Beechcraft King Air 360 Er vs Bell 525 Relentless vs Bombardier Global 7500 vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop airplane in the light business/utility category. It typically carries about 6–9 passengers and offers roughly 1,500–1,800 nautical miles of range depending on payload and conditions, making it suited to regional missions and shorter runways. The Bell 525 Relentless is a super‑medium helicopter focused on offshore and executive transport. Cabin layouts vary, but it commonly accommodates about 12–16 passengers, with a typical range around 500–600 nautical miles, emphasizing point‑to‑point access where runways are unavailable. The Bombardier Global 7500 is an ultra‑long‑range business jet. It’s usually configured for about 8–19 passengers and provides around 7,700 nautical miles of range, targeting intercontinental nonstop flights at high speed and altitude. The Sikorsky S‑92 is a heavy helicopter widely used for offshore and SAR/VIP roles. It generally seats about 19 passengers and offers roughly 500–600 nautical miles of range, prioritizing lift, all‑weather capability, and overwater operations rather than long nonstop distance.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 18 | 14 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Bombardier | Sikorsky |
| Aircraft Name | 525 Relentless | Global 7500 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 439 |
| Max Cabin Seats | 16 | 19 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — | 7417 |
| Standard Cabin Seats | 16 | 12 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | EFIS |
| Max Cruise Speed (ktas) | 160 | 516 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $30,650,000 |
| DOC / nm | — | $ 9.50 | $ 19.79 |
| Aircraft Type | — | Business Jet | — |
| DOC / nm / Seat | — | $ 0.79 | $ 0.94 |
| Direct Operating Cost | — | $ 4,900 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 18 | 14 | 21 |
| Max Cabin Seats | 16 | 19 | 19 |
| Standard Cabin Seats | 16 | 12 | 19 |
| Lavatory | — | 2 Enclosed Flushing | — |
| Crew Rest | — | Yes | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Galley / Refreshment | — | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | Passport | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | On-Condition | 4000 |
| Horsepower | 1800 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | 760 |
| Flat Rating | — | ISA + 15 | — |
| Thrust (lbs) | — | 18920 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 111 | — |
| Cabin Width (ft) | 7.58 | 8 | — |
| Cabin Height (ft) | 4.5 | 6.2 | — |
| Cabin Length (ft) | 15.5 | 54.5 | — |
| Overall Height (ft) | 18.18 | 27 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 140 |
| Wingspan (ft) | — | 104 | — |
| Cabin Volume (cu. ft) | — | — | 775 |