CS ACNS.C.PBN.605 System performance demonstration

• ED Decision 2019/011/R found in: GM Remote Aerodrome Air Traffic Services (ED 2019/004/R) Issue 2 (Jul 2020)

CS ACNS.C.PBN.605 System performance demonstration ED Decision 2019/011/R (See [AMC1 ACNS.C.PBN.605](#_DxCrossRefBm573002587) and [GM1 ACNS.C.PBN.605](#_DxCrossRefBm573002586)) The performance (including the RF function) of the aircraft’s system is demonstrated under a variety of operational, meteorological, and failure conditions, commensurate with the intended operation. Criteria for assessing RNP significant failures under design limit performance conditions are the following: (a) the lateral excursions observed as a result of probable failures are contained within a 1 × RNP corridor; (b) the lateral excursions observed as a result of one-engine-inoperative (OEI) are contained within a 1 × RNP corridor; (c) the lateral excursions observed as a result of remote failures are contained within a 2 × RNP corridor; and (d) a demonstration is made that the aircraft remains manoeuvrable and a safe extraction can be flown for all extremely remote failures. For criteria (a), (b), and (c) above, the vertical excursion does not exceed 75 feet below the desired path. [Issue: CS-ACNS/2]