What was found
DURING A STRUCTURAL INSPECTION, FOUND BS 348.2, STRINGER 15L, AN INTERNAL ATTACH ANGLE FOUND CRACKED. THE ATTACH ANGLE WAS REPLACED IAW SB 737-53A1240, WORK INSTRUCTIONS, PART 4, PARAGRAPH C, REV. 1 AND EAM 3553020-4, SECTION 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A STRUCTURAL INSPECTION, FOUND BS 348.2, STRINGER 15L, AN INTERNAL ATTACH ANGLE FOUND CRACKED. THE ATTACH ANGLE WAS REPLACED IAW SB 737-53A1240, WORK INSTRUCTIONS, PART 4, PARAGRAPH C, REV. 1 AND EAM 3553020-4, SECTION 3.