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Structure

The airframe design is based on the damage tolerance concept. Main structural elements are made of aluminum alloys, titanium alloys and steel in specific areas. Most of the fuselage skin, access doors and panels, air intakes and ducts are made of composites (carbon fiber, Kevlar). Metal-to-metal bonding is used for control surfaces to minimize the parts count. A structural S-HUMS segment evaluates expired/residual airframe fatigue life of individual aircraft usage.

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Embedded Tactical Training Simulation (ETTS)

The Embedded Simulation reduces the need for additional aircraft in training missions typically requiring the presence of a leader or opponent aircraft. It also enables the simulation of the operational environment with no need for actual deployment of various threats or the installation of expensive on-board sensors like multimode radar and active/passive electronic countermeasures, greatly reducing logistics and pilot formation costs.

A set of different operating modes and options can be selected by the instructor through HOTAS controls and LAD. Data from simulated scenario are presented on the LAD and HUD in both cockpits.

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