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AMC 22.151(c)(3) Aerotowing
Available versions for ERULES-1963177438-5252
ED Decision 2003/13/RM
found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)
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Sailplane Rule Boo... (Nov 2022)
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AMC 22.151(c)(3) Aerotowing ED Decision 2003/13/RM In demonstrating compliance with this requirement, in addition to the requirements of [CS 22.21(a) and (b)](#_DxCrossRefBm2056272035), the effects of at least the following should be investigated: (1) Variations of tow cable length (2) Variations of pitch trim settings (3) Acceleration along the longitudinal axis of the sailplane (4) Snatch loads on tow (5) Wind gradient due to ground boundary layer effects.