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Edge Damage Rebuild Procedure.
Facilities, Equipment and Material

AVUM and AVIM Manual for General Aircraft Maintenance Sheet Metal Shop Volume 11
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TM 1-1500-204-23-11
DO NOT sand into laminate near patch edge
when sanding adhesive squeeze out.
(r)
Reinish.
1
Sand the area smooth with 180 grit
abrasive paper. Vacuum sanding
dust from repair area. Wipe with
clean, dry wiping cloth to remove
sanding residue.
Apply inish system in accordance
2
with paragraph 7-13b or the system
speciic technical manual.
c. Trailing Edge Repair. This repair is applicable
to structure consisting of composite skins bonded
to composite ribs with damage to the trailing edge
corner of the assembly. The procedure provided is
for a trailing edge corner repair but is also applicable
to a full trailing edge.  This repair procedure is
not necessarily applicable to a particular weapon
system.  The applicability of this repair depends
upon additional factors such as loading conditions
and laminate thickness. Consult the system speciic
technical manual or engineering for further guidance.
Refer to igure 7-46 for the Process Flow Diagram
for Flush Corner Repair.
Figure 7-46. Process Flow Diagram for Flush
Corner Repair
7-76


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