CS 22.483 One-wheel landing condition

• ED Decision 2003/13/RM found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)

CS 22.483 One-wheel landing condition ED Decision 2003/13/RM If the two wheels of a main landing gear arrangement are laterally separated (see [AMC 22.477(1)](#_DxCrossRefBm2056272161)) the conditions under [CS 22.479(a)(2), (b) and (c)](#_DxCrossRefBm2056272160) must be applied also to each wheel separately taking into account limiting effects of bank. In the absence of a more rational analysis the limit kinetic energy must be computed as follows:  where: mred =  Vv = rate of descent m = mass of the sailplane (kg) a = half the track (m) ix = radius of gyration of the sailplane (m)