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DG Flugzeugbau LS8 - Page 46

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Maintenance Manual LS8
Issued: March 2016 TN8024
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
2-17
Remarks for empty mass C.G. range
Calculated C.G. position for weighed empty mass must be within limit values.
Related cockpit loads are permissible Minimum Cockpit Load and Maximum
Cockpit Load.
Some of the given values for Minimum Cockpit Load exceed permissible
Maximum Cockpit Load considerably. These values are needed to determine the
data for the use of the vertical tail fin ballast tank. In addition they are a distinct
warning, that its use is limited.

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