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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 section 4. (Smaller reinforcements on high stressed areas are
not given in the table below).
Part
Inboard wing panel
Exterior skin
Core
Inner skin
Outboard wing
Exterior skin
Core
Inner skin
Winglet of the
outboard wing
complete shell
Ailerons inboard
wings
Exterior skin
Core
Inner skin
Ailerons outboard wings
Exterior skin
Core
Inner skin
Issued December 2010
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Repair manual DG-1000
overlap b
fabric type, etc.
d=diagonal + 45°
(cm)
(in.) l= 0°, 90°
3
1,2 1 x 90070 l outside
+1x205g/m² carbonfibre d whole
wing
3
1,2 +1x205g/m² carbonfibre d from root
up to 3160 mm from root
/
H60 8mm thick up to y= 5240mm,
H60 6mm from y= 5240mm up to
parting
3
1,2 1x205g/m² carbonfibre d whole
wing
+1x carbonfibre 120g/m²
unidirectional l in direction of flight
in the tank area
3
1,2 1x90070 l outside
+1x205 g/m² carbonfibre d
/
H 60 3mm thick
1,5
0,6 1x92110 d
4
1,6 1x90070 l outside
+3x205 g/m² carbonfibre d
2
0,8 1x90070 l outside
+1x200 g/m² carbonfibre M40J d
/
H60 3 mm thick
2
0,8 1x200g/m² carbonfibre M40J d
2
0,8 1x90070l
+1x205g/m² carbonfibre d
/
1xDiolen fabric 158g/m²l
2
0,8 1x205g/m² carbonfibre d
6.1