Pilatus Pc 24 vs Robinson R66 vs Sikorsky S 92
The Pilatus PC-24 is a twin‑engine light business jet designed for fast point‑to‑point travel. It typically offers a range on the order of about 2,000 nautical miles depending on payload and conditions, and it commonly seats around 6 to 10 passengers in executive layouts. The Robinson R66 is a single‑engine light helicopter aimed at short, flexible missions with vertical access to tight landing areas. Its typical range is roughly 300 to 350 nautical miles, and it generally carries a pilot plus about 4 passengers (around 5 seats total). The Sikorsky S‑92 is a large, twin‑engine medium helicopter built for demanding offshore, SAR, and heavy passenger transport. Its typical range is roughly 500 to 600 nautical miles (often more with auxiliary fuel and mission tradeoffs), and it is commonly configured for about 19 passengers, with some layouts higher.
| 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 |