What was found
INSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER NR 6 RIB AT STRINGER 3L. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER NR 6 RIB AT STRINGER 3L. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.