CS 22.455 Ailerons

Navigate / EASA

Ask question Discover more Add to collection

ED Decision 2003/13/RM

The ailerons must be designed for control loads corresponding to the following conditions:

(a) at speed the greater of V_A and V_T the full deflection of the aileron; and

(b) at speed V_D, one-third of the full deflection of the aileron.

Source-Title: CS 22.455 Ailerons View latest amendments

Erulesid: ERULES-1963177438-5360 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