Airbus Helicopters H225 vs Cessna Citation Xls vs Dassault Falcon 8x vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are twin‑engine heavy helicopters, typically used for offshore energy support, search and rescue, and VIP shuttle missions where vertical access matters more than speed. Both generally carry around 16–19 passengers in high‑density layouts (often fewer for VIP) and offer practical ranges on the order of roughly 500–600 nautical miles, varying with payload and reserves. The Cessna Citation XLS+ is a super‑midsize business jet aimed at efficient short‑to‑mid range travel, commonly seating about 7–9 passengers in a standard executive cabin (up to around 12 with alternate layouts). Its range is roughly about 2,000 nautical miles, suited to regional and some transcontinental missions. The Dassault Falcon 8X is an ultra‑long‑range large‑cabin trijet designed for intercontinental flying, typically carrying 12–16 passengers in comfort (more in high‑density). Its range is about 6,450 nautical miles, enabling nonstop city pairs that the XLS+ cannot, while offering far greater cabin space than both the XLS+ and the helicopters.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Dassault Falcon 8X | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 7.66 | $ 19.79 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 17 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Dassault Falcon | Sikorsky |
| Aircraft Name | H225 | XLS+ | 8X | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 6450 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.64 | $ 0.94 |
| Max Cabin Seats | 28 | 9 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 36900 | 7417 |
| Standard Cabin Seats | 19 | 8 | 14 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 3,805 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 62,500,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 17 | 21 |
| Max Cabin Seats | 28 | 9 | 16 | 19 |
| Standard Cabin Seats | 19 | 8 | 14 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | 2 Enclosed Flushing | — |
| Crew Rest | — | No | No | — |
| Jump Seat | — | No | Yes | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | AFT | FWD / AFT | — |
| Cabin Pressure (psi) | — | 9.3 | 10.2 | — |
| Galley / Refreshment | — | Galley | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | 29200 | — |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | PW307D | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | On-Condition | 4000 |
| Horsepower | 2100 | — | — | 2520 |
| No. of Engines | 2 | 2 | 3 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 10 | ISA + 17 | — |
| Thrust (lbs) | — | 4119 | 6722 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 80.2 | — |
| Overall Height (ft) | 16.3 | 17.2 | 26.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | 775 |
| Wingspan (ft) | — | 56.3 | 86.3 | — |
| Aisle Step (ft) | — | 0.7 | — | — |
| Cabin Width (ft) | — | 5.5 | 7.7 | — |
| Cabin Height (ft) | — | 5.7 | 6.2 | — |
| Cabin Length (ft) | — | 18.5 | 42.7 | — |
| Cabin Width - Floor (ft) | — | 3.9 | 6.3 | — |
| Cabin Length - Seating (ft) | — | 14.3 | 29.2 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | 140 |
| Baggage Volume Int. (cu. ft) | — | 10 | 140 | — |