What was found
INSPECTION FOUND FUSELAGE SKIN BULGED AT STA 259, STRINGER 24L. THE BULGED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN BULGED AT STA 259, STRINGER 24L. THE BULGED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.