LS10-s / LS10-st - DG Flugzeugbau

Flight manual <strong>LS10</strong>-s,-st
2.7 Mass (weight)
Maximum take-off and landing mass with waterballast
Variants <strong>LS10</strong>-s,-st
wingspan 15 m 540 kg ( 1190 lbs.)
wingspan 18 m 600 kg ( 1323 lbs.)
Maximum take-off and landing mass without waterballast:
Maximum take-off and landing mass = WNLP + Wwings
WNLP = Maximum mass of the non lifting parts (see below)
Wwings = actual mass of the wings
Maximum mass of the non lifting parts
Variant <strong>LS10</strong>-s <strong>LS10</strong>-st
15 &18m wingspan 284 (626 lbs.) 324 kg (714 lbs)
Maximum waterballast
Variants <strong>LS10</strong>-s,-st
wingtanks approx. 189 kg (417 lbs)
fintanks 8,5 kg (18.7 lbs).
Caution: Ballast in the fin tanks is part of the weight of the non lifting parts.
The max. take-off mass must not be exceeded with this ballast.
Note: It is recommended to dump the waterballast before landing on airfields.
Caution: Always dump the ballast before an outlanding.
Maximum mass in baggage compartment: 5 kg (11 lbs)
Caution: Heavy pieces of baggage must be adequately fixed in the baggage
compartment. The max. mass secured on one half of the floor (left and right
of fuselage centre line) should not exceed 2,5 kg (5.5 lbs.).
Caution: Follow the loading procedures described in section 6
Note: Further limitations for waterballast see section 2.17.
Issued: October 2009 2.7
EASA app.