What was found
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 755, STRINGER 19R. THE CRACKED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER WAS 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 2 INCH CRACK IN FUSELAGE SKIN AT BS 755, STRINGER 19R. THE CRACKED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.