Daher Tbm 960 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Piper Seminole
The Daher TBM 960, Piaggio Avanti EVO, and Pilatus PC-12 NGX are pressurized, single‑pilot capable turboprop aircraft aimed at fast business and utility travel, while the Piper Arrow is a smaller, unpressurized, retractable‑gear piston single typically used for personal travel and training. In range terms, the PC-12 NGX generally offers the longest practical legs thanks to its efficient cruise and large fuel capacity, often used for missions in the roughly 1,500–1,800 nm class. The TBM 960 is also a long‑range, high‑speed single‑engine turboprop, commonly flown around the 1,400–1,700 nm class depending on power settings and payload. The Avanti EVO, a twin‑turboprop optimized for speed, typically delivers solid but somewhat shorter range than the longest‑leg PC‑12/TBM missions, often around the 1,200–1,500 nm class. For passenger capacity, the PC‑12 is the most flexible, commonly seating 6–9, the Avanti EVO typically carries about 6–7, and the TBM 960 usually seats about 4–6. The Piper Arrow is a four‑seat aircraft with a much shorter range, commonly in the roughly 500–900 nm class depending on variant and reserves.
| Spec | Daher TBM 960 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Piper Arrow |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 2.78 | $ 1.36 |
| Min Crew | 1 | 1 | 1 | — |
| Total Seats | 6 | 8 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Piaggio | Pilatus | Piper |
| Aircraft Name | TBM 960 | Avanti EVO | PC-12 NGX | Arrow |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 1803 | 700 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.46 | $ 0.23 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2908 | 3775 | — | 1191 |
| Standard Cabin Seats | 4 | 6 | 6 | 4 |
| Direct Operating Cost | $ 744 | — | $ 793 | $ 221 |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 330 | 400 | 290 | 162 |
| Base Aircraft Price (USD) | $4,450,000 | $ 7,695,000 | $5,350,000 | $765,000 |
| 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 | — |
| 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 | O-360-AIH6 |
| TBO (hrs) | 3500 | 3600 | 5000 | 2000 |
| Horsepower | 850 | 850 | 1200 | 180 |
| Flat Rating | ISA + 49 | ISA + 28 | ISA + 35 | — |
| No. of Engines | — | 2 | 1 | 2 |
| Fuel Burn (gph) | — | 100 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Fuel Type | — | — | — | AvGas |
| TBO (yrs) | — | — | — | 12 |
| Fuel Delivery | — | — | — | Carbureted |
| Fuel Capacity (gal) | — | — | — | 108 |
| Dimensions | ||||
| Length (ft) | 35.3 | 47.3 | 47.25 | 27.6 |
| Wingspan (ft) | 42.1 | 47.1 | 53.33 | 38.6 |
| Cabin Width (ft) | 4 | 6.1 | 5 | — |
| Cabin Height (ft) | 4.1 | 5.8 | 4.9 | — |
| Cabin Length (ft) | 13.4 | 14.9 | 16.9 | — |
| Cabin Volume (cu. ft) | 123 | — | — | — |
| Overall Height (ft) | — | 13.1 | 14 | 8.5 |
| Cabin Width - Floor (ft) | — | 3.5 | 4.25 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 40 | — |