Cessna Citation Xls vs Dassault Falcon 8x vs Leonardo Aw189 vs Sikorsky S 92
The Cessna Citation XLS+ and Dassault Falcon 8X are business jets, while the Leonardo AW189 and Sikorsky S-92 are medium and heavy twin‑engine helicopters used for offshore, VIP, and utility missions. The Citation XLS+ is a super‑midsize jet optimized for regional and transcontinental trips, typically carrying about 7–9 passengers with a range around 2,100 nautical miles. The Falcon 8X is a large‑cabin, ultra‑long‑range jet designed for intercontinental missions, commonly configured for roughly 12–16 passengers and capable of about 6,450 nautical miles. By contrast, helicopters trade speed and range for vertical access: the AW189 generally seats about 16–19 passengers (depending on layout) with a typical range on the order of 450 nautical miles, while the larger S-92 often carries about 19 passengers in transport layouts and offers a similar typical range around 500 nautical miles. Overall, the Falcon 8X dominates long‑distance range, the XLS+ suits shorter jet missions, and the AW189 and S-92 provide access to places without runways with comparable, shorter-range profiles.
| Spec | Cessna Citation XLS+ | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 7.66 | $ 15.57 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 10 | 17 | 21 | 21 |
| Manufacturer | Cessna Citation | Dassault Falcon | Leonardo | Sikorsky |
| Aircraft Name | XLS+ | 8X | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 6450 | 651 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.64 | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 9 | 16 | 19 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | 36900 | — | 7417 |
| Standard Cabin Seats | 8 | 14 | 19 | 19 |
| Direct Operating Cost | $ 2,303 | $ 3,805 | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | EFIS | EFIS |
| Max Cruise Speed (ktas) | 430 | 516 | 155 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $ 62,500,000 | $2,413,000 | $30,650,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | 2 Enclosed Flushing | — | — |
| Min Crew | 2 | 2 | 1 | 2 |
| Crew Rest | No | No | — | — |
| Jump Seat | No | Yes | — | — |
| Total Seats | 10 | 17 | 21 | 21 |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 9 | 16 | 19 | 19 |
| Lavatory Location | AFT | FWD / AFT | — | — |
| Cabin Pressure (psi) | 9.3 | 10.2 | — | — |
| Galley / Refreshment | Galley | Galley | — | — |
| Standard Cabin Seats | 8 | 14 | 19 | 19 |
| SL Cabin Altitude (ft) | 25230 | 29200 | — | — |
| Max Cabin Altitude (ft) | — | 3900 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW545C | PW307D | CT7-2E1 | CT7-8A |
| TBO (hrs) | 5000 | On-Condition | 4000 | 4000 |
| Flat Rating | ISA + 10 | ISA + 17 | — | — |
| Thrust (lbs) | 4119 | 6722 | — | — |
| No. of Engines | 2 | 3 | 2 | 1 |
| Fuel Type | — | — | JetFuel | JetFuel |
| Horsepower | — | — | 1983 | 2520 |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 52.5 | 80.2 | 57.8 | — |
| 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 | — | — |
| Overall Height (ft) | 17.2 | 26.1 | 16.6 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | 6.3 | — | — |
| Cabin Length - Seating (ft) | 14.3 | 29.2 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | 85 | 140 |
| Baggage Volume Int. (cu. ft) | 10 | 140 | — | — |
| Cabin Volume (cu. ft) | — | 1695 | 395 | 775 |
| Rotor Diameter (ft) | — | — | 48 | — |