Beechcraft King Air 360 Er vs Cessna Citation Xls vs Enstrom 480b vs Leonardo Aw189
The Beechcraft King Air 360ER is a pressurized twin‑turboprop airplane suited to regional and remote operations, offering long endurance for its class with a typical range around 1,800–2,000 nautical miles and usually carrying about 6–9 passengers depending on configuration. The Cessna Citation XLS+ is a midsize business jet optimized for faster point‑to‑point travel; it generally carries 7–9 passengers and delivers roughly 1,800–2,100 nautical miles of range, trading turboprop field flexibility for higher cruise speed and jet cabin refinement. The Enstrom 480B is a light single‑engine helicopter aimed at utility, training, and short‑range transport, typically seating 4–5 people with practical range commonly in the 250–350 nautical mile area. The Leonardo AW189 is a medium twin‑engine helicopter designed for offshore, SAR, and utility missions; it can seat around 16–19 passengers in transport layouts, with range typically about 450–550 nautical miles (mission‑dependent). Overall, the Citation prioritizes speed, the King Air balances range and access, and the helicopters emphasize vertical lift and mission flexibility.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 |
| Min Crew | 2 | 1 |
| Total Seats | 10 | 21 |
| Manufacturer | Cessna Citation | Leonardo |
| Aircraft Name | XLS+ | AW189 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 |
| Max Cabin Seats | 9 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | — |
| Standard Cabin Seats | 8 | 19 |
| Direct Operating Cost | $ 2,303 | $ 2,413 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 430 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — |
| Min Crew | 2 | 1 |
| 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 | CT7-2E1 |
| TBO (hrs) | 5000 | 4000 |
| Flat Rating | ISA + 10 | — |
| Thrust (lbs) | 4119 | — |
| No. of Engines | 2 | 2 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 1983 |
| 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 |
| Cabin Width - Floor (ft) | 3.9 | — |
| Cabin Length - Seating (ft) | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | 80 | 85 |
| Baggage Volume Int. (cu. ft) | 10 | — |
| Rotor Diameter (ft) | — | 48 |
| Cabin Volume (cu. ft) | — | 395 |