Piper M350 vs Piper M500 vs Piper M600 Sls vs Piper Seneca
The Piper M350, M500, and M600 SLS are all single‑engine, pressurized turboprop (or in the M350’s case, pressurized piston) aircraft aimed at owner‑pilots who want cabin-class comfort, while the Piper Seneca is a light twin‑engine piston aircraft often used for training, personal travel, and light commercial missions. In range terms, the M350 and Seneca typically occupy the shorter end of this group, suited to regional trips, while the M500 generally stretches farther, and the M600 SLS is usually the longest‑legged of the four, optimized for longer nonstop cross‑country flights. For passenger capacity, all are broadly in the six‑seat class, but real‑world usable seating varies: the M350 and M500 commonly carry a pilot plus four to five passengers depending on fuel and baggage, the M600 SLS similarly targets six seats but is often flown with a practical load of four to five plus luggage on longer legs, and the Seneca offers up to six seats with flexibility, though payload and fuel tradeoffs can also reduce practical passenger count on longer trips.
| Spec | Piper M350 | Piper M500 | Piper M600 SLS | Piper Seneca |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.34 | $ 3.11 | $ 2.19 | $ 1.69 |
| Total Seats | 6 | 6 | 6 | 6 |
| Flight Rules | VFR | IFR | IFR | IFR |
| Manufacturer | Piper | Piper | Piper | Piper |
| Aircraft Name | M350 | M500 | M600 | Seneca |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1343 | 1000 | 1406 | 828 |
| DOC / nm / Seat | $ 0.22 | $ 0.78 | $ 0.55 | $ 0.28 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 1308 | 1698 | 2200 | 1331 |
| Standard Cabin Seats | 4 | 4 | 4 | 4 |
| Direct Operating Cost | $ 285 | $ 579 | $ 603 | $ 337 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 213 | 260 | 274 | 200 |
| Base Aircraft Price (USD) | $1,195,000 | $2,122,600 | $3,081,400 | $1,095,000 |
| Min Crew | — | 1 | 1 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 5 | 5 | 6 |
| Cabin Pressure (psi) | 5.6 | 5.5 | 5.6 | — |
| Standard Cabin Seats | 4 | 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 | No |
| Model | TIO-540-AE2A | PT6A-42A | PT6A-42A | TSIO-360-RB |
| Fuel Type | AvGas | — | — | AvGas |
| TBO (hrs) | 2000 | 3600 | 3600 | 1800 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 350 | 500 | 600 | 220 |
| Fuel Delivery | Fuel Injected | — | — | Fuel Injected |
| No. of Engines | 1 | 1 | 1 | 2 |
| Fuel Capacity (gal) | 120 | 170 | 260 | 122 |
| Flat Rating | — | ISA + 55 | ISA + 55 | — |
| Dimensions | ||||
| Length (ft) | 29 | 29.6 | 29.7 | 28.6 |
| Wingspan (ft) | 43 | 43.2 | 43.2 | 39 |
| 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 | 10 |
| Cabin Volume (cu. ft) | 165 | 165 | 165 | — |
| Baggage Volume Ext. (cu. ft) | 13 | — | — | — |
| Baggage Volume Int. (cu. ft) | 20 | 20 | 20 | — |