Piper M600 Sls vs Robinson R66
The Piper M600 SLS is a single‑engine turboprop airplane, while the Robinson R66 is a single‑engine turbine helicopter. As an airplane, the M600 SLS is generally optimized for efficient point‑to‑point travel between airports at higher cruise speeds and with longer legs, whereas the R66 trades speed and cruise efficiency for vertical takeoff and landing, the ability to use helipads or unimproved sites, and better access to confined areas. On range, the M600 SLS typically offers substantially greater range than the R66, making it better suited to longer cross‑country trips without refueling. The R66’s practical range is shorter and more sensitive to payload, wind, and reserve requirements, but it can provide more direct routing and access where runways are unavailable. On passenger capacity, both are commonly configured for up to about five seats including the pilot, but real‑world usable seats depend on weight, fuel, and baggage. The M600 SLS generally carries passengers and baggage farther with more margin, while the R66 often requires closer tradeoffs between fuel and load.
| Spec | Piper M600 SLS |
|---|---|
| Summary | |
| Cockpit | 2 |
| DOC / nm | $ 2.19 |
| Min Crew | 1 |
| Total Seats | 6 |
| Flight Rules | IFR |
| Manufacturer | Piper |
| Aircraft Name | M600 |
| Certification | FAA / EASA |
| Max Range (nm) | 1406 |
| DOC / nm / Seat | $ 0.55 |
| OEM Verification | VERIFIED |
| Useful Load (lbs) | 2200 |
| Standard Cabin Seats | 4 |
| Direct Operating Cost | $ 603 |
| Flight Deck (Base Spec) | Garmin G3000 |
| Max Cruise Speed (ktas) | 274 |
| Base Aircraft Price (USD) | $3,081,400 |
| Cabin | |
| Cockpit | 2 |
| Lavatory | No |
| Min Crew | 1 |
| Total Seats | 5 |
| Galley Location | MID |
| Cabin Pressure (psi) | 5.6 |
| Galley / Refreshment | Refreshment Centre |
| Standard Cabin Seats | 4 |
| SL Cabin Altitude (ft) | 12600 |
| Max Cabin Altitude (ft) | 8644 |
| Engine | |
| FADEC | No |
| Model | PT6A-42A |
| TBO (hrs) | 3600 |
| Horsepower | 600 |
| Flat Rating | ISA + 55 |
| No. of Engines | 1 |
| Fuel Capacity (gal) | 260 |
| Dimensions | |
| Length (ft) | 29.7 |
| Wingspan (ft) | 43.2 |
| Cabin Width (ft) | 4.1 |
| Cabin Height (ft) | 4 |
| Cabin Length (ft) | 12.3 |
| Overall Height (ft) | 11.3 |
| Cabin Volume (cu. ft) | 165 |
| Baggage Volume Int. (cu. ft) | 20 |