ASTM F3316/F3316M-18
(Specification)Standard Specification for Electrical Systems for Aircraft with Electric or Hybrid-Electric Propulsion
Standard Specification for Electrical Systems for Aircraft with Electric or Hybrid-Electric Propulsion
SCOPE
1.1 This specification covers the electrical systems, electrical equipment, and electrical power distribution aspects of airworthiness and design for aircraft with Electric or Hybrid-Electric Propulsion. This material was developed through open consensus of international experts in general aviation. This material was created by focusing on Normal Category Airplanes. 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 a means of compliance for 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 a Means of Compliance to their regulatory requirements (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMMITTEE/F44.htm).
1.3 Units—This standard may present information in either SI units, English Engineering units, or both; the values stated in each system may not be exact equivalents. Each system shall be used independently of the other; combining values from the two systems may result in nonconformance 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.
General Information
Relations
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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.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: F3316/F3316M −18
Standard Specification for
Electrical Systems for Aircraft with Electric or Hybrid-
1
Electric Propulsion
ThisstandardisissuedunderthefixeddesignationF3316/F3316M;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 2. Referenced Documents
2
2.1 ASTM Standards:
1.1 This specification covers the electrical systems, electri-
cal equipment, and electrical power distribution aspects of F2490–05Standard Guide forAircraft Electrical Load and
Power Source Capacity Analysis
airworthiness and design for aircraft with Electric or Hybrid-
ElectricPropulsion.Thismaterialwasdevelopedthroughopen F3060Terminology for Aircraft
F3061/F3061MSpecification for Systems and Equipment in
consensus of international experts in general aviation. This
material was created by focusing on Normal Category Air- Small Aircraft
F3066/F3066MSpecification forAircraft Powerplant Instal-
planes. The content may be more broadly applicable; it is the
responsibility of the applicant to substantiate broader applica- lation Hazard Mitigation
bility as a specific means of compliance. F3235Specification for Aircraft Storage Batteries
3
2.2 FAA Standard:
1.2 An applicant intending to propose this information as a
DOT/FAA/AR-00/12Aircraft Materials Fire Test Handbook
means of compliance for design approval must seek guidance
from their respective oversight authority (for example, pub-
3. Terminology
lishedguidancefromapplicableCAAs)concerningtheaccept-
3.1 Terminology specific to this specification is provided
able use and application thereof. For information on which
below. For general terminology, refer to Terminology F3060.
oversight authorities have accepted this standard (in whole or
in part) as a Means of Compliance to their regulatory require-
3.2 Definitions of Terms Specific to This Standard:
ments (Hereinafter referred to as “the Rules”), refer to ASTM
3.2.1 aircraft type code, n—anAircraft Type Code (ATC) is
F44 webpage (www.ASTM.org/COMMITTEE/F44.htm).
defined by considering both the technical considerations re-
garding the design of the aircraft and the airworthiness level
1.3 Units—This standard may present information in either
established based upon risk-based criteria; the method of
SI units, English Engineering units, or both; the values stated
defining an ATC applicable to this specification is defined in
ineachsystemmaynotbeexactequivalents.Eachsystemshall
Specification F3061/F3061M.
be used independently of the other; combining values from the
3.2.2 continued safe flight and landing, n—continued safe
two systems may result in nonconformance with the standard.
flight and landing as applicable to this specification is defined
1.4 This standard does not purport to address all of the
in Specification F3061/F3061M.
safety concerns, if any, associated with its use. It is the
3.2.3 Battery Management System (BMS)—a battery man-
responsibility of the user of this standard to establish appro-
agement system is any electronic system that manages a
priate safety, health, and environmental practices and deter-
rechargeable battery (cell or battery pack), such as by protect-
mine the applicability of regulatory limitations prior to use.
ing the battery from operating outside its Safe OperatingArea,
1.5 This international standard was developed in accor-
monitoring its state, calculating secondary data, reporting that
dance with internationally recognized principles on standard-
data,controllingitsenvironment,authenticatingitorbalancing
ization established in the Decision on Principles for the
it, or both.
Development of International Standards, Guides and Recom-
mendations issued by the World Trade Organization Technical
3.2.4 Electric Propulsion System (EPS)—installation that
Barriers to Trade (TBT) Committee.
includes at least one EPU and hardware required to produce
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Aviation Aircraft and is the direct responsibility of Subcommittee F44.50 on Standards volume information, refer to the standard’s Document Summary page on
Systems and Equipment. the ASTM website.
3
Current edition approved May 15, 2018. Published June 2018. DOI: 10.1520/ Available from Federal Aviation Administration (FAA), 800 Independence
F3316_F3316M-18. 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
---------------------- Pag
...
Questions, Comments and Discussion
Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.