What was found
LHW O/B FORE FLAP L/E FOUND DELAMINATION (77" TO O/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LHW O/B FORE FLAP L/E FOUND DELAMINATION (77" TO O/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)