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6.
Types of materials and overlap dimensions
The following overlap dimensions are to be maintained. Use the materials
given, see also pages 6 and 7.(Smaller reinforcements on high stressed
areas are not given in the table below).
Part
_______________________________________________________________
Wing skin outside
core
inside
_______________________________________________________________
Flaperons
outside
core
inside
_______________________________________________________________
Horizontal stabilizer
outside
core
inside
______________________________________________________________
Elevator
______________________________________________________________
Issued: April 1997
Repair manual DG-800S
overlap
(cm) (in.)
3
1.2
/
/
3
1.2
3
1.2
/
/
2
.8
2
.8
/
/
1
.4
2
.8
fabric type, etc.
d= + 45°
l= + 90°
1 x 90070 l outside
+1x245g/m² carbonfibre d
H 60 - 6mm thick,
18m tip 3 mm thick
1 x 285 g/m² carbonfibre d
from root up to y = 2000
1x245g/m² carbonfibre d
y = 2000 up to tip
+1x carbonfibre 120 g/m²
in flight direction in the
waterballast tank
compartment
1 x 90070 l outside
+1x245g/m² carbonfibre d
1xDiolenfabric 158 g/m²l
1x245g/m² carbonfibre d
1x90070 d +1 x 92110 d
H 60 - 5 mm thick
1 x 90070 d +1 x 90070 d in
the centre of the stabilizer
up to y = 300
1x 92110 d outside
+ 2 x 9d2125 d
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