CS-VLA 1 Applicability

Navigate / EASA

Ask question Discover more Add to collection

ED Decision 2003/18/RM

This airworthiness code is applicable to aeroplanes with a single engine (spark- or compression-ignition) having not more than two seats, with a Maximum Certificated Take-off Weight of not more than 750 kg and a stalling speed in the landing configuration of not more than 83 km/h (45 knots)(CAS), to be approved for day-VFR only.

Details

Source-Title: CS-VLA 1 Applicability View latest amendments

Erulesid: ERULES-1963177438-8056 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