What was found
DURING SHOP INSP, THE COVE SKIN WAS FOUND CRACKED AT THE I/B AFT CORNER OF I/B AFT FLAP DRIVE ROD CUTOUT. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 09.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP INSP, THE COVE SKIN WAS FOUND CRACKED AT THE I/B AFT CORNER OF I/B AFT FLAP DRIVE ROD CUTOUT. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 09.