As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE SKIN BULGED AT BS 950F PLUS 10.0 AT STRINGER 4R. REPAIRED FUSELAGE SKIN LEVEL 2 CORROSION FROM BS 950F PLUS 8.00 TO BS 950F PLUS 19.5 BETWEEN STRINGER 3R AND STRINGER 5R IAW SRM 53-30-3 FIG 14 DETAIL IV. (M)