ASTM F3083/F3083M-20a

Standard Specification for Emergency Conditions, Occupant Safety and Accommodations

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: Historical
• Publication Date: 14-Oct-2020
• ICS: 49.020 - Aircraft and space vehicles in general
• Technical Committee: F44 - General Aviation Aircraft
• Drafting Committee: F44.30 - Structures

Standards Content (Sample)

NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: F3083/F3083M − 20a
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
Small 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 Oct. 15, 2020. Published November 2020. Originally Street NW, Washington, D.C. 20401, http://www.ecfr.gov.
4
approved in 2015. Last previous edition approved in 2020 as F3083/F3083M–20. Available from the European Aviation Safety Agency (EASA), Postfach 10 12
DOI: 10.1520/F3083_F3083M-20A. 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 [e-mail]. 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

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F3083/F3083M − 20a
4.1.2.2 The occupant experiences the static inertia loads 4.1.7.1 Ca
...

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 − 20 F3083/F3083M − 20a
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 Small 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 Aug. 15, 2020Oct. 15, 2020. Published September 2020November 2020. Originally approved in 2015. Last previous edition approved in
20192020 as F3083/F3083M–19.–20. DOI: 10.1520/F3083_F3083M-20.10.1520/F3083_F3083M-20A.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at [e-mail]. 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 − 20a
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
...