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AMC 22.347  Unsymmetrical flight conditions

ED Decision 2003/13/RM

The sailplane is assumed to maintain its attitude after the control surfaces have been activated to initiate roll or yaw until the resulting incremental loads have reached their highest value.
Details
Source-Title: AMC 22.347 Unsymmetrical flight conditions View latest amendments
Erulesid: ERULES-1963177438-5268 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 22.347 Unsymmetrical flight conditions
Origin: EASA
Category: EAR