What was found
LHW I/B FORE FLAP UPPER SURFACE 145" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LHW I/B FORE FLAP UPPER SURFACE 145" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)