{"data":{"id":"us/14-cfr-25.1531","jurisdiction":"us","citation":"14 CFR 25.1531","heading":"Maneuvering flight load factors.","body":"Load factor limitations, not exceeding the positive limit load factors determined from the maneuvering diagram in § 25.333(b), must be established.","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 G—Operating Limitations and Information"],"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":"879eeb44efc96afa64936edb86ac4175a8114b20fb488d6b6b088e9ca0804600","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-25.1529","next":"us/14-cfr-25.1533"},"notice":"GroundRules: Original legal text. Not legal advice."}