Venn Group Bristol, England (2 – 3 days per week on site) Stress Engineer’s x 2 9-month Contract (Subject to ext) Up to £46 per hour umbrella (Inside IR35) (£50 if Signature/Approver)BPSS Required Fatigue & Damage Tolerance Engineer An exciting opportunity has arisen for a Fatigue & Damage Tolerance Engineer to join the Wing Analysis Engineering team. Key Responsibilities: Approve F&DT deliverables and lead the resolution of F&DT problems through the use of appropriate methods Responsible for the technical scope of assigned projects and tasks Contribute to engineering solutions and ways of working borne from experience in aerospace, other industries or research environments Support the development of less experienced team members on both technical and behavioural aspects. Key Attributes: Experience and know-how of structures engineering and analytical techniques Good knowledge of overall aircraft structural design principles and techniques Hold or be close to holding approval signatory in F&DT analysis Ability to step back and propose new ideas Studied engineering and have a structural analysis background, particularly fatigue and damage tolerance Repair Stress Engineer An exciting opportunity has arisen for a Repair Stress Engineer to join their Engineering team. Responsibilities Perform static strength analysis for repairs using approved methods and tools Create, compile and co-ordinate static strength justification reports and associated engineering documentation Ensure all tasks and activities required for Repair Engineering are correctly planned, monitored and executed to achieve customer time scales Work in conjunction with the Repair Design and F&DT Engineers to develop optimum repairs Key Attributes Essential Experience of how airframe repairs are developed and justified Manage multiple priorities to time, cost and quality in a challenging and fast paced environment Experience of static analysis of aircraft structures using a range of hand and computer methods Understanding of the fundamental methods of static stress analysis and an ability to develop these methods Knowledge and experience of using static strength analysis tools and methods (including ISAMI and Mathcad) Experience of compiling static strength justification reports to Aerospace standards Aerospace Engineering degree (or equivalent) and relevant engineering experience Desirable conversant with technical requirements for repair design Some knowledge of the application of FE analysis Stress Engineering background, aerospace preferred Delegated signature for structural analysis (or significant development towards)