|Lift type||Fixed wing|
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The three forward sections - wing carry through, rear and aft - are all aluminium.
The radome is glass epoxy with a Nomex core. The avionics bay doors are carbon fibre and Nomex. The tailcone bulkhead is titanium.
The fuselage is based on that of the G200 with the fuselage fuel tank deleted to increase interior space.
The T tail has sweptback surfaces and the transonic wing has winglets. Dual hydraulic systems actuate rudder and elevators, and two hydraulic accumulators support emergency braking and the parking brake.
It has tricycle type, retractable, trailing-link landing gear.
|Variant||Launch/First flight||Production end|
|Gulfstream G280||2005 / 2009||Twin-engine business jet.|
View full news archive for the Gulfstream G280.
|Gulfstream Aerospace Corporation||News|
Other aircraft programs: Gulfstream G650, Gulfstream G500, Gulfstream G600, Gulfstream G700, Gulfstream G400
|Components||Actuation (2) Lighting (1) Non-Mechanical Components (1) Structural Components (3) Switches (1)|
|Airframe Systems||Airframe Assemblies (6) Environmental Systems (1) Landing Assemblies (3) Safety & Security Systems (1)|
|Avionics||Avionic Components (1) Communications (Airborne) (2) Flight and Data Management (3) Imaging and Visual Systems (1) Indicators and Instruments (2)|
|Power Systems||Auxiliary Power (1) Electrical Power Systems (1) Engine Components (1) Engines (1) Fuel Systems (1)|
|Production||Surface Treatment (1)|