Beechcraft King Air 360 Er vs Cessna Citation Xls vs Leonardo Aw189 vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop airplane typically used for regional missions; it generally offers the longest endurance among the fixed‑wing options here, with range on the order of roughly 1,500–1,800+ nautical miles depending on load, and it commonly carries about 6–9 passengers in executive layouts. The Cessna Citation XLS+ is a midsize business jet focused on higher cruise speed and comfort; its typical range is about 1,800–2,100 nautical miles, and it usually seats around 7–9 passengers (often up to 9) depending on configuration. The Leonardo AW189 is a large twin‑engine helicopter aimed at offshore and utility/VIP transport; helicopter range is more mission‑dependent, but it is commonly roughly 450–500+ nautical miles, and it can seat about 16–19 passengers in high‑density layouts (fewer for VIP). The Sikorsky S‑92 is a heavy twin helicopter widely used offshore; typical range is roughly 500–600+ nautical miles, and it generally carries about 19 passengers in offshore configuration (variable by interior).
| 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 |