What was found
LAP SEAM RIVETS PULLING SKIN BULGING SEPARATING BS 1088 AT AFT FUSELAGE JACK POINT, LEVEL 2 CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REO. PERMANENT REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LAP SEAM RIVETS PULLING SKIN BULGING SEPARATING BS 1088 AT AFT FUSELAGE JACK POINT, LEVEL 2 CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REO. PERMANENT REPAIR.