ASTM F3657-23 PDF
Standard Specification for Verification of Lightweight Unmanned Aircraft Systems (UAS)
Standard Specification for Verification of Lightweight Unmanned Aircraft Systems (UAS)
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 13
- Дата публикации:
- 1 декабря 2023 г.
- Издание:
- F3657
- Технический комитет:
- F38 - Unmanned Aircraft Systems
SCOPE 1.1 This specification covers the airworthiness requirements for the design of light unmanned aircraft systems. This specification defines the baseline verification requirements for an unmanned aircraft system (UAS). 1.2 As 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. 1.3 The 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) 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. 1.4 This 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. 1.5 Units—The values in Imperial units are to be regarded as the standard. The values in SI are for information only. 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.
Abstract
Overview
ASTM F3657-23: Standard Specification for Verification of Lightweight Unmanned Aircraft Systems (UAS) provides an internationally recognized baseline for verifying the airworthiness of light UAS. Developed by ASTM Committee F38, this standard outlines the core requirements to ensure the safety and reliability of unmanned aircraft systems, supporting compliance with national and international aviation regulations. The specification covers design verification, operational limitations, documentation, and testing procedures fundamental to lightweight UAS certification and approval.
Key Topics
- Airworthiness Requirements: Defines baseline criteria for UAS components, subsystems, command and control (C2) links, and associated launch, recovery, and operational support systems.
- System Verification: Requires manufacturers and applicants to use a combination of analysis, inspection, demonstration, and testing to verify functional performance and compliance.
- Risk-Based Approvals: Supports Civil Aviation Authorities (CAA), self-, or third-party airworthiness determinations using operational risk categories for lightweight UAS.
- Comprehensive Documentation: Specifies requirements for maintaining clear records, including flight manuals, maintenance logs, verification reports, and configuration control throughout the UAS lifecycle.
- Operating Limitations: Enforces detailed operational boundaries such as speed, altitude, payload, and environmental conditions to ensure safe UAS use.
- Best Practices: Introduces verification practices for performance, stability, controllability, component strength, and resilience under normal and emergency scenarios.
Applications
The ASTM F3657-23 standard is highly relevant for multiple stakeholders in the unmanned aircraft system sector, offering practical value for:
- Manufacturers and Developers: Enables systematic verification of UAS airworthiness and supports initial type certification, product improvements, and compliance with global aviation requirements.
- Aviation Authorities and Regulators: Provides a common framework to assess and approve lightweight UAS for various operational scenarios, including those beyond visual line of sight (BVLOS) or operations over people.
- Operators and Service Providers: Facilitates safe and documented deployment of UAS in commercial, public safety, research, and industrial applications by ensuring rigorous pre-flight and operational checks.
- Third-Party Assessors and Consultants: Establishes criteria for independent or self-assessment, contributing to transparent, risk-based airworthiness evaluations, and acceptance for expanded or specialized UAS operations.
This standard additionally guides organizations in creating and maintaining practices for documentation control, maintenance, upgrade verification, and safe operational procedures-building stakeholder confidence and streamlining regulatory interactions.
Related Standards
ASTM F3657-23 references and aligns with several key standards to provide a cohesive approach to UAS verification and operation, including:
- ASTM F2908: Unmanned Aircraft Flight Manual specification, ensuring clear and complete operational documentation.
- ASTM F2909: Continued Airworthiness of Lightweight UAS, supporting ongoing safe operation and maintenance.
- ASTM F3002: Command and Control System Design for Small UAS, addressing reliable communications and control requirements.
- ASTM F3201: Dependability of Software Used in UAS, focusing on assurance in onboard software functions.
- CS-LUAS/CS-LURS: EASA Certification Specifications for light unmanned systems.
- FAA Order 8130.34D / 14 CFR Part 107: Federal Aviation Administration requirements for UAS airworthiness and operational authorizations.
- ANSI Z535.1: Safety colors for warning and hazard information.
Summary
ASTM F3657-23 elevates the safety and reliability standards for lightweight unmanned aircraft systems in design, manufacturing, operation, and verification. Compliance ensures that UAS are properly verified for airworthiness, documented for regulatory approval, and prepared for diverse operational conditions, promoting trust among operators, regulators, and end users alike. For organizations and professionals engaged in UAS development, operation, or regulation, adhering to ASTM F3657-23 facilitates safer skies and streamlined market acceptance.
Технические детали
- SKU
- ASTM F3657-23
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