Location
Bangalore | India
Job description
Job Description :
- Static Analysis with Airbus Methods and Procedures.
- Minimum of 4 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)
- Minimum of 1 year execution experience on MSI, ESI, Hydraulic Brackets static stress analysis
- Hands on execution experience on GFEM Load extraction , DFEM Creation, Validation and Post processing
- Hands on execution experience on Metallic and composite primary/secondary structures
- Strong Fundamentals in hand calculations (e.g. HSB Methods)and strength of Materials (e.g. Brhun)
- Able to create calculation templates with aid of excel forumla and VBA Macro
- Exposure to Fatigue and Damage tolerance analysis
- Exposure to SRM, Repairs static justification and Concessions process
- Responsible for providing deliverables to specification, within agreed timescale, meeting the necessary quality standards and to customer satisfaction
- Responsible for mentoring and training the juniors
Primary Skills :
- ISAMI MODULES:MSP/MFA/MGF/FC/CFA/CSPS/ Non- Generic Modules
- ISAMI: Lug/Unfolding/FH/OH/Tension Fitting
- Excel Scripts (VBA) /Python/AWK - Value addition
- Patran and Hyperworks Pre/Postprocessing of a FEM results
- Nastran - SOL 101/103/105/400/106
Secondary Skills (Behavioral / Role Based) :
- Excellent verbal and written communication skills
- Work Collabrative working environment between onshore/offshore
- Can lead cross functional team
Job tags
Salary
