What was found
G5/AFT COMPLEX GALLEY WORK TOP PANEL DAMAGED AND LOWER FRONT TRIM WITH LOOSE SCREWS. REPLACED UPPER FUSELAGE G5/AFT COMPLEX GALLEY WORK TOP PANEL IAW CMM 25-31-546X-01001-720A-C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
G5/AFT COMPLEX GALLEY WORK TOP PANEL DAMAGED AND LOWER FRONT TRIM WITH LOOSE SCREWS. REPLACED UPPER FUSELAGE G5/AFT COMPLEX GALLEY WORK TOP PANEL IAW CMM 25-31-546X-01001-720A-C.