Beechcraft King Air 360 Er vs Bell 525 Relentless vs Cessna Citation Xls vs Enstrom 480b
The Beechcraft King Air 360ER is a twin‑turboprop airplane in the utility/business category, typically carrying about 6–9 passengers depending on layout, with long endurance and an approximate range around 1,500–1,800 nautical miles. The Cessna Citation XLS+ is a midsize business jet, generally seating about 7–9 passengers, optimized for faster point‑to‑point travel with an approximate range around 1,800–2,100 nautical miles. The Bell 525 Relentless is a fly‑by‑wire, super‑medium helicopter aimed at corporate and offshore missions, commonly configured for roughly 12–16 passengers (higher in utility layouts), with a typical range on the order of about 500–600 nautical miles. The Enstrom 480B is a light single‑engine helicopter suited to short‑range corporate, utility, or training roles, usually carrying 4–5 people including the pilot, with a typical range roughly around 300–400 nautical miles. Overall, the airplanes offer far greater range and speed, while the helicopters trade range for vertical access and operational flexibility.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 10 |
| Flight Rules | IFR | — |
| Manufacturer | Bell | Cessna Citation |
| Aircraft Name | 525 Relentless | XLS+ |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 |
| Max Cabin Seats | 16 | 9 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 7540 |
| Standard Cabin Seats | 16 | 8 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 430 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 |
| DOC / nm | — | $ 5.34 |
| DOC / nm / Seat | — | $ 0.67 |
| Direct Operating Cost | — | $ 2,303 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 10 |
| Max Cabin Seats | 16 | 9 |
| Standard Cabin Seats | 16 | 8 |
| 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 |
| Model | CT7-2F1 | PW545C |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | 5000 |
| Horsepower | 1800 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 641 | — |
| Flat Rating | — | ISA + 10 |
| Thrust (lbs) | — | 4119 |
| Dimensions | ||
| Width (ft) | 25.77 | — |
| Length (ft) | 61.58 | 52.5 |
| 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 |
| Rotor Diameter (ft) | 54.5 | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 |
| 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 |