CS 22.233 Directional stability and control

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ED Decision 2003/13/RM

(a) With cross-wind components not less than 0.2 V_S0or 15 km/h, whichever is the greater, there must be no uncontrollable ground-loop tendency at any speed at which the powered sailplane may be expected to be operated on the ground.

(b) The powered sailplane must have adequate directional control during taxying.

Details

Source-Title: CS 22.233 Directional stability and control View latest amendments

Erulesid: ERULES-1963177438-5321 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