{"data":{"id":"us/14-cfr-29.1015","jurisdiction":"us","citation":"14 CFR 29.1015","heading":"Oil tank tests.","body":"Each oil tank must be designed and installed so that—\n(a) It can withstand, without failure, any vibration, inertia, and fluid loads to which it may be subjected in operation; and\n(b) It meets the requirements of § 29.965, except that instead of the pressure specified in § 29.965(b)—\n(1) For pressurized tanks used with a turbine engine, the test pressure may not be less than 5 p.s.i. plus the maximum operating pressure of the tank; and\n(2) For all other tanks, the test pressure may not be less than 5 p.s.i.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT","Subpart E—Powerplant"],"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":"4ee66981e58d0a282b53f660935a2aa45244076066af851359229ae16434b796","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-29.1013","next":"us/14-cfr-29.1017"},"notice":"GroundRules: Original legal text. Not legal advice."}