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Technical Committees / Committee F44 / Committee F44.30 on Structures Subcommittees and Standards
Showing results 1-0 of 0 matching ACTIVE standards under the jurisdiction of F44.30 F44 Home
Showing results 1-18 of 18 matching Proposed New Standards under the jurisdiction of F44.30 F44 Home WK41222 New Specification for Standard Specification for Airframe Strength Requirements of General Aviation Aircraft (Subpart C C01) WK41304 New Specification for Mass and Mass Distribution (C02) WK41305 New Specification for the Protection of Structure from Deterioration and Loss of Strength of General Aviation Aircraft (D03) WK41307 New Specification for Materials, Processes and Methods of Fabrication of General Aviation Aircraft.(D02) WK41308 New Specification for Special Factors of Safety of the Structure of General Aviation Aircraft (D04) WK41309 New Specification for Airspeeds used for determining the Flight Loads of General Aircraft Aircraft (C04) WK41310 New Specification for WK41311 New Specification for Electrical Bonding and Light Protection of General Aviation Aircraft (D07) WK41312 New Specification for Structure and Design Appendices for Part 23 General Aviation Aircraft (C11) WK41313 New Specification for Emergency Conditions and Occupant Safety WK41314 New Specification for Personnel and Cargo Accomadations and Occupant Safety Systems of General Aviation Aircraft (D05) WK41315 New Specification for Ground and Water Structural Load Requirements of the Airframe of General Aviation Aircraft(C07) WK41317 New Specification for Fatigue Loading of General Aviation Aircraft (C10) WK41321 New Specification for Engine Mount Structural Load Requirements of General Aviation Aircraft (C05) WK41323 New Specification for the Flight Control Structural Load Requirements for the Airframe (C06) WK41324 New Specification for Aeroelasticity Requirements of General Aviation Aircraft (C08) WK41325 New Specification for the General Design and Construction Requirements that Apply to all Parts and Assemblies of General Aviation Aircraft (D01) WK41326 New Specification for Flight Loads and Strength Requirements of the Airframe of General Aviation Aircraft(C03) | ||
