What was found
LHW OB MID FLAP AFT UPPER SKIN FOUND 2EA SCREW HOLES ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LHW OB MID FLAP AFT UPPER SKIN FOUND 2EA SCREW HOLES ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)