Navigate / EASA

AMC1 ACNS.E.LAD.620 Integrity

ED Decision 2021/008/R

ACCEPTABLE MEANS OF COMPLIANCE APPLICABLE TO ALL SOLUTIONS

(a)     The erroneous automatic activation of the system should be considered a major failure condition.

(b)     The transmission of activation signals that contain an erroneous aircraft position or erroneous aircraft identification should be considered a minor failure condition.

(c)      The transmission of deactivation signals that contain erroneous aircraft identification should be considered a minor failure condition.

[Issue: CS-ACNS/3]