Cirrus Sr22t G6 vs Diamond Aircraft Da42 Vi vs Piper M500
The Cirrus SR22T G6 and Piper M500 are both high-performance single‑engine aircraft, while the Diamond DA42 VI is a twin‑engine piston aircraft optimized for efficiency and redundancy. In category terms, the SR22T G6 is a turbocharged piston single aimed at fast personal and business travel; the DA42 VI is a light twin often used for touring, training, and special-mission roles; and the M500 is a pressurized single‑engine turboprop positioned as a step up in capability and altitude performance. For range, the SR22T G6 and DA42 VI are broadly similar in real-world mission flexibility, typically supporting medium-length trips, whereas the M500 generally offers longer legs and higher-speed, higher-altitude cruise options, making it better suited to longer cross-country travel and more challenging weather. Passenger capacity differs: the SR22T G6 typically seats up to five, the DA42 VI usually seats four, and the Piper M500 generally seats up to five, with more payload and cabin comfort potential than the piston singles.
| Spec | Diamond Aircraft DA42 VI | Piper M500 |
|---|---|---|
| Summary | ||
| DOC / nm | $ 1.11 | $ 3.11 |
| Total Seats | 4 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Diamond Aircraft | Piper |
| Aircraft Name | DA42 VI | M500 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1273 | 1000 |
| DOC / nm / Seat | $ 0.28 | $ 0.78 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1298 | 1698 |
| Direct Operating Cost | $ 211 | $ 579 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 190 | 260 |
| Base Aircraft Price (USD) | $869,000 | $2,122,600 |
| Cockpit | — | 2 |
| Min Crew | — | 1 |
| Standard Cabin Seats | — | 4 |
| Cabin | ||
| Total Seats | 4 | 5 |
| Cockpit | — | 2 |
| Lavatory | — | No |
| Min Crew | — | 1 |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 5.5 |
| Galley / Refreshment | — | Refreshment Centre |
| Standard Cabin Seats | — | 4 |
| SL Cabin Altitude (ft) | — | 12600 |
| Max Cabin Altitude (ft) | — | 8244 |
| Engine | ||
| FADEC | Yes | No |
| Model | AE300 | PT6A-42A |
| Fuel Type | Diesel / Jet Fuel | — |
| TBO (hrs) | 1800 | 3600 |
| Horsepower | 168 | 500 |
| Fuel Delivery | Fuel Injected | — |
| No. of Engines | 2 | 1 |
| Usable Fuel (gal) | 76.4 | — |
| Fuel Capacity (gal) | 79.4 | 170 |
| Flat Rating | — | ISA + 55 |
| Dimensions | ||
| Length (ft) | 28.1 | 29.6 |
| Wingspan (ft) | 44.5 | 43.2 |
| Overall Height (ft) | 8.2 | 11.3 |
| Cabin Width (ft) | — | 4.1 |
| Cabin Height (ft) | — | 4 |
| Cabin Length (ft) | — | 12.3 |
| Cabin Volume (cu. ft) | — | 165 |
| Baggage Volume Int. (cu. ft) | — | 20 |