Piaggio Avanti Evo vs Piper M600 Sls vs Robinson R66 vs Sikorsky S 92
The Piaggio Avanti EVO and Piper M600 SLS are both pressurized, fixed‑wing aircraft, but they serve different missions: the Avanti EVO is a twin‑turboprop executive aircraft optimized for fast point‑to‑point travel, typically offering roughly 1,300–1,800 nm range and seating commonly 6–8 passengers (with space for 9 in some layouts). The M600 SLS is a single‑engine turboprop aimed at owner‑pilots and small corporate trips, generally around 1,400–1,600 nm range with seating typically 4–6 passengers (up to about 6 plus pilot, configuration‑dependent). The Robinson R66 is a light single‑engine turbine helicopter focused on shorter hops and utility missions, usually about 300–400 nm range with capacity around 4 passengers plus pilot. The Sikorsky S‑92 is a heavy, twin‑engine helicopter used for offshore, VIP, and SAR roles, offering substantially greater lift than the R66 with typical range around 500–600 nm and passenger capacity commonly in the high‑teens (often about 19), depending on interior and mission equipment.
| 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 |