Daher Tbm 960 vs Piaggio Avanti Evo vs Piper M600 Sls
All three are single‑pilot‑friendly turboprops, but they target different missions. The Daher TBM 960 is best described as a high‑performance, pressurized single‑engine personal/business aircraft, optimized for speed and efficient point‑to‑point travel. The Piper M600 SLS sits in the same general category—pressurized single‑engine turboprop—but emphasizes simplified operations and avionics/automation for owner‑pilots, typically trading a bit of outright performance for approachability and cost consciousness. The Piaggio Avanti EVO is a distinct step into the light business aircraft class with a pressurized twin‑turboprop design, geared more toward corporate transport and cabin comfort. On range, the TBM 960 generally offers the longest reach among these, suitable for longer nonstop legs; the M600 SLS is usually somewhat shorter‑range but still solid for regional missions; the Avanti EVO is typically in the same broad bracket as the singles, often comparable to the M600 and depending on payload and reserves. For passenger capacity, the TBM 960 and M600 SLS are commonly arranged for about five to six passengers plus a pilot, while the Avanti EVO typically accommodates more—often six to seven passengers—thanks to its larger cabin.
| Spec | Daher TBM 960 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 2.19 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Piaggio | Piper |
| Aircraft Name | TBM 960 | Avanti EVO | M600 |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | 3775 | 2200 |
| Standard Cabin Seats | 4 | 6 | 4 |
| Direct Operating Cost | $ 744 | — | $ 603 |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 400 | 274 |
| Base Aircraft Price (USD) | $4,450,000 | $ 7,695,000 | $3,081,400 |
| Max Cabin Seats | — | 7 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | No |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 5 |
| Galley Location | MID | — | MID |
| Cabin Pressure (psi) | 6.2 | 9 | 5.6 |
| Standard Cabin Seats | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 14390 | 24000 | 12600 |
| Max Cabin Seats | — | 7 | — |
| Galley / Refreshment | — | No | Refreshment Centre |
| Max Cabin Altitude (ft) | — | 6600 | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | TBM 960 | PT6A–66B | PT6A-42A |
| TBO (hrs) | 3500 | 3600 | 3600 |
| Horsepower | 850 | 850 | 600 |
| Flat Rating | ISA + 49 | ISA + 28 | ISA + 55 |
| No. of Engines | — | 2 | 1 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 35.3 | 47.3 | 29.7 |
| Wingspan (ft) | 42.1 | 47.1 | 43.2 |
| Cabin Width (ft) | 4 | 6.1 | 4.1 |
| Cabin Height (ft) | 4.1 | 5.8 | 4 |
| Cabin Length (ft) | 13.4 | 14.9 | 12.3 |
| Cabin Volume (cu. ft) | 123 | — | 165 |
| Overall Height (ft) | — | 13.1 | 11.3 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 20 |