Daher Tbm 960 vs Leonardo Aw189 vs Piaggio Avanti Evo vs Sikorsky S 92
The Daher TBM 960 and Piaggio Avanti EVO are fixed‑wing turboprop airplanes, while the Leonardo AW189 and Sikorsky S‑92 are twin‑engine medium helicopters. In category terms, the TBM 960 is a high‑performance single‑engine business/utility aircraft optimized for speed and efficiency; the Avanti EVO is a twin‑engine executive turboprop aimed at fast, comfortable regional travel. The AW189 is typically used for offshore, EMS, and SAR-type missions with strong vertical-lift flexibility, and the S‑92 is a larger heavy‑use offshore/utility helicopter designed for higher payload and longer overwater legs. For range, the fixed‑wing aircraft generally travel farther and faster: the TBM 960 offers roughly 1,700+ nautical miles class range, and the Avanti EVO is in a similar long‑range bracket (about 1,500+ nautical miles). Helicopter ranges are usually shorter: the AW189 is commonly around 450–500 nautical miles, while the S‑92 is often around 500+ nautical miles depending on configuration and reserves. Passenger capacity also differs: TBM 960 typically carries up to about 6 passengers, Avanti EVO about 7–9, AW189 roughly 16–19, and S‑92 about 19.
| Spec | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 15.57 | — | $ 19.79 |
| Min Crew | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 21 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Leonardo | Piaggio | Sikorsky |
| Aircraft Name | TBM 960 | AW189 | Avanti EVO | S-92 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 651 | 1530 | 439 |
| DOC / nm / Seat | $ 0.56 | $ 0.74 | — | $ 0.94 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | — | 3775 | 7417 |
| Standard Cabin Seats | 4 | 19 | 6 | 19 |
| Direct Operating Cost | $ 744 | $ 2,413 | — | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 330 | 155 | 400 | 155 |
| Base Aircraft Price (USD) | $4,450,000 | $2,413,000 | $ 7,695,000 | $30,650,000 |
| Max Cabin Seats | — | 19 | 7 | 19 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | — | No | — |
| Min Crew | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 21 | 8 | 21 |
| Galley Location | MID | — | — | — |
| Cabin Pressure (psi) | 6.2 | — | 9 | — |
| Standard Cabin Seats | 4 | 19 | 6 | 19 |
| SL Cabin Altitude (ft) | 14390 | — | 24000 | — |
| Max Cabin Seats | — | 19 | 7 | 19 |
| Galley / Refreshment | — | — | No | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | TBM 960 | CT7-2E1 | PT6A–66B | CT7-8A |
| TBO (hrs) | 3500 | 4000 | 3600 | 4000 |
| Horsepower | 850 | 1983 | 850 | 2520 |
| Flat Rating | ISA + 49 | — | ISA + 28 | — |
| Fuel Type | — | JetFuel | — | JetFuel |
| No. of Engines | — | 2 | 2 | 1 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Capacity (gal) | — | — | — | 760 |
| 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 | — | 775 |
| Overall Height (ft) | — | 16.6 | 13.1 | 17.8 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | 140 |
| Cabin Width - Floor (ft) | — | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | — |