{"data":{"id":"us/14-cfr-22.185","jurisdiction":"us","citation":"14 CFR 22.185","heading":"Quality assurance system.","body":"The aircraft must have been designed, produced, and tested under a documented quality assurance system to ensure each product and article conforms to its design and is in a condition for safe operation.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 22—DESIGN, PRODUCTION, AND AIRWORTHINESS REQUIREMENTS FOR NON-TYPE CERTIFICATED AIRCRAFT","Subpart B—Light-Sport Category Aircraft"],"source_url":"https://www.ecfr.gov/api/versioner/v1/full/2026-08-25/title-14.xml","current_through":"2026-08-25","vintage":"","retrieved_at":"2026-08-27T02:24:20Z","sha256":"c4049822a6e67a5c66b2d59805839af3b9a79acd6228aed172a0f786cafddd78","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-22.180","next":"us/14-cfr-22.190"},"notice":"GroundRules: Original legal text. Not legal advice."}