Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS-VLA 1589 Loading information
Available versions for ERULES-1963177438-8006
ED Decision 2003/18/RM
found in: CS-VLA Amdt 1 - Very Light Aeroplanes (Mar 2009)
Version
CS-VLA Amdt 1 - Ve... (Mar 2009)
Section
Share
Version
Show details
Hide details
Version
CS-VLA 1589 Loading information ED Decision 2003/18/RM The following loading information must be furnished: (a) The weight and location of each item of equipment installed when the aeroplane was weighed under [CS-VLA 25](#_DxCrossRefBm584936618). (b) Appropriate loading instructions for each possible loading condition between the maximum and minimum weights determined under [CS-VLA 25](#_DxCrossRefBm584936618) that can result in a centre of gravity beyond - (1) The extremes selected by the applicant; (2) The extremes within which the structure is proven; or (3) The extremes within which compliance with each functional requirement is shown.