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AMC1 ACNS.C.PBN.101 Applicability
Available versions for ERULES-1963177438-16501
ED Decision 2019/011/R
found in: GM Remote Aerodrome Air Traffic Services (ED 2019/004/R) Issue 2 (Jul 2020)
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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](#_DxCrossRefBm573002384) 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]