What was found
INSPECTION FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 778 BETWEEN LBL 6 AND RBL 6. THE CORRODED AREA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 204.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 778 BETWEEN LBL 6 AND RBL 6. THE CORRODED AREA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 204.