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Standard Specification for Low-Speed Flight Characteristics of Aircraft
ASTM F3180/F3180M-25
Organization:
ASTM - ASTM International
Year: 2025
Abstract: This specification establishes the airworthiness design requirements for low-speed aeroplane flight characteristics. The applicant for a design approval shall seek the individual guidance to their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan.
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Standard Specification for Low-Speed Flight Characteristics of Aircraft
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| contributor author | ASTM - ASTM International | |
| date accessioned | 2025-09-30T19:20:57Z | |
| date available | 2025-09-30T19:20:57Z | |
| date copyright | 2025 | |
| date issued | 2025 | |
| identifier other | f3180_f3180m-25.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/342975 | |
| description abstract | This specification establishes the airworthiness design requirements for low-speed aeroplane flight characteristics. The applicant for a design approval shall seek the individual guidance to their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan. | |
| language | English | |
| title | Standard Specification for Low-Speed Flight Characteristics of Aircraft | en |
| title | ASTM F3180/F3180M-25 | num |
| type | standard | |
| status | Active | |
| tree | ASTM - ASTM International:;2025 | |
| contenttype | fulltext | |
| scope | 1.1 This specification covers the low-speed flight characteristics of fixed-wing aircraft and provides standards for departure characteristics, spinning, and stall warning. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on 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. The topics covered within this specification are: (Section 4) Applicability, (Section 5) Base Stall Characteristics and Stall Warning, (Section 6) Enhanced Single Engine Departure Characteristics, (Section 7) Enhanced Multiengine Departure Characteristics, (Section 8) Stall Characteristics and Spinning Characteristics for Aerobatic Aeroplanes, and (Section 9) Spin Characteristics for Aerobatic Aeroplanes. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval shall seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) 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 the ASTM Committee F44 webpage (www.astm.org/COMMITTEE/F44.htm). 1.3 Units—This standard may present information in either SI units, English Engineering units, or both; 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. | |
| identifier DOI | 10.1520/F3180_F3180M-25 |