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GM1 ADR-DSN.B.020 Choice of maximum permissible crosswind components
Available versions for ERULES-1963177438-2349
ED Decision 2014/013/R
found in: Aerodromes (139/2014) Part-ADR.AR Part-ADR.OR Part-ADR.OPS CS-ADR-DSN CS-HPT-DSN (Jun 2023)
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GM1 ADR-DSN.B.020 Choice of maximum permissible crosswind components ED Decision 2014/013/R (a) In the application of [GM1 ADR-DSN.B.015(a)](#_DxCrossRefBm1800047439) it should be assumed that landing or take-off of aeroplanes is, in normal circumstances, precluded when the crosswind component exceeds: (1) 37 km/h (20 kt) in the case of aeroplanes whose reference field length is 1 500 m or over, except that when poor runway braking action owing to an insufficient longitudinal coefficient of friction is experienced with some frequency, a crosswind component not exceeding 24 km/h (13 kt) should be assumed; (2) 24 km/h (13 kt) in the case of aeroplanes whose reference field length is 1 200 m or up to but not including 1 500 m; and (3) 19 km/h (10 kt) in the case of aeroplanes whose reference field length is less than 1 200 m.
GM1 ADR-DSN.B.020 Choice of maximum permissible crosswind components ED Decision 2014/013/R (a) In the application of [GM1 ADR-DSN.B.015(a)](#_DxCrossRefBm151830577) it should be assumed that landing or take-off of aeroplanes is, in normal circumstances, precluded when the crosswind component exceeds: (1) 37 km/h (20 kt) in the case of aeroplanes whose reference field length is 1 500 m or over, except that when poor runway braking action owing to an insufficient longitudinal coefficient of friction is experienced with some frequency, a crosswind component not exceeding 24 km/h (13 kt) should be assumed; (2) 24 km/h (13 kt) in the case of aeroplanes whose reference field length is 1 200 m or up to but not including 1 500 m; and (3) 19 km/h (10 kt) in the case of aeroplanes whose reference field length is less than 1 200 m.
##### GM1 ADR-DSN.B.020 Choice of maximum permissible crosswind components *ED Decision 2014/013/R* (a) In the application of [GM1 ADR-DSN.B.015(a)](#_DxCrossRefBm1262885016) it should be assumed that landing or take-off of aeroplanes is, in normal circumstances, precluded when the crosswind component exceeds: (1) 37 km/h (20 kt) in the case of aeroplanes whose reference field length is 1 500 m or over, except that when poor runway braking action owing to an insufficient longitudinal coefficient of friction is experienced with some frequency, a crosswind component not exceeding 24 km/h (13 kt) should be assumed; (2) 24 km/h (13 kt) in the case of aeroplanes whose reference field length is 1 200 m or up to but not including 1 500 m; and (3) 19 km/h (10 kt) in the case of aeroplanes whose reference field length is less than 1 200 m.