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1.1 This specification covers international standards for ice protection aspects of airworthiness and design for “general aviation” aircraft.
1.2 The applicant for a design approval must seek the individual guidance of their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan. For information on which CAA regulatory bodies have accepted this specification (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/COMMITTEE/F44.htm) which includes CAA website links.
1.3 Units—The values are stated in units common to the field of aircraft icing. Typically SI or inch-pound units are used, but in some cases this has resulted in the use of mixed units due to the historical development of these values. In cases where values are given in one system with the other system following in brackets, the values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined.
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.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
Federal Standards14 CFR Part 33 (Amdt 34) Airworthiness Standards: Aircraft Engines 14 CFR Part 33 Rule 68 Airworthiness Standards: Induction System Icing
F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in Small Aircraft
F3066/F3066M Specification for Aircraft Powerplant Installation Hazard Mitigation
F3093/F3093M Specification for Aeroelasticity Requirements
F3117/F3117M Specification for Crew Interface in Aircraft
F3173/F3173M Specification for Aircraft Handling Characteristics
F3179/F3179M Specification for Performance of Aircraft
F3180/F3180M Specification for Low-Speed Flight Characteristics of Aircraft
F3231/F3231M Specification for Electrical Systems for Aircraft with Combustion Engine Electrical Power Generation
F3316/F3316M Specification for Electrical Systems for Aircraft with Electric or Hybrid-Electric Propulsion
ICS Number Code 49.045 (Structure and structure elements); 49.100 (Ground service and maintenance equipment)
UNSPSC Code 25130000(Aircraft)
|Link to Active (This link will always route to the current Active version of the standard.)|
ASTM F3120 / F3120M-20, Standard Specification for Ice Protection for General Aviation Aircraft, ASTM International, West Conshohocken, PA, 2020, www.astm.orgBack to Top