Enstrom 480b vs Piaggio Avanti Evo vs Piper M600 Sls vs Sikorsky S 92
The Enstrom 480B is a light single‑engine piston helicopter aimed at short‑range utility flying; it typically carries a pilot plus up to four passengers, with practical range on the order of a few hundred nautical miles depending on reserves and payload. The Piaggio Avanti EVO is a twin‑turboprop, pressurized business aircraft optimized for fast, efficient regional trips; it generally seats six to nine passengers and offers roughly 1,500–1,800 nautical miles of range. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft in a smaller category than the Avanti; it commonly seats five passengers plus a pilot and delivers about 1,400–1,600 nautical miles of range. The Sikorsky S‑92 is a large, twin‑engine transport helicopter used for offshore and VIP/utility missions; it can be configured for roughly 19 passengers (or more in high‑density layouts) with range typically around 500–600 nautical miles. Overall, the fixed‑wing turboprops provide the longest range and higher cruise efficiency, while the helicopters trade range for vertical‑lift access and mission flexibility.
| 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 |