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As part of the European consortium EPI, alongside Rolls-Royce, MTU and Safran Aircraft Engines, ITP is responsible for the design, development, manufacturing and maintenance of the TP400 engine.

ITP is responsible for designing and manufacturing the low-pressure turbine, the turbine exit case (TEC), the exhaust nozzle, the front bearing structure (FBS) and the engine gearbox support bars and dressings.

The TP400 engine powers the military transport airplane A400M. With a propeller diameter of 5.33 m, it obtains a thrust of 11,000 hp.


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