-
TR
- Türkiye
Gulfstream G650
“Farther Faster, First of its Kind”
The G650 – Speed and grace paired with style and comfort.Enjoy The World Standard™ at its best.
Innovation and excellence have taken flight in the Gulfstream G650.
Gulfstream engineers partnered with a customer advisory board to envision an aircraft that would set a new standard in business travel. Working from that input, engineers rejected the status quo with a clean-sheet design. They pushed for more performance in every aspect. With the G650’s long, unfettered wing, they redefined how air flows over an aircraft wing, creating a highly efficient airfoil that delivers speed and an incredibly smooth ride.
What Gulfstream delivers in the G650 is a jet that flies at more than 92 percent of the speed of sound for thousands of miles with fly-by-wire precision. That same design innovation created a quieter, roomier, more adaptable cabin teeming with advanced technology.
| Performance | |
|---|---|
| Maximum Range * | 12,964 km |
| High-Speed | Mach 0.90 |
| Long-Range | Mach 0.85 |
| Maximum Operating Mach number | Mach 0.925 |
| Takeoff Distance | 1.786 m |
| Initial Cruise Altitude | 12,497m |
| Maximum Cruise Altitude | 15,545m |
| * NBAA IFR theoretical range. Actual range will be affected by ATC routing,> operating speed, weather, outfitting options and other factors |
| External Dimensions | |
|---|---|
| Lenght | 30.41 m |
| Overall Span | 30.36 m |
| Height | 7.82 m |
| Interior | |
| Total Interior Length | 16.33 m |
| Cabin Length (excluding baggage) |
14.27 m |
| Cabin Height | 1.96 m |
| Cabin Width | 2.59 m |
| Cabin Volume | 60.54 cu m |
| Baggage Compartment (usable volume) |
5.52 cu m |
| Weights | |
|---|---|
| Maximum take off | 45,178 Kg |
| Maximum landing | 37,875 Kg |
| Maximum zero fuel | 27,442 Kg |
| Basic Operating (including 4 crew*) |
24,494 Kg |
| Maximum Payload* | 2,948 Kg |
| Payload with Maximum Fuel* | 816 Kg |
| Maximum Fuel* | 20,049 Kg |
| * Standard weights are based on theoretical standard outfitting configurations. Actual weights will be affected by outfitting options and other factors) |
|
| Design Standards | |
|---|---|
| Avionics | Gulfstream PlaneView™ II |
| Engines | Two Rolls-Royce BR725 A1-12 |
| Rated Takeoff Thrust (each) |
75.20 kN |
| Passengers | Up to 19 |