Beechcraft King Air 360 Er vs Gulfstream G700 vs Leonardo Aw189 vs Sikorsky S 92
The Beechcraft King Air 360ER is a pressurized twin‑turboprop fixed‑wing aircraft suited to regional missions and shorter runways, offering roughly 1,500 nautical miles of range and typically carrying about 6–9 passengers in executive layouts (up to around 11 depending on configuration). The Gulfstream G700 is an ultra‑long‑range business jet in a different class, designed for intercontinental travel with about 7,500 nautical miles of range and commonly seating 12–19 passengers (higher-density options possible). The Leonardo AW189 is a super‑medium twin‑engine helicopter optimized for offshore, SAR, and utility/VIP roles; its practical range is typically around 450–500 nautical miles, with passenger capacity usually about 16–19 depending on mission fit. The Sikorsky S‑92 is a larger heavy helicopter used widely for offshore transport and SAR, generally offering roughly 500+ nautical miles of range and commonly carrying about 19 passengers (higher capacity possible in some layouts). Overall, the G700 leads in range and cruise speed, the King Air balances efficiency and access, and the AW189 and S‑92 prioritize vertical lift and mission flexibility over distance.
| Spec | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 3 | 2 | 2 |
| Min Crew | 4 | 1 | 2 |
| Total Seats | 16 | 21 | 21 |
| Manufacturer | Gulfstream | Leonardo | Sikorsky |
| Aircraft Name | G700 | AW189 | S-92 |
| Certification | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7500 | 651 | 439 |
| Max Cabin Seats | 19 | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Standard Cabin Seats | 12 | 19 | 19 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | EFIS | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 | 155 |
| Base Aircraft Price (USD) | $78,000,000 | $2,413,000 | $30,650,000 |
| DOC / nm | — | $ 15.57 | $ 19.79 |
| Flight Rules | — | IFR | IFR |
| DOC / nm / Seat | — | $ 0.74 | $ 0.94 |
| Direct Operating Cost | — | $ 2,413 | $ 3,068 |
| Useful Load (lbs) | — | — | 7417 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 2 |
| Crew Rest | Optional | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 16 | 21 | 21 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 19 | 19 | 19 |
| Lavatory Location | FWD / AFT | — | — |
| Standard Cabin Seats | 12 | 19 | 19 |
| Engine | |||
| Model | Pearl 700 | CT7-2E1 | CT7-8A |
| TBO (hrs) | On Condition | 4000 | 4000 |
| Thrust (lbs) | 18250 | — | — |
| No. of Engines | 2 | 2 | 1 |
| FADEC | — | Yes | Yes |
| Fuel Type | — | JetFuel | JetFuel |
| Horsepower | — | 1983 | 2520 |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 109.9 | 57.8 | — |
| Wingspan (ft) | 103 | — | — |
| Aisle Step (ft) | Flat Floor | — | — |
| Cabin Width (ft) | 8.2 | — | — |
| Cabin Height (ft) | 6.25 | — | — |
| Cabin Length (ft) | 56.9 | — | — |
| Overall Height (ft) | 25.4 | 16.6 | 17.8 |
| Baggage Volume Int. (cu. ft) | 195 | — | — |
| Rotor Diameter (ft) | — | 48 | — |
| Cabin Volume (cu. ft) | — | 395 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 85 | 140 |