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 ollabrative working environment between onshore/offshore
Can lead cross functional team