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CS 23.2540 Flight in icing conditions

ED Decision 2017/013/R

An applicant who requests certification for flight in icing conditions must show the following in the icing conditions for which certification is requested:

(a) the ice protection system provides for safe operation; and

(b) the aeroplane design must provide protection from stalling when the autopilot is operating.
Details
Source-Title: CS 23.2540 Flight in icing conditions View latest amendments
Erulesid: ERULES-1963177438-6855 Compare versions
Domain: Initial airworthiness
Amendedby: Amendment 5
Applicabilitydate: 15 August, 2017
Entryintoforcedate: 15 August, 2017
Regulatorysource: ED Decision 2017/013/R Navigate
Regulatorysubject: CS-23
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR
Related sections: