CESA is in charge of Design and Development, Production, Qualifi cation, Reliability, Maintainability and Product Support (O level) of the Turkish Light Helicopter Utility Programme (TLUH, an indigenous 5Tn Bi-Turbine programme, EASA certifi ed).
• COMPLETE HYDRAULIC SYSTEM: dual system (redundancy) + Landing Gear extension / retraction.
• Two independent systems.
CESA is responsible for the complete architecture of the system and TAI support in the defi nition of the Performance Hydraulic Test Rig.
CESA is also in charge of development and production of the Landing Gear and the actuation package for the TLUH Landing Gear.
Regarding the landing gear package (struts and shock absorber) TAI is responsible for the conceptual design and its integration with the helicopter. In this phase, CESA will support TAI in the conceptual design and is responsible for designing the details, manufacture of prototypes, assessment including drop and stress tests for the entire landing gear, and product support for the development phase.
With the actuation package, CESA is responsible for conceptual design, detailed design, manufacture, unit assessment and production of development units.