Beechcraft Baron G58 vs Cessna Caravan vs Daher Tbm 960 vs Piper M600 Sls
The Beechcraft Baron G58 is a piston-powered, twin‑engine light aircraft typically used for short to medium trips. It generally carries 4–6 people and offers a useful range in the mid‑1,000‑mile class depending on load and reserves. The Cessna Caravan is a single‑engine turboprop utility aircraft optimized for hauling people or cargo; it commonly seats 9–14 passengers in commuter configurations and trades speed for versatility, with typical ranges around roughly 900–1,200 miles. The Daher TBM 960 is a high‑performance single‑engine turboprop in the personal/business category, usually seating about 4–6 with a notably longer, faster cross‑country capability, often around roughly 1,400–1,700 miles. The Piper M600 SLS is also a single‑engine turboprop personal aircraft, generally seating 4–6 and offering solid cross‑country range, commonly around roughly 1,200–1,500 miles. In broad terms, the Caravan leads on passenger capacity and utility, while the TBM 960 emphasizes speed and longer legs; the M600 SLS is a strong middle ground, and the Baron G58 is the piston twin option for smaller groups.
| Spec | Beechcraft Baron G58 | Cessna Caravan | Daher TBM 960 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | $ 3.07 | $ 2.25 | $ 2.19 |
| Total Seats | 6 | 10 | 6 | 6 |
| Flight Rules | IFR | VFR | IFR | IFR |
| Manufacturer | Beechcraft | Cessna | Daher TBM | Piper |
| Aircraft Name | Baron G58 | Caravan | TBM 960 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 1070 | 1730 | 1406 |
| DOC / nm / Seat | $ 0.29 | $ 0.38 | $ 0.56 | $ 0.55 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1450 | 3305 | 2908 | 2200 |
| Standard Cabin Seats | 4 | 8 | 4 | 4 |
| Direct Operating Cost | $ 347 | $ 571 | $ 744 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 | Garmin G3000 |
| Max Cruise Speed (ktas) | 202 | 186 | 330 | 274 |
| Base Aircraft Price (USD) | $1,495,000 | $2,355,000 | $4,450,000 | $3,081,400 |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 9 | — | — |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 10 | 6 | 5 |
| Standard Cabin Seats | 4 | 8 | 4 | 4 |
| Lavatory | — | No | No | No |
| Min Crew | — | 1 | 1 | 1 |
| Cargo Door | — | Yes | — | — |
| Max Cabin Seats | — | 9 | — | — |
| Cabin Pressure (psi) | — | Un-Pressurized | 6.2 | 5.6 |
| Galley / Refreshment | — | No | — | Refreshment Centre |
| Galley Location | — | — | MID | MID |
| SL Cabin Altitude (ft) | — | — | 14390 | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | No | Yes | Yes | No |
| Model | IO-550-C | PT6A-114A | TBM 960 | PT6A-42A |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 1700 | 3600 | 3500 | 3600 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 300 | 675 | 850 | 600 |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 2 | 1 | — | 1 |
| Fuel Capacity (gal) | 194 | — | — | 260 |
| Flat Rating | — | ISA + 31 | ISA + 49 | ISA + 55 |
| Dimensions | ||||
| Length (ft) | 29.9 | 37.6 | 35.3 | 29.7 |
| Wingspan (ft) | 37.9 | 52.1 | 42.1 | 43.2 |
| Cabin Width (ft) | 3.5 | 5.4 | 4 | 4.1 |
| Cabin Height (ft) | 4.2 | 4.5 | 4.1 | 4 |
| Cabin Length (ft) | 12.6 | 12.8 | 13.4 | 12.3 |
| Overall Height (ft) | 9.8 | 15 | — | 11.3 |
| Cabin Volume (cu. ft) | 150 | — | 123 | 165 |
| Baggage Volume Int. (cu. ft) | 46 | 32 | — | 20 |