What was found
INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT FS 765, STRINGER 19R. THE CRACKED AREA OF SKIN WAS REMOVED, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT FS 765, STRINGER 19R. THE CRACKED AREA OF SKIN WAS REMOVED, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.