Pilatus Pc 24 vs Piper M600 Sls vs Robinson R66
The Pilatus PC-24 and Piper M600 SLS are fixed‑wing airplanes, while the Robinson R66 is a light turbine helicopter, so they differ most in speed, runway requirements, and mission flexibility. In category, the PC-24 is a twin‑engine light jet aimed at fast business travel and frequent legs; the M600 SLS is a single‑engine turboprop optimized for owner‑pilot efficiency and simpler operations; the R66 is a single‑engine turbine helicopter focused on point‑to‑point access where runways aren’t available. On range, the PC-24 generally offers the longest reach (roughly around 2,000 nautical miles depending on configuration and reserves), the M600 SLS is typically next (about 1,400–1,600 nautical miles), and the R66 is shorter (commonly on the order of 300–400 nautical miles, varying with fuel load and conditions). For passenger capacity, the PC-24 can be configured for about 6–10 occupants depending on interior and crew assumptions, the M600 SLS typically carries 1 pilot plus up to 5 passengers, and the R66 commonly seats 1 pilot plus up to 4 passengers.
| Spec | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.71 | $ 2.19 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 6 |
| Manufacturer | Pilatus | Piper |
| Aircraft Name | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2076 | 1406 |
| DOC / nm / Seat | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 10 | — |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6680 | 2200 |
| Standard Cabin Seats | 6 | 4 |
| Direct Operating Cost | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 440 | 274 |
| Base Aircraft Price (USD) | $11,800,000 | $3,081,400 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | No |
| Min Crew | 1 | 1 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Cargo Door | Yes | — |
| Total Seats | 6 | 5 |
| Galley Location | FWD | MID |
| Max Cabin Seats | 10 | — |
| Lavatory Location | FWD | — |
| Cabin Pressure (psi) | 9.3 | 5.6 |
| Galley / Refreshment | Optional Refreshment Center | Refreshment Centre |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | 8644 |
| Engine | ||
| FADEC | Yes | No |
| Model | FJ44-4A-QPM | PT6A-42A |
| TBO (hrs) | 5000 | 3600 |
| Flat Rating | ISA + 23 | ISA + 55 |
| Thrust (lbs) | 3435 | — |
| No. of Engines | 2 | 1 |
| Horsepower | — | 600 |
| Fuel Capacity (gal) | — | 260 |
| Dimensions | ||
| Length (ft) | 52.2 | 29.7 |
| Wingspan (ft) | 55.8 | 43.2 |
| Aisle Step (ft) | Flat Floor | — |
| Cabin Width (ft) | 5.6 | 4.1 |
| Cabin Height (ft) | 5.1 | 4 |
| Cabin Length (ft) | 23 | 12.3 |
| Overall Height (ft) | 17.4 | 11.3 |
| Cabin Width - Floor (ft) | 3.8 | — |
| Cabin Length - Seating (ft) | 17 | — |
| Baggage Volume Int. (cu. ft) | 90 | 20 |
| Cabin Volume (cu. ft) | — | 165 |