Piper M500 vs Piper M600 Sls vs Piper Seneca
The Piper M500 and M600 SLS are single‑engine turboprops intended for high‑performance personal or owner‑flown business travel, while the Piper Seneca is a twin‑engine piston aircraft typically positioned for multi‑engine touring, training, and light utility missions. In range, the M600 SLS generally offers the longest legs of the three, edging the M500 with more capability for longer nonstop trips, whereas the Seneca’s typical practical range is shorter and more dependent on power settings, payload, and reserves. For passenger capacity, all can be configured to carry up to about six occupants including the pilot, but the M500 and M600 SLS usually deliver that capacity with greater speed and altitude capability, making them better suited to efficient point‑to‑point travel. The Seneca’s cabin and seating can be comparable in count, yet it is more often used with fewer passengers to balance fuel, baggage, and performance, trading turbine speed and high‑altitude cruise for twin‑engine redundancy and lower acquisition and operating costs relative to the turboprops.
| Spec | Piper M500 | Piper M600 SLS | Piper Seneca |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 3.11 | $ 2.19 | $ 1.69 |
| Min Crew | 1 | 1 | — |
| Total Seats | 6 | 6 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Piper | Piper | Piper |
| Aircraft Name | M500 | M600 | Seneca |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1000 | 1406 | 828 |
| DOC / nm / Seat | $ 0.78 | $ 0.55 | $ 0.28 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 1698 | 2200 | 1331 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Direct Operating Cost | $ 579 | $ 603 | $ 337 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 260 | 274 | 200 |
| Base Aircraft Price (USD) | $2,122,600 | $3,081,400 | $1,095,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | — |
| Min Crew | 1 | 1 | — |
| Total Seats | 5 | 5 | 6 |
| Galley Location | MID | MID | — |
| Cabin Pressure (psi) | 5.5 | 5.6 | — |
| Galley / Refreshment | Refreshment Centre | Refreshment Centre | — |
| Standard Cabin Seats | 4 | 4 | 4 |
| SL Cabin Altitude (ft) | 12600 | 12600 | — |
| Max Cabin Altitude (ft) | 8244 | 8644 | — |
| Engine | |||
| FADEC | No | No | No |
| Model | PT6A-42A | PT6A-42A | TSIO-360-RB |
| TBO (hrs) | 3600 | 3600 | 1800 |
| Horsepower | 500 | 600 | 220 |
| Flat Rating | ISA + 55 | ISA + 55 | — |
| No. of Engines | 1 | 1 | 2 |
| Fuel Capacity (gal) | 170 | 260 | 122 |
| Fuel Type | — | — | AvGas |
| Fuel Delivery | — | — | Fuel Injected |
| Dimensions | |||
| Length (ft) | 29.6 | 29.7 | 28.6 |
| Wingspan (ft) | 43.2 | 43.2 | 39 |
| Cabin Width (ft) | 4.1 | 4.1 | — |
| Cabin Height (ft) | 4 | 4 | — |
| Cabin Length (ft) | 12.3 | 12.3 | — |
| Overall Height (ft) | 11.3 | 11.3 | 10 |
| Cabin Volume (cu. ft) | 165 | 165 | — |
| Baggage Volume Int. (cu. ft) | 20 | 20 | — |