Beechcraft King Air 360 Er vs Gulfstream G700 vs Leonardo Aw189 vs Robinson R66
The Beechcraft King Air 360ER is a pressurized twin‑turboprop airplane best suited to regional missions, typically offering a few hours of endurance and an approximate range on the order of 1,500–2,000 nautical miles depending on payload and conditions, with passenger capacity commonly around 6–9. The Gulfstream G700 is an ultra‑long‑range business jet designed for intercontinental travel, roughly in the 7,000+ nautical mile class, and usually carries about 10–19 passengers in a high‑comfort cabin. The Leonardo (Agusta) AW189 is a medium twin‑engine helicopter optimized for offshore, SAR, and utility roles, with practical range generally a few hundred nautical miles (often extended with auxiliary tanks) and seating typically around 12–16. The Robinson R66 is a light single‑engine turbine helicopter for short‑range transport and training, usually in the 300–400 nautical mile range with about 4–5 seats including the pilot.
| Spec | Gulfstream G700 | AGUSTA / LEONARDO AW189 |
|---|---|---|
| Summary | ||
| Cockpit | 3 | 2 |
| Min Crew | 4 | 1 |
| Total Seats | 16 | 21 |
| Manufacturer | Gulfstream | Leonardo |
| Aircraft Name | G700 | AW189 |
| Certification | In Development | FAA / EASA |
| Max Range (nm) | 7500 | 651 |
| Max Cabin Seats | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 12 | 19 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 |
| Base Aircraft Price (USD) | $78,000,000 | $2,413,000 |
| DOC / nm | — | $ 15.57 |
| Flight Rules | — | IFR |
| DOC / nm / Seat | — | $ 0.74 |
| Direct Operating Cost | — | $ 2,413 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 4 | 1 |
| Crew Rest | Optional | — |
| Jump Seat | Yes | — |
| Total Seats | 16 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 19 | 19 |
| Lavatory Location | FWD / AFT | — |
| Standard Cabin Seats | 12 | 19 |
| Engine | ||
| Model | Pearl 700 | CT7-2E1 |
| TBO (hrs) | On Condition | 4000 |
| Thrust (lbs) | 18250 | — |
| No. of Engines | 2 | 2 |
| FADEC | — | Yes |
| Fuel Type | — | JetFuel |
| Horsepower | — | 1983 |
| 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 |
| Baggage Volume Int. (cu. ft) | 195 | — |
| Rotor Diameter (ft) | — | 48 |
| Cabin Volume (cu. ft) | — | 395 |
| Baggage Volume Ext. (cu. ft) | — | 85 |