Dr. David Endler

Systems Engineering

SE-Knowledge

  • Systems Engineering
    • ISO/IEC 15288:2008, Systems and software engineering – System life cycle processes
    • ISO/IEC TR 19760:2003, Systems engineering – A guide for the application of ISO/IEC 15288 (System life cycle processes)
    • ISO/IEC 26702 (IEEE 1220), Systems engineering – Application and management of the systems engineering process
    • ANSI/EIA–632–1998 Processes for Engineering a System
    • INCOSE Systems Engineering Handbook, v3.2.2
    • MIL–STD 499C, Systems Engineering
    • FAA Systems Engineering Manual
    • Systems Engineering Fundamentals (Defense Acquisition University)
  • System Safety
    • MIL–STD 882C and E System Safety
    • SAE ARP 4761, Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment
    • ISO/IEC 26262 Road vehicles -- Functional safety
    • FAA System Safety Handbook
    • FAA Safety Risk Management Guidance for System Acquisitions (SRMGSA)
    • ESARR 4, Risk Assessment and Mitigation in ATM
  • Reliability and Maintainability
    • MIL–STD 785B, Reliability Program for Systems and Equipment Development and Production
    • MIL–STD 1629A, Procedures for Performing a Failure Mode, Effects and Criticality Analysis
    • SAE ARP 5580, Recommended Failure Modes and Effects Analysis (FMEA) Practices for Non–Automobile Applications
    • MIL–STD 470B, Maintainability Program for Systems and Equipment
    • MIL–HDBK 472, Maintainability Prediction
  • Configuration Management
    • MIL–STD 973, Configuration Management
    • MIL–HDBK 61B (Draft) Configuration Management Guidance
  • Aircraft Industry
    • SAE ARP 4754A, Guidelines For Development Of Civil Aircraft and Systems
    • SAE ARP 4754, Certification Considerations for Highly–Integrated or Complex Aircraft Systems
    • RTCA DO–160, Environmental Conditions and Test Procedures for Airborne Equipment
    • RTCA DO–254, Design Assurance Guidance for Airborne Electronic Hardware
    • EASA CS–25, Certification Specification
    • FAA FAR Part 25,
    • Airbus ABD0100 and ABD0200

“Worth It!”