Embraer Legacy 650 E vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Piper M600 Sls
The Embraer Legacy 650E is a long-range large-cabin business jet, typically offering intercontinental capability of roughly 3,900–4,000 nautical miles and seating about 13 passengers in a standard executive layout. The Piaggio Avanti EVO is a high-speed twin‑turboprop business aircraft aimed at efficient regional-to-medium missions, with an approximate range around 1,700–1,900 nautical miles and seating commonly 7–9. The Piper M600 SLS is a single‑engine turboprop positioned for owner-operators and shorter business trips, with a typical range near 1,400–1,500 nautical miles and seating usually 5–6 plus a pilot, depending on configuration. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter optimized for vertical-access missions rather than long distance, generally offering a few hundred nautical miles of range (often around 300–400) and seating typically 6–8 including the pilot(s), depending on interior and mission kit. Overall, the Legacy 650E leads on range and cabin capacity, the Avanti EVO balances speed and efficiency, the M600 SLS prioritizes simplicity and cost for smaller groups, and the 902 emphasizes access over distance.
| 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 |