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TR
- Türkiye
Gulfstream 550
“Legendary Quality, Flexible Performance”
The Gulfstream G550 has earned many admirers, whether by winning the prestigious Robert J. Collier Trophy or by being named by owners as the best-in-value business aircraft.
The G550 has the efficiency to fly 6,750 nautical miles/12,501 kilometers nonstop, but also is capable of operating out of short-field, high-altitude airports. Payload is a plus, too. The G550 can transport up to 19 passengers and still has the range to fly nonstop more than 12 hours.
The G550’s quiet interior also improves the cabin experience. Advanced sound suppression techniques keep engine noise outside the aircraft. Gulfstream G550 offers flexible cabin design to satisfy a variety of travel needs. Some layouts accommodate beds for eight people, and the option of up to four distinct living areas creates a combination of uses, including a dedicated crew rest area, a private stateroom, conference area and entertainment space. The G550 also provides the option of locating the full-size galley forward or aft―the only aircraft in its class to offer such flexibility.
Performance | |
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Maximum Range * | 12,501 km |
High-Speed | Mach 0.85 |
Long-Range | Mach 0.80 |
Maximum Operating Mach number | Mach 0.885 |
Takeoff Distance | 1.801 m |
Landing Distance | 844 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 | |
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Lenght | 29.39 m |
Overall Span | 28.50 m |
Height | 7.87 m |
Interior | |
Total Interior Length | 15.27 m |
Cabin Length (excluding baggage) |
13.39 m |
Cabin Height | 1.88 m |
Cabin Width | 2.24 m |
Cabin Volume | 47.26 cu m |
Baggage Compartment (usable volume) |
4.81 cu m |
Weights | |
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Maximum take off | 41,277 Kg |
Maximum landing | 34,156 Kg |
Maximum zero fuel | 24,721 Kg |
Basic Operating (including 4 crew*) |
21,909 Kg |
Maximum Payload* | 2,812 Kg |
Payload with Maximum Fuel* | 816 Kg |
Maximum Fuel* | 18,733 Kg |
* Standard weights are based on theoretical standard outfitting configurations. Actual weights will be affected by outfitting options and other factors) |
Design Standards | |
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Avionics | Gulfstream PalneView |
Engines | Two Rolls-Royce BR710 C4-11 |
Rated Takeoff Thrust (each) |
68.40 kN |
Passengers | Up to 19 |