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ASTM F2506-10e1

Historical Revision

Standard Specification for Design and Testing of Light Sport Aircraft Propellers (Withdrawn 2022)

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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.

1.2 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 and health practices and to determine the applicability of regulatory limitations prior to use.


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.


SDO ASTM: ASTM International
Document Number F2506
Publication Date May 15, 2010
Language en - English
Page Count 4
Revision Level 10e1
Supercedes
Committee F37.70
Publish Date Document Id Type View
Oct. 1, 2022 F2506-22 Revision
Sept. 1, 2013 F2506-13 Revision
May 15, 2010 F2506-10E01 Revision
May 15, 2010 F2506-10 Revision
Jan. 1, 2007 F2506-07 Revision