Technical Committees / Committee F38/


Committee F38.01 on Airworthiness


Subcommittees and Standards

Showing results 1-10 of 10 matching ACTIVE standards under the jurisdiction of F38.01     F38 Home

F2411-07 Standard Specification for Design and Performance of an Airborne Sense-and-Avoid System

F2501-06 Standard Practices for Unmanned Aircraft System Airworthiness

F2505-07 Standard Practice for Application of Federal Aviation Administration (FAA) Federal Aviation Regulations Part 21 Requirements to Unmanned Aircraft Systems (UAS)

F2512-07 Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System

F2584-06 Standard Practice for Maintenance and Development of Maintenance Manuals for Light Unmanned Aircraft System (UAS)

F2585-08 Standard Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System
    See also WK20322 proposed revision

F2612-07 Standard Practice for Design and Manufacture of Turbine Engines for Unmanned Aircraft System

F2667-07 Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Unmanned Aircraft Systems

F2689-08 Standard Practice for Design and Manufacture of Reciprocating Spark Ignition Engines for Unmanned Aircraft Systems

F2690-08 Standard Guide for Suggested Procedures for Applying for a Flight Authority for an Unmanned Aircraft System: Part I and Part II

Showing results 1-6 of 6 matching Proposed New Standards under the jurisdiction of F38.01     F38 Home

WK7067 Continued Operational Safety Monitoring of the Light Unmanned Airplane Systems (UAS)

WK7977 Standard Practice for Design and Manufacture of Reciprocating Engines for Unmanned Aircraft Systems

WK13686 Guide for Suggested Procedures for Applying for a Special Certificate of Airworthiness (CofA) Experimental (UAS) or a Type Certificate for an Unmanned Aircraft System

WK13935 title

WK15881 Specification for Design and Performance of UAS Recovery Systems

WK16285 Specification for Design and Performance of an Unmanned Aircraft System-Class 1320 (550# Gross Weight to 1320# Gross Weight)



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