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 and Damage Tolerance, Static Stress, Aerodynamics, MandP and Authoring teams, and will also appropri click apply for full job details