{"data":{"id":"us/14-cfr-27.1195","jurisdiction":"us","citation":"14 CFR 27.1195","heading":"Fire detector systems.","body":"Each turbine engine powered rotorcraft must have approved quick-acting fire detectors in numbers and locations insuring prompt detection of fire in the engine compartment which cannot be readily observed in flight by the pilot in the cockpit.","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 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":"dd2887d828ac3c313db6b9f55794a2cef4049953054c5bdff060ba22f6ac68a9","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.1194","next":"us/14-cfr-27.1301"},"notice":"GroundRules: Original legal text. Not legal advice."}