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The Emergency Accumulator proposed by CESA includes an accumulator with the following components attached to it: the charging valve and the manometer are at the top, while the rest of the components (the solenoid valve, check valves, depress valve, etc.) are at the bottom.

CESA is also in charge of the Design and Development, Production, Qualifi cation, Reliability, Maintainability and Product Support of the HTT40 Emergency Accumulator for the Hydraulic Power System for the HTT40 Indian trainer developed by HAL (Hindustan Aeronautics Limited).

The HTT40 will be an all-metal tandem-seat aircraft powered by a 950 hp (708 kW) turbo-prop engine.

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