Engineer F&DT
Airbus
Engineer F&DT
Job Description
Job Description:
Experience Range: 5-7 Years Only
- Knowledge Fatigue and Damage Tolerance analysis
- Theoretical knowledge in aircraft crack propagation analysis
- Knowledge of aircraft loads and experienced in spectrum generation
- Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases.
- Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules.
- Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis)
- Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.,)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)
- Ability to read the drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment to be useful for fatigue calculations.
- Possess strong foundation in the area of load/stress analysis with abilities to formulate ""free body diagrams"" and identify load path of structures
- ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,)
- Experienced in documents (like PDR/CDR/Certification reports, Concessions, Repairs) and report creation and getting validated.
This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.
Company:
Airbus India Private LimitedEmployment Type:
Permanent-------
Experience Level:
ProfessionalJob Family:
Structure & Dynamic Systems Analysis <JF-EN-EN>By submitting your CV or application you are consenting to Airbus using and storing information about you for monitoring purposes relating to your application or future employment. This information will only be used by Airbus.
Airbus is committed to achieving workforce diversity and creating an inclusive working environment. We welcome all applications irrespective of social and cultural background, age, gender, disability, sexual orientation or religious belief.
Airbus is, and always has been, committed to equal opportunities for all. As such, we will never ask for any type of monetary exchange in the frame of a recruitment process. Any impersonation of Airbus to do so should be reported to emsom@airbus.com.
At Airbus, we support you to work, connect and collaborate more easily and flexibly. Wherever possible, we foster flexible working arrangements to stimulate innovative thinking.
Locations
- Bangalore Area,
Salary
Skills Required
- Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.)intermediate
- Fatigue and Damage Tolerance analysisintermediate
- Load/stress analysisintermediate
- ISAMI modules expertiseintermediate
- DFEM, GFEMintermediate
- Hand calculations for static and fatigueintermediate
- Spectrum generationintermediate
- Rainflow counting, Miner's ruleintermediate
- Drawing interpretation for fatigue calculationsintermediate
- Free body diagrams and load path identificationintermediate
- Report writing and validationintermediate
Required Qualifications
- 5-7 years of experience (experience)
- Theoretical knowledge in aircraft crack propagation analysis (experience)
- Knowledge of aircraft loads and experience in spectrum generation (experience)
- Awareness of compliance risks and commitment to act with integrity (experience)
Responsibilities
- Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases
- Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules
- Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)
- Read drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment for fatigue calculations
- Formulate free body diagrams and identify load path of structures
- Work with ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.)
- Experience in documents (PDR/CDR/Certification reports, Concessions, Repairs) and report creation and validation
Benefits
- general: Permanent employment
- general: Flexible working arrangements
- general: Commitment to workforce diversity and inclusive working environment
- general: Equal opportunities for all
Tags & Categories
Answer 10 quick questions to check your fit for Engineer F&DT @ Airbus.
Related Books and Jobs
Engineer F&DT
Airbus
Engineer F&DT
Job Description
Job Description:
Experience Range: 5-7 Years Only
- Knowledge Fatigue and Damage Tolerance analysis
- Theoretical knowledge in aircraft crack propagation analysis
- Knowledge of aircraft loads and experienced in spectrum generation
- Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases.
- Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules.
- Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis)
- Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.,)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)
- Ability to read the drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment to be useful for fatigue calculations.
- Possess strong foundation in the area of load/stress analysis with abilities to formulate ""free body diagrams"" and identify load path of structures
- ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,)
- Experienced in documents (like PDR/CDR/Certification reports, Concessions, Repairs) and report creation and getting validated.
This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.
Company:
Airbus India Private LimitedEmployment Type:
Permanent-------
Experience Level:
ProfessionalJob Family:
Structure & Dynamic Systems Analysis <JF-EN-EN>By submitting your CV or application you are consenting to Airbus using and storing information about you for monitoring purposes relating to your application or future employment. This information will only be used by Airbus.
Airbus is committed to achieving workforce diversity and creating an inclusive working environment. We welcome all applications irrespective of social and cultural background, age, gender, disability, sexual orientation or religious belief.
Airbus is, and always has been, committed to equal opportunities for all. As such, we will never ask for any type of monetary exchange in the frame of a recruitment process. Any impersonation of Airbus to do so should be reported to emsom@airbus.com.
At Airbus, we support you to work, connect and collaborate more easily and flexibly. Wherever possible, we foster flexible working arrangements to stimulate innovative thinking.
Locations
- Bangalore Area,
Salary
Skills Required
- Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.)intermediate
- Fatigue and Damage Tolerance analysisintermediate
- Load/stress analysisintermediate
- ISAMI modules expertiseintermediate
- DFEM, GFEMintermediate
- Hand calculations for static and fatigueintermediate
- Spectrum generationintermediate
- Rainflow counting, Miner's ruleintermediate
- Drawing interpretation for fatigue calculationsintermediate
- Free body diagrams and load path identificationintermediate
- Report writing and validationintermediate
Required Qualifications
- 5-7 years of experience (experience)
- Theoretical knowledge in aircraft crack propagation analysis (experience)
- Knowledge of aircraft loads and experience in spectrum generation (experience)
- Awareness of compliance risks and commitment to act with integrity (experience)
Responsibilities
- Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases
- Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules
- Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)
- Read drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment for fatigue calculations
- Formulate free body diagrams and identify load path of structures
- Work with ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.)
- Experience in documents (PDR/CDR/Certification reports, Concessions, Repairs) and report creation and validation
Benefits
- general: Permanent employment
- general: Flexible working arrangements
- general: Commitment to workforce diversity and inclusive working environment
- general: Equal opportunities for all
Tags & Categories
Answer 10 quick questions to check your fit for Engineer F&DT @ Airbus.
Related Books and Jobs