Beechcraft Baron G58 vs Beechcraft King Air 260 vs Piper M600 Sls vs Piper Seneca
The Beechcraft Baron G58 and Piper Seneca are piston twins typically used for personal and light business travel. They generally seat about five to six people, with real-world ranges commonly in the roughly 800–1,300 nm neighborhood depending on load and reserves; the Baron is often viewed as the simpler, higher-performance personal twin, while the Seneca is frequently positioned as a more economical, training-friendly cabin-class twin. The Piper M600 SLS is a single-engine turboprop, usually configured for five to six passengers plus a pilot. It steps up in speed and altitude capability versus piston twins, and commonly offers about 1,200–1,500 nm of range, making it a strong owner-flown business aircraft. The Beechcraft King Air 260 is a twin-engine turboprop in a higher class altogether, aimed at corporate and special-mission use. It typically carries six to nine passengers in executive layouts and can stretch to roughly 1,400–1,700 nm range depending on configuration. In short, piston twins prioritize cost and simplicity, the M600 SLS offers turboprop performance with single-engine ownership, and the King Air 260 delivers the most capacity and operational flexibility.
| Spec | Beechcraft Baron G58 | Beechcraft King Air 260 | Piper M600 SLS | Piper Seneca |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | $ 4.30 | $ 2.19 | $ 1.69 |
| Total Seats | 6 | 8 | 6 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Beechcraft | Piper | Piper |
| Aircraft Name | Baron G58 | KingAir 250 | M600 | Seneca |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 1420 | 1406 | 828 |
| DOC / nm / Seat | $ 0.29 | $ 0.72 | $ 0.55 | $ 0.28 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 1450 | 3760 | 2200 | 1331 |
| Standard Cabin Seats | 4 | 6 | 4 | 4 |
| Direct Operating Cost | $ 347 | $ 1,333 | $ 603 | $ 337 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 202 | 310 | 274 | 200 |
| Base Aircraft Price (USD) | $1,495,000 | $6,450,000 | $3,081,400 | $1,095,000 |
| Min Crew | — | 1 | 1 | — |
| Max Cabin Seats | — | 8 | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 8 | 5 | 6 |
| Standard Cabin Seats | 4 | 6 | 4 | 4 |
| Lavatory | — | 1 Flushing | No | — |
| Min Crew | — | 1 | 1 | — |
| Max Cabin Seats | — | 8 | — | — |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 6.5 | 5.6 | — |
| Galley / Refreshment | — | No | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | 15293 | 12600 | — |
| Galley Location | — | — | MID | — |
| Max Cabin Altitude (ft) | — | — | 8644 | — |
| Engine | ||||
| FADEC | No | Yes | No | No |
| Model | IO-550-C | PT6A-52 | PT6A-42A | TSIO-360-RB |
| Fuel Type | AvGas | — | — | AvGas |
| TBO (hrs) | 1700 | 3600 | 3600 | 1800 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 300 | 850 | 600 | 220 |
| Fuel Delivery | Fuel Injected | — | — | Fuel Injected |
| No. of Engines | 2 | 1 | 1 | 2 |
| Fuel Capacity (gal) | 194 | 544 | 260 | 122 |
| Flat Rating | — | ISA + 37 | ISA + 55 | — |
| Dimensions | ||||
| Length (ft) | 29.9 | 43.8 | 29.7 | 28.6 |
| Wingspan (ft) | 37.9 | 57.9 | 43.2 | 39 |
| Cabin Width (ft) | 3.5 | 4.5 | 4.1 | — |
| Cabin Height (ft) | 4.2 | 4.8 | 4 | — |
| Cabin Length (ft) | 12.6 | 16.7 | 12.3 | — |
| Overall Height (ft) | 9.8 | 14.8 | 11.3 | 10 |
| Cabin Volume (cu. ft) | 150 | — | 165 | — |
| Baggage Volume Int. (cu. ft) | 46 | 55 | 20 | — |
| Cabin Width - Floor (ft) | — | 4.1 | — | — |
| Cabin Length - Seating (ft) | — | 16.7 | — | — |