Engineer- Airframe Stress Analysis

Tata Technologies; Pune District; On-site; INR 1,200,000 - 1,800,000; Full time

Job summary

Tata Technologies is seeking an experienced Airframe Stress Analysis professional to investigate and produce substantiations for primary and secondary structures of metallic fuselage. The role requires familiarity with Airbus Static and F&DT methodologies and a solid grasp of aircraft fuselage configurations (A320/A321/A330).

Responsibilities include developing stress reports, preparing static and F&DT substantiations, reviewing technical documents, and coordinating with customers to ensure

Qualifications

• Conversant with Airbus Static and/or F&DT methods, processes & terminologies
• In-depth knowledge of F&DT based design philosophy
• Good understanding of Aircraft Fuselage structure (A320/A321/A330)

Responsibilities

• Conversant with Airbus Static and/or F&DT methods, processes & terminologies.
• In depth knowledge of F&DT based design philosophy.
• Good understanding of the Aircraft Fuselage structure (A320/A321/A330).
• Understand repair history of the damaged part.
• Develop stress reports for the substantiation carried out for primary and secondary structures of aircraft with utmost accuracy.
• Preparation of Static and/or F&DT stress justification
• Identification of repair and solution.
• Review of related technical documents for any discrepancies
• Liaise with the customer for input requirement.
• Timely delivery of work based on a set completion target with high quality.

Skills

Airbus Static & F&DT methods

Job description

Job Summary

Airframe Stress Analysis job involves investigating and producing Static or Fatigue and damage tolerance justifications solutions for design deviations and existing repairs for simple and complex Primary Structures of metallic Fuselage Structure.

Responsibilities

• Conversant with Airbus Static and/or F&DT methods processes & terminologies
• In depth knowledge of F&DT based design philosophy
• Good understanding of the Aircraft Fuselage structure (A320/A321/A330) will be added advantage).
• Understand repair history of the damaged part.
• Develop stress reports for the substantiation carried out for primary and secondary structures of aircraft with utmost accuracy.
• Preparation of Static and/or F&DT stress justification
• Identification of repair and solution.
• Review of related technical documents for any discrepancies
• Liaise with the customer for input requirement.
• Timely delivery of work based on a set completion target with high quality.