What was found
LOWER FUSELAGE FR 88, BETWEEN STR 27 AND STR 29 WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-71. FRAME SECTION WAS REPLACED UNDER DWG INSTRUCTIONS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE FR 88, BETWEEN STR 27 AND STR 29 WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-71. FRAME SECTION WAS REPLACED UNDER DWG INSTRUCTIONS.