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ASTM F 3298 : 2018

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Standard Specification for Design, Construction, and Verification of Fixed-Wing Unmanned Aircraft Systems (UAS)

Available format(s)

Hardcopy , PDF

Superseded date

04-04-2019

Superseded by

ASTM F 3298 : 2019

Language(s)

English

Published date

01-05-2018

€96.91
Excluding VAT

CONTAINED IN VOL. 15.11, 2018 Provides the airworthiness requirements for the design of fixed-wing unmanned aircraft systems.

Committee
F 38
DocumentType
Standard
Pages
30
PublisherName
American Society for Testing and Materials
Status
Superseded
SupersededBy

1.1This specification covers the airworthiness requirements for the design of fixed-wing unmanned aircraft systems. This specification defines the baseline design, construction, and verification requirements for an unmanned aircraft system (UAS).

1.2As a minimum, a UAS is defined as a system composed of the unmanned aircraft and all required on-board subsystems, payload, control station, other required off-board subsystems, any required launch and recovery equipment, all required crew members, and command and control (C2) links between UA and the control station.

1.3The intent is for this standard of practice for CAA, self- or third-party determinations of airworthiness for UAS. This specification provides the core requirements for airworthiness certification of lightweight (UAS) (not necessarily limited to UAs under 55 lb GTOW) or for certain CAA operational approvals using risk-based categories. Additional requirements are envisioned to address the requirements for expanded operations and characteristics not addressed by this specification.

1.4This specification is intended to support UAS operations. It is assumed that the risk of UAS will vary based on concept of operations, environment, and other variables. The fact that there are no human beings onboard the UAS may reduce or eliminate some hazards and risks. However, at the discretion of the CAA, this specification may be applied to other UAS operations.

1.5The values in Imperial units are to be regarded as the standard. The values in SI are for information only.

1.6This 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.

1.7This 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.

ASTM F 3196 : 2018 Standard Practice for Seeking Approval for Beyond Visual Line of Sight (BVLOS) Small Unmanned Aircraft System (sUAS) Operations
ASTM F 3366 : 2019 Standard Specification for General Maintenance Manual (GMM) for a small Unmanned Aircraft System (sUAS)
ASTM F 2908 : 2018 Standard Specification for Unmanned Aircraft Flight Manual (UFM) for an Unmanned Aircraft System (UAS)
ASTM F 3266 : 2018 Standard Guide for Training for Remote Pilot in Command of Unmanned Aircraft Systems (UAS) Endorsement

ASTM F 3005 : 2014 Standard Specification for Batteries for Use in Small Unmanned Aircraft Systems (sUAS)
ASTM F 3003 : 2014 Standard Specification for Quality Assurance of a Small Unmanned Aircraft System (sUAS) (Withdrawn 2023)
ASTM F 3178 : 2016 Standard Practice for Operational Risk Assessment of Small Unmanned Aircraft Systems (sUAS)
ASTM F 3201 : 2016 Standard Practice for Ensuring Dependability of Software Used in Unmanned Aircraft Systems (UAS)
ASTM F 2909 : 2014 Standard Practice for Maintenance and Continued Airworthiness of Small Unmanned Aircraft Systems (sUAS)

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