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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), 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.
Details
Source-Title: AMC 22.151(c)(3) Aerotowing View latest amendments
Erulesid: ERULES-1963177438-5252 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 14 November, 2003
Entryintoforcedate: 14 November, 2003
Regulatorysource: ED Decision 2003/13/RM Navigate
Regulatorysubject: CS-22
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 22.151 Aerotowing
Origin: EASA
Category: EAR