What was found
LHW O/B AFT FLAP T/E WEDGE LOWER SKIN BETWEEN #2 AND #3 DRIVE ARM FOUND DELAMINATION(<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.
LHW O/B AFT FLAP T/E WEDGE LOWER SKIN BETWEEN #2 AND #3 DRIVE ARM FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)