What was found
DURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON DOUBLER AT FR 19 LBL 14, CORROSION ON DOUBLER REMOVED BY BLEND-OUT IAW SRM 51-10-03 AND FOUND WITHIN LIMITS IAW SRM 53-10-10 AD06 REV 49.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON DOUBLER AT FR 19 LBL 14, CORROSION ON DOUBLER REMOVED BY BLEND-OUT IAW SRM 51-10-03 AND FOUND WITHIN LIMITS IAW SRM 53-10-10 AD06 REV 49.