Diamond Aircraft Da42 Vi vs Diamond Aircraft Da62 vs Piper M500
The Diamond DA42 VI and DA62 are both modern, efficient piston twins, while the Piper M500 is a pressurized single‑engine turboprop aimed at faster, higher‑altitude travel. In category terms, the DA42 VI is a light twin optimized for economy and training or owner‑operator touring; the DA62 is a larger, more capable light twin positioned for comfortable family and business travel; the M500 sits in a higher performance class as a personal turboprop with cabin pressurization and typical cruise operations in the flight levels. For range, the DA42 VI generally offers solid cross‑country capability but is the shortest‑legged of the three; the DA62 typically matches or slightly exceeds the DA42 in real‑world touring range thanks to greater fuel capacity and efficiency at similar piston‑twin speeds; the M500 usually delivers the longest practical range, benefiting from turboprop cruise at higher altitudes and greater usable fuel. Passenger capacity also separates them: the DA42 VI is commonly configured for four seats, the DA62 is typically a seven‑seat aircraft, and the M500 generally seats five to six, depending on interior configuration.
| Spec | Diamond Aircraft DA42 VI | Diamond Aircraft DA62 | Piper M500 |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 1.11 | $ 1.18 | $ 3.11 |
| Total Seats | 4 | 5 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Diamond Aircraft | Diamond Aircraft | Piper |
| Aircraft Name | DA42 VI | DA62 | M500 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1273 | 1283 | 1000 |
| DOC / nm / Seat | $ 0.28 | $ 0.24 | $ 0.78 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1298 | 1565 | 1698 |
| Direct Operating Cost | $ 211 | $ 225 | $ 579 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 190 | 190 | 260 |
| Base Aircraft Price (USD) | $869,000 | $1,290,000 | $2,122,600 |
| Cockpit | — | 2 | 2 |
| Max Cabin Seats | — | 5 | — |
| Standard Cabin Seats | — | 3 | 4 |
| Min Crew | — | — | 1 |
| Cabin | |||
| Total Seats | 4 | 5 | 5 |
| Cockpit | — | 2 | 2 |
| Max Cabin Seats | — | 5 | — |
| Standard Cabin Seats | — | 3 | 4 |
| Lavatory | — | — | No |
| Min Crew | — | — | 1 |
| Galley Location | — | — | MID |
| Cabin Pressure (psi) | — | — | 5.5 |
| Galley / Refreshment | — | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 12600 |
| Max Cabin Altitude (ft) | — | — | 8244 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | AE300 | AE330 | PT6A-42A |
| Fuel Type | Diesel / Jet Fuel | Diesel / Jet Fuel | — |
| TBO (hrs) | 1800 | 1800 | 3600 |
| Horsepower | 168 | 180 | 500 |
| Fuel Delivery | Fuel Injected | Fuel Injected | — |
| No. of Engines | 2 | 2 | 1 |
| Usable Fuel (gal) | 76.4 | 86 | — |
| Fuel Capacity (gal) | 79.4 | 89 | 170 |
| Flat Rating | — | — | ISA + 55 |
| Dimensions | |||
| Length (ft) | 28.1 | 30.1 | 29.6 |
| Wingspan (ft) | 44.5 | 47.8 | 43.2 |
| Overall Height (ft) | 8.2 | 9.3 | 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 |