What was found
DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED IN TWO PLACES AT THE I/B AFT FLAP DRIVE ROD CUTOUT. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED IN TWO PLACES AT THE I/B AFT FLAP DRIVE ROD CUTOUT. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809.