Embraer Legacy 650 E vs Piaggio Avanti Evo vs Piper M600 Sls vs Sikorsky S 92
The Embraer Legacy 650E is a long‑range, large‑cabin business jet suited to intercontinental missions. It typically offers a range around 3,900 nautical miles and seats about 13 passengers in executive configuration. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft, generally positioned for shorter to midrange travel than large jets; it offers roughly 1,500–1,800 nautical miles of range and commonly seats about 7–9 passengers. The Piper M600 SLS is a single‑engine turboprop personal and owner‑flown aircraft in a much smaller category; its range is about 1,000–1,500 nautical miles depending on payload and reserves, and it typically carries up to 6 occupants. The Sikorsky S‑92 is a medium twin‑engine helicopter primarily used for offshore, SAR, and VIP transport; compared with fixed‑wing aircraft it has much shorter range (roughly 500+ nautical miles typical) but strong point‑to‑point capability, and it commonly accommodates around 12–19 passengers depending on configuration.
| Spec | Piaggio Avanti EVO | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 8 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Piaggio | Piper | Sikorsky |
| Aircraft Name | Avanti EVO | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 1406 | 439 |
| Max Cabin Seats | 7 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3775 | 2200 | 7417 |
| Standard Cabin Seats | 6 | 4 | 19 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 400 | 274 | 155 |
| Base Aircraft Price (USD) | $ 7,695,000 | $3,081,400 | $30,650,000 |
| DOC / nm | — | $ 2.19 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.55 | $ 0.94 |
| Direct Operating Cost | — | $ 603 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | — |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 8 | 5 | 21 |
| Max Cabin Seats | 7 | — | 19 |
| Cabin Pressure (psi) | 9 | 5.6 | — |
| Galley / Refreshment | No | Refreshment Centre | — |
| Standard Cabin Seats | 6 | 4 | 19 |
| SL Cabin Altitude (ft) | 24000 | 12600 | — |
| Max Cabin Altitude (ft) | 6600 | 8644 | — |
| Galley Location | — | MID | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | PT6A–66B | PT6A-42A | CT7-8A |
| TBO (hrs) | 3600 | 3600 | 4000 |
| Horsepower | 850 | 600 | 2520 |
| Flat Rating | ISA + 28 | ISA + 55 | — |
| No. of Engines | 2 | 1 | 1 |
| Fuel Burn (gph) | 100 | — | — |
| Fuel Capacity (gal) | — | 260 | 760 |
| Fuel Type | — | — | JetFuel |
| 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 | 17.8 |
| Cabin Width - Floor (ft) | 3.5 | — | — |
| Baggage Volume Int. (cu. ft) | 35.2 | 20 | — |
| Cabin Volume (cu. ft) | — | 165 | 775 |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |