Beechcraft Baron G58 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Piper M600 Sls
The Beechcraft Baron G58 is a piston-powered twin in the light aircraft category, typically suited to shorter regional trips. Its real-world range is roughly in the 1,000–1,300 nautical mile class depending on payload and reserves, and it generally carries about 4–5 passengers in addition to the pilot, with six seats installed but limited by weight for full occupancy with fuel. The Piper M600 SLS is a single‑engine turboprop in the personal/business category. It offers a longer typical range than the Baron, roughly around 1,200–1,500 nautical miles, and usually seats 4–5 passengers plus a pilot (six seats total), again with load tradeoffs. The Pilatus PC‑12 NGX is a larger, utility‑oriented single‑engine turboprop, commonly used for executive and special-mission work. It provides about 1,500–1,800 nautical miles of range and usually carries 6–8 passengers plus one or two pilots depending on configuration. The Piaggio Avanti EVO is a twin‑engine turboprop in the high‑performance business aircraft category. It typically offers around 1,400–1,700 nautical miles of range and seats about 6–7 passengers plus one or two pilots, emphasizing speed and cabin comfort.
| Spec | Beechcraft Baron G58 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.72 | — | $ 2.78 | $ 2.19 |
| Total Seats | 6 | 8 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Piaggio | Pilatus | Piper |
| Aircraft Name | Baron G58 | Avanti EVO | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1480 | 1530 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.29 | — | $ 0.46 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 1450 | 3775 | — | 2200 |
| Standard Cabin Seats | 4 | 6 | 6 | 4 |
| Direct Operating Cost | $ 347 | — | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 202 | 400 | 290 | 274 |
| Base Aircraft Price (USD) | $1,495,000 | $ 7,695,000 | $5,350,000 | $3,081,400 |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 7 | 9 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 8 | 8 | 5 |
| Standard Cabin Seats | 4 | 6 | 6 | 4 |
| Lavatory | — | No | Optional | No |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 7 | 9 | — |
| Cabin Pressure (psi) | — | 9 | 5.8 | 5.6 |
| Galley / Refreshment | — | No | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 24000 | 13100 | 12600 |
| Max Cabin Altitude (ft) | — | 6600 | — | 8644 |
| Cargo Door | — | — | Yes | — |
| Lavatory Location | — | — | FWD | — |
| Galley Location | — | — | — | MID |
| Engine | ||||
| FADEC | No | Yes | Yes | No |
| Model | IO-550-C | PT6A–66B | PT6E-67XP | PT6A-42A |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 1700 | 3600 | 5000 | 3600 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 300 | 850 | 1200 | 600 |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 194 | — | — | 260 |
| Flat Rating | — | ISA + 28 | ISA + 35 | ISA + 55 |
| Fuel Burn (gph) | — | 100 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 29.9 | 47.3 | 47.25 | 29.7 |
| Wingspan (ft) | 37.9 | 47.1 | 53.33 | 43.2 |
| Cabin Width (ft) | 3.5 | 6.1 | 5 | 4.1 |
| Cabin Height (ft) | 4.2 | 5.8 | 4.9 | 4 |
| Cabin Length (ft) | 12.6 | 14.9 | 16.9 | 12.3 |
| Overall Height (ft) | 9.8 | 13.1 | 14 | 11.3 |
| Cabin Volume (cu. ft) | 150 | — | — | 165 |
| Baggage Volume Int. (cu. ft) | 46 | 35.2 | 40 | 20 |
| Cabin Width - Floor (ft) | — | 3.5 | 4.25 | — |