AMC1 ACNS.C.PBN.101 Applicability
ED Decision 2019/011/R
RNAV certification is granted as follows:
(a) Aircraft that comply with the requirements of Subsection 2 comply with all the criteria of the RNAV 1, RNAV 2, and RNAV 5 specifications.
(b) Aircraft equipped with dual multi-sensor RNP systems which integrate inertial position source(s) that meet the criteria of Appendix B and which conform to the requirements of Subsection 2 comply with the criteria of the RNAV 10 specification.
(c) Aircraft that are equipped with dual stand-alone RNP systems with integrated GNSS sensors that comply with the requirements of Subsection 2, comply with the criteria of the RNAV 10 specification if the AFM (or equivalent) contains a requirement stating that:
— an approved fault detection and exclusion (FDE) availability-prediction program is used, and;
— the maximum allowable time for which FDE capability is projected to be unavailable is 34 minutes for any one occasion.
[Issue: CS-ACNS/2]
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