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CS 22.349  Rolling conditions

ED Decision 2003/13/RM

The sailplane must be designed for the rolling loads resulting from the aileron deflections and speeds specified in CS 22.455 in combination with a load factor of at least two-thirds of the positive manoeuvring load factors prescribed in CS 22.337.

Details
Source-Title: CS 22.349 Rolling conditions View latest amendments
Erulesid: ERULES-1963177438-5338 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: CS (Certification specification)
Origin: EASA
Category: EAR