As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE LWR LOBE FRAME IN THE AFT PIT STA 1420 STR 26L HAS DAMAGE. SUPPLEMENTAL DATA UPDATE ACP'D MAJOR REPAIR ON FUSELAGE LOWER LOBE FRAME IN THE AFT PIT STA 1420, STR 26L, REF SRM 53-00-07, RPR 5 AT C-04 VISIT ON W-U F5477P. THIS IS A CATEGORY 'B' REPAIR. THRESHOLD TO BEGIN SUPPLEMENTAL HFEC AND DVI IS 12000 FLIGHT CYCLES AFTER THE REPAIR, WITH REINSP INTERVAL OF 11000 FLIGHT CYCLES.