WEIGHING SHEET
a
Bezugsebene
Datum li
ne
Xs
G,
Incidence boord
Ke
i I
1000
:
40
b--
---
-
Datum Line: Wing leading edge at the root
rib
Glider Attitude: Fuselage upper surface at a tail down slope of 1000:40 measured
300mm forward of the fin.
Weight at the
landing wheel G
1
=
Weight at the
tailskid G2 =
Empty weight GL = G1 + G2 =
Datum to
landing wheel
Datum to tailskid
Centre of gravity of Empty Glider
X = (G2 x b I GL)
+a=
a=
b=
kg
kg
kg
mm
mm
mm Aft of Datum
The determination
of
the empty weight and the centre of gravity are always determined
without water
ballast.
17
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