What was found
DURING THE STRUCTURAL INSPECTION OF THE UPPER REAR FUSELAGE IT WAS FOUND THE FUSELAGE SKIN WITH AN OIL CAN AT BS 1006 3 INCH BELOW STRG 16L. THE AFFECTED SKIN AREA HAS BEEN REPAIRED IAW SRM 53-80-01, REPAIR 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING THE STRUCTURAL INSPECTION OF THE UPPER REAR FUSELAGE IT WAS FOUND THE FUSELAGE SKIN WITH AN OIL CAN AT BS 1006 3 INCH BELOW STRG 16L. THE AFFECTED SKIN AREA HAS BEEN REPAIRED IAW SRM 53-80-01, REPAIR 6.