As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION (C53-224-01) ON INSIDE SKIN BS 1006 BETWEEN STR 1 TO 2 RT. *S/D* REMOVED CORROSION ON INNER SKIN BS 1006 BETWEEN STR 1 TO 2 RT. REMOVED .043 FROM .063 ORIGINAL THICKNESS IN AREA OF 2 X 1. FOUND TO BE OUT OF LIMITS PER FED SRM 53-30-1. TRIMMED DAMAGED AREA PER FED SRM 53-30-3. FABRICATED DOUBLER PER FED SRM 53-30-3 AND INSTALLED DOUBLER PER FED SRM 51-30-2.