CS 22.443 Gust loads

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ED Decision 2003/13/RM

(a) Vertical tail surfaces must be designed to withstand lateral gusts to the values described in CS 22.333(c).

(b) In the absence of a more rational analysis, the gust load must be computed as follows:

where:

= gust load (N)

= slope of vertical tail lift curve per radian

= area of vertical tail (m²)

= density of air at sea-level (kg/m³)

V = speed of flight (m/s)

U = gust speed (m/s)

K = gust factor, should be taken as 1.2

Source-Title: CS 22.443 Gust loads View latest amendments

Erulesid: ERULES-1963177438-5356 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: CS (Certification specification)

Origin: EASA

Category: EAR