Daher Tbm 960 vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Sikorsky S 92
The Daher TBM 960 is a single‑engine turboprop in the high‑performance owner‑pilot category, typically carrying about 4 to 6 passengers in a pressurized cabin with range roughly in the 1,400–1,700 nautical mile class, optimized for efficient point‑to‑point regional trips. The Piaggio Avanti EVO is a twin‑turboprop business aircraft, generally seating around 6 to 7 passengers (often up to 8–9 in some layouts) with a similar-to-slightly-longer regional range of about 1,500–1,800 nautical miles, offering jet‑like cruise speeds with turboprop economics. The Dassault Falcon 8X is a long‑range, large‑cabin trijet business jet, commonly configured for about 12 to 16 passengers, with intercontinental range around 6,000–6,500 nautical miles, suited to nonstop transoceanic missions and premium cabin comfort. The Sikorsky S‑92 is a medium‑lift twin‑engine helicopter used for offshore and transport roles, typically carrying about 19 passengers, with far shorter range—generally a few hundred nautical miles (often around 400–600)—but with vertical takeoff/landing capability that fixed‑wing aircraft cannot match.
| Spec | Daher TBM 960 | Dassault Falcon 8X | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 7.66 | — | $ 19.79 |
| Min Crew | 1 | 2 | 1 | 2 |
| Total Seats | 6 | 17 | 8 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Daher TBM | Dassault Falcon | Piaggio | Sikorsky |
| Aircraft Name | TBM 960 | 8X | Avanti EVO | S-92 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 6450 | 1530 | 439 |
| DOC / nm / Seat | $ 0.56 | $ 0.64 | — | $ 0.94 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 36900 | 3775 | 7417 |
| Standard Cabin Seats | 4 | 14 | 6 | 19 |
| Direct Operating Cost | $ 744 | $ 3,805 | — | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 330 | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $4,450,000 | $ 62,500,000 | $ 7,695,000 | $30,650,000 |
| Max Cabin Seats | — | 16 | 7 | 19 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | No | 2 Enclosed Flushing | No | — |
| Min Crew | 1 | 2 | 1 | 2 |
| Total Seats | 6 | 17 | 8 | 21 |
| Galley Location | MID | FWD | — | — |
| Cabin Pressure (psi) | 6.2 | 10.2 | 9 | — |
| Standard Cabin Seats | 4 | 14 | 6 | 19 |
| SL Cabin Altitude (ft) | 14390 | 29200 | 24000 | — |
| Crew Rest | — | No | — | — |
| Jump Seat | — | Yes | — | — |
| Max Cabin Seats | — | 16 | 7 | 19 |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | No | — |
| Max Cabin Altitude (ft) | — | 3900 | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | TBM 960 | PW307D | PT6A–66B | CT7-8A |
| TBO (hrs) | 3500 | On-Condition | 3600 | 4000 |
| Horsepower | 850 | — | 850 | 2520 |
| Flat Rating | ISA + 49 | ISA + 17 | ISA + 28 | — |
| Thrust (lbs) | — | 6722 | — | — |
| No. of Engines | — | 3 | 2 | 1 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Type | — | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 35.3 | 80.2 | 47.3 | — |
| Wingspan (ft) | 42.1 | 86.3 | 47.1 | — |
| Cabin Width (ft) | 4 | 7.7 | 6.1 | — |
| Cabin Height (ft) | 4.1 | 6.2 | 5.8 | — |
| Cabin Length (ft) | 13.4 | 42.7 | 14.9 | — |
| Cabin Volume (cu. ft) | 123 | 1695 | — | 775 |
| Overall Height (ft) | — | 26.1 | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.5 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |