Daher Tbm 910 vs Piper M350
The Daher TBM 910 and Piper M350 are both single‑engine turboprop aircraft aimed at owner‑operators, but they sit in slightly different niches. The TBM 910 is typically positioned as a higher‑performance, faster cross‑country turboprop, while the M350 emphasizes a more traditional, comfort‑oriented personal transport mission with a strong focus on cabin environment and workload management. In range, both are designed for serious traveling, yet the TBM 910 generally offers a longer usable cross‑country reach and is more often chosen for longer nonstop legs at higher cruise speeds. The M350’s range is competitive for regional and medium‑length trips, but it is commonly viewed as somewhat more range‑limited compared with the TBM 910’s typical mission profile. For passenger capacity, each is commonly operated with one pilot and up to about five passengers in typical seating configurations, although real‑world comfort and baggage needs often reduce practical occupancy for longer trips. Overall, the TBM 910 tends to favor speed and longer legs, while the M350 leans toward a refined personal‑transport experience.
| Spec | Daher TBM 910 | Piper M350 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.25 | $ 1.34 |
| Min Crew | 1 | — |
| Total Seats | 6 | 6 |
| Flight Rules | IFR | VFR |
| Manufacturer | Daher TBM | Piper |
| Aircraft Name | TBM 910 | M350 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1343 |
| DOC / nm / Seat | $ 0.56 | $ 0.22 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 1308 |
| Standard Cabin Seats | 4 | 4 |
| Direct Operating Cost | $ 744 | $ 285 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 330 | 213 |
| Base Aircraft Price (USD) | $4,250,000 | $1,195,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | — |
| Min Crew | 1 | — |
| Total Seats | 6 | 6 |
| Galley Location | MID | — |
| Cabin Pressure (psi) | 6.2 | 5.6 |
| Galley / Refreshment | Refreshment Centre | — |
| Standard Cabin Seats | 4 | 4 |
| SL Cabin Altitude (ft) | 14390 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | PT6A-66D | TIO-540-AE2A |
| TBO (hrs) | 3500 | 2000 |
| Horsepower | 850 | 350 |
| Flat Rating | ISA + 49 | — |
| No. of Engines | 1 | 1 |
| Fuel Burn (gph) | 37 | — |
| Fuel Capacity (gal) | 291 | 120 |
| Fuel Type | — | AvGas |
| TBO (yrs) | — | 12 |
| Fuel Delivery | — | Fuel Injected |
| Dimensions | ||
| Length (ft) | 35.3 | 29 |
| Wingspan (ft) | 42.1 | 43 |
| Cabin Width (ft) | 4 | 4.1 |
| Cabin Height (ft) | 4.1 | 4 |
| Cabin Length (ft) | 13.4 | 12.3 |
| Overall Height (ft) | 14.3 | 11.4 |
| Cabin Volume (cu. ft) | 123 | 165 |
| Baggage Volume Int. (cu. ft) | 30 | 20 |
| Baggage Volume Ext. (cu. ft) | — | 13 |