Page 591 - engelsk
P. 591

Operational procedures






















                To accommodate any wind jumps, we practically increase the approach speed

                and change the use of flaps to suit the conditions.

                If the wind is given as 240/16g26, for example, we add the higher of either ¼ of

                the mean wind or ½ of the wind difference.


                A quarter of the mean wind of 16 Kt. is 4 Kt.


                The difference between the mean wind of 16 Kt and the wind in the gusts is 10
                Kt. Half of the wind difference is then 5 Kt, and since it is the higher of the two,

                the addition to the approach speed is 5 KT.




                You  should  also  be  able  to  calculate  how  much  the  current  crosswind

                component is and whether it exceeds the pilot's or aircraft's maximum limit.


                                                           Difference in degrees       Number of 6ths


                As  an  aid  to  quickly  calculating                    10                      1/6
                                                                         20                      2/6
                crosswinds,  you  can  use  the  1/6
                                                                         30                      3/6
                method,  as  you  see  in  the  table
                                                                         40                      4/6
                here.
                                                                         50                      5/6
                For example, if you want to land on                60 (and above)                6/6

                runway 27 (270 degrees in direction), and the wind is coming from 260 degrees,

                then it is 10 degrees off-center in relation to the runway direction. For every 10

                degrees up to 60 degrees, the crosswind will increase by 1/6.


           Flight Theory PPL(A)(UL)/LAPL             Henning Andersen, Midtjysk Flyveskole© 2025           591
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