{"data":{"id":"us/14-cfr-27.723","jurisdiction":"us","citation":"14 CFR 27.723","heading":"Shock absorption tests.","body":"The landing inertia load factor and the reserve energy absorption capacity of the landing gear must be substantiated by the tests prescribed in §§ 27.725 and 27.727, respectively. These tests must be conducted on the complete rotorcraft or on units consisting of wheel, tire, and shock absorber in their proper relation.","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 D—Design and Construction"],"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":"097cb63cac728915ba806fa5b81157baf3d24a2acc4a46185b8a273b9b7a089e","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.695","next":"us/14-cfr-27.725"},"notice":"GroundRules: Original legal text. Not legal advice."}