CS 29.659 Mass balance

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ED Decision 2003/16/RM

(a) The rotor and blades must be mass balanced as necessary to:

(1) Prevent excessive vibration; and

(2) Prevent flutter at any speed up to the maximum forward speed.

(b) The structural integrity of the mass balance installation must be substantiated.

Source-Title: CS 29.659 Mass balance View latest amendments

Erulesid: ERULES-1963177438-5562 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/16/RM Navigate

Regulatorysubject: CS-29

Typeofcontent: CS (Certification specification)

Origin: EASA

Category: EAR