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; SHOWING COMPOSITE DELAMINATION. SEE DOT HT-5 AND DOT HT-12<[01] REMOVED AND INSTALLED DAMAGE PHENOLIC STRIPS 2 EACH ON TOP SURFACE OF PANEL AS MARKED AS PER B737 AMM. 51-51-00-340-803 AND AMM 51-31-00-390-804 MATERIALS USED PO#2026993;[02] INSP./ VERIFIED WORK WAS ACCOMPLISHED.