Skip to main content
  • Development of internal component design approaches (CCA partitioning, layout and mounting)
  • Evaluation of internal component clearances, tolerance analysis, interferences, potting gaps, and subassembly outlines
    Improved thermal conductivity of mounted components
  • Reliability improvement
  • Evaluation of repairability and maintainability
  • NASA Crew Launch Vehicle (CLV) System: Automatic Destruct Unit (ADU)
  • Army UH-60: Power Supply, CPU, and EMI filter for the EMC-101 avionics equipment
  • Army Forward Observation Vehicle (FOV): Vehicle Reference Unit (VRU)
  • Army M142 High Mobility Artillery Rocket System (HIMARS): Position Navigation Unit
  • Sikorsky CH-148: Blade Fold Actuator
  • Boeing 767: Actuation Control System
  • Test Program Set (TPS) – Test Requirement Documents (TRDs), Interface Test Adapter (ITA) Design, Atlas Test Programs, Test Strategy Reports and Software Documentation
  • Test Equipment and Support Equipment Design
  • Test Procedures, LABVIEW programming
  • Hardware and Test Software Integration
  • Qualification Testing: Test Procedures, Test Conduct and Reports
  • Design for Testability, Selection of Test Points and Improve Fault Detection and Fault Isolation
  • Re-host TPSs to advanced ATE
  • Support Depot (D) Level, Intermediate (I) Level and Organizational (O) Level Maintenance
  • AES has set exceptional quality standards
  • QA Manuals, Procedures, Method Sheets, Quality Audits and Training
  • Six Sigma Green Belt, Black Belt Certified
  • Statistical Process Control, Control Charts, Defects per Unit, Process Optimization, Pareto Analysis
  • AES’ Quality Management System (QMS) is certified to ISO 9001:2008 Standard

Technical Excellence & Commitment to our Warfighters

Partner with us for your aviation needs