What was found
DURING A STRUCTURAL INSPECTION, FOUND THE BS 348.2FRAME CRACKED AT STRINGER 15L, THE FRAME SECTION WAS REPLACED IAW SB 737-53A1240, WORK INSTRUCTIONS PART 4A, REV 1, AND EAM 3553020-4, SECTION 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A STRUCTURAL INSPECTION, FOUND THE BS 348.2FRAME CRACKED AT STRINGER 15L, THE FRAME SECTION WAS REPLACED IAW SB 737-53A1240, WORK INSTRUCTIONS PART 4A, REV 1, AND EAM 3553020-4, SECTION 1.