Performs system design and integration activities on landing gear system including subsystems as brakes steering and arresting hookResponsible for the landing gear system design integration and verificationDevelops system design requirements and validation verification methods qualification certification with authoritiesManages system architecture development and functional allocation activitiesDefines landing gear system and equipment technical specificationDefines system and equipment test requirements & analysing test resultsProvides support for system sub-contractor monitoring and management activitiesBroad knowledge about military and civil aviation standards for Landing Gear Systems

Parametric modelling of landing gear systems for conceptual design and preliminary performance definitionFundamental system analysis as A/C level LG layout definition, shock absorber sizing, brake sizing, tyre selection etc.Landing gear retraction mechanism dynamic modeling and multi-body simulationPerforming the kinematic concepts of nose gear, main gears and landing gear doors by using CATIAPerforming floatation analysisPreparing the ADAMS models for ground loads/attachment loads of the nose and main landing gearDynamic modelling of hydraulic equipment behavior with numerical simulationDynamic modelling of main and nose landing gear shock absorbersPreliminary arresting hook positioning and sizing