DG Flugzeugbau DG-800S Reparatur-Handbuch - Seite 5
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2.
Definition of minor damage
Only the damage listed below can be considered as minor damage
repairable by oneself.
1.
Any damage limited to gelcoat or filler.
2.
Holes in the fuselage underside where the average diameter does
not exceed:
Forward fuselage
Rear fuselage
Cracks in fuselage underside max.
Forward fuselage
Rear fuselage
The fuselage glued joint (rear fuselage) should not be damaged.
3.
Holes, cracks and tears, bubbles etc. in the wings, horizontal
stabilizer and control surfaces skins where the damage does not
exceed:
Wings
Horiz. stabiliser
Rudder
Flaperon, Elevator 30 mm (1.2 in.)
The above parts should not be damaged in the spar area.
When repairing control surface refer to sect. 5.6 page 13.
4.
Replacement of bent fittings: Part numbers, see diagrams in the
maintenance manual. Damaged fittings should not be repaired but
replaced.
Issued: April 1997
Repair manual DG-800S
average diameter
100 mm (4 in.)
50 mm (2
in.)
50 mm (2
in.)
80 mm (3 in.)
40 mm (1.5 in.)
120 mm (5 in.)
80 mm (3 in.)
cracklength
150 mm (6 in.)
80 mm (3 in.)
80 mm (3 in.)
50 mm (2 in.)
4