What was found
L/H I/B MAIN FLAP LOWER SKIN IS DELAMINATED AT O/B AFT CORNER. (MARKED)<[01] REMOVED; REPLACED; AND INSTALLED A NEW WEDGE AT L/H INBOARD MAIN FLAP IAW SOPM 20-50-01.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H I/B MAIN FLAP LOWER SKIN IS DELAMINATED AT O/B AFT CORNER. (MARKED)<[01] REMOVED; REPLACED; AND INSTALLED A NEW WEDGE AT L/H INBOARD MAIN FLAP IAW SOPM 20-50-01.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.