As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND OLD BLEND OUT REPAIRS WITH NEW CORROSION SIGNS ON LT WING UPPER SKIN BETWEEN RIB 3 TO 5 NEAR THE REAR SPAR AND BETWEEN RIB 7 TO 8 AND RIB 10 TO 11 AT THE FRONT SPAR. THE CORRODED AREAS HAVE BEEN REPAIRED IAW WITH SRM 57-00-00/PG 201/PARA 4C PART B AND TD/B/2004/0443 ISSUE B, APPROVED BY EA 6-5720-81121 AND RAS/BAE/1409/2004 ISSUE A.