What was found
DURING WALKAROUND INSPECTION, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 761, 1 INCH ABOVE S17L. A 2.25 INCH CRACK AT BS 814 S16L, AND A 2.75 INCH CRACK AT BS 831, 2 INCHES ABOVE S25R. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING WALKAROUND INSPECTION, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 761, 1 INCH ABOVE S17L. A 2.25 INCH CRACK AT BS 814 S16L, AND A 2.75 INCH CRACK AT BS 831, 2 INCHES ABOVE S25R. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.