What was found
INSPECTION FOUND #1 SLAT SKIN CRACKED AT AFT ROW OF RIVETS APPROXIMATELY 1/8" ON EITHER SIDE OF RIVET, 43" O/B OF I/B END. A REPAIR WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND #1 SLAT SKIN CRACKED AT AFT ROW OF RIVETS APPROXIMATELY 1/8" ON EITHER SIDE OF RIVET, 43" O/B OF I/B END. A REPAIR WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.