As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CREW REPORT: A PREVIOUS PATCH OF THE ACOUSTIC PANEL ON THE NR 2 ENGINE APPEARS TO BE DELAMINATED. SAMC TEXT: FBO REPORTS 2 AREAS OF PREVIOUS ATTRITION LINER REPAIR IS SEPARATING. ONE AREA IS APPROX 2 INCH IN DIAMETER AND THE OTHER IS 1 INCH IN DIAMETER. OK TO CONTINUE PER MT72-017 FOR 20 FLIGHT CYCLES. AREA INSPECTED AND MEETS MT72-017 CRITERIA. REPAIR MUST BE ACCOMPLISHED WITHIN 20 FLIGHT CYCLES MAX LIMIT IS PTC 17673. APPLIED ACOUSTIC FILLER TO THE TWO LOCATIONS IN ACOUSTIC PANEL.