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DG Flugzeugbau LS8 - LS8, LS8-A, LS8-B, LS8-18

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Maintenance Manual LS8
Issued: February 2011 TN8019
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
7-5
7.5 LS8, LS8-a, LS8-b, LS8-18
Numbers refer to placards, for positions of placards see drawings at end of this section.
Use vertical tail fin battery only When using a battery in the
With main fuse at battery vertical tail fin. Minimum
(under battery box cover of vertical tail, Cockpit Load must be
if fitted) redetermined by weighing
(under battery box cover of
Canopy Emergency Release: open left side
normally,
Vertical tail, if fitted)
Pull right side with approx.15 kg/33 lbs force to stop
>19< at right canopy frame
Airspeed Indicator
(Diameter 80 mm <3.15 in>)
When the airspeed indicator is not equipped with these altitude related
VNE markings, a placard must be near the ASI. For possible versions see next page.

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