Daher Tbm 960 vs Piaggio Avanti Evo vs Sikorsky S 92
The Daher TBM 960 and Piaggio Avanti EVO are pressurized, single‑pilot-capable turboprop airplanes aimed at fast personal or small business travel, while the Sikorsky S‑92 is a large, twin‑engine helicopter typically used for offshore energy, SAR, and VIP/utility transport. In range, the TBM 960 is generally the longest-legged of the two airplanes, commonly quoted around 1,700 nautical miles depending on payload and reserves, whereas the Avanti EVO is typically in the roughly 1,400–1,500 nautical mile class. The S‑92’s range is substantially shorter than either fixed‑wing option, commonly around 500–600 nautical miles (mission equipment, reserves, and seating layout can change this). Passenger capacity also differs: a TBM 960 is usually configured for about 4–6 passengers plus a pilot, the Avanti EVO commonly seats about 6–8 passengers plus pilots, and an S‑92 can carry far more—often around 12–19 passengers depending on configuration—trading cruise speed and range for vertical lift, hover, and point-to-point access without runways.
| Spec | Daher TBM 960 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 6 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Piaggio | Sikorsky |
| Aircraft Name | TBM 960 | Avanti EVO | S-92 |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 439 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.94 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 3775 | 7417 |
| Standard Cabin Seats | 4 | 6 | 19 |
| Direct Operating Cost | $ 744 | — | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 330 | 400 | 155 |
| Base Aircraft Price (USD) | $4,450,000 | $ 7,695,000 | $30,650,000 |
| Max Cabin Seats | — | 7 | 19 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | — |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 6 | 8 | 21 |
| Galley Location | MID | — | — |
| Cabin Pressure (psi) | 6.2 | 9 | — |
| Standard Cabin Seats | 4 | 6 | 19 |
| SL Cabin Altitude (ft) | 14390 | 24000 | — |
| Max Cabin Seats | — | 7 | 19 |
| Galley / Refreshment | — | No | — |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | TBM 960 | PT6A–66B | CT7-8A |
| TBO (hrs) | 3500 | 3600 | 4000 |
| Horsepower | 850 | 850 | 2520 |
| Flat Rating | ISA + 49 | ISA + 28 | — |
| No. of Engines | — | 2 | 1 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Type | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 35.3 | 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 | — | 775 |
| Overall Height (ft) | — | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |