Data Analyst

• Nov 2022 - Present

Engineering Analyst

• 2017 - Nov 2022

Main Responsibilities: • Acted as first point of contact on Aircraft assembly line to quickly resolve production issues and promptly proposed solution to ensure continuous Aircraft assembly • Planned assembly sequence and accurately calculated labor and material requitement for entire Global 7500 production line at every five aircrafts • Accurately planned and prepared detailed instruction and product specifications for Structural, Electrical and Systems installations in SAP to build Aircraft to configuration • Liaised with Engineering, Quality, Suppliers and Production in order to resolve in-house and vendor technical problems and proposed continuous improvement opportunities to achieve maximum efficiency in Aircraft assembly and reduce reoccurring costs • Designed and developed Methods Organizational website to incorporate all Aircraft Manufacturing related technical information into one consistent source of information Extra Responsibilities (Data Analyst): • Successfully derived methodology and developed SQL queries to auto generate live reports of Aircraft Manufacturing System involving two (2) sub-systems resulting in improved Cycle Time for resolving Aircraft assembly line issues • Built visually impactful dashboards and reports to show meaningful and actionable information at Directors level using SQL and in-house reporting tools • Performed unprecedented comprehensive data mining and analysis on Non-conformances reports for the entire 2019 year in order to determine each function’s performance and drive strategies for turnaround time (TAT) improvement • Managed Dashboard and Reports for the Methods department consulted by Directors on daily basis to take immediate actions across department Show less

Engineering Professional Thermodynamics

• 2013 - 2015

• Served as a key member of the CSeries Integrated Product Development Team, earning a promotion to a lead role managing high and low pressure ducts, wing anti ice ducts, and finite element models (FEM) of the entire aircraft • Used NASTRAN and PATRAN to conduct thermal finite element analysis (FEA) • Built pneumatic models in Flowmaster to properly size ventilation ducts and determined pressure loss in high and low pressure ducts responsible for environment control system • Analyzed flow rate, pressure drop and temperature drop for wing anti-ice ducts by building thermal pneumatic model and performing simulation in Flowmaster • Conducted analyses on a variety of aerospace components including HVAC loads, air conditioner sizing, pressure loss, and thermal analysis • Tested and troubleshot the CL-415 environment control system through creation of a thermodynamic model for the Vapor Cycle Machine • Optimized and predicted ram air turbine (RAT) deployment performance through thermodynamic and heat transfer analysis on hydraulic fluid accumulator • Designed the tubes used on aircraft for high altitude ozone concentration testing by performing compressible fluid dynamic analysis • Accurately calculated a wide range of thermodynamic, heat transfer, fluid mechanic, and psychrometric figures • Reviewed the thermal performance analysis report for the CRJ900 new landing gear brake system in order to verify the analysis and determine design modifications and opportunities • Prepared technical reports and made engaging project presentations during staff meetings Show less

Mechanical Engineering Student

• 2007 - 2012

Capstone Engineering Project: MAV: Micro Air Vehicle (Fall 2011 – Winter 2012) • Designed the Propulsion System for the Micro Air Vehicle. • Tested propulsion system’s performance and performed flight tests. • Performed aerodynamic analysis of the airfoil. • Prepared technical reports. • Project Management. Design Proposal: Solar Powered Hybrid Vehicle (Winter 2012) • Designed proposal for a future internal combustion engine vehicle, which is environmentally friendly and fuel efficient. • Conducted research into current hybrid vehicles. • Implemented the solar panels alongside internal combustion engine to power the vehicle. Design Proposal: Advance Propulsion System for Spacecraft (Fall 2011) • Designed proposal for an advanced propulsion system to power future spaceships. • Conducted research into current propulsion systems for spacecraft. • Proposed The Dual Propulsion system: Nuclear and Electrical Propulsion combined. • Suggested the use of solar panels to generate electricity and power the electric propulsion system. Design of Landing Gear for Piper Aero IV (Fall 2010) • Redesigned the landing gear with reduced weight and maintain the minimum safety factor. • Project management. • Selection of proper material for the design. • Performed stress analysis on the landing gear. • Used FAR regulations to design the landing gear. Show less