Beechcraft King Air 360 Er vs Bell 525 Relentless vs Cessna Citation Xls vs Leonardo Aw189
The Beechcraft King Air 360ER and the Cessna Citation XLS+ are fixed‑wing aircraft, while the Bell 525 Relentless and Leonardo AW189 are helicopters, so their “range” and “capacity” reflect different mission profiles. The King Air 360ER is a twin‑turboprop optimized for long, flexible regional legs; it offers the longest endurance of this group and typically carries about 6–9 passengers in an executive layout. The Citation XLS+ is a super‑midsize business jet focused on faster point‑to‑point travel; it generally seats about 7–9 passengers and delivers a solid jet range suited to transcontinental-style business missions, though usually less endurance than the 360ER. The Bell 525 Relentless is a fly‑by‑wire, long‑range medium helicopter; it typically carries roughly 12–16 passengers depending on configuration and prioritizes offshore, VIP, and utility missions with strong helicopter range. The Leonardo AW189 is a super‑medium helicopter in a similar offshore/utility class; it commonly accommodates about 16–19 passengers and offers comparable long‑range rotorcraft performance, trading some speed and range versus fixed‑wing for vertical lift and access.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Cessna Citation | Leonardo |
| Aircraft Name | 525 Relentless | XLS+ | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 651 |
| Max Cabin Seats | 16 | 9 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | — |
| Standard Cabin Seats | 16 | 8 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 160 | 430 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $2,413,000 |
| DOC / nm | — | $ 5.34 | $ 15.57 |
| DOC / nm / Seat | — | $ 0.67 | $ 0.74 |
| Direct Operating Cost | — | $ 2,303 | $ 2,413 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 21 |
| Max Cabin Seats | 16 | 9 | 19 |
| Standard Cabin Seats | 16 | 8 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | — |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW545C | CT7-2E1 |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 5000 | 4000 |
| Horsepower | 1800 | — | 1983 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 52.5 | 57.8 |
| Cabin Width (ft) | 7.58 | 5.5 | — |
| Cabin Height (ft) | 4.5 | 5.7 | — |
| Cabin Length (ft) | 15.5 | 18.5 | — |
| Overall Height (ft) | 18.18 | 17.2 | 16.6 |
| Rotor Diameter (ft) | 54.5 | — | 48 |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | 85 |
| Wingspan (ft) | — | 56.3 | — |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | — |
| Cabin Volume (cu. ft) | — | — | 395 |