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About This Item

 

Full Description

1.1 This specification addresses the airworthiness requirements related to structural durability for the design of small aeroplanes. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Levels 1 through 4 Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance.

1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable Civil Aviation Authorities (CAAs), including the guidance noted in Appendix X2 Guidance Material) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this standard (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to ASTM F44 webpage (www.astm.org/COMMITTEE/F44.htm).

1.3 Units - This document may present information in either SI units, English Engineering units, or both; the values stated in each system may not be exact equivalents. Each system shall be used independently of the other; combining values from the two systems may result in nonconformance with the standard.

1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.

1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

 

Document History

  1. ASTM F3115/F3115M-23


    Standard Specification for Structural Durability for Small Aeroplanes

    • Most Recent
  2. ASTM F3115/F3115M-22


    Standard Specification for Structural Durability for Small Aeroplanes

    • Historical Version
  3. ASTM F3115/F3115M-20


    Standard Specification for Structural Durability for Small Aeroplanes

    • Historical Version
  4. ASTM F3115/F3115M-19

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    Standard Specification for Structural Durability for Small Aeroplanes

    • Historical Version
  5. ASTM F3115/F3115M-15


    Standard Specification for Structural Durability for Small Airplanes

    • Historical Version