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CS ACNS.D.EHS.020 Integrity

ED Decision 2013/031/R

The Mode S EHS airborne surveillance system integrity is designed commensurate with a ‘minor’ failure condition  for the downlink aircraft parameters listed in CS ACNS.D.EHS.015.

Details
Source-Title: CS ACNS.D.EHS.020 Integrity View latest amendments
Erulesid: ERULES-1963177438-15933 Compare versions
Domain: Air traffic management/Air navigation services
Applicabilitydate: 1 January, 2014
Entryintoforcedate: 1 January, 2014
Regulatorysource: ED Decision 2013/031/R Navigate
Regulatorysubject: CS-ACNS
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR