As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON FUSELAGE SKIN FOUND RIVET HEAD POPPED AND AREA OF CORROSION DAMAGE FRAME STATION 780 AT STRINGER 39R. PARTIALLY CUT OUT DAMAGED AREA IAW L1011 SRM 53-31-00. FABRICATED PARTS IAW SRM 53-31-00 FIG 802. INSTALLED REPAIR PARTS IAW SRM 53-31-00 FIG 802. AREA CLOSED. PRESSURE CHECK ACCOMPLISHED IAW MM 21-31-00. (M)