Static -fuselage

Overview: Stress - Static Composite, Fuselage - EFR **Responsibilities**: - Knowledge of aircraft Fuselage structure and aircraft loads - Experienced in the static calculations of Airbus aircrafts (fuselage section) - Knowledge and experience on composites and sandwich structures - Sizing and stress analysis of the fuselage Structure and interfaces by...

Overview: Stress - Static Composite **Responsibilities**: Knowledge of aircraft Fuselage structure and aircraft load Experienced in the static calculations of Airbus aircrafts (wing section Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) Well versed in ISAMI static modules and...

ResponsibilitiesThe 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...

ResponsibilitiesEstablishing (with Head of Function where appropriate) the engineering plan of tasks necessary to properly discharge the project requirements including any derived requirements.The configuration control to secure a baseline and any consequent change management of the engineering baseline.Optimising the achievement of engineering...

**Responsibilities**: "- Knowledge of aircraft loads - Experienced in spectrum generation, - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section) - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section, Flaps, Carriages) - Well versed in ISAMI modules and ISAMI template...

**Job Description**: - Static Analysis with Airbus Methods and Procedures. - Minimum of 4 years execution experience on any of the two main Aircraft Primary structures (NCF, Center Fuselage, - Empenage,Wing upper cover, VTP, HTP, Door Surrounds, Doors, Pylon) - Minimum of 1 year execution experience on MSI, ESI, Hydraulic Brackets static stress analysis -...

Key responsibilities include:Good knowledge in fuselage structure, both primary and secondary structure.Understanding of in-service and operator requirementPreparation of Technical Disposition (TD), repair schemes, and TAS.Analyze and design the modifications or corrective actions referring to the Structural Repair Manual.Preparation of Static Stress...

Overview: Strructural stress engineer - F& DT **Responsibilities**: "- Knowledge of aircraft loads - Experienced in spectrum generation, - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section) - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section, Flaps, Carriages) - Well versed...

ResponsibilitiesThe 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...

This position is for Fatigue and Damage Tolerance Lead EngineerResponsibilitiesEstablishing (with Head of Function where appropriate) the engineering plan of tasks necessary to properly discharge the project requirements including any derived requirements.The configuration control to secure a baseline and any consequent change management of the engineering...