Cessna Citation Xls vs Leonardo Aw189 vs Sikorsky S 92
The Cessna Citation XLS+ is a fixed‑wing business jet, optimized for fast point‑to‑point travel between airports. It typically carries about 7–9 passengers and offers a practical range around 2,000 nautical miles, making it well suited to medium‑distance regional missions where runway access is available. The Agusta/Leonardo AW189 is a twin‑engine medium helicopter designed for offshore, search and rescue, and utility transport. It commonly seats roughly 16–19 passengers depending on configuration, and its range is generally on the order of 450–500 nautical miles, trading speed and distance for vertical lift and the ability to operate without runways. The Sikorsky S‑92 is a larger twin‑engine medium‑heavy helicopter widely used for offshore transport and SAR. It typically carries about 19 passengers in offshore seating and offers a broadly similar helicopter-class range, often around 500 nautical miles. Compared with the AW189, the S‑92 emphasizes higher payload and cabin volume, while the XLS+ leads decisively in speed and range but cannot match helicopter access to remote sites.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 10 | 21 | 21 |
| Manufacturer | Cessna Citation | Leonardo | Sikorsky |
| Aircraft Name | XLS+ | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 9 | 19 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | — | 7417 |
| Standard Cabin Seats | 8 | 19 | 19 |
| Direct Operating Cost | $ 2,303 | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS | EFIS |
| Max Cruise Speed (ktas) | 430 | 155 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | No | — | — |
| Jump Seat | No | — | — |
| Total Seats | 10 | 21 | 21 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 9 | 19 | 19 |
| Lavatory Location | AFT | — | — |
| Cabin Pressure (psi) | 9.3 | — | — |
| Galley / Refreshment | Galley | — | — |
| Standard Cabin Seats | 8 | 19 | 19 |
| SL Cabin Altitude (ft) | 25230 | — | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PW545C | CT7-2E1 | CT7-8A |
| TBO (hrs) | 5000 | 4000 | 4000 |
| Flat Rating | ISA + 10 | — | — |
| Thrust (lbs) | 4119 | — | — |
| No. of Engines | 2 | 2 | 1 |
| Fuel Type | — | JetFuel | JetFuel |
| Horsepower | — | 1983 | 2520 |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 52.5 | 57.8 | — |
| Wingspan (ft) | 56.3 | — | — |
| Aisle Step (ft) | 0.7 | — | — |
| Cabin Width (ft) | 5.5 | — | — |
| Cabin Height (ft) | 5.7 | — | — |
| Cabin Length (ft) | 18.5 | — | — |
| Overall Height (ft) | 17.2 | 16.6 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | — | — |
| Cabin Length - Seating (ft) | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | 85 | 140 |
| Baggage Volume Int. (cu. ft) | 10 | — | — |
| Rotor Diameter (ft) | — | 48 | — |
| Cabin Volume (cu. ft) | — | 395 | 775 |