Enstrom 480b vs Piaggio Avanti Evo vs Piper M600 Sls
The Enstrom 480B, Piaggio Avanti EVO, and Piper M600 SLS sit in very different categories. The Enstrom 480B is a single‑engine light helicopter suited to short-range utility and regional hops, with typical practical legs on the order of a few hundred nautical miles and seating generally for a pilot plus up to four passengers depending on configuration and payload. The Piaggio Avanti EVO is a twin‑turboprop executive aircraft designed for fast, longer-range business travel; it typically carries six to seven passengers in a pressurized cabin and offers roughly 1,500+ nautical miles of range, making it the most capable for multi-city trips. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft that bridges the gap: it’s pressurized, commonly seats a pilot plus five passengers, and delivers about 1,400–1,500 nautical miles of range, favoring owner-operators who want near-business-jet usability with simpler operations than a twin. Overall, the helicopter prioritizes access and vertical lift, while the Avanti prioritizes speed and cabin comfort, and the M600 balances range with simplicity.
| Spec | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piaggio | Piper |
| Aircraft Name | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 1406 |
| Max Cabin Seats | 7 | — |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3775 | 2200 |
| Standard Cabin Seats | 6 | 4 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 400 | 274 |
| Base Aircraft Price (USD) | $ 7,695,000 | $3,081,400 |
| DOC / nm | — | $ 2.19 |
| DOC / nm / Seat | — | $ 0.55 |
| Direct Operating Cost | — | $ 603 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | No |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 5 |
| Max Cabin Seats | 7 | — |
| Cabin Pressure (psi) | 9 | 5.6 |
| Galley / Refreshment | No | Refreshment Centre |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 24000 | 12600 |
| Max Cabin Altitude (ft) | 6600 | 8644 |
| Galley Location | — | MID |
| Engine | ||
| FADEC | Yes | No |
| Model | PT6A–66B | PT6A-42A |
| TBO (hrs) | 3600 | 3600 |
| Horsepower | 850 | 600 |
| Flat Rating | ISA + 28 | ISA + 55 |
| No. of Engines | 2 | 1 |
| Fuel Burn (gph) | 100 | — |
| Fuel Capacity (gal) | — | 260 |
| Dimensions | ||
| Length (ft) | 47.3 | 29.7 |
| Wingspan (ft) | 47.1 | 43.2 |
| Cabin Width (ft) | 6.1 | 4.1 |
| Cabin Height (ft) | 5.8 | 4 |
| Cabin Length (ft) | 14.9 | 12.3 |
| Overall Height (ft) | 13.1 | 11.3 |
| Cabin Width - Floor (ft) | 3.5 | — |
| Baggage Volume Int. (cu. ft) | 35.2 | 20 |
| Cabin Volume (cu. ft) | — | 165 |