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ASTM F3586-22

(Practice)

Standard Practice for Remote ID Means of Compliance to Federal Aviation Administration Regulation 14 CFR Part 89

Standard Practice for Remote ID Means of Compliance to Federal Aviation Administration Regulation 14 CFR Part 89<refdocr rid="r00001"/>

SIGNIFICANCE AND USE
3.1 The general approach to this practice is to serve as an “overlay” of requirements to the ASTM F3411-22a Standard Specification for Remote ID and Tracking by identifying mandatory portions, substituting values as needed, overriding items that may be optional, and providing additional requirements that are beyond the scope of Specification F3411, yet are necessary to provide proper guidance to meet the requirements set forth in Part 89.  
3.2 Furthermore, this practice provides additional details on minimal testing requirements for those submitting a DOC based on this MOC.
SCOPE
1.1 This practice provides a Means of Compliance (MOC) that gives sufficient clarity to the Unmanned Aircraft System (UAS) or Broadcast Module manufacturers to produce a compliant Remote ID (RID) System (RIDS) such that submitting a Declaration of Compliance2 (DOC) to this MOC will satisfy the requirements of the Federal Aviation Administration (FAA) 14 CFR Part 89 (Part 89) rule.3 This practice also explains what to expect from aircraft operating in compliance to this MOC.  
1.2 The FAA provided three options to comply with the Remote ID regulations: Standard Remote ID UAS, Remote ID Broadcast Modules, and FAA-recognized identification areas (FRIAs). The scope of this MOC is to cover both Standard RID and RID Broadcast Modules.  
1.3 The FRIA portion of the rule is out of scope since it provides a means to avoid the technical RID requirements by operating within administrative boundaries.  
1.4 Both SI and non-SI units are used in this document. Since this is an aviation standard and it addresses FAA rules, some units are used in preference of being consistent with industry and regulatory norms.  
1.5 Table of Contents:    
Title  
Section  
Scope  
1  
Referenced Documents  
2  
Significance and Use  
3  
Subset of Options in the F3411 Specification Considered  
4  
Requirements and Exceptions from the F3411 Specification  
5  
Alternative Applications of Specification F3411 to Meet Part 89
Requirements  
6  
MOC Requirements Not Covered by the Practice  
7  
Test Methods  
8  
Precision and Bias  
9  
Satisfaction of Rule Requirements  
10  
Keywords  
11  
ANNEX A1—Simulation Option for Accuracy Testing  
Annex A1  
APPENDIX X1—External Device for GCS Location Source Rationale  
Appendix X1  
APPENDIX X2—Power Level Rationale  
Appendix X2  
1.6 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.  
1.7 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-May-2022
ICS
03.220.50 - Air transport
49.020 - Aircraft and space vehicles in general
Technical Committee
F38 - Unmanned Aircraft Systems
Drafting Committee
F38.02 - Flight Operations
Current Stage
Ref Project

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ASTM F3586-22 - Standard Practice for Remote ID Means of Compliance to Federal Aviation Administration Regulation 14 CFR Part 89<refdocr rid="r00001"/>ASTM F3586-22 - Standard Practice for Remote ID Means of Compliance to Federal Aviation Administration Regulation 14 CFR Part 89<refdocr rid="r00001"/>
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ASTM F3586-22 - Standard Practice for Remote ID Means of Compliance to Federal Aviation Administration Regulation 14 CFR Part 89<refdocr rid="r00001"/>
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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: F3586 − 22
Standard Practice for
Remote ID Means of Compliance to Federal Aviation
1
Administration Regulation 14 CFR Part 89
This standard is issued under the fixed designation F3586; 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
Precision and Bias 9
Satisfaction of Rule Requirements 10
1.1 This practice provides a Means of Compliance (MOC)
Keywords 11
that gives sufficient clarity to the Unmanned Aircraft System ANNEX A1—Simulation Option for Accuracy Testing Annex A1
APPENDIX X1—External Device for GCS Location Source Ra- Appendix X1
(UAS) or Broadcast Module manufacturers to produce a
tionale
compliant Remote ID (RID) System (RIDS) such that submit-
APPENDIX X2—Power Level Rationale Appendix X2
2
ting a Declaration of Compliance (DOC) to this MOC will
1.6 This standard does not purport to address all of the
satisfy the requirements of the FederalAviationAdministration
safety concerns, if any, associated with its use. It is the
3
(FAA) 14 CFR Part 89 (Part 89) rule. This practice also
responsibility of the user of this standard to establish appro-
explains what to expect from aircraft operating in compliance
priate safety, health, and environmental practices and deter-
to this MOC.
mine the applicability of regulatory limitations prior to use.
1.2 The FAA provided three options to comply with the
1.7 This international standard was developed in accor-
Remote ID regulations: Standard Remote ID UAS, Remote ID
dance with internationally recognized principles on standard-
Broadcast Modules, and FAA-recognized identification areas
ization established in the Decision on Principles for the
(FRIAs).ThescopeofthisMOCistocoverbothStandardRID
Development of International Standards, Guides and Recom-
and RID Broadcast Modules.
mendations issued by the World Trade Organization Technical
1.3 The FRIA portion of the rule is out of scope since it
Barriers to Trade (TBT) Committee.
provides a means to avoid the technical RID requirements by
operating within administrative boundaries.
2. Referenced Documents
1.4 Both SI and non-SI units are used in this document.
4
2.1 ASTM Standard:
Since this is an aviation standard and it addresses FAA rules,
F3411 Specification for Remote ID and Tracking
some units are used in preference of being consistent with
2.2 Other Documents:
industry and regulatory norms.
14 CFR Part 89 Remote Identification of Unmanned Air-
1.5 Table of Contents:
3
craft
Title Section
5
47 CFR Part 15 Radio Frequency Devices
Scope 1
Referenced Documents 2 Advisory CircularAC 89-2 Declaration of Compliance Pro-
2
Significance and Use 3
cess for Remote Identification of Unmanned Aircraft
Subset of Options in the F3411 Specification Considered 4
ANSI/CTA-2063-A Small Unmanned Aerial Systems Serial
Requirements and Exceptions from the F3411 Specification 5
6
Alternative Applications of Specification F3411 to Meet Part 89 6
Numbers
Requirements
TechnicalStandardOrderTSO-C199 TrafficAwarenessBea-
MOC Requirements Not Covered by the Practice 7
7
con System (TABS)
Test Methods 8
1 4
This practice is under the jurisdiction ofASTM Committee F38 on Unmanned For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Aircraft Systems and is the direct responsibility of Subcommittee F38.02 on Flight contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Operations. Standards volume information, refer to the standard’s Document Summary page on
Current edition approved June 1, 2022. Published July 2022. DOI: 10.1520/ the ASTM website.
5
F3586-22. Available from https://www.ecfr.gov/current/title-47/chapter-I/subchapter-A/
2
See FAA Advisory Circular 89-2, https://www.faa.gov/documentLibrary/ part-15.
6
media/Advisory_Circular/AC_89-2.pdf. Available from Consumer Technology Association, 1919 S. Eads Street,
3
Available from https://www.federalregister.gov/documents/2021/01/15/2020- Arlington, VA 22202, https://www.cta.tech/.
7
28948/remote-identification-of-unmanned-aircraft. Portions of Part 89 are repro- Available from https://rgl.faa.gov/Regulatory_and_Guidance_Library/
duced (in italics) in Section 7 and Appendix X1. rgTSO.nsf/0/1600df588a6f53ae86257d710070d105/$FILE/TSO-C199.pdf.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F3586 − 22
8
WGS-84 World Geodetic System 5.1.2 Either (or
...

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ASTM F3411-22a(Specification)
Standard Specification for Remote ID and Tracking

SCOPE
1.1 This specification covers the performance requirements for remote identification (Remote ID) of unmanned aircraft systems (UAS). Remote ID allows governmental and civil identification of UAS for safety, security, and compliance purposes. The objective is to increase UAS remote pilot accountability by removing anonymity while preserving operational privacy for remote pilots, businesses, and their customers. Remote ID is an enabler of enhanced operations such as beyond visual line of sight (BVLOS) operations as well as operations over people.  
1.2 This specification defines message formats, transmission methods, and minimum performance standards for two forms of Remote ID: broadcast and network. Broadcast Remote ID is based on the transmission of radio signals directly from a UAS to receivers in the UAS’s vicinity. Network Remote ID is based on communication by means of the internet from a network Remote ID service provider (Net-RID SP) that interfaces directly or indirectly with the UAS, or with other sources in the case of intent-based network participants.  
1.3 This specification addresses the communications and test requirements of broadcast or network Remote ID, or both, in UAS and Net-RID SP systems.  
1.4 Applicability:  
1.4.1 This specification is applicable to UAS that operate at very low level (VLL) airspace over diverse environments including but not limited to rural, urban, networked, network degraded, and network denied environments, regardless of airspace class.  
1.4.2 This specification neither purports to address UAS operating with approval to use ADS-B or secondary surveillance radar transponders, nor does it purport to solve ID needs of UAS for all operations.  
1.4.3 In particular, this specification does not purport to address identification needs for UAS that are not participating in Remote ID or operators that purposefully circumvent Remote ID.  
1.5 The values stated in SI units are to be regarded as standard. The values given in parentheses after SI units are provided for information only and are not considered standard.  
1.5.1 Units of measurement included in this specification:    
m  
meters  
deg, °  
degrees of latitude and longitude, compass direction  
s  
seconds  
Hz  
Hertz (frequency)  
dBm  
decibel-milliwatts (radio frequency power)  
ppm  
parts per million (radio frequency variation)  
μs  
microseconds  
ms  
milliseconds  
1.6 Table of Contents:    
Title  
Section  
Scope  
1  
Referenced Documents  
2  
Terminology  
3  
Remote ID and Network Interoperability Conceptual Overview  
4  
Performance Requirements  
5  
TEST METHODS  
Scope  
6  
Significance and Use  
7  
Hazards  
8  
Test Units  
9  
Procedure  
10  
Precision and Bias  
11  
Product Marking  
12  
Packaging and Package Marking  
13  
Keywords  
14  
ANNEX A1—Broadcast Authentication Verifier Service  
Annex A1  
ANNEX A2—Network Remote ID Interoperability Requirements, APIs, and Testing  
Annex A2  
ANNEX A3—Tables of Values  
Annex A3  
ANNEX A4—USS-DSS and USS-USS OpenAPI YAML Description  
Annex A4  
ANNEX A5—Number Registrar Management Policy  
Annex A5  
APPENDIX X1—Performance Characteristics  
Appendix X1  
APPENDIX X2—List of Subcommittee Participants and Contributors  
Appendix X2  
APPENDIX X3—Background Information  
Appendix X3  
1.7 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. Some specific hazards statements are given in Section 8 on Hazards.  
1.8 This international standard was developed in accordance with internationally recognized principles on standardization established in the D...

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ASTM F3478-20(Practice)
Standard Practice for Development of a Durability and Reliability Flight Demonstration Program for Low-Risk Unmanned Aircraft Systems (UAS) under FAA Oversight

SIGNIFICANCE AND USE
4.1 Demonstration plans developed in accordance with this practice will include all necessary content and key considerations to support an effective flight demonstration program aimed at approval or certification of UAS by the FAA through D&R demonstration.  
4.2 This practice does not address planning requirements for UAS development testing. It is assumed that a manufacturer has completed all UAS design and development and is preparing demonstration programs to support compliance demonstration on a stable and controlled system configuration. Manufacturers who wish to prepare a detailed design and development program should review Specification F3298 for programmatic examples.  
4.3 This practice is intended to be used on low-risk UAS that meet the following design criteria and operating limitations.  
4.3.1 The UAS has a command and control link that enables the pilot-in-command to take contingency action.  
4.3.2 The unmanned aircraft (UA) has a kinetic energy of ≤25 000 ft-lb calculated in accordance with methods specified within the MOC.  
4.3.3 The UA is operated ≤400 ft above ground level (AGL).  
4.3.4 No operations over open-air assemblies (operations over people are acceptable).  
4.3.5 No flight into known icing.  
4.3.6 Maximum of 20:1 aircraft to pilot ratio.  
4.3.7 The UA is electrically powered (excludes internal combustion engines and fuel cells).
SCOPE
1.1 This standard practice is intended for low-risk UAS seeking type certification by the Federal Aviation Administration (FAA) under 14 CFR Part 21.17(b) in accordance with the FAA durability and reliability (D&R) means of compliance (MOC). The definition of “low-risk UAS” does not necessarily align with other definitions found within corresponding ASTM standards (F3442/F3442M) or other UAS-related standards. For the purposes of this practice, “low-risk” is defined as a UAS operated in accordance with the concept of operations (CONOPs), eligibility criteria, and kinetic energy threshold specified in the G-1 Issue Paper (which will be provided to the applicant by the FAA). See 4.3 for design criteria and operating limitations for low-risk UAS.  
1.2 This standard practice establishes a common methodology and key considerations for the development of minimum flight plans for low-risk UAS that demonstrate aircraft reliability as part of a D&R MOC.  
1.3 The scope of this standard practice encompasses D&R planning, data collection, and reporting.  
1.4 The values stated in SI units are to be regarded as standard. This is not intended to limit the systems of units used for design, development testing, or demonstration testing. However, the units of measurement used on pilot-facing placards and markings and manuals must be the same as those used on the corresponding equipment with recognition that international aviation utilizes feet for altitude and knots for airspeed as operational parameters.  
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.

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ASTM F3411-22a(Specification)
Standard Specification for Remote ID and Tracking

SCOPE
1.1 This specification covers the performance requirements for remote identification (Remote ID) of unmanned aircraft systems (UAS). Remote ID allows governmental and civil identification of UAS for safety, security, and compliance purposes. The objective is to increase UAS remote pilot accountability by removing anonymity while preserving operational privacy for remote pilots, businesses, and their customers. Remote ID is an enabler of enhanced operations such as beyond visual line of sight (BVLOS) operations as well as operations over people.  
1.2 This specification defines message formats, transmission methods, and minimum performance standards for two forms of Remote ID: broadcast and network. Broadcast Remote ID is based on the transmission of radio signals directly from a UAS to receivers in the UAS’s vicinity. Network Remote ID is based on communication by means of the internet from a network Remote ID service provider (Net-RID SP) that interfaces directly or indirectly with the UAS, or with other sources in the case of intent-based network participants.  
1.3 This specification addresses the communications and test requirements of broadcast or network Remote ID, or both, in UAS and Net-RID SP systems.  
1.4 Applicability:  
1.4.1 This specification is applicable to UAS that operate at very low level (VLL) airspace over diverse environments including but not limited to rural, urban, networked, network degraded, and network denied environments, regardless of airspace class.  
1.4.2 This specification neither purports to address UAS operating with approval to use ADS-B or secondary surveillance radar transponders, nor does it purport to solve ID needs of UAS for all operations.  
1.4.3 In particular, this specification does not purport to address identification needs for UAS that are not participating in Remote ID or operators that purposefully circumvent Remote ID.  
1.5 The values stated in SI units are to be regarded as standard. The values given in parentheses after SI units are provided for information only and are not considered standard.  
1.5.1 Units of measurement included in this specification:    
m  
meters  
deg, °  
degrees of latitude and longitude, compass direction  
s  
seconds  
Hz  
Hertz (frequency)  
dBm  
decibel-milliwatts (radio frequency power)  
ppm  
parts per million (radio frequency variation)  
μs  
microseconds  
ms  
milliseconds  
1.6 Table of Contents:    
Title  
Section  
Scope  
1  
Referenced Documents  
2  
Terminology  
3  
Remote ID and Network Interoperability Conceptual Overview  
4  
Performance Requirements  
5  
TEST METHODS  
Scope  
6  
Significance and Use  
7  
Hazards  
8  
Test Units  
9  
Procedure  
10  
Precision and Bias  
11  
Product Marking  
12  
Packaging and Package Marking  
13  
Keywords  
14  
ANNEX A1—Broadcast Authentication Verifier Service  
Annex A1  
ANNEX A2—Network Remote ID Interoperability Requirements, APIs, and Testing  
Annex A2  
ANNEX A3—Tables of Values  
Annex A3  
ANNEX A4—USS-DSS and USS-USS OpenAPI YAML Description  
Annex A4  
ANNEX A5—Number Registrar Management Policy  
Annex A5  
APPENDIX X1—Performance Characteristics  
Appendix X1  
APPENDIX X2—List of Subcommittee Participants and Contributors  
Appendix X2  
APPENDIX X3—Background Information  
Appendix X3  
1.7 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. Some specific hazards statements are given in Section 8 on Hazards.  
1.8 This international standard was developed in accordance with internationally recognized principles on standardization established in the D...

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ASTM F3478-20(Practice)
Standard Practice for Development of a Durability and Reliability Flight Demonstration Program for Low-Risk Unmanned Aircraft Systems (UAS) under FAA Oversight

SIGNIFICANCE AND USE
4.1 Demonstration plans developed in accordance with this practice will include all necessary content and key considerations to support an effective flight demonstration program aimed at approval or certification of UAS by the FAA through D&R demonstration.  
4.2 This practice does not address planning requirements for UAS development testing. It is assumed that a manufacturer has completed all UAS design and development and is preparing demonstration programs to support compliance demonstration on a stable and controlled system configuration. Manufacturers who wish to prepare a detailed design and development program should review Specification F3298 for programmatic examples.  
4.3 This practice is intended to be used on low-risk UAS that meet the following design criteria and operating limitations.  
4.3.1 The UAS has a command and control link that enables the pilot-in-command to take contingency action.  
4.3.2 The unmanned aircraft (UA) has a kinetic energy of ≤25 000 ft-lb calculated in accordance with methods specified within the MOC.  
4.3.3 The UA is operated ≤400 ft above ground level (AGL).  
4.3.4 No operations over open-air assemblies (operations over people are acceptable).  
4.3.5 No flight into known icing.  
4.3.6 Maximum of 20:1 aircraft to pilot ratio.  
4.3.7 The UA is electrically powered (excludes internal combustion engines and fuel cells).
SCOPE
1.1 This standard practice is intended for low-risk UAS seeking type certification by the Federal Aviation Administration (FAA) under 14 CFR Part 21.17(b) in accordance with the FAA durability and reliability (D&R) means of compliance (MOC). The definition of “low-risk UAS” does not necessarily align with other definitions found within corresponding ASTM standards (F3442/F3442M) or other UAS-related standards. For the purposes of this practice, “low-risk” is defined as a UAS operated in accordance with the concept of operations (CONOPs), eligibility criteria, and kinetic energy threshold specified in the G-1 Issue Paper (which will be provided to the applicant by the FAA). See 4.3 for design criteria and operating limitations for low-risk UAS.  
1.2 This standard practice establishes a common methodology and key considerations for the development of minimum flight plans for low-risk UAS that demonstrate aircraft reliability as part of a D&R MOC.  
1.3 The scope of this standard practice encompasses D&R planning, data collection, and reporting.  
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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.

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ASTM F3450-20(Guide)
Standard Guide for Flight Hazard and Surveillance Systems Personnel Certification

SIGNIFICANCE AND USE
4.1 The guide is intended to be used to assess competencies of qualified individuals who wish to become certified as an FHSS technician through a certification program.  
4.2 The guide is intended to be used in concert with a certification provider’s structure and materials for management, exam delivery, and candidate preparation.
SCOPE
1.1 The purpose of this guide is to address the basic fundamental subject knowledge activities and functions for avionics professionals to be titled Flight Hazard and Surveillance Systems (FHSS) Technicians.  
1.2 This guide does not cover weather detection and avoidance systems. These systems will be addressed in a future Aircraft Electronics Technician (AET) endorsement standard.  
1.3 This guide is the basis for the FHSS certification, an endorsement to the AET certification. Candidates must be a certified AET to take the certification exam associated with this guide.  
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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ASTM A370-23(Test Method)
Standard Test Methods and Definitions for Mechanical Testing of Steel Products

SIGNIFICANCE AND USE
4.1 The primary use of these test methods is testing to determine the specified mechanical properties of steel, stainless steel, and related alloy products for the evaluation of conformance of such products to a material specification under the jurisdiction of ASTM Committee A01 and its subcommittees as designated by a purchaser in a purchase order or contract.  
4.1.1 These test methods may be and are used by other ASTM Committees and other standards writing bodies for the purpose of conformance testing.  
4.1.2 The material condition at the time of testing, sampling frequency, specimen location and orientation, reporting requirements, and other test parameters are contained in the pertinent material specification or in a general requirement specification for the particular product form.  
4.1.3 Some material specifications require the use of additional test methods not described herein; in such cases, the required test method is described in that material specification or by reference to another appropriate test method standard.  
4.2 These test methods are also suitable to be used for testing of steel, stainless steel and related alloy materials for other purposes, such as incoming material acceptance testing by the purchaser or evaluation of components after service exposure.  
4.2.1 As with any mechanical testing, deviations from either specification limits or expected as-manufactured properties can occur for valid reasons besides deficiency of the original as-fabricated product. These reasons include, but are not limited to: subsequent service degradation from environmental exposure (for example, temperature, corrosion); static or cyclic service stress effects, mechanically-induced damage, material inhomogeneity, anisotropic structure, natural aging of select alloys, further processing not included in the specification, sampling limitations, and measuring equipment calibration uncertainty. There is statistical variation in all aspects of mechanical testin...
SCOPE
1.1 These test methods2 cover procedures and definitions for the mechanical testing of steels, stainless steels, and related alloys. The various mechanical tests herein described are used to determine properties required in the product specifications. Variations in testing methods are to be avoided, and standard methods of testing are to be followed to obtain reproducible and comparable results. In those cases in which the testing requirements for certain products are unique or at variance with these general procedures, the product specification testing requirements shall control.  
1.2 The following mechanical tests are described:    
Sections  
Tension  
7 to 14  
Bend  
15  
Hardness  
16  
Brinell  
17  
Rockwell  
18  
Portable  
19  
Impact  
20 to 30  
Keywords  
32  
1.3 Annexes covering details peculiar to certain products are appended to these test methods as follows:    
Annex  
Bar Products  
Annex A1  
Tubular Products  
Annex A2  
Fasteners  
Annex A3  
Round Wire Products  
Annex A4  
Significance of Notched-Bar Impact Testing  
Annex A5  
Converting Percentage Elongation of Round Specimens to
Equivalents for Flat Specimens  
Annex A6    
Testing Multi-Wire Strand  
Annex A7  
Rounding of Test Data  
Annex A8  
Methods for Testing Steel Reinforcing Bars  
Annex A9  
Procedure for Use and Control of Heat-cycle Simulation  
Annex A10  
1.4 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.  
1.5 When these test methods are referenced in a metric product specification, the yield and tensile values may be determined in inch-pound (ksi) units then converted into SI (MPa) units. The elongation determined in inch-pound gauge lengths of 2 in. or 8 in. may be report...

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ASTM F3565-23(Practice)
Standard Practice for Electrofusion Joining Polyethylene (PE) Pipe and Fittings for Pressure Pipe Service

SIGNIFICANCE AND USE
4.1 Using the procedures and apparatus in Sections 8 and 9 and the manufacturer's instructions, pressure-tight joints as strong as the pipe itself can be made between manufacturer-recommended combinations of pipe and fittings. See Specification F1055 for performance requirements of polyethylene electrofusion fittings.
SCOPE
1.1 This practice describes procedures for making joints suitable for pressure service with polyethylene (PE) pipe and fittings by means of electrofusion joining techniques in, but not limited to, a field environment. Other suitable electrofusion joining procedures are available from various sources including fitting manufacturers. This standard does not purport to address all possible electrofusion joining procedures, or to preclude the use of qualified procedures developed by other parties that have been proven to produce reliable electrofusion joints. (Note 1)
Note 1: Reference to the manufacturer in this practice refers to the electrofusion fitting manufacturer.  
1.2 The parameters and procedure are applicable only to joining polyethylene pipe and fittings (Note 2) which are intended for PE fuel gas pipe per Specification D2513 and PE potable water, sewer and industrial pipe manufactured per Specification F714, Specification D3035, Specification F2619, and AWWA C901 and C906.
Note 2: Commercially available materials classified with a thermoplastic pipe material designation code beginning with PE 14, PE 23, PE 24, PE 27, PE 33, PE 34, PE 36, and PE 46, and PE 47 in accordance with Specification D3350 and Terminology F412 are generally acceptable for electrofusion joining using this practice. Consult with the pipe or fitting manufacturer for specific compatibility information.  
1.3 Parts that are within the dimensional tolerances given in present ASTM specifications are required to produce sound joints between polyethylene pipe and fittings when using the joining techniques described in this practice.  
1.4 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.  
1.5 The text of this practice references notes, footnotes, and appendices which provide explanatory material. These notes and footnotes (excluding those in tables and figures) shall not be considered as requirements of the practice.  
1.6 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.  
1.7 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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ASTM
ASTM D5141-23(Test Method)
Standard Test Method for Determining Filtering Efficiency and Flow Rate of the Filtration Component of a Sediment Retention Device

SIGNIFICANCE AND USE
5.1 This test method is used to determine the filtering efficiency and flow rate of the filtration component of a sediment retention device, such as a silt fence, a silt barrier, or a silt curtain, for specific soil tested.  
5.2 This test method may be used for the design of the filtration component of a sediment retention device to meet requirements of regulatory agencies in filtering efficiency or flow rate for the specific soil tested.  
5.2.1 The designer can use this test method to determine the spacing between sediment retention devices.  
5.3 This test method is intended for performance evaluation, as the results will depend on the specific soil evaluated. Unless testing with the default soil is desired, it is recommended that the user or representative perform the test to pre-approve products, as sediment retention device manufacturers are not typically equipped to handle or test soil requirements.  
5.4 This test method provides a means of evaluating the filtration component of sediment retention devices with different soils under various conditions that simulate the conditions that exist in a sediment retention device installation. This test method may be used to simulate several storm events on the same sediment retention device specimen. Therefore, the number of times this test is repeated per specimen is dependent upon the user and the site conditions.
SCOPE
1.1 This test method is used to determine the filtering efficiency and the flow rate of the filtration component of a sediment retention device, such as a silt fence, silt barrier, or inlet protector.  
1.1.1 The results are shown as a percentage for filtering efficiency and cubic metres per square metre per minute (m3/m2/min) or gallons per square foot per minute (gal/ft2/min) for flow rate.  
1.1.2 The filtering efficiency indicates the percent of sediment removed from sediment-laden water.  
1.1.3 The flow rate is the average rate of passage of the sediment-laden water through the filtration component of a sediment retention device.  
1.2 This test method requires several specialized pieces of equipment, such as an integrated water sampler and an analytical balance, or a vacuum filtration system. At the client’s discretion, the test soil is either a site-specific soil or a soil that is representative of a target default gradation.  
1.3 The values stated in SI units are the standard, while the inch-pound units are provided for information. The values expressed in each system may not be exact equivalents; therefore, each system must be used independently of the other, without combining values in any way.  
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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ASTM
ASTM F2647-07(2023)(Guide)
Standard Guide for Approved Methods of Installing a CVS (Central Vacuum System)

SIGNIFICANCE AND USE
4.1 The suggestions of this guide are intended to provide proper installation materials and practices to be used during the installation of a central-vacuum system.
SCOPE
1.1 This guide demonstrates proper methods for installing a central-vacuum system.  
1.2 Appendix X1 contains additional sources of information that may be helpful to the user of this guide.  
1.3 The values stated in inch-pound units are to be regarded as the standard. The values given in parentheses are for information only.  
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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ASTM
ASTM F2886-17(2023)(Specification)
Standard Specification for Metal Injection Molded Cobalt-28Chromium-6Molybdenum Components for Surgical Implant Applications

ABSTRACT
This specification covers chemical, mechanical, and metallurgical general requirements for metal injection molded (MIM) cobalt-28chromium-6molybddenum components to be used in manufacturing surgical implants. In this specification, the MIM components covered may have been densified beyond their as-sintered density by post-sinter processing. For the chemical requirements, the components supplied in this specification must conform in accordance to the chemical requirements specified herein in Table 1. The product analysis tolerances must also conform to the product tolerances presented in Table 2. The specification also enumerates the mechanical requirements for MIM components wherein the tensile properties of the MIM must conform to the mechanical properties in Table 3. The microstructural requirements and specimen preparation shall be in accordance with Guide E3 and Practice E407.
SCOPE
1.1 This specification covers chemical, mechanical, and metallurgical requirements for metal injection molded (MIM) cobalt-28chromium-6molybdenum components to be used in the manufacture of surgical implants  
1.2 The MIM components covered by this specification may have been densified beyond their as-sintered density by post-sinter processing.  
1.3 Units—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 nonconformance with the standard.  
1.4 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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