Saturday, June 12, 2021
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Aerospace Engineering

Aircraft Stress Analysis

  • Design support during the initial phase of the program by providing structural sizes for each component.
  • Ensure the methodology correctness, applicability and compliance.
  • Provide margin of safety table for every metallic or composite component with the corresponding mode of failure, critical load case and free body diagram.
  • Provide critical part and critical path analysis.
  • Maintain fail safe and safe fail philosophy by establishing structural redundancy.
  • Coordinate the component design with the methods, MRB and laison engineering  procedures and requirements for manufacturability and repairability.
  • Ensure the calculation and methodology compliance with governing authorities such FAR and JAR requirements.
  • Produce Stress and Damage Tolerance Certification Report ensuring complete compliance.
  • Preparation of the structural finite element models for the generation of internal loads with realistic boundary conditions reflecting the drawing configuration.
  • Management of finite element models for both static and fatigue analysis.
  • Hand calculation of components based on client manuals or available open sources such as Bruhn, Timoshenko, Peterson, Roark and Niu, ensuring structural strength and stability.
  • Providing support for maintenance manuals and repair approval.
  • Creating automatic tools for calculation by using Excel and VBA in order to enhance the accuracy and the speed of calculation.
  • Providing support for test articles and test coupons.
  • Produce fatigue and reliability analysis based on the design service life using either client methods and procedures or available open sources such as Peterson.




Aircraft Weight Analysis

  • Weight management.
  • Weight control, analysis and reporting.
  • Inertia analysis.
  • Weight management plans.
  • Targets for work packages.
  • Supplier management.
  • Actual weighting.
  • Database management and tracking.
  • Predict, define, weigh, record and control all mass properties of the aircraft/components and maintain current weight.
  • Support Design Engineering in achieving the optimum design within the target weight.
  • Provide mass properties data for the movement of aircraft/components.
  • Analyze CG impact due to fuel migration.
  • Verify aircraft buoyancy characteristics.
  • Provide Weight and Balance.
  • Provide weight, payload and center of gravity.




Aircraft DER Services

  • FAR Parts 23, 25, 27 and 29
  • Certification Plan, TC and STC
  • Aircraft and Helicopter Major Alterations and Repairs
  • Stress Analysis Reports and Documentation
  • Design and New Part development Support
  • Addition of New Accessories
  • Finite Element Modeling
  • Avionic Rack Installations
  • Structural Repair Not in SRM
  • Law Enforcement Conversions
  • Electronic News Gathering
  • Airframe Modification
  • Ambulance Conversions
  • Airframe Conversion




Aircraft Electrical

Design to Build Aircraft Shipside & Interior Wiring Harnesses, Conforming to New EWIS Regulations.

  • Electrical Wire Interconnect System (EWIS) Including Electrical Wire Harness Design and Installation.
  • Design, Qualification and Documentation.
  • Project Management.
  • Advisory Services.




Aerostructural Experience


  • Galleys, Overhead Bins and Rails
  • Floors, Floor Beams, Seat, Seat Tracks and Egress
  • Partitions, Vestibules and Closets
  • Baggage Compartment and Nets
  • Cockpit, Cockpit Floor, Pilot Seats, Windshield Surround
  • Bulkheads and Pressure Boundary
  • Wing, Wing Spar, Rib, Skin, Stringers, Pods and Racks
  • Fuselage Frame, Cut-Outs, Skin, Stringer & Keel
  • Empennage VSTAB, HSTAB, Dorsal Fin, Tail Cone, APU & Fairings
  • Edges (FTE, FLE), Winglet
Mechanical Systems
  • Doors (Pax & Cargo), Thrust Reverser, Aerial Refuelling
  • Feathers (Aileron, Spoiler, Flap, Rudder & Elevator)




Design and Analysis Tools

  • Catia
  • Nastran, Linear and Non-Linear
  • Patran
  • Mathcad and MATLAB




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