Piper M350 vs Piper M600 Sls vs Piper Seneca
The Piper M350 and M600 SLS are pressurized, single‑engine turboprop/propeller personal aircraft aimed at efficient high‑altitude travel, while the Piper Seneca is an unpressurized (in most variants) light twin‑engine piston aircraft often used for training, charter, and utility missions. For range, the M600 SLS generally offers the longest reach, typically around the 1,000‑nautical‑mile class depending on power settings, winds, and payload. The M350 is also a long‑range cross‑country platform, commonly in the high‑600 to mid‑700‑nautical‑mile class under typical cruise planning. The Seneca’s range is usually shorter than both pressurized singles, often in roughly the 700–800‑nautical‑mile class but strongly dependent on variant and reserves. In passenger capacity, all three commonly seat about six occupants in practical configurations, though real‑world comfort and baggage vary: the M600 SLS and M350 are typically arranged for a pilot plus up to five, while the Seneca often carries a similar count but trades pressurization and speed for twin‑engine redundancy and multi‑role flexibility.
| Spec | Piper M350 | Piper M600 SLS | Piper Seneca |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 1.34 | $ 2.19 | $ 1.69 |
| Total Seats | 6 | 6 | 6 |
| Flight Rules | VFR | IFR | IFR |
| Manufacturer | Piper | Piper | Piper |
| Aircraft Name | M350 | M600 | Seneca |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1343 | 1406 | 828 |
| DOC / nm / Seat | $ 0.22 | $ 0.55 | $ 0.28 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 1308 | 2200 | 1331 |
| Standard Cabin Seats | 4 | 4 | 4 |
| Direct Operating Cost | $ 285 | $ 603 | $ 337 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 213 | 274 | 200 |
| Base Aircraft Price (USD) | $1,195,000 | $3,081,400 | $1,095,000 |
| Min Crew | — | 1 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Total Seats | 6 | 5 | 6 |
| Cabin Pressure (psi) | 5.6 | 5.6 | — |
| Standard Cabin Seats | 4 | 4 | 4 |
| Lavatory | — | No | — |
| Min Crew | — | 1 | — |
| Galley Location | — | MID | — |
| Galley / Refreshment | — | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | 12600 | — |
| Max Cabin Altitude (ft) | — | 8644 | — |
| Engine | |||
| FADEC | No | No | No |
| Model | TIO-540-AE2A | PT6A-42A | TSIO-360-RB |
| Fuel Type | AvGas | — | AvGas |
| TBO (hrs) | 2000 | 3600 | 1800 |
| TBO (yrs) | 12 | — | — |
| Horsepower | 350 | 600 | 220 |
| Fuel Delivery | Fuel Injected | — | Fuel Injected |
| No. of Engines | 1 | 1 | 2 |
| Fuel Capacity (gal) | 120 | 260 | 122 |
| Flat Rating | — | ISA + 55 | — |
| Dimensions | |||
| Length (ft) | 29 | 29.7 | 28.6 |
| Wingspan (ft) | 43 | 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) | 11.4 | 11.3 | 10 |
| Cabin Volume (cu. ft) | 165 | 165 | — |
| Baggage Volume Ext. (cu. ft) | 13 | — | — |
| Baggage Volume Int. (cu. ft) | 20 | 20 | — |