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CS 22.1511  Wing-flap operating speed

ED Decision 2003/13/RM

For each positive wing-flap position (see AMC 22.335), the maximum wing-flap operating speed VFE must not be greater than 0.95 times the speed VF as defined in CS 22.335(b) for which the structure has been designed.
Details
Source-Title: CS 22.1511 Wing-flap operating speed View latest amendments
Erulesid: ERULES-1963177438-5173 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