§25.1519 Weight, centre of gravity and weight distribution

CS-25 · Subpart G — Operating Limitations And Information · at CS25-28 (current)

Text in force at CS25-28: from CS25-18, effective 24 Jun 2016.

(See AMC 25.1519) The aeroplane weight, centre of gravity, and weight distribution limitations determined under CS 25.23 to CS 25.27 must be established as operating limitations.

ED Decision 2016/010/R · Source

Version history

Version	Effective	Published
CS25-18	24 Jun 2016	ED Decision 2016/010/R
CS25-0	17 Oct 2003	ED Decision 2003/002/RM

Rulemaking for CS25-18

easa npa NPA 2015-11
easa decision ED Decision 2016/010/R source

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