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1.1 This standard defines the production acceptance requirements for a small unmanned aircraft system (sUAS).
1.2 This standard is applicable to sUAS that comply with design, construction, and test requirements identified in Specification F2910. No sUAS may enter production until such compliance is demonstrated.
1.3 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.
F2585 Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System
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)
F2910 Specification for Design, Construction, and Test of a Small Unmanned Aircraft System (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)