Piper M500 vs Piper Seneca
The Piper M500 is a single‑engine, pressurized turboprop designed primarily for efficient, higher‑altitude personal and business travel with simpler engine management and strong climb performance. The Piper Seneca (typically the Seneca V) is a light, pressurized twin‑engine piston aircraft, often chosen for multi‑engine capability, training, and shorter business or regional missions where redundancy is a priority. In range, the M500 generally offers longer legs, commonly around the 1,000–1,200 nautical mile class depending on power settings, payload, and reserves. The Seneca’s typical ranges are shorter, often in the several‑hundred to roughly 900 nautical mile range, again depending heavily on configuration and how much fuel versus payload is carried. For passenger capacity, both are commonly configured for about five to six seats (pilot plus four to five passengers). In practice, the M500 tends to be used with fewer passengers when maximizing range and climb, while the Seneca’s cabin can accommodate similar headcounts but may be more payload‑sensitive on longer trips.
| Spec | Piper M500 | Piper Seneca |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.11 | $ 1.69 |
| Min Crew | 1 | — |
| Total Seats | 6 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piper | Piper |
| Aircraft Name | M500 | Seneca |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1000 | 828 |
| DOC / nm / Seat | $ 0.78 | $ 0.28 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 1698 | 1331 |
| Standard Cabin Seats | 4 | 4 |
| Direct Operating Cost | $ 579 | $ 337 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 260 | 200 |
| Base Aircraft Price (USD) | $2,122,600 | $1,095,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | — |
| Min Crew | 1 | — |
| Total Seats | 5 | 6 |
| Galley Location | MID | — |
| Cabin Pressure (psi) | 5.5 | — |
| Galley / Refreshment | Refreshment Centre | — |
| Standard Cabin Seats | 4 | 4 |
| SL Cabin Altitude (ft) | 12600 | — |
| Max Cabin Altitude (ft) | 8244 | — |
| Engine | ||
| FADEC | No | No |
| Model | PT6A-42A | TSIO-360-RB |
| TBO (hrs) | 3600 | 1800 |
| Horsepower | 500 | 220 |
| Flat Rating | ISA + 55 | — |
| No. of Engines | 1 | 2 |
| Fuel Capacity (gal) | 170 | 122 |
| Fuel Type | — | AvGas |
| Fuel Delivery | — | Fuel Injected |
| Dimensions | ||
| Length (ft) | 29.6 | 28.6 |
| Wingspan (ft) | 43.2 | 39 |
| Cabin Width (ft) | 4.1 | — |
| Cabin Height (ft) | 4 | — |
| Cabin Length (ft) | 12.3 | — |
| Overall Height (ft) | 11.3 | 10 |
| Cabin Volume (cu. ft) | 165 | — |
| Baggage Volume Int. (cu. ft) | 20 | — |