Maintenance Manual LS8
Issued: June 2016 TN8024
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
10-1
10 Materials for repair
Resin systems for repairs
Resin Hexion EPIKOTE
TM
Resin MGS LR 285 with
Hardener EPIKURE
TM
Curing Agent MGS LH 286
mixing ratio 100:40 +2 by weight
or
Resin Hexion EPIKOTE
TM
Resin MGS LR 385 with
Hardener EPIKURE
TM
Curing Agent MGS LH 386
mixing ratio 100:35 +
2 by weight
Caution: This resin system is not suitable for repair of glasfibre structures, use
only with Aramid or carbon fibres.
The repaired areas must be post-cured for 20 hours at a min. of 54°C
(129°F) before the next take-off.
Fibre Glass Fabric
:
Alkalifree E-glass with finish I-550 or FK 144 Manufacturer: Interglas
Interglas No. Kind of weave mass(g/m²) Usage
90070 Linen 79 elevator
92110 2/2 twill 163 stabiliser
92125 2/2 twill 280 local reinforcing
92145 Unidir. Plain 216 fuselage
92146 Unidir. Plain 440 fuselage
Carbon Fibre Fabric
: Manufacturer Interglas
98320 Linen 132 wings, spar box,
stabiliser and
elevator, aileron
Aramid Fibre Fabric (Kevlar)
: Manufacturer Interglas
98605 Linen 61 Rudder, Elevator
Polyester (Diolen) Fabric Manufacturer: Lückenhaus
No. Kind of weave mass(g/m²) Usage
34048 Linen 206 Fuselage
To Next Page
Loading...
