{"data":{"id":"us/14-cfr-25.1327","jurisdiction":"us","citation":"14 CFR 25.1327","heading":"Magnetic direction indicator.","body":"(a) Each magnetic direction indicator must be installed so that its accuracy is not excessively affected by the airplane's vibration or magnetic fields.\n(b) The compensated installation may not have a deviation, in level flight, greater than 10 degrees on any heading.","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 F—Equipment"],"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":"ce07bce162a6e163df3984af66f06b801360869f2a7a0809f4fa4dd7be5f83f1","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-25.1326","next":"us/14-cfr-25.1329"},"notice":"GroundRules: Original legal text. Not legal advice."}