Beechcraft King Air 360 Er vs Bell 525 Relentless vs Cessna Citation Xls vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft best suited to short and medium missions, typically carrying about 6–9 passengers (up to roughly 11 in high‑density layouts) with long endurance for its class, around 1,500–1,800 nautical miles depending on payload and reserves. The Cessna Citation XLS+ is a light/midsize business jet, generally seating 7–9 passengers, optimized for faster point‑to‑point travel with a typical range around 1,800–2,100 nautical miles. The Bell 525 Relentless is a modern super‑medium helicopter aimed at executive and offshore roles, commonly configured for about 12–16 passengers, with range roughly 500–600 nautical miles (higher with auxiliary fuel and lighter loads). The Sikorsky S‑92 is a larger heavy helicopter widely used offshore; it often carries around 16–19 passengers in typical transport seating and has a similar order of range, roughly 500–600 nautical miles, trading speed and runway independence for shorter legs than fixed‑wing aircraft.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 18 | 10 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Cessna Citation | Sikorsky |
| Aircraft Name | 525 Relentless | XLS+ | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 439 |
| Max Cabin Seats | 16 | 9 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | 7417 |
| 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 | $30,650,000 |
| DOC / nm | — | $ 5.34 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.67 | $ 0.94 |
| Direct Operating Cost | — | $ 2,303 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| 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 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 5000 | 4000 |
| Horsepower | 1800 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | 760 |
| 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 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | 140 |
| 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) | — | — | 775 |