Daher Tbm 910 vs Piaggio Avanti Evo vs Piper M350
The Daher TBM 910 is a high-performance single‑engine turboprop, positioned as a fast, owner‑flown cross‑country aircraft. It typically offers a practical range around 1,400–1,700 nautical miles depending on payload and reserves, and commonly seats a pilot plus up to five passengers (six seats total in many configurations). The Piaggio Avanti EVO is a twin‑engine turboprop in a small business-aircraft class, optimized for speed and cabin comfort with strong cruise efficiency. Its typical range is broadly similar or slightly higher than the TBM in many missions, often around 1,400–1,800 nautical miles, and it generally accommodates one or two pilots plus six to seven passengers (usually seven to eight seats total, depending on layout). The Piper M350 is a pressurized single‑engine piston aircraft, aimed at owner‑pilots wanting lower operating costs than turboprops. Its range is usually shorter, roughly 1,000–1,300 nautical miles, and seating is commonly a pilot plus up to five passengers (six seats total).
| Spec | Daher TBM 910 | Piaggio Avanti EVO | Piper M350 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 1.34 |
| Min Crew | 1 | 1 | — |
| Total Seats | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | VFR |
| Manufacturer | Daher TBM | Piaggio | Piper |
| Aircraft Name | TBM 910 | Avanti EVO | M350 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 1343 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.22 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 3775 | 1308 |
| Standard Cabin Seats | 4 | 6 | 4 |
| Direct Operating Cost | $ 744 | — | $ 285 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line 21 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 330 | 400 | 213 |
| Base Aircraft Price (USD) | $4,250,000 | $ 7,695,000 | $1,195,000 |
| Max Cabin Seats | — | 7 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | — |
| Min Crew | 1 | 1 | — |
| Total Seats | 6 | 8 | 6 |
| Galley Location | MID | — | — |
| Cabin Pressure (psi) | 6.2 | 9 | 5.6 |
| Galley / Refreshment | Refreshment Centre | No | — |
| Standard Cabin Seats | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 14390 | 24000 | — |
| Max Cabin Seats | — | 7 | — |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | PT6A-66D | PT6A–66B | TIO-540-AE2A |
| TBO (hrs) | 3500 | 3600 | 2000 |
| Horsepower | 850 | 850 | 350 |
| Flat Rating | ISA + 49 | ISA + 28 | — |
| No. of Engines | 1 | 2 | 1 |
| Fuel Burn (gph) | 37 | 100 | — |
| Fuel Capacity (gal) | 291 | — | 120 |
| Fuel Type | — | — | AvGas |
| TBO (yrs) | — | — | 12 |
| Fuel Delivery | — | — | Fuel Injected |
| Dimensions | |||
| Length (ft) | 35.3 | 47.3 | 29 |
| Wingspan (ft) | 42.1 | 47.1 | 43 |
| 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 |
| Overall Height (ft) | 14.3 | 13.1 | 11.4 |
| Cabin Volume (cu. ft) | 123 | — | 165 |
| Baggage Volume Int. (cu. ft) | 30 | 35.2 | 20 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 13 |