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CS-VLA 363  Side load on engine mount

ED Decision 2003/18/RM

(a)                            The engine mount and its supporting structure must be designed for a limit load factor in a lateral direction, for the side load on the engine mount, of not less than 1·33.

(b)                            The side load prescribed in subparagraph (a) of this paragraph may be assumed to be independent of other flight conditions.
Details
Source-Title: CS-VLA 363 Side load on engine mount View latest amendments
Erulesid: ERULES-1963177438-8061 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