Daher Tbm 960 vs Leonardo Aw189 vs Piper M600 Sls
The Daher TBM 960 and Piper M600 SLS are single‑engine turboprop airplanes, while the Agusta/Leonardo AW189 is a twin‑engine helicopter, so they serve different mission profiles. For category, the TBM 960 is a high‑performance, pressurized personal/business aircraft optimized for fast point‑to‑point travel; the M600 SLS is also pressurized and business‑oriented but positioned a step below the TBM in overall performance and cabin/avionics sophistication. The AW189 is a medium twin helicopter aimed at utility, offshore, EMS, and VIP transport where vertical lift and hover matter more than cruise efficiency. On range, the TBM 960 generally offers the longest fixed‑wing reach (roughly around 1,500+ nautical miles depending on reserves and payload), the M600 SLS is typically somewhat shorter (around the 1,400‑nautical‑mile class), and the AW189’s range is usually lower (often around 450–500 nautical miles, configuration dependent). For passenger capacity, the TBM 960 commonly carries 4–6 passengers plus a pilot in executive use, the M600 SLS is similar (about 4–5 passengers plus pilot), while the AW189 can carry significantly more, typically up to around 16–19 passengers depending on layout and mission equipment.
| Spec | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 15.57 | $ 2.19 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 21 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Leonardo | Piper |
| Aircraft Name | TBM 960 | AW189 | M600 |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 651 | 1406 |
| DOC / nm / Seat | $ 0.56 | $ 0.74 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | — | 2200 |
| Standard Cabin Seats | 4 | 19 | 4 |
| Direct Operating Cost | $ 744 | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | Garmin G3000 | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 155 | 274 |
| Base Aircraft Price (USD) | $4,450,000 | $2,413,000 | $3,081,400 |
| Max Cabin Seats | — | 19 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | — | No |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 21 | 5 |
| Galley Location | MID | — | MID |
| Cabin Pressure (psi) | 6.2 | — | 5.6 |
| Standard Cabin Seats | 4 | 19 | 4 |
| SL Cabin Altitude (ft) | 14390 | — | 12600 |
| Max Cabin Seats | — | 19 | — |
| Galley / Refreshment | — | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | TBM 960 | CT7-2E1 | PT6A-42A |
| TBO (hrs) | 3500 | 4000 | 3600 |
| Horsepower | 850 | 1983 | 600 |
| Flat Rating | ISA + 49 | — | ISA + 55 |
| Fuel Type | — | JetFuel | — |
| No. of Engines | — | 2 | 1 |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 35.3 | 57.8 | 29.7 |
| Wingspan (ft) | 42.1 | — | 43.2 |
| Cabin Width (ft) | 4 | — | 4.1 |
| Cabin Height (ft) | 4.1 | — | 4 |
| Cabin Length (ft) | 13.4 | — | 12.3 |
| Cabin Volume (cu. ft) | 123 | 395 | 165 |
| Overall Height (ft) | — | 16.6 | 11.3 |
| Rotor Diameter (ft) | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |
| Baggage Volume Int. (cu. ft) | — | — | 20 |