Standard Specification for Design and Testing of Light Sport Aircraft Propellers
Standard Specification for Design and Testing of Light Sport Aircraft Propellers
ABSTRACT This specification covers the establishment of the minimum requirements for the design, testing, and quality assurance of fixed-pitch or ground adjustable propellers for light sport aircraft. The propeller may not have design features that have been shown to be hazardous or unreliable unless the suitability of each questionable design detail or part can be established by tests. Strength testing; stress measurement, fatigue strength, and fatigue analysis, endurance testing, and teardown inspection shall be performed to meet the requirements prescribed. SCOPE 1.1 This specification covers the establishment of the minimum requirements for the design, testing, and quality assurance of fixed-pitch or ground adjustable propellers for light sport aircraft. These propellers are used on light aircraft, and could be used with engines conforming to Practice F2339. 1.1.1 When applying the additions provided in Appendix X1, this specification also covers the establishment of the minimum requirements for the design, testing and quality assurance of in-flight adjustable propellers for light-sport aircraft. 1.2 This specification is intended for use by manufacturers of propellers for light sport aircraft. 1.3 This specification does not address the airframe installation requirements for propellers. 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 to 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.
ASTM F2506-22: Standard Specification for Design and Testing of Light Sport Aircraft Propellers establishes the minimum requirements for the design, testing, and quality assurance of fixed-pitch and ground adjustable propellers specifically for light sport aircraft. Developed by ASTM International, this standard supports manufacturers in ensuring that propellers used in light sport aviation are safe, reliable, and durable throughout their operational lifecycle. The specification also provides optional requirements for in-flight adjustable propellers when referenced.
The standard aims to deliver comprehensive criteria for propeller construction, materials evaluation, performance testing, and required documentation, supporting global harmonization for manufacturers and regulators alike.
Design Requirements
Testing and Inspection
Quality Assurance
Documentation and Traceability
Scope and Limitations
ASTM F2506-22 is specifically targeted at manufacturers designing and producing propellers for light sport aircraft, ensuring propeller safety, performability, and durability. Key practical applications include:
Другие стандарты ASTM
Propeller Development and Certification
Regulatory Compliance
Operational Safety
Aftermarket Support
Adaptation for Adjustable Propellers
ASTM F2506-22 is internationally recognized and harmonized with principles set forth by the WTO Technical Barriers to Trade (TBT) Committee, providing manufacturers and stakeholders with a reliable reference for light sport aircraft propeller standards.
Keywords: ASTM F2506-22, light sport aircraft, aircraft propellers, propeller design, endurance testing, propeller standards, quality assurance, aviation safety, ground adjustable propeller, fixed-pitch propeller, in-flight adjustable propeller