As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOOSE RIVETS AT FORWARD SPAR UPPER CAP BETWEEN ENGINE NR 3 AND NR 4. REPAIR OF WORN WING SKIN COUNTERSINKS CAUSED BY LOOSE RIVETS BETWEEN WING STA 201 AND 280. PERFORM SKIN CUTOUT AT FRONT SPAR AFT TANG BETWEEN WING STA 201R AND 280R. PERFORM NEW FASTENER LAY-OUT AND MFG DOUBLER FROM 2024-T3 0.071" IAW DWG 1615-01.