{"data":{"id":"us/14-cfr-22.110","jurisdiction":"us","citation":"14 CFR 22.110","heading":"Structural integrity.","body":"(a) The design and construction of the aircraft must provide sufficient structural integrity to enable safe operations within the aircraft's flight envelope throughout the aircraft's intended life cycle; and\n(b) The aircraft must be able to withstand all likely flight and ground loads, including towing and any aerial work operation, when operated within its operational limits.","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":"b55b6c748a901db0e5d2f12a2ccaa723706aab9ea498da69b6bb26180ed3c35d","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-22.105","next":"us/14-cfr-22.115"},"notice":"GroundRules: Original legal text. Not legal advice."}