CS 27.481 Tail-down landing conditions

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ED Decision 2003/15/RM

(a) The rotorcraft is assumed to be in the maximum nose-up attitude allowing ground clearance by each part of the rotorcraft.

(b) In this attitude, ground loads are assumed to act perpendicular to the ground.

Source-Title: CS 27.481 Tail-down landing conditions View latest amendments

Erulesid: ERULES-1963177438-4909 Compare versions

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