Airbus Helicopters H225 vs Dassault Falcon 8x vs Pilatus Pc 24 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters built for offshore transport, search and rescue, and utility missions rather than point‑to‑point business travel. Both typically offer roughly 450–550 nautical miles of range depending on payload and reserves, and they can carry about 19 passengers in high‑density configurations (often fewer in VIP layouts), emphasizing vertical access over speed. The Dassault Falcon 8X is a long‑range, three‑engine business jet optimized for intercontinental trips. It offers around 6,450 nautical miles of range and is usually configured for about 12–16 passengers in an executive cabin, trading vertical capability for high cruise speed and global reach. The Pilatus PC‑24 is a versatile “light jet” designed for short and medium missions, including operation from shorter or less‑prepared runways. Its range is about 2,000 nautical miles (varies with load), and it typically seats 6–10 passengers in executive layouts, with higher‑density options available.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 6 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Pilatus | Sikorsky |
| Aircraft Name | H225 | 8X | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 2076 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 28 | 16 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 36900 | 6680 | 7417 |
| Standard Cabin Seats | 19 | 14 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 440 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $11,800,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 6 | 21 |
| Max Cabin Seats | 28 | 16 | 10 | 19 |
| Standard Cabin Seats | 19 | 14 | 6 | 19 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Flushing | — |
| Crew Rest | — | No | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | FWD | — |
| Cabin Pressure (psi) | — | 10.2 | 9.3 | — |
| Galley / Refreshment | — | Galley | Optional Refreshment Center | — |
| SL Cabin Altitude (ft) | — | 29200 | 23500 | — |
| Max Cabin Altitude (ft) | — | 3900 | — | — |
| Cargo Door | — | — | Yes | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 5000 | 4000 |
| Horsepower | 2100 | — | — | 2520 |
| No. of Engines | 2 | 3 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 17 | ISA + 23 | — |
| Thrust (lbs) | — | 6722 | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 52.2 | — |
| Overall Height (ft) | 16.3 | 26.1 | 17.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — | 775 |
| Wingspan (ft) | — | 86.3 | 55.8 | — |
| Cabin Width (ft) | — | 7.7 | 5.6 | — |
| Cabin Height (ft) | — | 6.2 | 5.1 | — |
| Cabin Length (ft) | — | 42.7 | 23 | — |
| Cabin Width - Floor (ft) | — | 6.3 | 3.8 | — |
| Cabin Length - Seating (ft) | — | 29.2 | 17 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 90 | — |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |