What was found
INSPECTION FOUND A 1.5 INCH CRACK IN ATTACH ANGLE AT STA 360, STRINGER 21R. THE ATTACH ANGLE WAS REMOVED IAW SRM 51-30-2, REPAIR ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 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 1.5 INCH CRACK IN ATTACH ANGLE AT STA 360, STRINGER 21R. THE ATTACH ANGLE WAS REMOVED IAW SRM 51-30-2, REPAIR ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.