LS10-s / LS10-st - DG Flugzeugbau
LS10-s / LS10-st - DG Flugzeugbau
LS10-s / LS10-st - DG Flugzeugbau
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Flight manual <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-s,-<strong>st</strong><br />
Sy<strong>st</strong>em 2 consi<strong>st</strong>s of the inner wing tank (106 kg / 234 lbs total) and a fin tank<br />
(right hand side outlet) (4.6 kg / 10.1 lbs). All tanks of sy<strong>st</strong>em 2 are controlled<br />
via the rear water balla<strong>st</strong> control handle in<strong>st</strong>alled on the RH side of the<br />
cockpit.<br />
closed open<br />
fin tank<br />
innerwing tanks<br />
4.2.3.3 Filling procedure<br />
Filling up the water balla<strong>st</strong> sy<strong>st</strong>em mu<strong>st</strong> be performed according to the<br />
following procedure, use only clean water:<br />
1. Fir<strong>st</strong> determine and note the exact amount of water balla<strong>st</strong> according to the<br />
loading chart described in section 6.8 depending on the actual empty mass<br />
and C.G position.<br />
To compensate C.G. movements caused by the balla<strong>st</strong> in the wing tanks,<br />
the corresponding fin tanks should be filled up according to balla<strong>st</strong> chart in<br />
section 6.8.10.<br />
The wings mu<strong>st</strong> be horizontally aligned and fixed during the whole filling<br />
process.<br />
2. open both water balla<strong>st</strong> tanks by rotating both balla<strong>st</strong> handles to the<br />
rearward position.<br />
Issued: October 2009 EASA app. 4.6
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