As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE NOSE COWL INNER PANEL HAS 2 AREAS OF DAMAGE AT APPROXIMATELY 5 O'CLOCK 1 APPROXIMATELY 2" X .50" & 1 AT 6 O'CLOCK 2" X .50". PREVIOUS REPAIR IS COMING LOOSE APPROXIMATELY 5" X 5" & ENTIRE PANEL FROM NOSE LIP TO FAN ATTRITION LINER FROM EDGE OF PREVIOUS JOB. REPLACED INLET COWL IAW MM. PERFORMED TESTS REQUIRED IAW MM. ALL CHECKED GOOD.