DG Flugzeugbau LS4 - Page 34

Maintenance Manual LS4
Issued: May 2011
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
2-8
235 616 -786 616 -808 616 -830 616 -853 -876 -900 -926
236 615 -784 615 -806 615 -828 615 -851 -874 -898 -924
237 613 -783 613 -804 613 -827 613 -849 -872 -896 -922
238 611 -781 611 -803 611 -825 611 -847 -870 -894 -919
239 610 -780 610 -801 610 -823 610 -846 -868 -892 -917
240 608 -778 608 -799 608 -821 608 -844 -866 -890 -915
241 607 -776 607 -798 607 -820 607 -842 -864 -888 -913
242 605 -775 605 -796 605 -818 605 -840 -862 -886 -911
243 603 -773 603 -794 603 -816 603 -838 -860 -884 -909
244 602 -772 602 -793 602 -814 602 -836 -859 -882 -907
245 600 -770 600 -791 600 -813 600 -835 -857 -880 -905
246 599 -769 599 -789 599 -811 599 -833 -855 -878 -903
247 597 -767 597 -788 597 -809 597 -831 -853 -876 -901
248 596 -766 596 -786 596 -808 596 -829 -851 -874 -898
249 594 -764 594 -785 594 -806 594 -828 -849 -872 -896
250 593 -763 593 -783 593 -804 593 -826 -848 -870 -895
251 591 -761 591 -782 591 -803 591 -824 -846 -869 -893
252 590 -760 590 -780 590 -801 590 -823 -844 -867 -891
253 588 -759 588 -779 588 -800 588 -821 -842 -865 -889
254 587 -757 587 -777 587 -798 587 -819 -841 -863 -887
255 586 -756 586 -776 586 -797 586 -818 -839 -861 -885
256 584 -754 584 -774 584 -795 584 -816 -837 -859 -883
257 583 -753 583 -773 583 -793 583 -814 -835 -858 -881
258 581 -752 581 -771 581 -792 581 -813 -834 -856 -879
259 580 -750 580 -770 580 -790 580 -811 -832 -854 -877
260 579 -749 579 -768 579 -789 579 -810 -830 -852 -875
261 577 -748 577 -767 577 -787 577 -808 -829 -851 -874
262 576 -746 576 -766 576 -786 576 -806 -827 -849 -872
263 575 -745 575 -764 575 -784 575 -805 -825 -847 -870
264 573 -744 573 -763 573 -783 573 -803 -824 -845 -868
265 572 -742 572 -762 572 -782 572 -802 -822 -844 -867
266 571 -741 571 -760 571 -780 571 -800 -821 -842 -865
267 569 -740 569 -759 569 -779 569 -799 -819 -840 -863
268 568 -739 568 -757 568 -777 568 -797 -818 -839 -861
269 567 -737 567 -756 567 -776 567 -796 -816 -837 -860
270 566 -736 566 -755 566 -775 566 -794 -814 -836 -858
271 564 -735 564 -754 564 -773 564 -793 -813 -834 -856
272 563 -734 563 -752 563 -772 563 -791 -811 -832 -855
Empty mass C.G. range tables cont.
(empty mass up to 272 kg, cockpit load 95 – 110 kg) Table for <kg> and <mm>
Partly, given values for Minimum Cockpit Load exceed permissible Maximum
Cockpit Load considerably. These values are required for the use of the vertical tail fin
ballast tank as a distinct warning, that its use is limited.
Empty
mass
<kg>
Cockpit load <kg> / Empty mass C.G. range <mm>
max. + min. cockpit load
min. cockpit load
110-95
110-100
110-105
110-110
- 115
- 120
-125