CS-VLA 171 General

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ED Decision 2003/18/RM

The aeroplane must be longitudinally, directionally, and laterally stable under CS-VLA 173 to 181. In addition, the aeroplane must show suitable stability and control 'feel' (static stability) in any condition normally encountered in service, if flight tests show it is necessary for safe operation.

Details

Source-Title: CS-VLA 171 General View latest amendments

Erulesid: ERULES-1963177438-8010 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/18/RM Navigate

Regulatorysubject: CS-VLA

Typeofcontent: CS (Certification specification)

Origin: EASA

Category: EAR