What was found
INSPECTION FOUND A .125 INCH CRACK IN FRAME AT STA 500A, STRINGER 20L AND 21L. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .125 INCH CRACK IN FRAME AT STA 500A, STRINGER 20L AND 21L. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-2.