This Job is for Fatigue and Damage tolerance Engineer

• The translation of customer specifications into engineering solutions including the identification and mitigation of technical risk.
• The production of engineering calculations that are necessary to support any conceptual or detail engineering solution for which they are responsible.
• The detailing of engineering solutions in accordance with Industry Standards or client standards, sufficient for manufacture or purchase of such items.
• Contributing to technical reports and feasibility studies. Also for ensuring that any contractual, safety or legislative requirements have been taken into account.
• Guidance of technicians, sub-contractors or suppliers in support of projects ensuring that this is carried out in a safe manner.
• Engineering contribution in support of sales proposals.
• The production of clear written technical reports and presentations.
• Right first time and on time delivery of their work. The ability to estimate the time to carry out tasks and to plan their own work. 
• The Company's Quality Assurance Policies in any work undertaken. In particular to be fully conversant with the requirements of the Company's Processes Manual.
• Continuous improvement contribution to their personal development and company development in all appropriate areas.

BTech/MTech

•Knowledge of aircraft Fuselage and wing structure and aircraft loads  

• Experienced in spectrum generation and Kt Calculation 

• Autonomous in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section)  

• Well versed in ISAMI modules (including crack models, joint models) and ISAMI template preparation  

• Should have Fatigue and Damage Tolerance experience related to Single Aisle, Long Range and A350 programs  

• F&DT Analysis of Junctions, notches, unfolding radius, lugs & pins

• Sizing and stress analysis of the Fuselage and Wing Structure and interfaces by means of hand calculations, numerical simulations (FEM)  

• Experience in numerical modeling, post-processing and reporting of the results  

• Very well-versed in stress dossier writing  

• Good in excel macros  

Below tools knowledge is requitred.

• ISAMI
• Hyperview (post processing knowledge)
• Catia V5, PASS SSI (Basic Knowledge)
• Nastran/Patran
• Microsoft Office
• Airbus Supply

• Knowledge of Airbus processes and procedures
• Visual basic and or python programming knowledge.
• Automation of repeatable tasks / processes.
• Experience in initial Design Stress (Static, FDT and FEM) tasks of Aircraft Structures.

4-8 Years