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This specification establishes the design, construction, and test requirements for a small unmanned aircraft system (sUAS). It is intended for all sUAS that are permitted to operate over a defined area and in airspace authorized by a nation's governing aviation authority (GAA). Unless otherwise specified by a nationís GAA, this specification applies only to UA that have a maximum takeoff gross weight of 55 lb/25 kg or less.
This abstract is a brief summary of the referenced standard. It is informational only and not an official part of the standard; the full text of the standard itself must be referred to for its use and application. ASTM does not give any warranty express or implied or make any representation that the contents of this abstract are accurate, complete or up to date.
1.1 This specification defines the design, construction, and test requirements for a small unmanned aircraft system (sUAS).
1.2 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 and health practices and determine the applicability of regulatory limitations prior to use.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
F2908 Specification for Aircraft Flight Manual (AFM) for a Small Unmanned Aircraft System (sUAS)
F2909 Practice for Maintenance and Continued Airworthiness of Small Unmanned Aircraft Systems (sUAS)
F2911 Practice for Production Acceptance of a Small Unmanned Aircraft System (sUAS)
F3002 Specification for Design of the Command and Control System for Small Unmanned Aircraft Systems (sUAS)
F3003 Specification for Quality Assurance of a Small Unmanned Aircraft System (sUAS)
F3005 Specification for Batteries for Use in Small Unmanned Aircraft Systems (sUAS)
ICS Number Code 49.020 (Aircraft and space vehicles in general)