• Design support is provided during the initial phase of the program by providing structural sizes for each component.
• Ensure the methodology's correctness, applicability, and compliance.
• Provide a 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 parts and critical path analysis.
• Maintain the fail-safe and safe-fail philosophy by establishing structural redundancy.
• Coordinate the component design with the methods, MRB, and liaison engineering procedures and requirements for manufacturability and repairability.
• Ensure the calculation and methodology are in compliance with governing authorities, such as FAR and JAR requirements.
• Produce a 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 ensures 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 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.

• 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 or components and maintain their current weight.
• Support design engineering in achieving the optimum design within the target weight.
• Provide mass property data for the movement of aircraft and components.
• Analyze the CG impact due to fuel migration.
• Verify aircraft buoyancy characteristics.
• Provide weight and balance.
• Provide weight, payload, and center of gravity.

• 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

Design to Build Aircraft Shipside and 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.

Interior  

• Galleys, Overhead Bins and Rails
• Floors, Floor Beams, Seats, Seat Tracks and Egress
• Partitions, Vestibules and Closets
• Baggage Compartment and Nets
• Cockpit, Cockpit Floor, Pilot Seats, Windshield Surround
• Bulkheads and Pressure Boundary

Exterior

• Wing, Wing Spar, Rib, Skin, Stringers, Pods and Racks
• Fuselage Frame, Cut-Outs, Skin, Stringer and Keel
• Empennage VSTAB, HSTAB, Dorsal Fin, Tail Cone, APU and Fairings
• Edges (FTE, FLE), Winglet

Mechanical Systems

• Doors (Pax & Cargo), Thrust Reverser, Aerial Refueling
• Feathers (Aileron, Spoiler, Flap, Rudder and Elevator)

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