraft aimed at personal and small business travel where redundancy and lower acquisition cost matter more than speed. It typically carries four to six people depending on seating configuration and loading, and is best suited to regional trips, with real-world range generally in the mid-hundreds of nautical miles to around 1,000 nautical miles with reserves depending on power settings and payload. The Daher TBM 960 is a single‑engine turboprop in the high‑performance personal/business category, optimized for fast, efficient point‑to‑point travel. It generally seats six (often used with four to five plus baggage for longer legs) and offers the longest range of the three, commonly around 1,500+ nautical miles depending on conditions and reserves. The Piper M600 SLS is also a single‑engine turboprop, positioned between the Baron and the TBM in performance and mission. It typically seats five to six and delivers solid cross‑country capability, with range commonly around 1,200–1,500 nautical miles depending on payload and settings.
| Spec | Beechcraft Baron G58 | Daher TBM 960 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | $ 2.25 | $ 2.19 |
| Total Seats | 6 | 6 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Piper |
| Aircraft Name | Baron G58 | TBM 960 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 1730 | 1406 |
| DOC / nm / Seat | $ 0.29 | $ 0.56 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1450 | 2908 | 2200 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Direct Operating Cost | $ 347 | $ 744 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Garmin G3000 |
| Max Cruise Speed (ktas) | 202 | 330 | 274 |
| Base Aircraft Price (USD) | $1,495,000 | $4,450,000 | $3,081,400 |
| Min Crew | — | 1 | 1 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Total Seats | 6 | 6 | 5 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Lavatory | — | No | No |
| Min Crew | — | 1 | 1 |
| Galley Location | — | MID | MID |
| Cabin Pressure (psi) | — | 6.2 | 5.6 |
| SL Cabin Altitude (ft) | — | 14390 | 12600 |
| Galley / Refreshment | — | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | No | Yes | No |
| Model | IO-550-C | TBM 960 | PT6A-42A |
| Fuel Type | AvGas | — | — |
| TBO (hrs) | 1700 | 3500 | 3600 |
| TBO (yrs) | 12 | — | — |
| Horsepower | 300 | 850 | 600 |
| Fuel Delivery | Fuel Injected | — | — |
| No. of Engines | 2 | — | 1 |
| Fuel Capacity (gal) | 194 | — | 260 |
| Flat Rating | — | ISA + 49 | ISA + 55 |
| Dimensions | |||
| Length (ft) | 29.9 | 35.3 | 29.7 |
| Wingspan (ft) | 37.9 | 42.1 | 43.2 |
| Cabin Width (ft) | 3.5 | 4 | 4.1 |
| Cabin Height (ft) | 4.2 | 4.1 | 4 |
| Cabin Length (ft) | 12.6 | 13.4 | 12.3 |
| Overall Height (ft) | 9.8 | — | 11.3 |
| Cabin Volume (cu. ft) | 150 | 123 | 165 |
| Baggage Volume Int. (cu. ft) | 46 | — | 20 |