Aircraft program
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.
The aircraft as engineered: what it is built from, the systems it flies with, and its configuration — each box a theme.
Notable technologies — each tag names a technology on our research record for this aircraft, with its fitting status: Primary, Standard, Option or Planned.
Technical reference compiled with AI research; a value appears only where two independent research passes and a web fact-check agree. Gaps are deliberate.
Supplier geography and market analysis for this program — with an Analytics subscription.
Subscribe| Variant | Launch / first flight | Production end | Notes |
|---|---|---|---|
| Gulfstream G280 | 2005 / 2009 | Production: 22 (2025) GAMA: Gulfstream Aerospace Corp. Gulfstream 280. Twin-engine business jet. | |
| Gulfstream G300 | 2025 / 2025 | Production: 7 (2026) GAMA: Gulfstream Aerospace Gulfstream G280. New generation variant with longest cabin in class and six-screen Harmony Flight Deck. In development, to replace Gulfstream G280. |
| Gulfstream Aerospace Corporation | News |
The program’s dated history — milestones, contracts, supplier selections and facilities, each linked to its source. Log in to view.
Information on this page is compiled from a variety of published sources; links do not necessarily imply recommendation or confirmation by the airframe manufacturer.
Corrections go straight to the editorial team that maintains this directory.