What was found
WORN AREA OB FLAP LEADING EDGE AT IB END. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 57-53-01 REPAIR 8 PG 204, DEFECT SIZE: 1".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WORN AREA OB FLAP LEADING EDGE AT IB END. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 57-53-01 REPAIR 8 PG 204, DEFECT SIZE: 1".