CS 22.585 Strength of launching hook attachment

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ED Decision 2003/13/RM

(a) The launching hook attachment must be designed to carry a limit load of 1.5 Q_nom, as defined in CS 22.581(b), acting in the directions specified in CS 22.581 and CS 22.583.

(b) The launching hook attachment must be designed to carry a limit load equal to the maximum weight of the sailplane, acting at an angle of 90° to the plane of symmetry.

Details

Source-Title: CS 22.585 Strength of launching hook attachment View latest amendments

Erulesid: ERULES-1963177438-5375 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