ASTM F3180/F3180M-21 PDF
Standard Specification for Low-Speed Flight Characteristics of Aircraft
Standard Specification for Low-Speed Flight Characteristics of Aircraft
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 26
- Дата публикации:
- 1 августа 2021 г.
- Издание:
- F3180/F3180M
- ICS:
- 49.020
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. This specification is applicable to small aeroplanes and covers departure characteristics, spinning, and stall warning. 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: (4.1) Low-Speed Flight Characteristics Score, (4.2) Stall Characteristics, (4.3) Stall Warning, (4.4) Departure Characteristics: Single Engine, (4.5) Departure Characteristics: Multiengine, (4.6) Spinning, and (4.7) Safety-Enhancing Features. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval must 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.
Abstract
Overview
ASTM F3180/F3180M-21: Standard Specification for Low-Speed Flight Characteristics of Aircraft sets forth comprehensive airworthiness requirements for the low-speed flight characteristics of fixed-wing, small aircraft. The standard, developed through international consensus under ASTM Committee F44, is primarily aimed at normal category aeroplanes in general aviation, but its methodologies may be adopted more broadly upon substantiation by the applicant and acceptance by relevant civil aviation authorities (CAAs).
This specification provides a structured means for aircraft developers, certification applicants, and regulatory authorities to measure, evaluate, and verify safe and controllable aircraft behavior during critical low-speed flight phases such as stalls, spins, and departures from controlled flight. It emphasizes clear guidance for compliance, incorporates a points-based evaluation, and recommends safety-enhancing features to support modern aviation safety practices.
Key Topics
Low-Speed Flight Characteristics The heart of ASTM F3180/F3180M-21 is its focus on low-speed flight dynamics, including:
- Stall Characteristics: Evaluation of controllability and recovery in straight, turning, and accelerated stalls.
- Stall Warning: Requirements for early, clear warning systems to alert pilots before loss of lift occurs.
- Departure Characteristics: Guidance to prevent inadvertent departures from controlled flight for both single- and multi-engine aircraft, utilizing alternative demonstration and scoring methods.
- Spinning: Criteria for spin entry behavior, spin recovery, and the handling of aeroplanes approved for aerobatics.
- Safety-Enhancing Features: Options for additional onboard systems that improve pilot awareness and reduce loss-of-control risks.
Scoring and Compliance The standard introduces a points-based system to quantify compliance:
- Low-Speed Flight Characteristics Score: Summed from stall warning, departure characteristics, and safety-enhancing features scores.
- Minimum Scores: Vary according to aircraft certification level, engine number, and aerobatic approval status.
- Means of Compliance: Applicants must consult their CAA about the use and acceptability of this standard in their certification approach.
Guidance and Applicability
- Applicants must use either SI or English units consistently; mixing units is not permitted.
- The Standard applies predominantly to normal category aircraft but can be referenced for broader types with proper justification.
- Not all safety, health, or environmental issues are addressed-users must verify regulatory fit for their region.
Applications
Certification and Aircraft Design
- Regulatory Approval: Serves as a reference or means of compliance for demonstrating low-speed safety in type certification plans, as recognized by CAAs such as the FAA and EASA.
- Aircraft Development: Offers manufacturers a clear framework to design or modify fixed-wing small aircraft, ensuring control and warning systems meet stringent performance criteria.
- Flight Testing: Guides flight test engineers in conducting and documenting specific maneuvers, stall warnings, and recovery scenarios in line with internationally harmonized standards.
Safety and Training
- Pilot Training: Provides a framework for establishing minimum low-speed handling qualities, essential for standardizing flight training curriculum and improving pilot proficiency.
- System Integration: Encourages the incorporation of advanced stall warning, flight envelope protection, and pilot awareness technology to further decrease the risk of loss-of-control accidents.
Related Standards
Referencing and complementing ASTM practices and other international standards, ASTM F3180/F3180M-21 works in conjunction with:
- ASTM F3060: Terminology for Aircraft
- ASTM F3061/F3061M: Systems and Equipment in Small Aircraft
- ASTM F3083/F3083M: Emergency Conditions and Occupant Safety
- ASTM F3117/F3117M: Crew Interface in Aircraft
- ASTM F3173/F3173M: Aircraft Handling Characteristics
- ASTM F3179/F3179M: Performance of Aircraft
- ASTM F3230: Safety Assessment for Systems and Equipment in Small Aircraft
- ASTM F3232/F3232M: Flight Controls in Small Aircraft
- FAA AC 23-15A & AC 23-8C: Guidance on small airplane certification and flight test compliance
Keywords: low-speed flight characteristics, aircraft stall behavior, spin resistance, stall warning systems, aircraft departure characteristics, aircraft certification, ASTM aviation standards, safety-enhancing features, small aircraft airworthiness, aviation compliance.
For updated acceptance of this standard by oversight authorities, refer to the ASTM Committee F44 webpage.
Технические детали
- Технический комитет
- F44 - General Aviation Aircraft
- SKU
- ASTM F3180/F3180M-21
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