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CS 22.1519  Weight and c.g.

ED Decision 2003/13/RM

(a)     The maximum weight determined under CS 22.25(a) must be established as an operating limitation.

(b)     The weight of non-lifting structural parts must be established.

(c)      The c.g. limitations determined under CS 22.23 must be established as operating limitations.

(d)     The empty weight and the corresponding c.g. positions must be determined in accordance with CS 22.29.
Details
Source-Title: CS 22.1519 Weight and c.g. View latest amendments
Erulesid: ERULES-1963177438-5180 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