AMC 22.375(a) Winglets

Navigate / EASA

Ask question Discover more Add to collection

ED Decision 2003/13/RM

For the wing the interactive effects between the winglets and the wing should be taken into account, as there are:

(1) Changes in wing lift distribution:

(2) Additional bending and torsion moments at the attachment point of the winglet due to aerodynamic and mass loads on the winglet;

(3) Effects of inertia; and

(4) Effects of drag on wing torsion.

Source-Title: AMC 22.375(a) Winglets View latest amendments

Erulesid: ERULES-1963177438-5269 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/13/RM Navigate

Regulatorysubject: CS-22

Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)

Parentir: CS 22.375 Winglets

Origin: EASA

Category: EAR