Leading Edge Repair - Cessna T182 Series Service Manual

MODEL 182 & T182 SERIES SERVICE MANUAL
NOTES:
1.
Dimple leading edge skin and filler material; countersink the doubler.
2.
Use MS20426AD4 rivets to install doubler.
3.
Use MS20426AD4 rivets to install filler, except where bucking is impossible. Use CR162-4
Cherry (blind) rivets where regular rivets cannot be bucked.
4.
Contour must be maintained; after repair has been completed, use epoxy filler as necessary
and sand smooth before painting.
5.
Vertical size is limited by ability to install doubler clear of front spar.
6.
Lateral size is limited to seven inches across trimmed out area.
7. Number of repairs is limited to one in each bay.
1" MAXIMUM RIVET
SPACING (TYPICAL)
DOUBLER NEED NOT
BE CUT OUT IF ALL 5/16" MINIMUM EDGE
RIVETS ARE ACCESSIBLE
MARGIN (TYPICAL)
FOR BUCKING
.040" THICKNESS
FILLER MATERIAL
AS SKIN
REPAIR PARTS
Figure 18-9. Leading Edge Repair
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