ASTM F3491-21
(Practice)Standard Practice for Enhanced Indication Methods in Aircraft
Standard Practice for Enhanced Indication Methods in Aircraft
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.
General Information
- Status
- Published
- Publication Date
- 31-Jul-2021
- Technical Committee
- F44 - General Aviation Aircraft
- Drafting Committee
- F44.10 - General
Relations
- Effective Date
- 01-Jan-2020
- Effective Date
- 01-Nov-2018
- Refers
ASTM F3180/F3180M-18 - Standard Specification for Low-Speed Flight Characteristics of Aircraft - Effective Date
- 01-Jun-2018
- Refers
ASTM F3180/F3180M-17 - Standard Specification for Low-Speed Flight Characteristics of Aircraft - Effective Date
- 15-Oct-2017
- Effective Date
- 01-Nov-2016
- Effective Date
- 01-Apr-2016
- Refers
ASTM F3180/F3180M-16 - Standard Specification for Low-Speed Flight Characteristics of Aeroplanes - Effective Date
- 01-Feb-2016
- Effective Date
- 15-Sep-2015
- Effective Date
- 01-May-2015
- Effective Date
- 01-Mar-2015
- Effective Date
- 01-Dec-2014
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
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Frequently Asked Questions
ASTM F3491-21 is a standard published by ASTM International. Its full title is "Standard Practice for Enhanced Indication Methods in Aircraft". This standard covers: 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.
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.
ASTM F3491-21 is classified under the following ICS (International Classification for Standards) categories: 49.020 - Aircraft and space vehicles in general. The ICS classification helps identify the subject area and facilitates finding related standards.
ASTM F3491-21 has the following relationships with other standards: It is inter standard links to ASTM F3060-20, ASTM F3117/F3117M-18c, ASTM F3180/F3180M-18, ASTM F3180/F3180M-17, ASTM F3060-16a, ASTM F3060-16, ASTM F3180/F3180M-16, ASTM F3060-15b, ASTM F3060-15a, ASTM F3060-15, ASTM F3060-14. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
ASTM F3491-21 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
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.
Designation: F3491 − 21
Standard Practice for
Enhanced Indication Methods in Aircraft
This standard is issued under the fixed designation F3491; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope responsibility of the user of this standard to establish appro-
priate safety, health, and environmental practices and deter-
1.1 This practice provides methods for how Enhanced
mine the applicability of regulatory limitations prior to use.
Indications are provided to the responsible crewmember when
1.6 This international standard was developed in accor-
an applicant uses these indications in support of compliance
dance with internationally recognized principles on standard-
with the requirements for Stall Characteristics, Stall Warning,
ization established in the Decision on Principles for the
and Spins applicable to Normal Category Aeroplanes, using
Development of International Standards, Guides and Recom-
Specification F3180/F3180M.
mendations issued by the World Trade Organization Technical
1.2 The specific types of enhanced indications identified in
Barriers to Trade (TBT) Committee.
Specification F3180/F3180M are as follows:
Type Description 2. Referenced Documents
2.1 ASTM Standards:
Angle of Attack Angle of attack indication
Angle of Attack Angle of attack indication with trend marker
2.1.1 The following is a list of external standards referenced
Pitch Limit Pitch limit indication displayed on attitude indication
throughout this practice. In all cases, later document revisions
Dynamic Low-Speed Indicated airspeed markings that change with
are acceptable if shown to be equivalent to the listed revision,
Markings flight condition
Airspeed Trend Indicated airspeed trend marker displayed on
or if otherwise formally accepted by the governing CAA;
airspeed indication
earlier revisions are not acceptable.
Flight Path Marker Flight path marker displayed on attitude indication
F3060 Terminology for Aircraft
LOC Alert Alert issued when loss of control likely within trend
window
F3180/F3180M Specification for Low-Speed Flight Charac-
teristics of Aircraft
1.3 An applicant intending to propose this information as
Means of Compliance for a design approval must seek guid- F3117/F3117M Specification for Crew Interface in Aircraft
ance from their respective oversight authority (for example, 2.2 SAE Standard:
published guidance from applicable civil aviation authority
ARP4102/7 Electronic Displays
(CAA) concerning the acceptable use and application thereof.
3. Terminology
For information on which oversight authorities have accepted
this practice (in whole or in part) as an acceptable Means of
3.1 Definitions—Terminology specific to this practice is
Compliance to their regulatory requirements (hereinafter “the
provided below. For general terminology, refer to Terminology
Rules”), refer to the ASTM Committee F44 web page
F3060.
(www.astm.org/COMMITTEE/F44.htm).
3.2 Definitions of Terms Specific to This Standard:
3.2.1 flight path marker, n—flight path marker shows the
1.4 Units—This document may present information in SI
aircraft’s predicted path based on horizontal and vertical speed,
units, English Engineering units, or both. The values stated in
heading, wind, and possibly other contributing factors.
each system are not necessarily exact equivalents; therefore, to
ensure conformance with the standard, each system shall be
4. Significance and Use
used independently of the other, and values from the two
systems shall not be combined.
4.1 The purpose of this practice is to discuss display or
functional characteristics, or both, of enhanced indications for
1.5 This standard does not purport to address all of the
low-speed awareness.
safety concerns, if any, associated with its use. It is the
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
This practice is under the jurisdiction of ASTM Committee F44 on General contact ASTM Customer Service at service@astm.org
...




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