Daher Tbm 960 vs Leonardo Aw189 vs Piaggio Avanti Evo vs Robinson R66
The Daher TBM 960 is a high-performance single‑engine turboprop airplane aimed at fast point‑to‑point travel, typically carrying a pilot plus about 4–6 passengers, with long legs around roughly 1,000–1,500 nautical miles depending on payload and reserves. The Piaggio Avanti EVO is a twin‑turboprop airplane positioned as a faster, higher‑capacity executive aircraft, often seating 6–8 passengers (up to 9 in some layouts) and offering broadly similar long-range capability, commonly around 1,000–1,700 nautical miles. The Leonardo AW189 is a super‑medium twin‑engine helicopter designed for offshore, SAR, and utility/VIP missions; it carries far more people than the airplanes in utility layouts (commonly 12–16 passengers, higher in dense seating) but with shorter range, typically on the order of roughly 400–500 nautical miles depending on mission equipment and fuel reserves. The Robinson R66 is a light single‑engine turbine helicopter for personal, training, and light utility use, generally carrying 4 passengers plus a pilot, with shorter range than the AW189, often roughly 300 nautical miles.
| Spec | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 15.57 | — |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 21 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Leonardo | Piaggio |
| Aircraft Name | TBM 960 | AW189 | Avanti EVO |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 651 | 1530 |
| DOC / nm / Seat | $ 0.56 | $ 0.74 | — |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | — | 3775 |
| Standard Cabin Seats | 4 | 19 | 6 |
| Direct Operating Cost | $ 744 | $ 2,413 | — |
| Flight Deck (Base Spec) | Garmin G3000 | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 330 | 155 | 400 |
| Base Aircraft Price (USD) | $4,450,000 | $2,413,000 | $ 7,695,000 |
| Max Cabin Seats | — | 19 | 7 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | — | No |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 21 | 8 |
| Galley Location | MID | — | — |
| Cabin Pressure (psi) | 6.2 | — | 9 |
| Standard Cabin Seats | 4 | 19 | 6 |
| SL Cabin Altitude (ft) | 14390 | — | 24000 |
| Max Cabin Seats | — | 19 | 7 |
| Galley / Refreshment | — | — | No |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | TBM 960 | CT7-2E1 | PT6A–66B |
| TBO (hrs) | 3500 | 4000 | 3600 |
| Horsepower | 850 | 1983 | 850 |
| Flat Rating | ISA + 49 | — | ISA + 28 |
| Fuel Type | — | JetFuel | — |
| No. of Engines | — | 2 | 2 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 35.3 | 57.8 | 47.3 |
| Wingspan (ft) | 42.1 | — | 47.1 |
| Cabin Width (ft) | 4 | — | 6.1 |
| Cabin Height (ft) | 4.1 | — | 5.8 |
| Cabin Length (ft) | 13.4 | — | 14.9 |
| Cabin Volume (cu. ft) | 123 | 395 | — |
| Overall Height (ft) | — | 16.6 | 13.1 |
| Rotor Diameter (ft) | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |
| Cabin Width - Floor (ft) | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 |