Daher Tbm 910 vs Daher Tbm 960 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx
The Daher TBM 910 and TBM 960 are high-performance single‑engine turboprops in the owner‑pilot and personal/business travel category. Both typically carry a pilot plus up to five or six passengers depending on seating and loading, and they offer broadly similar range suited to regional and some transcontinental legs, with the TBM 960 generally delivering slightly more usable efficiency and refinement in real-world operations. The Pilatus PC‑12 NGX is a larger, utility‑oriented single‑engine turboprop positioned for corporate, charter, and special-mission use. It usually accommodates more people than the TBMs, commonly up to eight or nine passengers in executive layouts, and it is known for long-range capability and flexibility with baggage and cabin volume. The Piaggio Avanti EVO is a distinctive twin‑engine turboprop aimed at business aviation, offering jet‑like cruise speeds with a quiet, stand‑up style cabin relative to its class. Passenger capacity is typically six to eight, and range is competitive for business missions, generally comparable to or slightly less than the longest‑leg PC‑12 configurations depending on payload.
| Spec | Daher TBM 910 | Daher TBM 960 | Piaggio Avanti EVO | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.25 | — | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Daher TBM | Piaggio | Pilatus |
| Aircraft Name | TBM 910 | TBM 960 | Avanti EVO | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1730 | 1530 | 1803 |
| DOC / nm / Seat | $ 0.56 | $ 0.56 | — | $ 0.46 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | 2908 | 3775 | — |
| Standard Cabin Seats | 4 | 4 | 6 | 6 |
| Direct Operating Cost | $ 744 | $ 744 | — | $ 793 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Rockwell Collins Pro Line 21 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 330 | 330 | 400 | 290 |
| Base Aircraft Price (USD) | $4,250,000 | $4,450,000 | $ 7,695,000 | $5,350,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Max Cabin Seats | — | — | 7 | 9 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | No | No | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 8 |
| Galley Location | MID | MID | — | — |
| Cabin Pressure (psi) | 6.2 | 6.2 | 9 | 5.8 |
| Galley / Refreshment | Refreshment Centre | — | No | No |
| Standard Cabin Seats | 4 | 4 | 6 | 6 |
| SL Cabin Altitude (ft) | 14390 | 14390 | 24000 | 13100 |
| Max Cabin Seats | — | — | 7 | 9 |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-66D | TBM 960 | PT6A–66B | PT6E-67XP |
| TBO (hrs) | 3500 | 3500 | 3600 | 5000 |
| Horsepower | 850 | 850 | 850 | 1200 |
| Flat Rating | ISA + 49 | ISA + 49 | ISA + 28 | ISA + 35 |
| No. of Engines | 1 | — | 2 | 1 |
| Fuel Burn (gph) | 37 | — | 100 | — |
| Fuel Capacity (gal) | 291 | — | — | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 35.3 | 35.3 | 47.3 | 47.25 |
| Wingspan (ft) | 42.1 | 42.1 | 47.1 | 53.33 |
| Cabin Width (ft) | 4 | 4 | 6.1 | 5 |
| Cabin Height (ft) | 4.1 | 4.1 | 5.8 | 4.9 |
| Cabin Length (ft) | 13.4 | 13.4 | 14.9 | 16.9 |
| Overall Height (ft) | 14.3 | — | 13.1 | 14 |
| Cabin Volume (cu. ft) | 123 | 123 | — | — |
| Baggage Volume Int. (cu. ft) | 30 | — | 35.2 | 40 |
| Cabin Width - Floor (ft) | — | — | 3.5 | 4.25 |