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AIRCRAFT PROGRAM

Gulfstream G280

Lift typeFixed wing
Construction typeFactory-built
Control typePiloted
Engine typeTurbofan
ApplicationBusiness
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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.

Type variants

Variant Launch/First flight Production end  
Gulfstream G280 2005 / 2009 Twin-engine business jet.

Recent news

View full news archive for the Gulfstream G280.

See recent updates (latest 03/08/2022)

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

Supply chain

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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)
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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.