{"data":{"id":"us/14-cfr-27.477","jurisdiction":"us","citation":"14 CFR 27.477","heading":"Landing gear arrangement.","body":"Sections 27.235, 27.479 through 27.485, and 27.493 apply to landing gear with two wheels aft, and one or more wheels forward, of the center of gravity.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT","Subpart C—Strength Requirements"],"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":"c09703851c64474b6fdb04ec994c30d342b0eb3c10764f6a842cdc875bad95ae","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.475","next":"us/14-cfr-27.479"},"notice":"GroundRules: Original legal text. Not legal advice."}