As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND TWO-INCH CRACK IN FUSELAGE ON AFT SIDE OF E AND E COOLING FAN EXHAUST PORT. ACCOMPLISHED PERMANENT SKIN REPAIR PER STRUCTURAL REPAIR MANUAL 53-30-3 USING .10 INCH THICK 2024-T3 CIRCULAR EXTERNAL REPAIR DOUBLER WITH THREE FASTENER ROWS.