Beechcraft King Air 360 Er vs Enstrom 480b vs Pilatus Pc 24 vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft optimized for efficient regional travel, typically offering roughly 1,500–1,800 nautical miles of range with about 6–9 passengers depending on interior and fuel/load tradeoffs. The Enstrom 480B is a single‑engine light helicopter focused on short‑range utility and training missions; its range is typically only a few hundred nautical miles and it generally carries up to 4–5 people. The Pilatus PC‑24 is a twin‑jet “super versatile jet” designed for faster point‑to‑point trips and operation from shorter or semi‑prepared runways; it commonly provides around 1,900–2,000 nautical miles of range with about 6–10 passengers in executive configurations. The Sikorsky S‑92 is a medium twin helicopter built for offshore transport, SAR, and VIP shuttle roles; it has a medium range (often around 500–600 nautical miles, mission dependent) and the highest capacity here, typically seating about 12–19 passengers depending on layout. Overall, the helicopters trade speed and range for vertical access, while the PC‑24 leads on speed and the S‑92 leads on passenger volume.
| Spec | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.71 | $ 19.79 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 21 |
| Manufacturer | Pilatus | Sikorsky |
| Aircraft Name | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2076 | 439 |
| DOC / nm / Seat | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 10 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6680 | 7417 |
| Standard Cabin Seats | 6 | 19 |
| Direct Operating Cost | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 440 | 155 |
| Base Aircraft Price (USD) | $11,800,000 | $30,650,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | — |
| Min Crew | 1 | 2 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Cargo Door | Yes | — |
| Total Seats | 6 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 10 | 19 |
| Lavatory Location | FWD | — |
| Cabin Pressure (psi) | 9.3 | — |
| Galley / Refreshment | Optional Refreshment Center | — |
| Standard Cabin Seats | 6 | 19 |
| SL Cabin Altitude (ft) | 23500 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | 5000 | 4000 |
| Flat Rating | ISA + 23 | — |
| Thrust (lbs) | 3435 | — |
| No. of Engines | 2 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 52.2 | — |
| Wingspan (ft) | 55.8 | — |
| Aisle Step (ft) | Flat Floor | — |
| Cabin Width (ft) | 5.6 | — |
| Cabin Height (ft) | 5.1 | — |
| Cabin Length (ft) | 23 | — |
| Overall Height (ft) | 17.4 | 17.8 |
| Cabin Width - Floor (ft) | 3.8 | — |
| Cabin Length - Seating (ft) | 17 | — |
| Baggage Volume Int. (cu. ft) | 90 | — |
| Cabin Volume (cu. ft) | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |