As part of the Design Organization approval (EASA.21J.117) we offer:
- design of aviation structures, in particular composite structures;
- design of aviation installations (electric, hydraulic, fuel, etc.);
- designing system integration and airframe installations;
- design and implementation of special tests (static tests);
In accordance with the requirements of
PART 21 Subpart J
Complete design of a light aircraft, facilities meeting the requirements of EASA CS-22, CS-23.
Design of strength composite structures, including structures for aviation applications in accordance with the requirements of EASA CS-23.
Design of on-board light aircraft installations (electric, hydraulic, fuel, etc.).
Integration of airframe systems and installations (propulsion, undercarriage).
Installation of new elements of equipment (radio, transponder, additional avionics equipment, camera, optoelectronic head, etc.).