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.
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; ability to estimate time and plan own work.
Adherence to the Company's Quality Assurance Policies and Processes Manual.
Continuous improvement contribution to personal and company development.
Requirements
BTech/MTech
4-8 Years experience in Fatigue and Damage Tolerance analysis
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