Enstrom 480b vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Sikorsky S 92
The Enstrom 480B is a light single‑engine piston helicopter aimed at utility and short‑hop missions. Its range is typically on the order of a few hundred nautical miles, and passenger capacity is small, generally one pilot plus up to four passengers depending on configuration and fuel load. The Piaggio Avanti EVO is a twin‑turboprop business aircraft in the light/midsize executive category. It offers substantially longer range—roughly in the 1,000–1,700 nautical mile class—and typically carries about six to eight passengers in a pressurized cabin. The Pilatus PC‑24 is a twin‑engine light business jet designed for versatile operations, including shorter and less‑improved runways. It generally provides range comparable to or greater than the Avanti—about 1,800–2,000 nautical miles depending on payload—and usually seats around six to ten passengers. The Sikorsky S‑92 is a large twin‑engine helicopter built for offshore transport and heavy utility/VIP roles. Its range is typically several hundred nautical miles (often around 500+), and it can carry far more people than the Enstrom, commonly around 12–19 passengers in airline/offshore layouts (VIP fits vary).
| Spec | Piaggio Avanti EVO | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 8 | 6 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Piaggio | Pilatus | Sikorsky |
| Aircraft Name | Avanti EVO | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 2076 | 439 |
| Max Cabin Seats | 7 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3775 | 6680 | 7417 |
| Standard Cabin Seats | 6 | 6 | 19 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 400 | 440 | 155 |
| Base Aircraft Price (USD) | $ 7,695,000 | $11,800,000 | $30,650,000 |
| DOC / nm | — | $ 3.71 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.62 | $ 0.94 |
| Direct Operating Cost | — | $ 1,619 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing | — |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 8 | 6 | 21 |
| Max Cabin Seats | 7 | 10 | 19 |
| Cabin Pressure (psi) | 9 | 9.3 | — |
| Galley / Refreshment | No | Optional Refreshment Center | — |
| Standard Cabin Seats | 6 | 6 | 19 |
| SL Cabin Altitude (ft) | 24000 | 23500 | — |
| Max Cabin Altitude (ft) | 6600 | — | — |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Cargo Door | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A–66B | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | 3600 | 5000 | 4000 |
| Horsepower | 850 | — | 2520 |
| Flat Rating | ISA + 28 | ISA + 23 | — |
| No. of Engines | 2 | 2 | 1 |
| Fuel Burn (gph) | 100 | — | — |
| Thrust (lbs) | — | 3435 | — |
| Fuel Type | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 47.3 | 52.2 | — |
| Wingspan (ft) | 47.1 | 55.8 | — |
| Cabin Width (ft) | 6.1 | 5.6 | — |
| Cabin Height (ft) | 5.8 | 5.1 | — |
| Cabin Length (ft) | 14.9 | 23 | — |
| Overall Height (ft) | 13.1 | 17.4 | 17.8 |
| Cabin Width - Floor (ft) | 3.5 | 3.8 | — |
| Baggage Volume Int. (cu. ft) | 35.2 | 90 | — |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Length - Seating (ft) | — | 17 | — |
| Cabin Volume (cu. ft) | — | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |