What was found
INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 380, STRINGER 21R. THE CRACK WAS STOP DRILLED IAW SRM 53-10-4. A DOUBLER, FILLER AND CLIP 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 2 INCH CRACK IN FRAME AT STA 380, STRINGER 21R. THE CRACK WAS STOP DRILLED IAW SRM 53-10-4. A DOUBLER, FILLER AND CLIP WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.