Daher Tbm 910 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
By category, the Daher TBM 910 and Pilatus PC-12 NGX are single‑engine turboprop aircraft, the Piaggio Avanti EVO is a twin‑engine turboprop with a high‑speed, cabin‑forward design, and the Pilatus PC-24 is a light twin‑engine business jet. On range, the TBM 910 and PC-12 NGX are broadly similar long‑leg turboprops, typically suited to roughly 1,500–1,800 nautical‑mile missions depending on payload and reserves, while the Avanti EVO is also in the long‑range turboprop class, often around the 1,700–2,000 nautical‑mile neighborhood. The PC-24 generally offers comparable or somewhat greater range than many turboprops when flown with typical jet payloads, commonly around 2,000 nautical miles. On passenger capacity, the TBM 910 is usually configured for about 4–6 passengers plus a pilot, emphasizing speed and efficiency for smaller groups. The Avanti EVO and PC-12 NGX more commonly seat about 6–8 passengers in executive layouts, with the PC-12 also offering flexible high‑capacity seating in commuter/utility configurations. The PC-24 typically carries about 6–8 passengers in business configuration, with an emphasis on jet performance and cabin access.
| Spec | Daher TBM 910 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Daher TBM | Piaggio | Pilatus | Pilatus |
| Aircraft Name | TBM 910 | Avanti EVO | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.46 | $ 0.62 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 2908 | 3775 | — | 6680 |
| Standard Cabin Seats | 4 | 6 | 6 | 6 |
| Direct Operating Cost | $ 744 | — | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 330 | 400 | 290 | 440 |
| Base Aircraft Price (USD) | $4,250,000 | $ 7,695,000 | $5,350,000 | $11,800,000 |
| Max Cabin Seats | — | 7 | 9 | 10 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | No | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 8 | 6 |
| Galley Location | MID | — | — | FWD |
| Cabin Pressure (psi) | 6.2 | 9 | 5.8 | 9.3 |
| Galley / Refreshment | Refreshment Centre | No | No | Optional Refreshment Center |
| Standard Cabin Seats | 4 | 6 | 6 | 6 |
| SL Cabin Altitude (ft) | 14390 | 24000 | 13100 | 23500 |
| Max Cabin Seats | — | 7 | 9 | 10 |
| Max Cabin Altitude (ft) | — | 6600 | — | — |
| Cargo Door | — | — | Yes | Yes |
| Lavatory Location | — | — | FWD | FWD |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-66D | PT6A–66B | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 3500 | 3600 | 5000 | 5000 |
| Horsepower | 850 | 850 | 1200 | — |
| Flat Rating | ISA + 49 | ISA + 28 | ISA + 35 | ISA + 23 |
| No. of Engines | 1 | 2 | 1 | 2 |
| Fuel Burn (gph) | 37 | 100 | — | — |
| Fuel Capacity (gal) | 291 | — | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Length (ft) | 35.3 | 47.3 | 47.25 | 52.2 |
| Wingspan (ft) | 42.1 | 47.1 | 53.33 | 55.8 |
| Cabin Width (ft) | 4 | 6.1 | 5 | 5.6 |
| Cabin Height (ft) | 4.1 | 5.8 | 4.9 | 5.1 |
| Cabin Length (ft) | 13.4 | 14.9 | 16.9 | 23 |
| Overall Height (ft) | 14.3 | 13.1 | 14 | 17.4 |
| Cabin Volume (cu. ft) | 123 | — | — | — |
| Baggage Volume Int. (cu. ft) | 30 | 35.2 | 40 | 90 |
| Cabin Width - Floor (ft) | — | 3.5 | 4.25 | 3.8 |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | — | 17 |