Standard Specification for Installation and Integration of Propeller Systems
|Publication Date:||1 May 2015|
This specification addresses the airworthiness requirements for the installation and integration of propeller systems.
This specification is applicable to aeroplanes as defined in F44 terminology standard.
The applicant for a design approval must seek the individual
guidance to their respective CAA body concerning the use of this
standard as part of a certification plan. For information on which
CAA regulatory bodies have accepted this standard (in whole or in
part) as a means of compliance to their Small Aircraft
Airworthiness regulations (Hereinafter referred to as "the Rules"),
refer to ASTM F44 webpage (www.ASTM.org/COMITT
Units-The values stated are SI units followed by Imperial units in square brackets. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard.
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 determine the applicability of regulatory limitations prior to use.