Daher Tbm 960 vs Dassault Falcon 8x vs Gulfstream G700 vs Piaggio Avanti Evo
The Daher TBM 960 is a high-performance single‑engine turboprop, best suited to owner‑pilots and short‑to‑medium missions, with roughly 1,500 nautical miles of range and typically 4–6 passengers in a small, pressurized cabin. The Piaggio Avanti EVO is a twin‑turboprop positioned between turboprops and light jets in speed and comfort; it commonly carries about 6–8 passengers and offers around 1,700–1,800 nautical miles of range depending on configuration. The Dassault Falcon 8X is a long‑range large‑cabin business jet, designed for intercontinental flying; it generally seats 12–16 passengers and is known for about 6,400 nautical miles of range. The Gulfstream G700 sits at the ultra‑long‑range, ultra‑large‑cabin end of the market, emphasizing space and nonstop global legs; it typically accommodates around 12–19 passengers with roughly 7,500 nautical miles of range. In short, the TBM 960 and Avanti EVO prioritize efficiency and smaller groups, while the Falcon 8X and G700 target long‑haul, higher‑capacity executive travel.
| Spec | Daher TBM 960 | Dassault Falcon 8X | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 2.25 | $ 7.66 | — | — |
| Min Crew | 1 | 2 | 4 | 1 |
| Total Seats | 6 | 17 | 16 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Daher TBM | Dassault Falcon | Gulfstream | Piaggio |
| Aircraft Name | TBM 960 | 8X | G700 | Avanti EVO |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 1730 | 6450 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.56 | $ 0.64 | — | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 36900 | — | 3775 |
| Standard Cabin Seats | 4 | 14 | 12 | 6 |
| Direct Operating Cost | $ 744 | $ 3,805 | — | — |
| Flight Deck (Base Spec) | Garmin G3000 | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 330 | 516 | 516 | 400 |
| Base Aircraft Price (USD) | $4,450,000 | $ 62,500,000 | $78,000,000 | $ 7,695,000 |
| Max Cabin Seats | — | 16 | 19 | 7 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | No | 2 Enclosed Flushing | — | No |
| Min Crew | 1 | 2 | 4 | 1 |
| Total Seats | 6 | 17 | 16 | 8 |
| Galley Location | MID | FWD | FWD | — |
| Cabin Pressure (psi) | 6.2 | 10.2 | — | 9 |
| Standard Cabin Seats | 4 | 14 | 12 | 6 |
| SL Cabin Altitude (ft) | 14390 | 29200 | — | 24000 |
| Crew Rest | — | No | Optional | — |
| Jump Seat | — | Yes | Yes | — |
| Max Cabin Seats | — | 16 | 19 | 7 |
| Lavatory Location | — | FWD / AFT | FWD / AFT | — |
| Galley / Refreshment | — | Galley | — | No |
| Max Cabin Altitude (ft) | — | 3900 | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | TBM 960 | PW307D | Pearl 700 | PT6A–66B |
| TBO (hrs) | 3500 | On-Condition | On Condition | 3600 |
| Horsepower | 850 | — | — | 850 |
| Flat Rating | ISA + 49 | ISA + 17 | — | ISA + 28 |
| Thrust (lbs) | — | 6722 | 18250 | — |
| No. of Engines | — | 3 | 2 | 2 |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 35.3 | 80.2 | 109.9 | 47.3 |
| Wingspan (ft) | 42.1 | 86.3 | 103 | 47.1 |
| Cabin Width (ft) | 4 | 7.7 | 8.2 | 6.1 |
| Cabin Height (ft) | 4.1 | 6.2 | 6.25 | 5.8 |
| Cabin Length (ft) | 13.4 | 42.7 | 56.9 | 14.9 |
| Cabin Volume (cu. ft) | 123 | 1695 | — | — |
| Overall Height (ft) | — | 26.1 | 25.4 | 13.1 |
| Cabin Width - Floor (ft) | — | 6.3 | — | 3.5 |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 195 | 35.2 |
| Aisle Step (ft) | — | — | Flat Floor | — |