Key responsibilities include Good knowledge in fuselage structure both primary and secondary structure Understanding of inservice and operator requirement Preparation of Technical Disposition TD repair schemes and TAS Analyze and design the modifications or corrective actions referring to the Structural Repair Manual Preparation of Static Stress Assessment Sheets SAS Fatigue Approval Sheet FAS and TAS Knowledge of finding ACDs and relevant check stress files for the applicable WVs and Knowledge in the preparation of Static Repair work file Experience in Aircraft repairs Provide design solutions to inservice damages accidental and aging Sound knowledge in SRM chapters and repair principles Sound knowledge ATA and NDT inspection A C materials fastener types and rules A C Design Principles and GD T Valuable knowledge in fuselage structure Ability to adapt to changing schedules and highpriority tasks responsiveness Tools GILDA ZAMIZ CATIA V5 TREND VPM AIRNav SAP PCS