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AMC1 CAT.POL.A.235 Landing -- dry runways
Available versions for ERULES-1963177438-19642
ED Decision 2022/012/R
found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Sep 2023)
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AMC1 CAT.POL.A.235 Landing — dry runways ED Decision 2022/012/R FACTORING OF AUTOMATIC LANDING DISTANCE PERFORMANCE DATA In those cases where the landing requires the use of an automatic landing system, and the distance published in the AFM includes safety margins equivalent to thse contained in [CAT.POL.A.235](#_DxCrossRefBm318086302), the landing mass of the aeroplane should be the lesser of: (a) the landing mass determined in accordance with [CAT.POL.A.235](#_DxCrossRefBm318086302); or (b) the landing mass determined for the automatic landing distance for the appropriate surface condition, as given in the AFM or equivalent document. Increments due to system features such as beam location or elevations, or procedures such as use of overspeed, should also be included.
AMC1 CAT.POL.A.235 Landing — dry runways ED Decision 2022/012/R FACTORING OF AUTOMATIC LANDING DISTANCE PERFORMANCE DATA In those cases where the landing requires the use of an automatic landing system, and the distance published in the AFM includes safety margins equivalent to those contained in [CAT.POL.A.235](#_DxCrossRefBm927678682), the landing mass of the aeroplane should be the lesser of: (a) the landing mass determined in accordance with [CAT.POL.A.235](#_DxCrossRefBm927678682); or (b) the landing mass determined for the automatic landing distance for the appropriate surface condition, as given in the AFM or equivalent document. Increments due to system features such as beam location or elevations, or procedures such as use of overspeed, should also be included.
##### AMC1 CAT.POL.A.235 Landing — dry runways *ED Decision 2022/012/R* **FACTORING OF AUTOMATIC LANDING DISTANCE PERFORMANCE DATA** In those cases where the landing requires the use of an automatic landing system, and the distance published in the AFM includes safety margins equivalent to those contained in [CAT.POL.A.235](#_DxCrossRefBm523088238), the landing mass of the aeroplane should be the lesser of: (a) the landing mass determined in accordance with [CAT.POL.A.235](#_DxCrossRefBm523088238); or (b) the landing mass determined for the automatic landing distance for the appropriate surface condition, as given in the AFM or equivalent document. Increments due to system features such as beam location or elevations, or procedures such as use of overspeed, should also be included.