What was found
LHW T/E O/B AFT FLAP UPPER SURFACE FOUND WORN (COUNT FROM O/B EDGE 4")(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG 201</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LHW T/E O/B AFT FLAP UPPER SURFACE FOUND WORN (COUNT FROM O/B EDGE 4")(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG 201</P>)