What was found
INSPECTION FOUND A .1875 INCH CRACK IN FUSELAGE SKIN WITH CORROSION AT LAP SEAM BS 600, STRINGER 26L. THE CORROSION WAS REMOVED AND THE CRACKED AREA WAS CUT OUT, A 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 A .1875 INCH CRACK IN FUSELAGE SKIN WITH CORROSION AT LAP SEAM BS 600, STRINGER 26L. THE CORROSION WAS REMOVED AND THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.