Lead Engineer – Fatigue and Damage Tolerance

Expleo Group

full-time

Posted on: 9/6/2025

Location: 🇮🇳 India

✨ AI Apply

Senior

Python

About the role

Establish the engineering plan of tasks to discharge project requirements and derived requirements
Maintain configuration control and manage change control of the engineering baseline
Optimise the achievement of engineering requirements and record engineering justifications
Perform technical risk assessment
During project initiation set up checklists compliant to customer and internal requirements and maintain them during project life
Manage work to meet contract/order and regulatory requirements including engineering reviews performed by or on behalf of the Chief Engineer
Ensure subject-matter experts are invited to design reviews where appropriate
Refer conflicts between operational requirements and technical governance to the responsible Chief Engineer
Ensure correct procedures are adhered to for generation of analyses, design schemes and drawings and for carrying out engineering tasks
Ensure suitably authorised and qualified personnel are employed on the project and corrective actions are implemented prior to issue
Recommend training and contribute to appraisals of junior and graduate engineers
Hold or work towards delegated signatory

BTech or MTech in relevant engineering discipline
8 to 12 years of experience in Fatigue & Damage Tolerance (F&DT)
Knowledge of aircraft fuselage and wing structure and aircraft loads
Experience in spectrum generation and Kt calculation
Good in F&DT calculations of Airbus aircrafts (fuselage section)
Well versed in ISAMI modules (including crack models, joint models) and ISAMI template preparation
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 hand calculations and numerical simulations (FEM)
Experience in numerical modeling, post-processing and reporting of results
Very well-versed in stress dossier writing
Proficient with Excel macros
Knowledge of Airbus processes and procedures
Expertise in ISAMI, Hyperview (post processing), Catia V5, PASS SSI (basic), Nastran/Patran, Microsoft Office
Desired: Visual Basic and/or Python programming knowledge and automation of repeatable tasks
Desired: Experience in initial Design Stress (Static, FDT and FEM) tasks of Aircraft Structures
Is in possession of or working towards delegated signatory