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.
(b) Appropriate loading instructions for each possible loading condition between the maximum and minimum weights determined under CS-VLA 25 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.
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