As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON CLOUSURE ANGLE LOCATED BS1016 TO BS1088 AT LEVEL ST2L AND STR3L EXTERNAL SKIN AT UPPER FUSELAGE. REPLACED CLOUSURE ANGLE AND FASTENERS LOCATED BS1016 TO BS1121+ 10 INCHES APROX AT LEVEL ST2L AND STR3L EXTERNAL SKIN UPPER FUSELAGE IAW B737-700 SRM 51-10-02 AND BOEING DRAWING: 148A8300 SHEET 2 REV A; BOEING DRAWING: 148A3590 SHEET 99 REV-.