- Positive knowledge in Wing and fuselage structure, both primary and secondary structure of Airbus fleet. (Working experience in A350 and A220 is an added advantage)
- Understanding of in-service damages and operator requirement
- Preparation of repair definitions, Technical Disposition (TD), repair schemes, and RDTS.
- Analyse and design the modifications or corrective actions referring to the Structural Repair Manual.
- Provide required design inputs to Static & Fatigue Assessment teams for their investigation.
- Knowledge of finding relevant check stress files for the applicable WVs and Knowledge in the preparation of Static/fatigue Repair work file is an added advantage.
- Experience in Aircraft repairs – Provide design solutions to in-service damages (accidental and ageing).
- Sound knowledge in SRM chapters and repair principles.
- Sound knowledge in ATA chapters and NDT inspections.
- A/C materials specs, fastener types and rules.
- A/C Design Principles and GD&T;, Good knowledge in fuselage and wing structure and drawing reading.
- Ability to adapt to changing schedules and high-priority tasks, responsiveness.