As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H ENGINE STRUT TO WING. UNDER WING SKIN AREA OF STRUT PLATE IS DISBAND SEE DOT HT-4<[01] RE-BONDED PLATE AT R/H ENGINE STRUT TO WING. UNDER WING SKIN AREA OF STRUT AS PER REF B737 SOPM 20-50-19 AND SOPM 20-50-12;[02] ADD ON STEP # 1 BAC5010;[03] FINAL INSPECTION; VERIFIED STEPS #1 AND #2 RE-BONDED PLATE.