As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON UPPER SUPPORT ANGLE AT LEVEL WBL 188 TRAILING EDGE AREA R/T WING INTERNAL AREA. REPLACED SUPPORT ANGLE (CLIP) AT LEVEL WBL 188 TRAILING EDGE AREA R/T WING INTERNAL AREA IAW B737-500 SRM 51-10-02, SRM 51-40-02 AND DRAWING #65C26300.