Beechcraft King Air 360er vs Daher Tbm 960 vs Piaggio Avanti Evo vs Piper M600 Sls
In category, the Beechcraft King Air 360ER is a twin‑engine turboprop positioned as a pressurized business/utility aircraft with strong short‑field and redundancy advantages. The Daher TBM 960 and Piper M600 SLS are single‑engine turboprops aimed at owner‑operators, typically optimized for speed, simplicity, and lower operating complexity than twins. The Piaggio Avanti EVO is a twin‑turboprop business aircraft known for high cruise speed and a cabin feel closer to light jets. On range, the King Air 360ER generally offers the longest legs in this group, with the Avanti EVO and TBM 960 typically in a similar long‑range tier behind it, while the M600 SLS is usually shorter‑range than the others. On passenger capacity, the King Air 360ER commonly carries the most, often configured around 6–9 passengers depending on layout. The Avanti EVO is usually configured for about 6–7 passengers. The TBM 960 and M600 SLS are typically 4–6 passenger aircraft, with practical comfort favoring fewer seats on longer trips.
| Spec | Beechcraft King Air 360ER | Daher TBM 960 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 2.25 | — | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Piaggio | Piper |
| Aircraft Name | KingAir 350ER | TBM 960 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 1730 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.55 | $ 0.56 | — | $ 0.55 |
| Max Cabin Seats | 9 | — | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6585 | 2908 | 3775 | 2200 |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| Direct Operating Cost | $ 1,324 | $ 744 | — | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 303 | 330 | 400 | 274 |
| Base Aircraft Price (USD) | $8,750,000 | $4,450,000 | $ 7,695,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | No | No | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | Optional | — | — | — |
| Total Seats | 10 | 6 | 8 | 5 |
| Galley Location | FWD | MID | — | MID |
| Max Cabin Seats | 9 | — | 7 | — |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 6.5 | 6.2 | 9 | 5.6 |
| Galley / Refreshment | Refreshment Center | — | No | Refreshment Centre |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | — | 14390 | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PT6A-60A | TBM 960 | PT6A–66B | PT6A-42A |
| TBO (hrs) | 3600 | 3500 | 3600 | 3600 |
| Horsepower | 1050 | 850 | 850 | 600 |
| Flat Rating | ISA + 10 | ISA + 49 | ISA + 28 | ISA + 55 |
| No. of Engines | 1 | — | 2 | 1 |
| Fuel Capacity (gal) | 775 | — | — | 260 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 46.7 | 35.3 | 47.3 | 29.7 |
| Wingspan (ft) | 57.9 | 42.1 | 47.1 | 43.2 |
| Cabin Width (ft) | 4.5 | 4 | 6.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.1 | 5.8 | 4 |
| Cabin Length (ft) | 19.5 | 13.4 | 14.9 | 12.3 |
| Overall Height (ft) | 14.4 | — | 13.1 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | — | 35.2 | 20 |
| Cabin Volume (cu. ft) | — | 123 | — | 165 |