Gulfstream G280

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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.

Lift type	Fixed wing	Search for other aircraft programs with these properties on the Aircraft Programs directory page.
Construction type	Factory-built
Control type	Piloted
Engine type	Turbofan
Application	Business

Operations data

For detailed information about current charter operators, maintenance and training providers, and completions services for this aircraft, please consult our sister publication Business Air News: Gulfstream G280

Airframer

Gulfstream Aerospace Corporation

News

Other aircraft programs: Gulfstream G650, Gulfstream G500, Gulfstream G600, Gulfstream G700, Gulfstream G400

Supply chain

(37 links)

Components	Actuation (2) Lighting (1) Non-Mechanical Components (1) Structural Components (2) 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)

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Information on this page is compiled from a variety of published sources, and links do not necessarily imply recommendation or confirmation by the airframe manufacturer.