CS 27.601 Design

ED Decision 2003/15/RM

(a) The rotorcraft may have no design features or details that experience has shown to be hazardous or unreliable.

(b) The suitability of each questionable design detail and part must be established by tests.

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Source-Title: CS 27.601 Design

Erulesid: ERULES-1963177438-4925

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/15/RM Navigate

Regulatorysubject: CS-27

Typeofcontent: CS (Certification specification)

Origin: EASA

Category: EAR