What was found
INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT STA 804, STRINGER 14L. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT STA 804, STRINGER 14L. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3.