What was found
INSPECTION FOUND TWO, .5 INCH CRACKS IN FRAME AT BS 328 BETWEEN STRINGER 2OR AND 21R. THE CRACKED AREAS WERE REMOVED, FILLER AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO, .5 INCH CRACKS IN FRAME AT BS 328 BETWEEN STRINGER 2OR AND 21R. THE CRACKED AREAS WERE REMOVED, FILLER AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.