Daher Tbm 960 vs Piper M600 Sls vs Robinson R66 vs Sikorsky S 92
The Daher TBM 960 and Piper M600 SLS are single‑engine turboprop airplanes aimed at fast personal or small business travel. Both typically carry one pilot plus four to five passengers, with the TBM 960 generally offering the longer real‑world range and higher cruise speed, making it better suited to longer nonstop trips, while the M600 SLS is usually positioned slightly lower in speed and range but still solid for regional missions. The Robinson R66 is a light single‑engine turbine helicopter. It typically carries a pilot plus four passengers, trading lower cruise speed and shorter range than the turboprop airplanes for the ability to land in tight or unimproved areas and provide true vertical access. The Sikorsky S‑92 is a medium twin‑engine helicopter designed for commercial, offshore, and utility operations. It carries far more people—commonly around 12 to 19 passengers depending on configuration—and has substantially greater mission capability and redundancy than the R66, with longer range than most light helicopters, though it remains slower than the turboprop airplanes in cruise.
| Spec | Daher TBM 960 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 6 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Piper | Sikorsky |
| Aircraft Name | TBM 960 | M600 | S-92 |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1406 | 439 |
| DOC / nm / Seat | $ 0.56 | $ 0.55 | $ 0.94 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2908 | 2200 | 7417 |
| Standard Cabin Seats | 4 | 4 | 19 |
| Direct Operating Cost | $ 744 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 330 | 274 | 155 |
| Base Aircraft Price (USD) | $4,450,000 | $3,081,400 | $30,650,000 |
| Max Cabin Seats | — | — | 19 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | — |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 6 | 5 | 21 |
| Galley Location | MID | MID | — |
| Cabin Pressure (psi) | 6.2 | 5.6 | — |
| Standard Cabin Seats | 4 | 4 | 19 |
| SL Cabin Altitude (ft) | 14390 | 12600 | — |
| Galley / Refreshment | — | Refreshment Centre | — |
| Max Cabin Altitude (ft) | — | 8644 | — |
| Max Cabin Seats | — | — | 19 |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | TBM 960 | PT6A-42A | CT7-8A |
| TBO (hrs) | 3500 | 3600 | 4000 |
| Horsepower | 850 | 600 | 2520 |
| Flat Rating | ISA + 49 | ISA + 55 | — |
| No. of Engines | — | 1 | 1 |
| Fuel Capacity (gal) | — | 260 | 760 |
| Fuel Type | — | — | JetFuel |
| Dimensions | |||
| Length (ft) | 35.3 | 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 | 165 | 775 |
| Overall Height (ft) | — | 11.3 | 17.8 |
| Baggage Volume Int. (cu. ft) | — | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |