The Gulfstream G280 is a twin-engine business jet built under license by IAI in Israel for Gulfstream Aerospace. It began delivery to users in 2012.
PERFORMANCE
| Maximum Range *(Mach 0.80, 4 passengers, 2 crew and NBAA IFR reserves) | 6,667 km |
| High-Speed | Mach 0.84 |
| Long-Range | Mach 0.80 |
| MMO(maximum operating Mach number) | Mach 0.85 |
| Takeoff Distance(SL, ISA, MTOW) | 1,448 m |
| Landing Distance(SL, ISA, MLW) | 829 m |
| Initial Cruise Altitude | 13,106 m |
| Maximum Cruise Altitude | 13,716 m |
* NBAA IFR theoretical range. Actual range will be affected by ATC routing, operating speed, weather, outfitting options and other factors
WEIGHTS
| Maximum Takeoff | 17,962 kg |
| Maximum Landing | 14,832 kg |
| Maximum Zero Fuel | 12,791 kg |
| Basic Operating(including 2 crew **) | 10,954 kg |
| Maximum Payload ** | 1,837 kg |
| Payload with Maximum Fuel ** | 454 kg |
| Maximum Fuel | 6,622 kg |
** Stated weights are based on theoretical standard outfitting configurations. Actual weights will be affected by outfitting options and other factors.
EXTERNAL DIMENSIONS
| Length | 20.37 m |
| Overall Span | 19.20 m |
| Height | 6.50 m |
INTERIOR
| Total Interior Length | 9.83 m |
| Cabin Length(excluding baggage) | 7.87 m |
| Cabin Height | 1.91 m |
| Cabin Width | 2.18 m |
| Cabin Volume | 26.50 cu m |
| Baggage Compartment(usable volume) | 3.40 cu m |
DESIGN STANDARDS
| Avionics | Gulfstream PlaneView280™ |
| Engines | Two Honeywell HTF7250G |
| Rated Takeoff Thrust(each) | 33.90 kN |
| Passengers | Up to 10 |
Info :
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