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TOMARK Viper SD-4 RTC - Page 145

TOMARK Viper SD-4 RTC
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TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 51 Standard Practices Structure
Issue: 28.FEB 2017 Page 145
Use the same material for repairs as the material of a defective area.
Carry out repair of skin damaging by means of patches having the
same thickness as the original skin or higher.
Repair the angle defects with inserted angles with the section by 10 to
20% higher than the section of the damaged angle.
Ensure loading from one side of the repaired area is carried through
the repair element directly to the other side.
Ensure length of overlapping in the area of repair is satisfactorily big
so that loading can be equally distributed to non-defective part of the
structure.
Overlapping of 2 sheets must be at minimum 2D (diameters) of used
rivet from each side as shown in the following.
Use existing holes for riveted joints, if possible.
If these rivets are not able to transfer loading, drill other holes.
Use rivets around of the repaired area as a criterion for rivet size
selection.

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