Piper M350 vs Piper M500 vs Piper M600 Sls
The Piper M350 is the entry point of the three, positioned as a pressurized piston single. It typically offers the shortest range of the group and is best suited to regional trips; in practical terms it generally supports about five to six occupants depending on load and fuel, with seating for up to six in the cabin. The Piper M500 moves into the turboprop category, bringing higher cruise speeds and a meaningful step up in usable range versus the M350. Passenger capability is similar in layout—commonly flown with four to six aboard—but the turbine performance makes it better for longer legs and higher-altitude weather. The Piper M600 SLS sits at the top as the most capable turboprop in this lineup. It generally delivers the longest range and greatest payload flexibility, so it’s the most accommodating for carrying more people farther with bags and reserves. Like the others, it’s a single-engine pressurized cabin with up to six seats, but it tends to retain that capacity with less compromise on fuel and payload than the M350 and M500.
| Spec | Piper M350 | Piper M500 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 1.34 | $ 3.11 | $ 2.19 |
| Total Seats | 6 | 6 | 6 |
| Flight Rules | VFR | IFR | IFR |
| Manufacturer | Piper | Piper | Piper |
| Aircraft Name | M350 | M500 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1343 | 1000 | 1406 |
| DOC / nm / Seat | $ 0.22 | $ 0.78 | $ 0.55 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 1308 | 1698 | 2200 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Direct Operating Cost | $ 285 | $ 579 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 213 | 260 | 274 |
| Base Aircraft Price (USD) | $1,195,000 | $2,122,600 | $3,081,400 |
| Min Crew | — | 1 | 1 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Total Seats | 6 | 5 | 5 |
| Cabin Pressure (psi) | 5.6 | 5.5 | 5.6 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Lavatory | — | No | No |
| Min Crew | — | 1 | 1 |
| Galley Location | — | MID | MID |
| Galley / Refreshment | — | Refreshment Centre | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 12600 | 12600 |
| Max Cabin Altitude (ft) | — | 8244 | 8644 |
| Engine | |||
| FADEC | No | No | No |
| Model | TIO-540-AE2A | PT6A-42A | PT6A-42A |
| Fuel Type | AvGas | — | — |
| TBO (hrs) | 2000 | 3600 | 3600 |
| TBO (yrs) | 12 | — | — |
| Horsepower | 350 | 500 | 600 |
| Fuel Delivery | Fuel Injected | — | — |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 120 | 170 | 260 |
| Flat Rating | — | ISA + 55 | ISA + 55 |
| Dimensions | |||
| Length (ft) | 29 | 29.6 | 29.7 |
| Wingspan (ft) | 43 | 43.2 | 43.2 |
| Cabin Width (ft) | 4.1 | 4.1 | 4.1 |
| Cabin Height (ft) | 4 | 4 | 4 |
| Cabin Length (ft) | 12.3 | 12.3 | 12.3 |
| Overall Height (ft) | 11.4 | 11.3 | 11.3 |
| Cabin Volume (cu. ft) | 165 | 165 | 165 |
| Baggage Volume Ext. (cu. ft) | 13 | — | — |
| Baggage Volume Int. (cu. ft) | 20 | 20 | 20 |