ASTM F3083/F3083M-18
(Specification)Standard Specification for Emergency Conditions, Occupant Safety and Accommodations
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 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 may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard.
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.
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Designation:F3083/F3083M −18
Standard Specification for
Emergency Conditions, Occupant Safety and
1
Accommodations
ThisstandardisissuedunderthefixeddesignationF3083/F3083M;thenumberimmediatelyfollowingthedesignationindicatestheyear
of original adoption or, in the case of revision, the year of last revision.Anumber in parentheses indicates the year of last reapproval.
A superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope F3061/F3061MSpecification for Systems and Equipment in
Small Aircraft
1.1 This specification addresses emergency conditions, oc-
3
2.2 U.S. Code of Federal Regulations:
cupant safety and accommodations for occupants and cargo.
14 CFR Part 23Airworthiness Standards: Normal, Utility,
1.2 The applicant for a design approval must seek the
Aerobatic and Commuter Category Airplanes (Amend-
individual guidance of their respective CAA body concerning
ment 62)
the use of this standard as part of a certification plan. For
49CFRPart572AnthropomorphicTestDevices(SubpartB)
information on which CAA regulatory bodies have accepted
4
2.3 European Aviation Safety Agency Regulations:
this standard (in whole or in part) as a means of compliance to
CS-23 Certification Specifications for Normal, Utility,
their airworthiness regulations (Hereinafter referred to as “the
Aerobatic, and Commuter Category Aeroplanes (Amend-
Rules”), refer to ASTM F44 webpage (www.ASTM.org/
ment 3)
COMITTEE/F44.htm) which includes CAA website links.
CS-VLACertifications Specifications for Very Light Aero-
1.3 The values stated in either SI units or inch-pound units
planes (Amendment 1)
are to be regarded separately as standard. The values stated in
2.4 Other Standards:
5
each system may not be exact equivalents; therefore, each
DOT/FAA/AR-00Aircraft Materials Fire Test Handbook
system shall be used independently of the other. Combining
PH1.25Standard Specifications for Safety Photographic
values from the two systems may result in non-conformance
Film
with the standard.
3. Terminology
1.4 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the
3.1 See Terminology F3060 for definitions of terms used in
responsibility of the user of this standard to establish appro-
this standard.
priate safety, health, and environmental practices and deter-
3.2 Abbreviations:
mine the applicability of regulatory limitations prior to use.
3.2.1 g —peak deceleration for seat/restraint system test
p
1.5 This international standard was developed in accor-
3.2.2 HIC—head injury criteria
dance with internationally recognized principles on standard-
ization established in the Decision on Principles for the 3.2.3 t —rise time to the peak deceleration, g
r p
Development of International Standards, Guides and Recom-
4. Emergency Landing Conditions
mendations issued by the World Trade Organization Technical
Barriers to Trade (TBT) Committee.
4.1 General:
4.1.1 The airplane, although it may be damaged in emer-
2. Referenced Documents
gency landing conditions, must be designed as prescribed in
2
2.1 ASTM Standards: this section to protect each occupant under those conditions.
F3060Terminology for Aircraft 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
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral
shoulder harnesses provided for in the design.
Aviation Aircraft and is the direct responsibility of Subcommittee F44.30 on
Structures.
Current edition approved Dec. 1, 2018. Published December 2018. Originally
3
approved in 2015. Last previous edition approved in 2016 as F3083/F3083M–16. Available from U.S. Government Publishing Office (GPO), 732 N. Capitol
DOI: 10.1520/F3083_F3083M–18. Street NW, Washington, D.C. 20401, http://www.ecfr.gov.
2 4
For referenced ASTM standards, visit the ASTM website, www.astm.org, or Available from the EuropeanAviation SafetyAgency (EASA), Postfach 10 12
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM 53, D-50452 Cologne, Germany, https://www.easa.europa.eu/.
5
Standards volume information, refer to the standard’s Document Summary page on Available from Federal Aviation Administration (FAA), 800 Independence
the ASTM website. Ave., SW, Washington, DC 20591, http://www.faa.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3083/F3083M−18
4.1.2.2 The occupant experiences the static inertia loads 4.1.7.1 Can withstand a forward acting static ultimate iner-
corresponding to the following ultimate load factors: tia load factor of 18.0 g plus the maximum takeoff engine
thrust; or
(1)Upward,
...
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 − 16 F3083/F3083M − 18
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 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 may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the
two systems may result in non-conformance with the standard.
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 safety, health, and healthenvironmental 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
3
2.2 U.S. Code of Federal Regulations:
14 CFR Part 23 Airworthiness Standards: Normal, Utility, Aerobatic and Commuter Category Airplanes (Amendment 62)
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)
2.4 Other Standard:Standards:
5
DOT/FAA/AR-00 Aircraft Materials Fire Test Handbook
PH1.25 Standard SpecificationSpecifications 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
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 June 1, 2016Dec. 1, 2018. Published July 2016December 2018. Originally approved in 2015. Last previous edition approved in 20152016 as
F3083/F3083M – 15.F3083/F3083M–16. DOI: 10.1520/F3083_F3083M-16.10.1520/F3083_F3083M–18.
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’sstandard’s Document Summary page on the ASTM website.
3
Available from the U.S. Government Printing Office at www.ecfr.gov.Publishing Office (GPO), 732 N. Capitol Street NW, Washington, D.C. 20401, http://www.ecfr.gov.
4
Available from the European Aviation Safety Agency at www.easa.europa.eu.(EASA), Postfach 10 12 53, D-50452 Cologne, Germany, https://www.easa.europa.eu/.
5
Available from Federal Aviation Administration (FAA), 800 Independence Ave., SW, Washington, DC 20591, http://www.faa.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3083/F3083M − 18
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 und
...
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