DG Flugzeugbau LS4 - Page 108

Maintenance Manual LS4
Issued: May 2011
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
11-8
Types of materials and overlap dimensions cont.
Part
Fabric
type
No. of
layers
Fibre
orientation
overlap
Fuselage up to S/N. 4698
shell outside
92145
1
0°
20 mm / 0.79 in.
20 mm / 0.79 in.
92125
1
+ 45°
from 2.75 m behind nose
92125*
2
0°, 90°
20 mm / 0.79 in.
from 0.8 m behind nose
92146
1
0°
40 mm / 1.57 in.
Shell inside
92125
2
+ 45°
40 mm / 1.57 in.
Fin up to S/N. 4698
from outside to inside
92125
1
+ 45°
20 mm / 0.79 in.
92125*
6
0°, 90°
60 mm / 2.36 in.
92125
1
+ 45°
20 mm / 0.79 in.
Fuselage from S/N. 4699 on
shell outside
92145
1
0°
20 mm / 0.79 in.
20 mm / 0.79 in.
per layer
92145
2
+ 45°
from 2.75 m behind nose
92125*
2
0°, 90°
20 mm / 0.79 in.
from 0.8 m behind nose
92146
1
0°
40 mm / 1.57 in.
Shell inside
921425
2
+ 45°
20 mm / 0.79 in.
per layer
Fin from S/N. 4699 on
from outside to inside
92145
2
+ 45°
20 mm / 0.79 in.
per layer
92125*
6
0°, 90°
60 mm / 2.36 in.
92125
1
+ 45°
20 mm / 0.79 in.
* Instead of the Polyester fabric used during production
The overlap of the fin fabric to the fuselage is from the cross point of the
fin leading edge to the fuselage upper side 100 mm <3.94 in.> to the front.
The overlap of the fuselage fabric to the fin is from the fuselage upper side
100 mm <3.94 in.> up the fin.