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