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AMC2 ACNS.E.TAWS.010 Required functions

ED Decision 2013/031/R

In case of descent the TAWS should provide an automatic call out when descending through a predefined altitude (typically 150 m (500 ft) above terrain or above the elevation of nearest runway).

For a Class B TAWS in order to compensate for the lack of ‘excessive closure rate to terrain’ function the predefined altitude should be 500ft.
Details
Source-Title: AMC2 ACNS.E.TAWS.010 Required functions View latest amendments
Erulesid: ERULES-1963177438-15788 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: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS ACNS.E.TAWS.010 Required Functions and Interfaces
Origin: EASA
Category: EAR