As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON STIFFENER SUPPORT ANGLE LT SIDE AT FR 26 BL 0. CORROSION REMOVED ON STIFFENER SUPPORT ANGLE LT SIDE AT FR 26 BL 0 AS PER SRM 51-21-42, MATERIAL THICKNESS 0.040, MATERIAL REMOVED 0.003 WITHIN LIMITS AS PER SRM 53-51-00 FIG 301. SUPPLEMENTAL - SDR CLOSED 10/18/07.