DG Flugzeugbau LS10-s Керівництво з польотів - Сторінка 11

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Rule of thumb:

Installation of 1 trim ballast weight (2.45 kg, 5.4 lbs) in front support.............

...................................... reduces Minimum Cockpit Load by 5,5 kg / 12 lbs

Installation of 1 Battery (2.5 kg, 5.5 lbs) in front of the control stick.......

..................................... reduces Minimum Cockpit Load by 3,9 kg / 8.6 lbs

Installation of battery in the fin (2.6 kg, 5.7 lbs) .......................................

...............................increases Minimum Cockpit Load by 11,2 kg / 24.6 lbs

Installation of heavy tailwheel (mass difference to standard tail wheel 3 kg

6.6 lbs.)..................increases Minimum Cockpit Load by 12,9 kg / 28.5 lbs

Installation of trim weight rear fuselage (2,5 kg, 5.5 lbs.)

......................................increases Minimum Cockpit Load by 11kg / 24 lbs

Warning: In case of doubt: Mass and Balance must be determined by

reweighing the sailplane

C.G. Shift due to extension of the engine

XS2 = XS1 – 2,3/W

Issued: December 2011

Flight Manual LS10-s,-st

= total mass (kg)

XS2 = C.G. position with

engine extended (m)

XS1 = C.G. position with

engine retracted (m)

TN LS10-02

6.14