F&dt- Fuselage

Overview: F&DT- Fuselage - 1 Opening **Responsibilities**: - Knowledge of aircraft loads - Experienced in spectrum generation and Kt Calculation - Good 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 - Sizing and...

Responsibilities Knowledge of aircraft loads  • Experienced in spectrum generation and Kt Calculation • Good 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  • Sizing and stress analysis of the...

ResponsibilitiesKnowledge of aircraft loadsExperienced in spectrum generation and Kt CalculationGood 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 preparationSizing and stress analysis of the Fuselage Structure and interfaces by...

Responsibilities • Knowledge of aircraft loads  • Experienced in spectrum generation and Kt Calculation • Good 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  • Sizing and stress analysis of the...

Job Description: -Experience: 2 – 10 YearsKnowledge of aircraft loadsExperienced in spectrum generation and Kt Calculation Good 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 preparationSizing and stress analysis of the Fuselage...

Senior Airframe Engineer job involves investigating and producing Fatigue and damage tolerance justifications solutions for design deviations and existing repairs for simple and complex Primary Structures of metallic Fuselage Structure. **Following are the core responsibilities** Conversant with AIRBUS F&DT methods processes & terminologies In depth...

JobDescription: Experience:2 – 10 YearsKnowledgeof aircraftloadsExperiencedin spectrum generation and KtCalculationGoodin Fatigue and Damage Tolerance (F&DT) calculations ofAirbus aircrafts (fuselage section)Well versed in ISAMI modules (including crack models jointmodels)and ISAMI template preparationSizingand stress analysis of the Fuselage Structure...

Expertise in Fatigue and Damage tolerance of metallic structures using FEA and hand calculation - Good working experience of metallic primary and secondary structures. - Expertise in analyzing airframe structures - Expertise in Engineering mechanics and analytical calculation using classical methods - Stress/Load FEM extraction from GFEM/DFEM - Expertise in...

Static Analysis with Airbus Methods and Procedures Minimum of 4 6 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 Hands on execution experience on GFEM Load extraction DFEM Creation Validation and Post processing F DT Hands on execution experience...

Static Analysis with Airbus Methods and Procedures Minimum of 4 6 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 Hands on execution experience on GFEM Load extraction DFEM Creation Validation and Post processing F DT Hands on execution experience...

Static Analysis with Airbus Methods and Procedures Minimum of 4 6 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 Hands on execution experience on GFEM Load extraction DFEM Creation Validation and Post processing F DT Hands on execution experience...

Static Analysis with Airbus Methods and Procedures Minimum of 4 6 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 Hands on execution experience on GFEM Load extraction DFEM Creation Validation and Post processing F DT Hands on execution experience...

Job Description: Expertise in Fatigue and Damage tolerance of metallic structures using FEA and hand calculation Good working experience of metallic primary and secondary structures. Expertise in analyzing airframe structures Expertise in Engineering mechanics and analytical calculation using classical methods Stress/Load FEM extraction from GFEM/DFEM...

Overview: Structural stress Engineer - Static & FD&T **Responsibilities**: Static: Knowledge of aircraft loads Experienced in the static calculations of Airbus wing structures such as Flaps, slats, carriages etc Experience in numerical modeling, post-processing and reporting of the results Good understanding of load transfer between various high lift...

ResponsibilitiesGood Knowledge on Aerospace domain, Primary and Secondary Structures, loads & Aircraft drawingHands-on execution of Aero-structure Metallic and Composite concessions (Aircraft fuselage, Pylon and Wing components)In depth knowledge of stress, fatigue and damage tolerance analysis of metallic structures (Fatigue analysis as per M2841).In depth...

62192BRTitle:Design Signatory - ConcessionsJob Description:Quest Global is an organization at the forefront of innovation and one of the world's fastest growing engineering services firms with deep domain knowledge and recognized expertise in the top OEMs across seven industries. We are a twenty-five-year-old company on a journey to becoming a centenary one,...

Responsibilities Good Knowledge on Aerospace domain, Primary and Secondary Structures, loads & Aircraft drawing Hands-on execution of Aero-structure Metallic and Composite concessions (Aircraft fuselage, Pylon and Wing components) In depth knowledge of stress, fatigue and damage tolerance analysis of metallic structures (Fatigue analysis as per M2841). ...