DG Flugzeugbau LS4 Maintenance Manual page 108

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