Hi,

Greetings from Quest Global !!!

You are required to be available in person for the discussion being held on 10th October 2026, @ 9.00 AM (F2F Technical round interview).

"References from your friends and colleagues will be highly appreciated and strongly encouraged."

Contact person: Basavaraj -(phone hidden))

Date& Date : 10th October 2026 , Saturday

Time : 9.00 AM to 4.00 PM

Interview Venue Address:

Quest Global Engineering Services Pvt Ltd.,

Primrose Building ,2nd Floor, Embassy Tech Village, Sarjapura Marathahalli Outer Ring Road,

Devarabeesanahalli, Bengaluru 560103, India

1.Static and F&DT; Engineer

Job Requirements

Technically the job involves investigating and producing F&DT; justifications solutions for simple and complex Primary Structural Elements (PSEs) of Wing Structure.

Following are the core responsibilities:

Work as team offshore member/Team Lead to Support the customer in F&DT; stress substantiation for Design deviations in the form of Engineering Analysis using established standards and working procedures

Responsible for delivery of high-quality Static justifications to time, cost and quality requirements

Liaise with the customer SPOC to discuss queries and seek feedback on work delivered.

Ensure Customer and Quest KPI are achieved.

Develop training plan as required and ensure quick job deployment of new Engr added to team.

Work Experience

Holds relevant technical qualifications (Bachelor, Master or equivalent) or a relevant level of experience to perform the stress engineering tasks.

2-10 years of experience with strong knowledge of airframe static stress including FEA & hand calculation methods.

Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.,)

Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)

Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases, Spectra generation.

Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules.

Ability to read the drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment to be useful for fatigue calculations.

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.,)

Develop, implement,



and check technical solutions and compliance documentation to ensure they are compliant with all relevant customer, regulatory, and airworthiness requirements, within agreed program, schedule, and manufacturing constraints.

Sound knowledge of airframe fatigue substantiation including safe life and fracture mechanics techniques

2.Static Stress Engineer

Holds relevant technical qualifications (Bachelor, Master or equivalent) or a relevant level of experience to perform the stress engineering tasks.

3-8 years of experience with strong knowledge of airframe static stress including FEA & hand calculation methods.

Sound knowledge of structural design principles, aircraft loads and Airbus manuals.

Experience in Static analysis of aircraft structural components (Airbus methods and tools would be preferable).

Sound knowledge of the overall static structural substantiation process from definition of external loads through airframe finite element analysis to final check stress clearance.

Sound knowledge of Airworthiness Requirements.

Working experience on creating stress justification reports and related stress hand calculations in consultation with Check/Approval signatories.

Have strong working knowledge of. Hypermesh, MSC Nastran, Patran, ISAMI,

Able to execute/check finite element modelling methodology, interpret results and generally design assure the model output.

Strong experience in Metallic - Linear & Non-Linear Static, analysis.

Added advantage with working knowledge of Automation tools like Python and

Supporting continuous improvement initiatives to increase team efficiency.

Support or generate test specifications/plans and/or alternate means of compliance (analysis/similarity) as required to demonstrate design solution complies with certification requirements.

3.Concession Stress Engineer

Hands-on execution of Aerostructures composite/Metallic stress concession In depth Knowledge of Stress requirements as per airbus methods

Tool Knowledge of ISAME Mathcad and SAP in depth Knowledge/work experience on Hand calculation in depth Knowledge of stress Justification to justify the design solution as per the customer methods & process

Good understanding of Design requirements (drawing reading etc)

Good Verbal and written English skills





Work experience on the for static and fatigue Stress Assessment

Understand the standards and working procedures applicable in concessions

Reporting and resolve the critical technical issues through customer methods

Coordinate with Design assessment team for stress solution verifications

Ability to understand Load path on Wing/fuselage structure

Having knowledge on Primary and Secondary Structures of AircraftWork Experience

Hands-on execution of Aerostructures composite/Metallic Wing concessions In depth Knowledge/work experience on stress dossier

Hands-on experience on handle and worked the aerospace concession project

Managing customer requirements & proposal support Guide & mentor team members

3.Concession Senior Design Engineer

Hands-on execution of Aerostructures composite/Metallic Wing concessions.

Identify the non conformance of concessions from design point of view and to solve the same.

In depth Knowledge/work experience on drawing reading.

In depth Knowledge/work experience of Design solution to transparent the non-conformance in the Customer concession Methods & Process.

Having knowledge of ATA chapter is added skill advantage In depth tool Knowledge/Handson execution on Catia, SAP, DPDS, Zamiz /AIRINA, VPM/PDM.

Managing customer requirements & proposal support Guide & mentor team members

Having knowledge on Primary and Secondary Structures of Aircraft.

Understand the standards and working procedures applicable in concessions.

Good understanding of Airbus standards (SRM/ASR) of working procedures applicable in Wing concessions

Coordinate with stress assessment team for design solution verifications.

Supporting ongoing continuous improvement initiatives to increase team Efficiency through methods, process and other capability improvements.

Responsible for Quality & KPI of the project

Analysis of production/ in-service non conformities (concession/repairs)

Monitoring the delivery excellence aspects of the project

Good understanding of Stress requirements.

Good Verbal and written English skills.

Note: If the above roles and responsibilities are not aligned with your skills and experience, please kindly ignore this email.

Basavaraj A Gowder

Talent Acquisition Team

Quest Global

PRIMROSE 7B, Embassy Tech Village, Sarjapura – Marathahalli Outer Ring Road,

Devarabeesanahalli, Bengaluru – 560103, India

M: +91 9071 71 71 79

E-mail: [email protected]| Follow us on: W: http://www.quest-global.com

Linked-In: https://www.linkedin.com/in/basavaraj-gouder-83265169

📌 Walk-in || Static and F&DT Engineer / Concession Stress & Design Engineer (Bengaluru)
🏢 Quest Global
📍 Bengaluru