As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SKIN ATTACH ANGLE 6.7 IS CORRODED STR 24P-25P. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-20-23-02-01. REMOVED SKIN ATTACH ANGLE IAW SRM 51-42-05-02-01. RECEIVED NEW ATTACH ANGLE AND MATCH DRILLED TO WEB AND ACFT IAW SRM 51-40-07-02-01. INSTALLED NEW ANGLE IAW SRM 51-42-05-02-01, 51-23-00-00-01 AND 51-25-15-02-01. APPLIED SELF LEVELING GREEN AVDEC IAW AMM 53-20-03-290-801.