Fatigue and Damage Tolerance Engineer
Capgemini
Fatigue and Damage Tolerance Engineer
Job Description
Fatigue and Damage Tolerance Engineer
📋 Job Overview
The Fatigue and Damage Tolerance (F&DT) Lead role at Capgemini Engineering in Bangalore involves leading structural analysis for aircraft components, focusing on fatigue, crack propagation, and damage tolerance to ensure airworthiness. The position requires 8-12 years of experience in aerospace engineering, performing advanced stress calculations, and collaborating with cross-functional teams on certification and documentation. This role offers opportunities to mentor juniors, innovate processes, and contribute to cutting-edge R&D in aviation structures.
📍 Location: Bangalore
💼 Experience Level: Experienced Professionals
🏢 Business Unit: Engineering and RandD Services
🎯 Key Responsibilities
- Collaborate with cross-functional teams including Design, Stress, Materials, and Certification to ensure structural integrity and airworthiness
- Prepare and review technical documentation, certification reports, and compliance statements for regulatory approval
- Mentor junior engineers and contribute to technical reviews and process improvements
✅ Required Qualifications
- 8 to 12 years of experience in aerospace engineering
- Knowledge of Fatigue and Damage Tolerance analysis
- Knowledge of aircraft Fuselage and wing structure and aircraft loads
- Theoretical knowledge in aircraft crack propagation analysis
- Knowledge of aircraft loads and experience 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 drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment for fatigue calculations
- Strong foundation in load/stress analysis with abilities to formulate free body diagrams and identify load path of structures
- Experience 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.)
- Experienced in documents (PDR/CDR/Certification reports, Concessions, Repairs) and report creation and validation
⭐ Preferred Qualifications
- Visual basic and/or python programming knowledge
- Automation of repeatable tasks/processes
- Experience in initial Design Stress (Static, FDT and FEM) tasks of Aircraft Structures
🛠️ Required Skills
- Fatigue and Damage Tolerance analysis
- Aircraft Fuselage and wing structure analysis
- Aircraft loads and spectrum generation
- Crack propagation analysis
- Seq stresses calculation
- Mission profiles understanding
- Rainflow counting
- Miner's rule
- Stress files and FESPS databases
- Stress concentration (Kt) calculation using Petersons', DFEM, ISAMI
- Metallic and composite structures analysis (Plain Strength checks, Buckling, Bolted joint analysis)
- Static and fatigue design values (Ftu, Fty, Fcy, AFI, S-N curves, fracture toughness)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)
- Drawing interpretation for fasteners and surface treatments
- Load/stress analysis (free body diagrams, load path identification)
- 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)
- Technical documentation and report creation (PDR/CDR, Certification reports, Concessions, Repairs)
- Cross-functional collaboration
- Mentoring and process improvements
Locations
- Bangalore, India
Salary
Estimated Salary Rangemedium confidence
2,500,000 - 4,200,000 INR / yearly
Source: ai estimated
* This is an estimated range based on market data and may vary based on experience and qualifications.
Skills Required
- Fatigue and Damage Tolerance analysisintermediate
- Aircraft Fuselage and wing structure analysisintermediate
- Aircraft loads and spectrum generationintermediate
- Crack propagation analysisintermediate
- Seq stresses calculationintermediate
- Mission profiles understandingintermediate
- Rainflow countingintermediate
- Miner's ruleintermediate
- Stress files and FESPS databasesintermediate
- Stress concentration (Kt) calculation using Petersons', DFEM, ISAMIintermediate
- Metallic and composite structures analysis (Plain Strength checks, Buckling, Bolted joint analysis)intermediate
- Static and fatigue design values (Ftu, Fty, Fcy, AFI, S-N curves, fracture toughness)intermediate
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)intermediate
- Drawing interpretation for fasteners and surface treatmentsintermediate
- Load/stress analysis (free body diagrams, load path identification)intermediate
- 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)intermediate
- Technical documentation and report creation (PDR/CDR, Certification reports, Concessions, Repairs)intermediate
- Cross-functional collaborationintermediate
- Mentoring and process improvementsintermediate
Required Qualifications
- 8 to 12 years of experience in aerospace engineering (experience)
- Knowledge of Fatigue and Damage Tolerance analysis (experience)
- Knowledge of aircraft Fuselage and wing structure and aircraft loads (experience)
- Theoretical knowledge in aircraft crack propagation analysis (experience)
- Knowledge of aircraft loads and experience in spectrum generation (experience)
- Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases (experience)
- Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules (experience)
- Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis) (experience)
- Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.) (experience)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution) (experience)
- Ability to read drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment for fatigue calculations (experience)
- Strong foundation in load/stress analysis with abilities to formulate free body diagrams and identify load path of structures (experience)
- Experience 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)
- Experienced in documents (PDR/CDR/Certification reports, Concessions, Repairs) and report creation and validation (experience)
Preferred Qualifications
- Visual basic and/or python programming knowledge (experience)
- Automation of repeatable tasks/processes (experience)
- Experience in initial Design Stress (Static, FDT and FEM) tasks of Aircraft Structures (experience)
Responsibilities
- Collaborate with cross-functional teams including Design, Stress, Materials, and Certification to ensure structural integrity and airworthiness
- Prepare and review technical documentation, certification reports, and compliance statements for regulatory approval
- Mentor junior engineers and contribute to technical reviews and process improvements
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Fatigue and Damage Tolerance Engineer
Capgemini
Fatigue and Damage Tolerance Engineer
Job Description
Fatigue and Damage Tolerance Engineer
📋 Job Overview
The Fatigue and Damage Tolerance (F&DT) Lead role at Capgemini Engineering in Bangalore involves leading structural analysis for aircraft components, focusing on fatigue, crack propagation, and damage tolerance to ensure airworthiness. The position requires 8-12 years of experience in aerospace engineering, performing advanced stress calculations, and collaborating with cross-functional teams on certification and documentation. This role offers opportunities to mentor juniors, innovate processes, and contribute to cutting-edge R&D in aviation structures.
📍 Location: Bangalore
💼 Experience Level: Experienced Professionals
🏢 Business Unit: Engineering and RandD Services
🎯 Key Responsibilities
- Collaborate with cross-functional teams including Design, Stress, Materials, and Certification to ensure structural integrity and airworthiness
- Prepare and review technical documentation, certification reports, and compliance statements for regulatory approval
- Mentor junior engineers and contribute to technical reviews and process improvements
✅ Required Qualifications
- 8 to 12 years of experience in aerospace engineering
- Knowledge of Fatigue and Damage Tolerance analysis
- Knowledge of aircraft Fuselage and wing structure and aircraft loads
- Theoretical knowledge in aircraft crack propagation analysis
- Knowledge of aircraft loads and experience 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 drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment for fatigue calculations
- Strong foundation in load/stress analysis with abilities to formulate free body diagrams and identify load path of structures
- Experience 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.)
- Experienced in documents (PDR/CDR/Certification reports, Concessions, Repairs) and report creation and validation
⭐ Preferred Qualifications
- Visual basic and/or python programming knowledge
- Automation of repeatable tasks/processes
- Experience in initial Design Stress (Static, FDT and FEM) tasks of Aircraft Structures
🛠️ Required Skills
- Fatigue and Damage Tolerance analysis
- Aircraft Fuselage and wing structure analysis
- Aircraft loads and spectrum generation
- Crack propagation analysis
- Seq stresses calculation
- Mission profiles understanding
- Rainflow counting
- Miner's rule
- Stress files and FESPS databases
- Stress concentration (Kt) calculation using Petersons', DFEM, ISAMI
- Metallic and composite structures analysis (Plain Strength checks, Buckling, Bolted joint analysis)
- Static and fatigue design values (Ftu, Fty, Fcy, AFI, S-N curves, fracture toughness)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)
- Drawing interpretation for fasteners and surface treatments
- Load/stress analysis (free body diagrams, load path identification)
- 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)
- Technical documentation and report creation (PDR/CDR, Certification reports, Concessions, Repairs)
- Cross-functional collaboration
- Mentoring and process improvements
Locations
- Bangalore, India
Salary
Estimated Salary Rangemedium confidence
2,500,000 - 4,200,000 INR / yearly
Source: ai estimated
* This is an estimated range based on market data and may vary based on experience and qualifications.
Skills Required
- Fatigue and Damage Tolerance analysisintermediate
- Aircraft Fuselage and wing structure analysisintermediate
- Aircraft loads and spectrum generationintermediate
- Crack propagation analysisintermediate
- Seq stresses calculationintermediate
- Mission profiles understandingintermediate
- Rainflow countingintermediate
- Miner's ruleintermediate
- Stress files and FESPS databasesintermediate
- Stress concentration (Kt) calculation using Petersons', DFEM, ISAMIintermediate
- Metallic and composite structures analysis (Plain Strength checks, Buckling, Bolted joint analysis)intermediate
- Static and fatigue design values (Ftu, Fty, Fcy, AFI, S-N curves, fracture toughness)intermediate
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)intermediate
- Drawing interpretation for fasteners and surface treatmentsintermediate
- Load/stress analysis (free body diagrams, load path identification)intermediate
- 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)intermediate
- Technical documentation and report creation (PDR/CDR, Certification reports, Concessions, Repairs)intermediate
- Cross-functional collaborationintermediate
- Mentoring and process improvementsintermediate
Required Qualifications
- 8 to 12 years of experience in aerospace engineering (experience)
- Knowledge of Fatigue and Damage Tolerance analysis (experience)
- Knowledge of aircraft Fuselage and wing structure and aircraft loads (experience)
- Theoretical knowledge in aircraft crack propagation analysis (experience)
- Knowledge of aircraft loads and experience in spectrum generation (experience)
- Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases (experience)
- Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules (experience)
- Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis) (experience)
- Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.) (experience)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution) (experience)
- Ability to read drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment for fatigue calculations (experience)
- Strong foundation in load/stress analysis with abilities to formulate free body diagrams and identify load path of structures (experience)
- Experience 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)
- Experienced in documents (PDR/CDR/Certification reports, Concessions, Repairs) and report creation and validation (experience)
Preferred Qualifications
- Visual basic and/or python programming knowledge (experience)
- Automation of repeatable tasks/processes (experience)
- Experience in initial Design Stress (Static, FDT and FEM) tasks of Aircraft Structures (experience)
Responsibilities
- Collaborate with cross-functional teams including Design, Stress, Materials, and Certification to ensure structural integrity and airworthiness
- Prepare and review technical documentation, certification reports, and compliance statements for regulatory approval
- Mentor junior engineers and contribute to technical reviews and process improvements
Tags & Categories
Answer 10 quick questions to check your fit for Fatigue and Damage Tolerance Engineer @ Capgemini.
10 Questions
~2 Minutes
Instant Score
Related Books and Jobs