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ASTM F3083/F3083M-23a

(Specification)

Standard Specification for Emergency Conditions, Occupant Safety and Accommodations

Standard Specification for Emergency Conditions, Occupant Safety and Accommodations

ABSTRACT
This specification covers emergency conditions, occupant safety and accommodations for occupants and cargo. The applicant for a design approval must seek the individual guidance of their respective civil aviation authority (CAA) body concerning the use of this standard as part of a certification plan.
SCOPE
1.1 This specification addresses emergency conditions, occupant safety and accommodations for occupants and cargo.  
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 standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links.  
1.3 The values stated in either SI units or inch-pound units are to be regarded separately as standard. 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.

General Information

Status
Published
Publication Date
31-Aug-2023
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F44 - General Aviation Aircraft
Drafting Committee
F44.30 - Structures
Current Stage
Ref Project

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REDLINE ASTM F3083/F3083M-23a - Standard Specification for Emergency Conditions, Occupant Safety and AccommodationsREDLINE ASTM F3083/F3083M-23a - Standard Specification for Emergency Conditions, Occupant Safety and Accommodations
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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: F3083/F3083M − 23a
Standard Specification for
Emergency Conditions, Occupant Safety and
1
Accommodations
This standard is issued under the fixed designation F3083/F3083M; 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 F3061/F3061M Specification for Systems and Equipment in
Aircraft
1.1 This specification addresses emergency conditions, oc-
F3179/F3179M Specification for Performance of Aircraft
cupant safety and accommodations for occupants and cargo.
3
2.2 U.S. Code of Federal Regulations:
1.2 The applicant for a design approval must seek the
49 CFR Part 572 Anthropomorphic Test Devices (Subpart B)
individual guidance of their respective civil aviation authority
4
2.3 European Aviation Safety Agency Regulations:
(CAA) body concerning the use of this standard as part of a
CS-23 Certification Specifications for Normal, Utility,
certification plan. For information on which CAA regulatory
Aerobatic, and Commuter Category Aeroplanes (Amend-
bodies have accepted this standard (in whole or in part) as a
ment 3)
means of compliance to their airworthiness regulations (Here-
CS-VLA Certifications Specifications for Very Light Aero-
inafter referred to as “the Rules”), refer to ASTM F44 webpage
planes (Amendment 1)
(www.ASTM.org/COMITTEE/F44.htm) which includes CAA
2.4 Other Standards:
website links.
5
DOT/FAA/AR-00 Aircraft Materials Fire Test Handbook
1.3 The values stated in either SI units or inch-pound units
PH1.25 Standard Specifications for Safety Photographic
are to be regarded separately as standard. The values stated in
6
Film
each system are not necessarily exact equivalents; therefore, to
ensure conformance with the standard, each system shall be
3. Terminology
used independently of the other, and values from the two
3.1 See Terminology F3060 for definitions of terms used in
systems shall not be combined.
this standard.
1.4 This standard does not purport to address all of the
3.2 Abbreviations:
safety concerns, if any, associated with its use. It is the
3.2.1 g —peak deceleration for seat/restraint system test
responsibility of the user of this standard to establish appro-
p
priate safety, health, and environmental practices and deter-
3.2.2 HIC—head injury criteria
mine the applicability of regulatory limitations prior to use.
3.2.3 t —rise time to the peak deceleration, g
r p
1.5 This international standard was developed in accor-
dance with internationally recognized principles on standard-
4. Emergency Landing Conditions
ization established in the Decision on Principles for the
4.1 General:
Development of International Standards, Guides and Recom-
4.1.1 The airplane, although it may be damaged in emer-
mendations issued by the World Trade Organization Technical
gency landing conditions, must be designed as prescribed in
Barriers to Trade (TBT) Committee.
this section to protect each occupant under those conditions.
2. Referenced Documents
4.1.2 The structure must be designed to give each occupant
2
every reasonable chance of escaping serious injury when:
2.1 ASTM Standards:
4.1.2.1 Proper use is made of the seats, safety belts, and
F3060 Terminology for Aircraft
shoulder harnesses provided for in the design.
1
This specification is under the jurisdiction of ASTM Committee F44 on General
Aviation Aircraft and is the direct responsibility of Subcommittee F44.30 on
3
Structures. Available from U.S. Government Publishing Office (GPO), 732 N. Capitol
Current edition approved Sept. 1, 2023. Published September 2023. Originally Street NW, Washington, D.C. 20401, http://www.ecfr.gov.
4
approved in 2015. Last previous edition approved in 2023 as F3083/F3083M–23. Available from the European Aviation Safety Agency (EASA), Postfach 10 12
DOI: 10.1520/F3083_F3083M-23A. 53, D-50452 Cologne, Germany, https://www.easa.europa.eu/.
2 5
For referenced ASTM standards, visit the ASTM website, www.astm.org, or Available from Federal Aviation Administration (FAA), 800 Independence
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Ave., SW, Washington, DC 20591, http://www.faa.gov.
6
Standards volume information, refer to the standard’s Document Summary page on Available from American National Standards Institute (ANSI), 25 W. 43rd St.,
the ASTM website. 4th Floor, New York, NY 10036, http://www.ansi.org.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---
...

This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: F3083/F3083M − 23 F3083/F3083M − 23a
Standard Specification for
Emergency Conditions, Occupant Safety and
1
Accommodations
This standard is issued under the fixed designation F3083/F3083M; 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
1.1 This specification addresses emergency conditions, occupant safety and accommodations for occupants and cargo.
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 standard as part of a certification plan. For information on which CAA regulatory bodies have accepted
this standard (in whole or in part) as a means of compliance to their airworthiness regulations (Hereinafter referred to as “the
Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links.
1.3 The values stated in either SI units or inch-pound units are to be regarded separately as standard. 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
2
2.1 ASTM Standards:
F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in Aircraft
F3179/F3179M Specification for Performance of Aircraft
3
2.2 U.S. Code of Federal Regulations:
49 CFR Part 572 Anthropomorphic Test Devices (Subpart B)
4
2.3 European Aviation Safety Agency Regulations:
CS-23 Certification Specifications for Normal, Utility, Aerobatic, and Commuter Category Aeroplanes (Amendment 3)
CS-VLA Certifications Specifications for Very Light Aeroplanes (Amendment 1)
1
This specification is under the jurisdiction of ASTM Committee F44 on General Aviation Aircraft and is the direct responsibility of Subcommittee F44.30 on Structures.
Current edition approved Feb. 1, 2023Sept. 1, 2023. Published February 2023September 2023. Originally approved in 2015. Last previous edition approved in 20202023
as F3083/F3083M–20a. DOI: 10.1520/F3083_F3083M-23.–23. DOI: 10.1520/F3083_F3083M-23A.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
3
Available from U.S. Government Publishing Office (GPO), 732 N. Capitol Street NW, Washington, D.C. 20401, http://www.ecfr.gov.
4
Available from the European Aviation Safety Agency (EASA), Postfach 10 12 53, D-50452 Cologne, Germany, https://www.easa.europa.eu/.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F3083/F3083M − 23a
2.4 Other Standards:
5
DOT/FAA/AR-00 Aircraft Materials Fire Test Handbook
6
PH1.25 Standard Specifications for Safety Photographic Film
3. Terminology
3.1 See Terminology F3060 for definitions of terms used in this standard.
3.2 Abbreviations:
3.2.1 g —peak deceleration for seat/restraint system test
p
3.2.2 HIC—head injury criteria
3.2.3 t —rise time to the peak deceleration, g
r p
4. Emergency Landing Conditions
4.1 General:
4.1.1 The airplane, although it may be damaged in emergency landing conditions, must be designed as prescribed in this section
to protect each occupant under those conditions.
4.1.2 The structure must be designed to give each occupant every reasonable chance of escaping serious injury when:
4.1.2.1 Proper use is made of the seats, safety belts, and shoulder harnesses provided for in the design.
4
...

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SCOPE
1.1 This practice provides an acceptable means of meeting the airworthiness requirements for the flight design loads and conditions of small normal category level 1 and 2 aeroplanes. 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 practice are: Simplified Design Load Criteria, Acceptable Methods for Control Surface Loads Calculations, Acceptable Methods for Primary Control System Loads Calculations, and Control Surface Loading (Level 1 Aeroplanes).  
1.2 This practice is applicable to normal category, low-speed, level 1 and 2 aeroplanes. Use of the term aeroplane used throughout this practice will mean “normal category, low-speed, level 1 or 2 aeroplane,” unless otherwise stated.  
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 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 web page (www.astm.org/COMMITTEE/F44.htm).  
1.4 This document 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.  
1.5 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.

  • Standard
    12 pages
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  • Standard
    12 pages
    English language
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ASTM
ASTM F3117/F3117M-23a(Specification)
Standard Specification for Crew Interface in Aircraft

ABSTRACT
This specification covers international standards for the crew interface aspects of airworthiness and design for aircraft. 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.
The standards address pilot/occupant compartment; flight control systems controls; cockpit controls; motion and effect of cockpit controls; cockpit control knob shape; circuit breakers and fuses; master switch arrangement; flight control augmentation and auto flight system; primary flight information displays; primary flight guidance; and communication and audio systems. Also covered in this specification are pilot alerts; warning, caution, and advisory lights or indicators; continued airworthiness and maintenance; markings and placards; and airplane flight manual and approved manual material.
SCOPE
1.1 This specification covers international standards for the crew interface aspects of airworthiness and design for aircraft. “Crew” includes flight crew and maintenance crew. 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.  
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 specification (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to ASTM Committee F44 web page (https://www.astm.org/COMMITTEE/F44.htm).  
1.3 Units—This document 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.

  • Technical specification
    19 pages
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  • Technical specification
    19 pages
    English language
    sale 15% off