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 EXTERIOR FUSELAGE SKIN BULGED FROM BS 344 TO BS 360 BETWEEN STRINGER 19R AND 24R. REPAIRED FUSELAGE SKIN FROM BS 337.5 TO BS 360 BETWEEN STRINGER 19R AND 24R IAW SRM 53-30-4 FIG 12 WITH DOUBLER TO REMOVED LEVEL 2 CORROSION. (M)