Daher Tbm 960 vs Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Daher TBM 960 is a single‑engine turboprop in the high‑performance personal and owner‑pilot category. It typically carries about 4–6 passengers (up to 6 plus a pilot, depending on layout) and offers roughly 1,500–1,700 nautical miles of range, making it well suited to fast regional trips and smaller airports. The Dassault Falcon 8X is an ultra‑long‑range, large‑cabin business jet aimed at intercontinental missions. It commonly seats around 12–16 passengers (with higher-density options) and delivers about 6,400–6,450 nautical miles of range, enabling nonstops such as North America to Europe or deep transoceanic routes. The MD Helicopters 902 Explorer is a light twin‑engine helicopter for short‑range utility, corporate, or EMS-style missions. It generally carries 1–7 occupants total (often 5–6 passengers plus pilot) with a range on the order of about 300–400 nautical miles, prioritizing vertical access over distance. The Piaggio Avanti EVO is a twin‑turboprop business aircraft positioned between personal turboprops and light jets. It typically seats 6–8 passengers and offers about 1,500–1,800 nautical miles of range, combining cabin comfort with efficient medium‑range cruising.
| Spec | Daher TBM 960 | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 7.66 | — |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 6 | 17 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Daher TBM | Dassault Falcon | Piaggio |
| Aircraft Name | TBM 960 | 8X | Avanti EVO |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 6450 | 1530 |
| DOC / nm / Seat | $ 0.56 | $ 0.64 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2908 | 36900 | 3775 |
| Standard Cabin Seats | 4 | 14 | 6 |
| Direct Operating Cost | $ 744 | $ 3,805 | — |
| Flight Deck (Base Spec) | Garmin G3000 | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 330 | 516 | 400 |
| Base Aircraft Price (USD) | $4,450,000 | $ 62,500,000 | $ 7,695,000 |
| Max Cabin Seats | — | 16 | 7 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Lavatory | No | 2 Enclosed Flushing | No |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 6 | 17 | 8 |
| Galley Location | MID | FWD | — |
| Cabin Pressure (psi) | 6.2 | 10.2 | 9 |
| Standard Cabin Seats | 4 | 14 | 6 |
| SL Cabin Altitude (ft) | 14390 | 29200 | 24000 |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Max Cabin Seats | — | 16 | 7 |
| Lavatory Location | — | FWD / AFT | — |
| Galley / Refreshment | — | Galley | No |
| Max Cabin Altitude (ft) | — | 3900 | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | TBM 960 | PW307D | PT6A–66B |
| TBO (hrs) | 3500 | On-Condition | 3600 |
| Horsepower | 850 | — | 850 |
| Flat Rating | ISA + 49 | ISA + 17 | ISA + 28 |
| Thrust (lbs) | — | 6722 | — |
| No. of Engines | — | 3 | 2 |
| Fuel Burn (gph) | — | — | 100 |
| 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 | — |
| Overall Height (ft) | — | 26.1 | 13.1 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.5 |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 35.2 |