Daher Tbm 960 vs Dassault Falcon 8x vs Leonardo Aw189 vs Piper M600 Sls
The Daher TBM 960 and Piper M600 SLS are single‑engine turboprop airplanes aimed at fast, efficient personal or small‑team travel. In category terms they sit below business jets and helicopters in acquisition and operating complexity, typically carrying a pilot plus about four to six passengers depending on configuration and comfort. Range is in the “regional to cross‑country” class, generally around 1,000–1,700 nautical miles, with the TBM 960 usually offering the longer legs and higher cruise capability than the M600 SLS. The Dassault Falcon 8X is a long‑range, large‑cabin trijet business jet. It is designed for intercontinental missions, with range roughly in the 6,000‑plus nautical mile class, and typical passenger loads around 8–14 depending on cabin layout, far exceeding the turboprops in both distance and cabin volume. The Agusta/Leonardo AW189 is a twin‑engine medium helicopter, optimized for vertical lift missions (offshore, SAR, utility, corporate shuttle). Passenger capacity is commonly in the mid‑teens, but range is shorter than fixed‑wing options, typically a few hundred nautical miles, trading speed and range for VTOL flexibility.
| Spec | Daher TBM 960 | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 7.66 | $ 15.57 | $ 2.19 |
| Min Crew | 1 | 2 | 1 | 1 |
| Total Seats | 6 | 17 | 21 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Daher TBM | Dassault Falcon | Leonardo | Piper |
| Aircraft Name | TBM 960 | 8X | AW189 | M600 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 6450 | 651 | 1406 |
| DOC / nm / Seat | $ 0.56 | $ 0.64 | $ 0.74 | $ 0.55 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | 36900 | — | 2200 |
| Standard Cabin Seats | 4 | 14 | 19 | 4 |
| Direct Operating Cost | $ 744 | $ 3,805 | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | Garmin G3000 | Honeywell Primus EASy II | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 516 | 155 | 274 |
| Base Aircraft Price (USD) | $4,450,000 | $ 62,500,000 | $2,413,000 | $3,081,400 |
| Max Cabin Seats | — | 16 | 19 | — |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | No | 2 Enclosed Flushing | — | No |
| Min Crew | 1 | 2 | 1 | 1 |
| Total Seats | 6 | 17 | 21 | 5 |
| Galley Location | MID | FWD | — | MID |
| Cabin Pressure (psi) | 6.2 | 10.2 | — | 5.6 |
| Standard Cabin Seats | 4 | 14 | 19 | 4 |
| SL Cabin Altitude (ft) | 14390 | 29200 | — | 12600 |
| Crew Rest | — | No | — | — |
| Jump Seat | — | Yes | — | — |
| Max Cabin Seats | — | 16 | 19 | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | 3900 | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | TBM 960 | PW307D | CT7-2E1 | PT6A-42A |
| TBO (hrs) | 3500 | On-Condition | 4000 | 3600 |
| Horsepower | 850 | — | 1983 | 600 |
| Flat Rating | ISA + 49 | ISA + 17 | — | ISA + 55 |
| Thrust (lbs) | — | 6722 | — | — |
| No. of Engines | — | 3 | 2 | 1 |
| Fuel Type | — | — | JetFuel | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 35.3 | 80.2 | 57.8 | 29.7 |
| Wingspan (ft) | 42.1 | 86.3 | — | 43.2 |
| Cabin Width (ft) | 4 | 7.7 | — | 4.1 |
| Cabin Height (ft) | 4.1 | 6.2 | — | 4 |
| Cabin Length (ft) | 13.4 | 42.7 | — | 12.3 |
| Cabin Volume (cu. ft) | 123 | 1695 | 395 | 165 |
| Overall Height (ft) | — | 26.1 | 16.6 | 11.3 |
| Cabin Width - Floor (ft) | — | 6.3 | — | — |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | — | 20 |
| Rotor Diameter (ft) | — | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 85 | — |