Grob ASTIR CS 77 User Manual

3. Simplified fabric construction layout for the ASTIR CS
Reinforcement within highly stressed areas and large load areas are not specified.
1. FIUgel
AuBenlaminat
1 Lage 92110 diagonal
1 Lage 92 125 diagonal
Kern
Conticell 60 8 mm
lnnenlaminat
1 Lage 92125
2. Rumpf
Von auBen nach innen
1 Lage
92 110 langs
1 Lage 92146 langs
3 Lagan 92 140 diagonal
3. Ruder
Hohenruder
Seitenruder
Querruder
2 Lagen 92125 diagonal
4. Hohenflosse
2 lagen 92110 diagonal
Kern:
Conticell 60 6 mm
1 Lage 92 110 diagonal
Wing
Outer laminate
1 Layer
92 11 O
1 Layer 92 125
Core
Conticell 60 8 mm
Inner laminate
1 Layer 92 125
Fuselage
From outside to inside
1 Layer 92
11 O lengths
1 Layer 92 146 lengths
3 Layers 92 140 diagonal
Controls
Elevator
Rudder
Aiieron
2 Layers 92 125 diagonal
Fin
2 Layers 92110 diagonal
Core:
Contlcell 60 6 mm
1 Layer 92110 diagonal
~ - -.3f - · l:
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Grob ASTIR CS 77 Specifications

General

Brand	Grob
Model	ASTIR CS 77
Category	Aircrafts
Language	English