Tasks include: Designing repairs and Allowable Damage Limits (AOL's) for composite and/ or metallic damage through to repair of major structural components. Interrogating published documentation relating to release of the aircraft to service. Typically, the work will involve liaison with Fatigue & Damage Tolerance, Static Stress, Aerodynamics, M&P and Authoring teams, and will also appropri... WKCL1_UKTJ