What was found
RH O/B FORE FLAP FOUND DELAMINATION (50" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR 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.
RH O/B FORE FLAP FOUND DELAMINATION (50" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)