Daher Tbm 960 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Piper M350
By category, the Daher TBM 960 and Pilatus PC-12 NGX are single‑engine turboprops, with the TBM aimed at fast owner‑pilot travel and the PC‑12 positioned as a larger, utility‑oriented executive turboprop. The Piaggio Avanti EVO is a twin‑turboprop business aircraft, typically operated more like a light jet alternative, while the Piper M350 is a pressurized single‑engine piston aircraft in the high‑performance personal transport class. For range, the TBM 960 and PC‑12 NGX generally offer the longest turboprop legs in this group at roughly 1,600–1,800 nautical miles depending on payload and reserves. The Avanti EVO is also a long‑range option, commonly around 1,500–1,700 nautical miles, varying with speed and load. The M350 typically trails the turboprops, commonly around 1,000–1,300 nautical miles depending on power settings and conditions. Passenger capacity follows size and mission: the TBM 960 usually seats about 4–6 passengers, the Avanti EVO typically 6–8, the PC‑12 NGX often 6–9 (and can be configured higher for commuter/utility use), and the M350 generally carries about 4–5 passengers plus the pilot.
| Spec | Daher TBM 960 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Piper M350 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 2.78 | $ 1.34 |
| Min Crew | 1 | 1 | 1 | — |
| Total Seats | 6 | 8 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | VFR |
| Manufacturer | Daher TBM | Piaggio | Pilatus | Piper |
| Aircraft Name | TBM 960 | Avanti EVO | PC-12 NGX | M350 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 1803 | 1343 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.46 | $ 0.22 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2908 | 3775 | — | 1308 |
| Standard Cabin Seats | 4 | 6 | 6 | 4 |
| Direct Operating Cost | $ 744 | — | $ 793 | $ 285 |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 330 | 400 | 290 | 213 |
| Base Aircraft Price (USD) | $4,450,000 | $ 7,695,000 | $5,350,000 | $1,195,000 |
| Max Cabin Seats | — | 7 | 9 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | No | Optional | — |
| Min Crew | 1 | 1 | 1 | — |
| Total Seats | 6 | 8 | 8 | 6 |
| Galley Location | MID | — | — | — |
| Cabin Pressure (psi) | 6.2 | 9 | 5.8 | 5.6 |
| Standard Cabin Seats | 4 | 6 | 6 | 4 |
| SL Cabin Altitude (ft) | 14390 | 24000 | 13100 | — |
| Max Cabin Seats | — | 7 | 9 | — |
| Galley / Refreshment | — | No | No | — |
| Max Cabin Altitude (ft) | — | 6600 | — | — |
| Cargo Door | — | — | Yes | — |
| Lavatory Location | — | — | FWD | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | TBM 960 | PT6A–66B | PT6E-67XP | TIO-540-AE2A |
| TBO (hrs) | 3500 | 3600 | 5000 | 2000 |
| Horsepower | 850 | 850 | 1200 | 350 |
| Flat Rating | ISA + 49 | ISA + 28 | ISA + 35 | — |
| No. of Engines | — | 2 | 1 | 1 |
| Fuel Burn (gph) | — | 100 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Fuel Type | — | — | — | AvGas |
| TBO (yrs) | — | — | — | 12 |
| Fuel Delivery | — | — | — | Fuel Injected |
| Fuel Capacity (gal) | — | — | — | 120 |
| Dimensions | ||||
| Length (ft) | 35.3 | 47.3 | 47.25 | 29 |
| Wingspan (ft) | 42.1 | 47.1 | 53.33 | 43 |
| Cabin Width (ft) | 4 | 6.1 | 5 | 4.1 |
| Cabin Height (ft) | 4.1 | 5.8 | 4.9 | 4 |
| Cabin Length (ft) | 13.4 | 14.9 | 16.9 | 12.3 |
| Cabin Volume (cu. ft) | 123 | — | — | 165 |
| Overall Height (ft) | — | 13.1 | 14 | 11.4 |
| Cabin Width - Floor (ft) | — | 3.5 | 4.25 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 40 | 20 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 13 |