{"data":{"id":"us/14-cfr-25.119","jurisdiction":"us","citation":"14 CFR 25.119","heading":"Landing climb: All-engines-operating.","body":"In the landing configuration, the steady gradient of climb may not be less than 3.2 percent, with the engines at the power or thrust that is available 8 seconds after initiation of movement of the power or thrust controls from the minimum flight idle to the go-around power or thrust setting—\n(a) In non-icing conditions, with a climb speed of VREF determined in accordance with § 25.125(b)(2)(i); and\n(b) In icing conditions with the most critical of the landing ice accretion(s) defined in Appendices C and O of this part, as applicable, in accordance with § 25.21(g), and with a climb speed of VREF determined in accordance with § 25.125(b)(2)(ii).","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 25—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES","Subpart B—Flight"],"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":"9c371ced4f35606eb16d6419dc94b78b29bcc1ebc14fc1eac30e5c7f6bcb1f88","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-25.117","next":"us/14-cfr-25.121"},"notice":"GroundRules: Original legal text. Not legal advice."}