Maximum Landing Weight 32,700 lb / 14,832 kg
Maximum Zero Fuel Weight 28,200 lb / 12,791 kg
Basic Operating Weight (including 2 crew)** 24,150 lb / 10,954 kg
Maximum Payload** 4,050 lb / 1,837 kg
Payload with Maximum Fuel** 1,000 lb / 454 kg
Maximum Fuel Weight 14,600 lb / 6,622 kg
DESIGN STANDARDS
Avionics Gulfstream PlaneView280.
Engines Two Honeywell HTF7250G
Rated Takeoff Thrust (each) 7,445 lb / 33 kN
Passengers: Typical Outfitting 8–10
66 ft 10 in / 20.37 m
INTERIOR
Total Interior Length 32 ft 3 in / 9.83 m
Cabin Length (excluding baggage) 25 ft 10 in / 7.87 m
Cabin Height 6 ft 3 in / 1.91 m
Cabin Width 7 ft 2 in / 2.18 m
Cabin Volume 935 cu ft / 26.5 cu m
Total Baggage Volume (interior and exterior) 154 cu ft / 4.4 cu m
COMFORT
19 Large Oval Windows
Forward Galley
Aft Lavatory
3 Select Floorplans
21 ft 4 in / 6.50 m
* NBAA IFR theoretical range. Actual range will be affected by ATC routing, operating speed, weather, outfitting options and other factors. ** Stated weights are based on theoretical standard outfitting configurations. Actual
800.810.GULF (4853) GULFstream.com
weights will be affected by outfitting options and other factors.
. 2011 Gulfstream Aerospace Corporation 11.10298 04.11.1M GS335E_V2 English
G280_ProductBrochure_English 產(chǎn)品宣傳冊英文
The World Standard.
Since 1958, when the Gulfstream I. was introduced as the world’s first purpose-built business airplane, we have manufactured, serviced and supported more than 1,800 jet aircraft.
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