ASTM F3491-21 PDF
Standard Practice for Enhanced Indication Methods in Aircraft
Standard Practice for Enhanced Indication Methods in Aircraft
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 2
- Дата публикации:
- 1 августа 2021 г.
- Издание:
- F3491
- ICS:
- 49.020
SIGNIFICANCE AND USE 4.1 The purpose of this practice is to discuss display or functional characteristics, or both, of enhanced indications for low-speed awareness. 4.2 The information in this practice may be used in developing enhanced indications that are part of the compliance approach for Normal Category Aeroplanes using Specification F3180/F3180M, Stall Warning, and Specification F3117/F3117M. SCOPE 1.1 This practice provides methods for how Enhanced Indications are provided to the responsible crewmember when an applicant uses these indications in support of compliance with the requirements for Stall Characteristics, Stall Warning, and Spins applicable to Normal Category Aeroplanes, using Specification F3180/F3180M. 1.2 The specific types of enhanced indications identified in Specification F3180/F3180M are as follows: Type Description Angle of Attack Angle of attack indication Angle of Attack Angle of attack indication with trend marker Pitch Limit Pitch limit indication displayed on attitude indication Dynamic Low-Speed Markings Indicated airspeed markings that change with flight condition Airspeed Trend Indicated airspeed trend marker displayed on airspeed indication Flight Path Marker Flight path marker displayed on attitude indication LOC Alert Alert issued when loss of control likely within trend window 1.3 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 civil aviation authority (CAA) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this practice (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm). 1.4 Units—This document may present information in 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. 1.5 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. 1.6 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 F3491-21: Standard Practice for Enhanced Indication Methods in Aircraft is an internationally recognized standard developed by ASTM International. This standard provides guidance on the use and implementation of enhanced indications for low-speed awareness and stall characteristics in normal category aeroplanes. It is particularly relevant to manufacturers and engineers aiming to comply with certification requirements using advanced cockpit displays and alerts as described in ASTM Specifications F3180/F3180M and F3117/F3117M.
Enhanced indications are crucial for improving flight safety, especially in complex flight conditions where clear, dynamic feedback to pilots can reduce the risk of loss of control, improve situational awareness, and support compliance with regulatory requirements.
Key Topics
Enhanced Indications Covered
ASTM F3491-21 identifies several types of enhanced cockpit indications intended for responsible crew members in support of regulatory compliance:
- Angle of Attack (AoA) Indication: Provides real-time feedback on the aircraft’s angle relative to airflow, helping to monitor stall margins.
- Angle of Attack with Trend Marker: Shows current AoA and predicted trends to enhance pilot decision-making.
- Pitch Limit Indication: Displays pitch limits on the attitude indicator, alerting pilots to safe operational boundaries.
- Dynamic Low-Speed Markings: Airspeed indications dynamically change based on current flight conditions, improving low-speed awareness.
- Airspeed Trend Marker: Presents the anticipated future airspeed as a trend on the primary airspeed indicator.
- Flight Path Marker: Projects the aircraft’s predicted flight path onto the attitude display, integrating information about velocity and direction.
- Loss of Control (LOC) Alert: Notifies the crew when loss of control is likely within a calculated future window, supplementing conventional stall alerts.
The standard discusses display and functional characteristics of these enhanced indications, emphasizing consistency in symbology and the importance of crew procedures for alerts, in alignment with referenced industry documents such as SAE ARP4102/7.
Applications
ASTM F3491-21 is primarily used in the development, evaluation, and certification of cockpit indication systems for normal category aeroplanes. Its applications include:
- Supporting Certification: Assisting applicants in demonstrating compliance with stall warning and low-speed flight characteristics as required by oversight authorities (e.g., aviation regulatory bodies).
- Design Guidance: Informing avionics manufacturers and design engineers about acceptable methods and best practices for implementing enhanced indications in aircraft displays.
- Crew Training and Procedures: Aiding in the development of flight crew operational procedures regarding the interpretation and response to enhanced indications and alerts.
- Flight Safety Enhancements: Contributing to the reduction of incidents related to stall, loss of situational awareness, and loss of control by providing pilots with real-time, predictive information.
Users intending to reference ASTM F3491-21 as a means of compliance for design approval should consult applicable authorities for acceptance and application requirements.
Related Standards
For optimal application and understanding, ASTM F3491-21 should be considered alongside the following key standards:
- ASTM F3180/F3180M: Specification for Low-Speed Flight Characteristics of Aircraft
- ASTM F3117/F3117M: Specification for Crew Interface in Aircraft
- SAE ARP4102/7: Recommended practices for electronic display markings and symbology
- ASTM F3060: Standard Terminology for Aircraft
These documents collectively provide a robust framework for aircraft cockpit indication systems, supporting safety, certification, and international harmonization.
Keywords: enhanced indication, aircraft indication standards, low-speed awareness, stall warning, cockpit display, angle of attack, airspeed trend, flight safety, ASTM F3491-21, normal category aeroplanes
Технические детали
- Технический комитет
- F44 - General Aviation Aircraft
- SKU
- ASTM F3491-21
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