What was found
BULGE AT BS 939 STR 27L, POSSIBLE CORROSION UNDER SKIN. REMOVED, CLEANED, AND TREATED PER SRM 51-10-6. INSTALLED FUSELAGE STRINGER REPAIR PER SRM 53-10-3 PAGE 10. TAT: 47,785.0 HOURS. TAC: 63,219. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BULGE AT BS 939 STR 27L, POSSIBLE CORROSION UNDER SKIN. REMOVED, CLEANED, AND TREATED PER SRM 51-10-6. INSTALLED FUSELAGE STRINGER REPAIR PER SRM 53-10-3 PAGE 10. TAT: 47,785.0 HOURS. TAC: 63,219. (X)