What was found
DURING SHOP VISIT, THE COVE SKIN WAS FOUND CRACKED AT I/B AFT FLAP DRIVE ROD CUTOUT. THE DAMAGE WAS REPAIRED PER 727 M/M 57-52-0, FIG 809 BY REMOVING THE CRACK AND INSTALLING A DOUBLER AND SKIN FILLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP VISIT, THE COVE SKIN WAS FOUND CRACKED AT I/B AFT FLAP DRIVE ROD CUTOUT. THE DAMAGE WAS REPAIRED PER 727 M/M 57-52-0, FIG 809 BY REMOVING THE CRACK AND INSTALLING A DOUBLER AND SKIN FILLER.