Diamond Aircraft Da42 Vi vs Piper M350 vs Piper M500 vs Piper M600 Sls
By category, the Diamond Aircraft DA42 VI is a light twin‑engine piston aircraft typically used for training, personal travel, and light commercial missions, while the Piper M350 is a pressurized single‑engine piston aircraft positioned as a high‑end personal/business traveler. The Piper M500 and M600 SLS step into the single‑engine turboprop category, with the M600 SLS representing the higher‑performance, more advanced version (notably with enhanced avionics and automation). In range, the DA42 VI generally offers solid cross‑country capability for a piston twin but is usually shorter‑legged than the pressurized Piper singles and notably behind the turboprops on long nonstop trips. The M350 typically provides longer range than many light twins thanks to pressurization and efficient high‑altitude cruise, while the M500 extends practical range further with turboprop efficiency at altitude. The M600 SLS is commonly the longest‑range of the four and is optimized for faster, higher, longer missions. For passenger capacity, all are broadly in the 4–6 seat class, with the DA42 VI and M350 commonly configured for around four adults plus baggage, and the M500 and M600 SLS typically accommodating up to six seats depending on interior and weight.
| Spec | Diamond Aircraft DA42 VI | Piper M350 | Piper M500 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| DOC / nm | $ 1.11 | $ 1.34 | $ 3.11 | $ 2.19 |
| Total Seats | 4 | 6 | 6 | 6 |
| Flight Rules | IFR | VFR | IFR | IFR |
| Manufacturer | Diamond Aircraft | Piper | Piper | Piper |
| Aircraft Name | DA42 VI | M350 | M500 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1273 | 1343 | 1000 | 1406 |
| DOC / nm / Seat | $ 0.28 | $ 0.22 | $ 0.78 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 1298 | 1308 | 1698 | 2200 |
| Direct Operating Cost | $ 211 | $ 285 | $ 579 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 190 | 213 | 260 | 274 |
| Base Aircraft Price (USD) | $869,000 | $1,195,000 | $2,122,600 | $3,081,400 |
| Cockpit | — | 2 | 2 | 2 |
| Standard Cabin Seats | — | 4 | 4 | 4 |
| Min Crew | — | — | 1 | 1 |
| Cabin | ||||
| Total Seats | 4 | 6 | 5 | 5 |
| Cockpit | — | 2 | 2 | 2 |
| Cabin Pressure (psi) | — | 5.6 | 5.5 | 5.6 |
| Standard Cabin Seats | — | 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 | Yes | No | No | No |
| Model | AE300 | TIO-540-AE2A | PT6A-42A | PT6A-42A |
| Fuel Type | Diesel / Jet Fuel | AvGas | — | — |
| TBO (hrs) | 1800 | 2000 | 3600 | 3600 |
| Horsepower | 168 | 350 | 500 | 600 |
| Fuel Delivery | Fuel Injected | Fuel Injected | — | — |
| No. of Engines | 2 | 1 | 1 | 1 |
| Usable Fuel (gal) | 76.4 | — | — | — |
| Fuel Capacity (gal) | 79.4 | 120 | 170 | 260 |
| TBO (yrs) | — | 12 | — | — |
| Flat Rating | — | — | ISA + 55 | ISA + 55 |
| Dimensions | ||||
| Length (ft) | 28.1 | 29 | 29.6 | 29.7 |
| Wingspan (ft) | 44.5 | 43 | 43.2 | 43.2 |
| Overall Height (ft) | 8.2 | 11.4 | 11.3 | 11.3 |
| Cabin Width (ft) | — | 4.1 | 4.1 | 4.1 |
| Cabin Height (ft) | — | 4 | 4 | 4 |
| Cabin Length (ft) | — | 12.3 | 12.3 | 12.3 |
| Cabin Volume (cu. ft) | — | 165 | 165 | 165 |
| Baggage Volume Ext. (cu. ft) | — | 13 | — | — |
| Baggage Volume Int. (cu. ft) | — | 20 | 20 | 20 |