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CS 27.1195  Fire detector systems

ED Decision 2003/15/RM

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.
Details
Source-Title: CS 27.1195 Fire detector systems View latest amendments
Erulesid: ERULES-1963177438-4793 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 14 November, 2003
Entryintoforcedate: 14 November, 2003
Regulatorysource: ED Decision 2003/15/RM Navigate
Regulatorysubject: CS-27
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR