Beechcraft King Air 360 Er vs Cessna Citation Xls vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop airplane typically used for regional missions and short, unimproved, or smaller runways. It offers long endurance for its class, with typical range around 1,500–1,800 nautical miles depending on payload and reserves, and usually seats about 6–9 passengers in an executive layout. The Cessna Citation XLS+ is a light/midsize business jet optimized for faster point‑to‑point travel and higher cruise altitudes. It generally carries about 7–9 passengers and has a typical range around 1,800–2,100 nautical miles, again varying with conditions. Compared with the King Air, it’s faster and more jet‑like in ride and altitude capability, but it needs more conventional runway infrastructure. The Sikorsky S‑92 is a large twin‑engine helicopter aimed at offshore transport, SAR, and utility/VIP roles. Its range is typically about 500–600 nautical miles (mission‑dependent), but it can move more people, commonly 12–19 passengers, and excels where vertical lift and access to helipads are decisive.
| Spec | Cessna Citation XLS+ | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 5.34 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 10 | 21 |
| Manufacturer | Cessna Citation | Sikorsky |
| Aircraft Name | XLS+ | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.94 |
| Max Cabin Seats | 9 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | 7417 |
| Standard Cabin Seats | 8 | 19 |
| Direct Operating Cost | $ 2,303 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 430 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $30,650,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — |
| Min Crew | 2 | 2 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 10 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 9 | 19 |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 9.3 | — |
| Galley / Refreshment | Galley | — |
| Standard Cabin Seats | 8 | 19 |
| SL Cabin Altitude (ft) | 25230 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW545C | CT7-8A |
| TBO (hrs) | 5000 | 4000 |
| Flat Rating | ISA + 10 | — |
| Thrust (lbs) | 4119 | — |
| No. of Engines | 2 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 52.5 | — |
| 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 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | — |
| Cabin Length - Seating (ft) | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | 80 | 140 |
| Baggage Volume Int. (cu. ft) | 10 | — |
| Cabin Volume (cu. ft) | — | 775 |