AMRITA MALLICK

Technical competence:

• Interpreting engineering drawings, repair drawings and manufacturer's specifications for varied ranges of Airbus aircraft
• Generate stress data based on static and F&DT point of view
• Performing Aircraft repair solutions and approval procedures (EASA Part 21)
• Providing repair solutions for accidental and environmental damages on both metallic and composite components like skin, frame, stringer, junction areas, door sill, door stops, gusset plate, lintel beam, door surrounds, potable and waste water service panels, APU access doors, firewall, hinge arm fittings, dorsal fin fairing, access panels
• Performing hand calculations for basic static and F&DT analysis
• Performing ISAMI analysis for various static ("Joint filled hole", "Beam properties", "Dent analysis") and F&DT ("1-D joint", "Initiation contouring", "Crack propagation", "Fillet hole analysis") modules
• Catering to deviations from SRM and/or production by providing rationals based on engineering judgment and analyses
• Analyzing different possible repair solutions, optimizing and making judgment keeping in mind safety, customer's requirements, feasibility of repair and cost effectiveness
• Optimizing structural performance through comprehensive evaluation of various materials, geometries, and loading conditions
• Re-analyzing from scratch the repair conditions beyond certification limits
• Collaborating with M&P, Systems, Aerodynamics and SRM experts whenever necessary.

Operational accomplishments:

• Managing complex technical activities autonomously
• Have highest work unit in the team since six months and counting
• Reduced material costs by optimizing repair designs through finite element analysis while avoiding part replacement
• Validating repair solutions, static and F&DT justifications and RDTS by compilers in RFE team
• Mentoring resources for introduction into composite structures
• Delivering AOG dossiers on time and with high quality
• Taken up the knowledge management focal role to increase and optimize efficiency of operations while ensuring effective capture and cascade of knowledge
• Mentoring junior engineers regarding best practices in stress analysis techniques, fostering an environment of continuous learning within the team
• Building and maintaining healthy relationship with all stakeholders including customers
• Adequate and timely communication with stakeholders
• Contributing towards healthy and professional environment.

Behavioral versatility:

• Acting efficiently under pressure environment
• Quick and creative in problem solving
• Collaborative way of working
• Effectively managing conflicts with stakeholders
• Constructive communication and influencing skills
• Solution oriented even in overwhelming situations.

Aerospace Structural Analysis Engineer, National Aerospace Laboratories (NAL) - Indigenous passenger aircraft SARAS MK II

• Part of R&D team for the project
• Creating 3D geometry and Finite Element Model (FEM) using HyperMesh and carrying out Finite Element Analysis (FEA) using MSC NASTRAN/PATRAN
• Performing hand calculations and design changes
• Performing FE analysis for both metallic and composite components
• Optimizing component designs for high performance while reducing material cost

Stress Engineer for Aerostructure Composite/Metallic Concessions - A350 XWB (Fuselage Side Shell-S13/S14 and S16/S18), AIRBUS

• Extracted material data, geometry details and fastener specifications from part & assembly drawings
• Handled non-conformities such as Flaking of glass ply, CFRP and copper foil; Thickness out of tolerance; Surface profile out of tolerance; Pressure mark; Fibre breakout; Flaking at hole edges; Unwanted drill start; Oversize fastener; Drilling/fastener not as per drawing
• Carried out KDF calculation and RF calculation for different failure modes such as strength, buckling, damage tolerance etc.
• Undergone entry level training on ISAMI.

Aerospace Structural Analysis Engineer Trainee

• Undergone training on aircraft structure, systems, mathematical modelling, FEM, FVM, simulation techniques and engineering mechanics of composite/metallic materials
• Designed aircraft structures and created FEM using Hypermesh and performed advanced stress analysis (FEA) on airframe using MSC NASTRAN/PATRAN
• Carried out metallic and composite stress analysis, fatigue analysis and repair stress analysis
• Undergone tool training on HyperMesh, MSC-NASTRAN/PATRAN.

Level 1 Reviewer for SRM (Structures Repair Manual) - AIRBUS

• Inspection of damage, identification and providing repair solutions for Airbus aircrafts
• Reviewed, identified and resolved problems in documents of teammates through root cause analysis and research
• Delivered in-depth training, imparted knowledge of best practices for meeting monthly targets and minimizing errors
• Imparted knowledge of best practices for meeting monthly targets and minimizing errors
• Always delivered workorders with more than 99% accuracy and 100% on time delivery (OTD)
• Reconstructed communication flow among 5 departments and cut down paperwork by 75%
• Validated results and performed quality assurance to assess accuracy of data
• Reviewed performance benchmarks and established metrics for future tracking
• Conducted workload assessments and devised new operational processes that led to a 40% increase in productivity.

Technical Author for AMM (Aircraft Maintenance Manual) and SRM (Structures Repair Manual) - AIRBUS

• Performed impact analysis, documentation, illustration, modification implementation and published technical reports
• Learned all the required knowledge on Airbus commercial aircrafts (Single Aisle (SA), Long Range (LR), Mega Body (MB) and Extra Wide Body (XWB)) from a technical point of view and implemented the same
• Certified as technical author in AMM and SRM Text
• Learned the art of solving problems with minimal errors within a very short period of time.