Hybrid
Full Time
• Experience of providing Design solutions for different damages on Aircraft primary and secondary structures. • Experience of Providing Static and Fatigue/Damage tolerance justification for design solutions for different damages on Aircraft primary and secondary structures. • Experience on Creation of Database(DB), Repair Instruction/Answer(AW), Repair Drawing(RD), Technical Disposition(TD), Static Justification Sheet (SAS), Fatigue Justification Sheet (FAS) and Technical Approval Sheet (TAS) • Experience on In-service Daily Repairs and Major Repairs • Experience on structural repair manual (SRM)/Air vehicle structure Repair (ASR) • Background in design and sizing of Aircraft primary structure components and parts. • A sound understanding of engineering materials and their applications • Good experience in hand calculation through classical approach • Static & Fatigue classical analysis • Basic knowledge on FEA • Knowledge of both metallic and composite materials
• Working knowledge of all Airbus Structures.
• Working knowledge of different Airbus programs.
• Knowledge of Airbus stress/fatigue manuals and tools.
• Demonstrated problem solving ability.
Capgemini
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